Disclub Golf: Disclub, Golfdisc & Discopter

Abstract

The Disclub Golf is to swivel the disclub to launch the golfdisc to fly. The golfdisc of has the nearly right triangle rim with straight bottom edge and triangle flap at the trail edge of the bottom edge. On the surface of rim, there are dimples to extend the flying distance of the golfdisc. There are smart phone, camera and video display, etc. embedded in the rim of golfdisc to be the head wearing discopter. The headwear discopter takes off from the head of the disc golfer to search the lost golfdisc in the golf course. The wrist-wearing monitor makes the remote surveillance with discopter. The disclub has the versatile combinations of straight pole and golf-style stick to adapt the different situations of disclub golf. The extendable disclub has the pole sliding inside the tube. There are joints for the self-portrait and golf-style disclub.

Claims

1. A gliding means comprising a closed rim airfoil, said rim airfoil has a substantially right angle triangular cross-section with a longer right-angle side being a bottom airfoil edge, an outer rounded corner and curved hypotenuse being upper airfoil edge of said closed rim airfoil, at rear portion of said bottom edge said closed rim airfoil further comprising a substantially right triangle flap, said triangle flap having a longer right-angle side connecting with said bottom airfoil edge, a shorter right-angle side of said rim airfoil and a shorter right-angle side of said triangle flap being in alignment to be nearly vertical curve edge of said closed rim airfoil. (FIG. 20A, FIG. 4F)

2. A gliding means according claim 1, said upper airfoil edge having dimples. (FIG. 22A, FIG. 6A1)

3. A gliding means according claim 1, said bottom airfoil edge having dimples. (FIG. 10B2, FIG. 11B, FIG. 11C)

4. A gliding means according claim 1, said closed rim airfoil further comprising an adaptor, said adaptor being parallel to said vertical curve edge of said closed rim airfoil having an open space between said adaptor and said vertical curve edge of said dosed rim airfoil. (FIG. 22C, FIG. 12C, FIG. 16C1)

5. A gliding means according claim 1, said closed rim airfoil further comprising a central section and an annular shoulder, said shoulder decreasing in thickness from said rim to said central section. (FIG. 21C2)

6. A gliding means according claim 1, further comprising a plurality of propellers to be discopter, said rim airfoil having multiple cavities, said propellers being embedded in said cavities of said rim airfoil, said propeller being mounted on a motor, said motor driving said propeller to rotate. (FIG. 23C)

7. A gliding means according claim 1, further comprising a smart phone and camera means, said smart phone and camera means being pivotally mounted on said rim airfoil; said gliding means having an option of solar cells to provide electrical power to said smart phone and camera means. (FIG. 23B)

8. A gliding means according claim 4, said adaptor having an open that said adaptor being able to adapt the different size of head. (FIG. 17A2 and FIG. 19A1)

9. A disclub golf means comprising a disclub means and disc means, said disclub means has a pole means and disclub head means, said disc means further comprising a discap means, said discap means being rotation mounted on said disclub head means, said disclub head means having screws notched on a cylinder wall, said discap means having a central plateau means fitting inside of said cylinder wall, said discap means having a plurality of locking, click points on the outside wall of said central plateau means, said disclub head means having a plurality of locking click points on the inside of said cylinder wall, a half circle closing near grip side of said pole means, at top of said screws, said cylinder wall of said disclub head means being removed from root of said screws to have slope to remove said disc horizontally. (FIG. 25B, FIG. 26B, FIG. 28B1, FIG. 28B2)

10. A disclub golf means comprising a gliding means and disclub means, said gliding means comprising a dosed rim airfoil, said rim airfoil has a substantially right angle triangular cross-section with a longer right-angle side being a bottom airfoil edge, an outer rounded corner and curved hypotenuse being upper airfoil edge of said closed rim airfoil, at rear portion of said bottom edge said closed rim airfoil further comprising a substantially right triangle flap, said triangle flap having a longer right-angle side connecting with said bottom airfoil edge, a shorter right-angle side of said rim airfoil and a shorter right-angle side of said triangle flap being in alignment to be vertical curve edge of said dosed rim airfoil, said dosed rim airfoil further comprising discap means, said disclub means further comprising disclub head means, said discap means rotationally mounting on and engaging with said disclub head means, swiveling said disclub means, due to eccentric force, said discap means and said gliding means rotating launch to fly in the sky. (FIG. 20A, FIG. 4F, FIG. 1A2, FIG. 1A4).

11. A disclub golf means according to claim 10, said discap moans and disclub head moans having a plurality of cam locking clicking point means to hold said discap means to said disclub head means, said cam locking clicking point being attached to inner wall of said discap means, said cam locking clicking point being attached to outer wall of said disclub head means. (FIG. 27A, FIG. 29C)

12. A disclub golf means according to claim 10, said disclub means has a straight pole, said disclub head means being mounted on an end of said straight pole. (FIG. 1A2, FIG. 33A)

13. A disclub golf means according to claim 10, said disclub means being golf-style disclub, said golf-style disclub haying one short bar connecting to main stick with one bent joint, said disclub head means being mounted on an end of said short bar. (FIG. 1B2, FIG. 34A)

14. A disclub golf means according to claim 10, said disclub means being extendable disclub, said extendable disclub further comprising a pole sliding in a tube, said disclub head means being mounted on an end of said pole; said extendable disclub having options to have elliptical or non-circular sections having long/major axis of the elliptical or non-circular cross section being transverse to a swivel direction of said extendable disclub having option of locking with cavity and bump. (FIG. 1C1, FIG. 1C2, FIG. 35A, FIG. 35B, FIG. 36A, FIG. 36B)

15. A disclub golf means according to claim 14, said extendable disclub being right-hand disclub having left-hand locking screws means and said disclub head having right-hand screw means; said extendable disclub being left-hand disclub having right-hand locking screws means and said disclub head having left-band screw means (FIG. 37A, FIG. 37B)

16. A gliding means according claim 7, wherein said smart phone and camera means comprising TubeFET and SmartCoil; said TubeFET having gate G, source S and drain D; a conducting channel between said source S and said gate D being completely surrounding and embedded in said gate G; said SmartCoil having magnet coil surrounding and driving magnet sensor. (FIG. 42B1, FIG. 42B2)

17. A gliding means according claim 7, wherein said smart phone and camera means comprising green power architecture made of voltage regulator means and current regulator means, a passive charging capacitor means connected between an input of said current regulator means and an input of said voltage regulator means, said current regulator means filtering out switching circuit noise in ground to be current noises, said passive charging capacitor converting said current noises in ground node to be voltage noises in power node, said voltage noises filtering with said voltage regulator means to be voltage potential energy of clean power supply (FIG. 39B, FIG. 44A)

18. A gliding means according claim 7, wherein said smart phone and camera means comprising active common mode choke, said active Common Mode Choke CM choke further comprising voltage regulator means and current regulator means, a noisy input power VDD being connected to said voltage regulator means as input power, an output of said voltage regulator means being clean power VCC, a noisy input ground GND being connected to said current regulator means, an output of said current regulator means being clean ground VSS. (FIG. 44G)

19. A gliding means according claim 7, wherein said camera means comprising bandgap generator, said bandgap generator further comprising a voltage bandgap generator and current bandgap generator, said voltage bandgap generator generating I.sub.PTAT current and V.sub.BG bandgap voltage and feeding them into said current bandgap generator, said current band generate I.sub.BG bandgap current and feeding it into said voltage bandgap generator. (FIG. 46)

20. A gliding means according claim 7, wherein said smart phone and camera means comprising a frequency phase lock loop and an analog front, said frequency phase lock loop further comprise a frequency detector and a phase detector and oscillator means, after said frequency detector detecting frequency, said phase detector detecting phase. said oscillator means having common mode feedback and constant amplitude feedback to control oscillation of said oscillator means, said oscillator having option of inductor to be a planar magnet with a magnet conductor loop inside said planar magnet, said analog front comprising variable gain amplifier and peak detector to convert input analog signal to be digital signal to measure delay and phase of said input analog signal accurately. (FIG. 40A, FIG. 42A, FIG. 45B)

Description

DESCRIPTION AND OPERATION

[0089] The disclub golf has versatile disclubs to play the disclub golf in different ways.

[0090] As shown in FIG. 1A1, FIG. 1A2, FIG. 1A3 and FIG. 1A4, they show the continuous operational pictures of the basic disclub golf.

[0091] As shown in FIG. 1A2, FIG. 1A4, FIG. 4F and FIG. 20A, the disclub golf comprises a gliding golfdisc 1 and disclub 2. The gliding golfdisc 1 comprises a closed rim airfoil 10.

[0092] As shown in FIG. 1A2 & FIG. 33A, the disclub 2 has a straight pole 20. The disclub head 205 being mounted on the end of said straight pole 20.

[0093] As shown in FIG. 20A, FIG. 20B and FIG. 20C, the rim airfoil 10 has a substantially right angle triangular cross-section. An outer rounded corner and curved hypotenuse are the upper airfoil edge of the closed rim airfoil 10. The closed rim airfoil 10 further comprises discap 105. The disclub 2 further comprises disclub head 205. The discap 105 rotationally screws on and engages with the disclub head 205. Swiveling the disclub 2, due to the eccentric force, the discap 105 and the gliding golfdisc 1 rotates and launches to fly in the sky.

[0094] The disclub golfer holds the adjustable handle 208 to swivel the disclub 20. In the FIG. 1A1, the disclub 20 is raised up to be ready to swivel. As shown in FIG. 1A2, the basic disclub 20 is swiveled to the horizontal position. As shown in FIG. 1A3, FIG. 28A1, FIG. 28A2, FIG. 29A and FIG. 29B, applying the snapping action, the cam locking clip mechanism in the discap 105 and disclub head 205 is suddenly released and the disclub golfdisc 1 rotates very fast 180 degrees. As shown in FIG. 1A4, the disclub golfdisc 1 takes off from the disclub head 205 flying in the sky. As shown in FIG. 14A1, FIG. 23B FIG. 30A and FIG. 30B, the disclub golfdisc 1 carries the smart phone and video camera. The video signal transmits back to the wristwatch monitor 3.

[0095] As shown in FIG. 1B2, FIG. 34A and FIG. 38I, the golf-style disclub 21 has one end of pole 211 connecting to short bar 213 with one bent joint 212. The disclub head 205 is mounted on the end of short bar 213.

[0096] As shown in FIG. 1B1, FIG. 1B2, FIG. 1B3 and FIG. 1B4, they show the continuous operational pictures of the golf-style disclub golf. The golfdisc 10 is mounted on the bent short bar 213 of the golf-style disclub 21. In the FIG. 1B1, the golf-style disclub 21 is raised up being ready to swivel. As shown in FIG. 1B2, the golf-style disclub 21 is swiveled to the horizontal position. As shown in FIG. 1B3, applying the snapping action, the cam locking clip mechanism in the discap 105 and disclub head 205 is suddenly released and the golfdisc 1 rotates very fast 180 degrees. As shown in FIG. 1B4, the golfdisc 1 takes off from the disclub head 205 flying in the sky.

[0097] As shown in FIG. 1C1, FIG. 1C2, FIG. 35A, FIG. 35B, FIG. 36A1, FIG. 36B1, FIG. 36A2, FIG. 36B2, FIG. 36A3 and FIG. 36B3, the disclub means is extendable disclub. The extendable disclub comprises a pole sliding in a tube. The disclub head is mounted on the end of the pole. As shown in FIG. 35A, FIG. 35B, FIG. 36A1, FIG. 36B1, FIG. 36A2 and FIG. 36B2, there are callouts to show the cross section of the extendable disclub. In the middle of the extendable disclub, there are elliptical or non-circular sections that the extendable disclub can resist the twist torque of the extendable disclub.

[0098] As shown in FIG. 1C1, the Tarng golfdisc 11 is mounted on the telescopic disclub 22 in the elongated position. As shown in FIG. 1C2, the telescopic disclub 22 in the shortened position. The pole 222 slides in the tube 221. The pole 222 is locked with the tube 221 with the locking screw 2212. The handle 208 is locked to the tube 221, The Tarng golfdisc 11 is mounted on the disclub head 205 with the discap 105.

[0099] As shown in FIG. 1D1, the golf-style disclub 23 has the angle-adjusted joint 2312 to adjust the launch angle of Tarng disc 11. The pole 231 has the bent end. The adjusted joint 2312 is mounted on the bent end of pole 231, The disclub head 205 is mounted on the end bar 232.

[0100] As shown in FIG. 1D2A, the golf-style telescope angle-adjusted disclub 24 comprises the bent pole 242 sliding in the tube 221. The bent pole 242 is locked to the tube 221 with the locking screw 2212. The disclub head 205 is mounted on the short bar 232. The Tarng golfdisc 11 is mounted on the disclub head 205 with discap 105. As shown in FIG. 1D2B, the bent pole 242 is retracted to be carried easily. The adjusted joint 2312 rotates to turn the short bar 232 to fold the golf-style telescope angle-adjusted disclub 24.

[0101] As shown in FIG. 1E1 and FIG. 30A, the telescopic disclub 26 and golfdisc 12 can serve as the self-portrait. The smart phone or camera means 151 is mounted on the Tarng golfdisc 12. The angle-adjusted joint 263 is mounted at the telescopic disclub 26. The Tarng golfdisc 12 is flipped at the self-portrait position to take the photo and video, etc with the smart phone and video camera 151. As shown in FIG. 1E2, the Tarng golfdisc 12 is flipped back to the normal disclub swiveling operation position. As shown in FIG. 19A1, the Tarng golfdisc 12 can be the head-wearing golfdisc 18 to wear on the head. The telescopic disclub 26 serves as the Alpenstock as shown in FIG. 1E2.

[0102] As shown in FIG. 2A, it is the golf bail-throwing trajectory. The golf ball-launching angle is 45 to have the maximum flying distance. As shown in FIG. 2B2, the golf ball 9 rotates. As shown in FIG. 2B1 and FIG. 2B2, the top airflow is speeded up and the pressure is reduced. As shown in FIG. 2B1 and FIG. 2B2 the speed of the bottom airflow is reduced and the pressure is increased. The golf ball floats up due to the pressure difference between the top air and the bottom air. This is referred to be Manus force.

[0103] As shown in FIG. 3A as the disc 10 flies, the speed reduced and the angle of attack is increased. As shown in FIG. 3B1, the disc 10 flies and rotates. Due to the conservation of the rotational momentum of gyroscopic force, the disc 10 keeps the same orientation. As the disc 10 Falls down, the angle of attack becomes much larger. The disc 10 is more like the parachute dropping to the ground. The potential energy of disc 10 does not convert to the dynamic flying energy of the glider. The flying distance of the falling trajectory of the disc 10 is much less than the flying distance of the rising trajectory of the disc 10. As shown in FIG. 3B2, with the Tarng golfdisc 11, the rising trajectory and falling trajectory are symmetrical. Therefore, the gliding Tarng golfdisc 11 is more like the glider to be named as the gliding disc. The flying distance of gliding Tarng golfdisc 11 is larger than the disc 10.

[0104] As shown in FIG. 4A1, it is the isometric top view of the frictionless super-lift golfdisc 10, As shown in FIG. 4A2, it is the transparent isometric top view of the frictionless super-lift solar cell golfdisc 1s. As shown in FIG. 4B1, it is the bottom view of the frictionless super-lift golfdisc 10. As shown in FIG. 4B2, it is the transparent isometric bottom view of the frictionless super-lift solar cell golfdisc 1s. As shown in FIG. 4C1, it is the isometric bottom view of the frictionless super-lift golfdisc 10. As shown in FIG. 4C2, it is the transparent isometric bottom view of the frictionless super-lift solar cell golfdisc 1s. The discap 105 is embedded in the frictionless super-lift golfdisc 10.

[0105] As shown in FIG. 4D, FIG. 4E and FIG. 4F, it shows the side view of the frictionless super-lift golfdisc 10. As shown in FIG. 20A, the bottom edge 101 of the frictionless super-lift golfdisc 10 is flat. The triangle flap 102 is at the tail end of said bottom edge 101. The stability edge 103 is to maintain the side stability of the frictionless super-lift golfdisc 10. However, the stability edge 103 will cause the stagnation point generating the drag force at the trailing edge of the frictionless super-lift golfdisc.

[0106] FIG. 4E is the transparent side view of the frictionless super-lift golfdisc 10. It shows the discap 105 embedded in the triangle rim of the frictionless super-lift golfdisc 10. FIG. 4F is the section view to show the structure of the discap 105 and the dome structure of the frictionless super-lift golfdisc 10.

[0107] As shown in FIG. 4E, FIG. 4F, FIG. 6C2 and FIG. 6C3, the plateau 1055 inside the discap 105 is to reduce the air flowing into the discap to minimize the air drag force. The hole 1050 embedded inside the plateau 1055 is for the plastic module injection of the golfdisc 10. The screw 1056 embedded inside the discap 105 is to rotationally mount the discap 105 on the screw 2056 of the disclub head 205 as shown in FIG. 26A and FIG. 26B.

[0108] As shown in FIG. 5A1, the disc 10 flies with velocity V.sub.DISC and rotates counter-clockwise with V.sub.SPIN. The weight of disc 10 is simplified to be the gravity force F.sub.G at the Center Of Gravity CG. All the air pressure force is simplified to be the F.sub.LIFT applied at the Center Of Pressure CP. As the Center Of Pressure CP is located after the Center Of Gravity CG, the lift force F.sub.LIFT generates positive pitch moment MP.sub.LIFT. To make the analysis simple with the intuition, due to the gyroscopic force, the lift force F.sub.LIFT and spin V.sub.SPIN generate the equivalent pseudo force PR.sub.LIFT to generate the left banking moment MB.sub.LIFT.

[0109] As shown in FIG. 5A2, the disc 10 flies with velocity V.sub.DISC and rotates counter-clockwise with V.sub.SPIN. The weight of disc 10 is simplified to be the gravity force F.sub.G at the Center Of Gravity CG. All the air pressure force is simplified to be the F.sub.LIFT applied at the Center Of Pressure CP. The Center Of Pressure CP is located before the Center Of Gravity CG. The lift force F.sub.LIFT generates negative pitch moment MP.sub.LIFT. The lift force F.sub.LIFT and spin V.sub.SPIN generate the pseudo force PR.sub.LIFT to generate the right banking moment MB.sub.LIFT.

[0110] As shown in FIG. 5B1, the disc 10 flies with velocity V.sub.DISC and rotates clockwise with V.sub.SPIN. The weight of disc 10 is simplified to be the gravity force F.sub.G at the Center Of Gravity CG. All the air pressure force is simplified to be the F.sub.LIFT applied at the Center Of Pressure CP. The Center Of Pressure CP is located after the Center Of Gravity CG. The lift force F.sub.LIFT generates positive pitch moment MP.sub.LIFT. The lift force F.sub.LIFT and spin V.sub.SPIN generate the pseudo force FR.sub.LIFT to generate the right banking moment MB.sub.LIFT.

[0111] As shown in FIG. 5B2, the disc 10 flies with velocity V.sub.DISC and rotates clockwise with V.sub.SPIN. The weight of disc 10 is simplified to be the gravity force F.sub.G at the Center Of Gravity CG. All the air pressure three is simplified to be the F.sub.LIFT applied at the Center Of Pressure CP. The Center Of Pressure CP is located before the Center Of Gravity CG. The lift force F.sub.LIFT generates negative pitch moment MP.sub.LIFT. The lift force F.sub.LIFT and spin V.sub.SPIN generate the pseudo force PR.sub.LIFT to generate the left banking moment MB.sub.LIFT.

[0112] As shown in FIG. 5C, it is the trajectory and attitude of the conventional disc. As shown in FIG. 5C, FIG. 5C1 and FIG. 3B1, at the beginning of trajectory, the velocity of disc 10 is fast and the CP is located after CG. The disc 10 rotates clockwise and the disc 10 bank right. The flying distance of the rising trajectory is much longer. As shown in FIG. 5C, FIG. 5C2 and FIG. 3B1, at the end of trajectory, the velocity of disc 10 is slow and the CP is located before CG. The disc 10 rotates clockwise and the disc 10 bank left. The flying distance of the l thing trajectory is much shorter.

[0113] As shown in FIG. 3B2, FIG. 6A1, FIG. 6A2, FIG. 6B1, FIG. 6B2 and FIG. 6C1, to enhance the flying distance of disc, the Tarng Disc 11 is adopted. There are many dimples on the rim of the Tarng Disc 11. As shown in FIG. 6C2, the dimples are concave holes. As shown in FIG. 6C3, the dimples are convex bumps.

[0114] As shown in FIG. 7A1, the Tarng Disc 11 having the dimples 110 on the rim of disc 1. The Tarng Disc 11 moves forward with velocity V.sub.DISC and spin counter clockwise with velocity. V.sub.SPIN. As shown in FIG. 7A1, on the left side of the Tarng Disc 11, the air velocity is V.sub.AIR+V.sub.SPIN. As shown in FIG. 7A2, the air pressure is reduced and there is up-lift force is +(F.sub.SPIN). As shown in FIG. 7A1, on the right side of the Tarng Disc 11, the air velocity is (V.sub.AIRV.sub.SPIN). As shown in FIG. 7A2, the air pressure increases and there is downward force is (F.sub.SPIN). Due to the counter-clockwise spin of Tarng Disc 11, the pseudo-force (+FR.sub.SPIN) and (FR.sub.SPIN) generate the positive pitching moment MP.sub.SPIN. The Tarng Disc 11 banks right.

[0115] As shown in FIG. 7B1, the Tarng Disc 11 has the dimples 110 on the rim of disc 11. The Tarng Disc 11 moves forward with velocity V.sub.DISC and spin clockwise with velocity V.sub.SPIN. As shown in FIG. 7B1, on the left side of the Tarng Disc 11, the air velocity is (V.sub.AIRV.sub.SPIN). As shown in FIG. 7B2, the air pressure is increased and there is downward force is (F.sub.SPIN). As shown in FIG. 7B1, on the right side of the Tarng Disc 11, the air velocity is (V.sub.AIR+V.sub.SPIN). As shown in FIG. 7B2, the air pressure reduces and there is upward force is (+F.sub.SPIN). Due to the clockwise spin of Tarng Disc 11, the pseudo-force (+FR.sub.SPIN) and (FR.sub.SPIN) also generate the positive pitching moment MP.sub.SPIN. The Tarng Disc 11 banks left. In other words, both clockwise and counter-clockwise rotations generate the positive pitching moment for the parabolic trajectory as shown in FIG. 3B2.

[0116] As shown in FIG. 8A1, the Tarng Disc 11 has all the forces and moments are included in one picture. The forces and moments are pressure, Tarng Force and weight threes and the momentums generated by the pressure and Tarng force on the flying and rotating disc. The Tarng Disc 11 rotates counter-clockwise. The Center of Pressure CP is located after the Center of Gravity CG. It is noted that both MP.sub.LIFT and MP.sub.SPIN are positive pitching moments. Therefore, the launch angle can be lamer than 0. As shown in FIG. 3B2 and FIG. 9A, the flying trajectory is parabolic and the flying distance is enhanced. The bank moments MB.sub.LIFT and MB.sub.SPIN cancel each other. Therefore, as shown in FIG. 9C, the Tarng Disc 11 moves forward without tilting as shown in FIG. 9B. This case is the best performance of the Tarng Disc 11. Therefore, we try to operate in this case.

[0117] As shown in FIG. 8A2, the Tarng Disc 11 has all the forces and moments are included in one picture. The forces and moments are pressure, Tarng Force and weight force and the momentums generated by the pressure and Tarng force on the flying and rotating disc. The Tarng Disc 11 rotates counter-clockwise. The Center of Pressure CP is located before the Center of Gravity CG. It is noted that MP.sub.LIFT is negative pitching moment and MP.sub.SPIN is positive pitching moment. The moments MP.sub.LIFT and MP.sub.SPIN cancel each other. Therefore, the launch angle is 0. Both the bank moments MB.sub.LIFT and MB.sub.SPIN bank right. The Tarng Disc 11 tilts right. Therefore, we try not to operate in this case. This is the launching angle limit for the Tarng Disc 11.

[0118] As shown in FIG. 8B1, the Tarng Disc 11 has all the forces and moments are included in one picture. The forces and moments are pressure, Tarng Force and weight force and the momentums generated by the pressure and Tarng force on the flying and rotating disc. The Tarng Disc 11 rotates clockwise. The Center of Pressure CP is located after the Center of Gravity CG. It is noted that both MP.sub.LIFT and MP.sub.SPIN are positive pitching moments. Therefore, the launch angle can be larger than 0. As shown in FIG. 3B2 and FIG. 9A, the flying trajectory is parabolic and the flying distance is enhanced. The bank moments MB.sub.LIFT and MB.sub.SPIN cancel each other. Therefore, as shown in FIG. 9C, the Tarng Disc 11 moves forward without tilting as shown in FIG. 9B. This case is the best performance of the Tarng Disc 11. Therefore, we try to operate in this case.

[0119] As shown in FIG. 8B2, the Tarng Disc 11 has all the forces and moments are included in one picture. The forces and moments are pressure, Tarng Force and weight force and the momentums generated by the pressure and Tarng force on the flying and rotating disc. The Tarng Disc 11 rotates clockwise. The Center of Pressure CP is located before the Center of Gravity CG. It is noted that MP.sub.LIFT is negative pitching moment and MP.sub.SPIN is positive pitching moment. The moments MP.sub.LIFT and MP.sub.SPIN cancel each other. Therefore, the launch angle is 0. The bank moments MB.sub.LIFT and MB.sub.SPIN bank left. Therefore, the Tarng Disc 11 tilts left. Therefore, we try not to operate in this case. This is the launching angle limit for the Tarng Disc 11.

[0120] As shown in FIG. 8A1 and FIG. 8B1, the dimples on the top surface of Tarng Disc 11 have the same effect for the clockwise direction and counter-clockwise direction. Therefore, the dimple on the top of Tarng Disc 11 can be the round bump or round cavity which is universal in all directions.

[0121] As shown in FIG. 10A1, FIG. 10A2, FIG. 10B1 and FIG. B2, the dimples 120 of Tarng Disc 12 also locate on the bottom plate of the Tarng Disc 12. However, as shown in FIG. 11B and FIG. 11C, the dimples 120 are uni-directional dimples. There are different lift forces in the right bottom plate and left bottom plate. The lift force is more like the aerofoil lift force. Therefore, the section of the dimple is different to be the uni-directional dimples,

[0122] As shown in the FIG. 11B and FIG. 11C, the dimple has the unsymmetrical concave. The unsymmetrical concave dimple is similar to the arch of the bottom plate of the aerofoil. It has the different lift forces in the different directions. As shown in FIG. 11B, the lift force is larger than the lilt force as shown in FIG. 11C. As shown in FIG. 11A, the (+F.sub.SPIN,BOTTOM) pushes the disc 12 upward and the (F.sub.SPIN,BOTTOM) pulls the disc 12 downward. Comparing FIG. 8A1 with FIG. 11A, the (+F.sub.SPIN,BOTTOM) in FIG. 11A is the addition to the (+F.sub.SPIN) FIG. 8A1; the (F.sub.SPIN,BOTTOM) in FIG. 11A is the addition to the (F.sub.SPIN) in FIG. 8A1.

[0123] As shown in FIG. 11A, FIG. 11B and FIG. 1C, on the bottom airfoil edge of the gliding golfdisc has dimples. The dimples on the bottom edge have directional sense. As shown in FIG. 11A, this is the clockwise Tarng disc 12 having the dimples on the bottom surface of Tarng disc 12. Being similar to the clockwise Tarng disc 12 in FIG. 11A, just flip the dimple in the horizontal direction as shown in the FIG. 11B and FIG. 11C, we can have the counter-clockwise Tarng disc.

[0124] As shown in FIG. 12A1, FIG. 12A2, FIG. 12B1, FIG. 12B2 and FIG. 12C, the super-lift Adaptive Tarng Disc 13 has the adaptive fin 130 to reduce the drag during the glide of the super-lift Adaptive Tarng Disc 13. The adaptive fin 130 is to reduce the drag force of the stagnation point of the stability edge 103 at the trailing edge of super-lift Adaptive Tarng Disc 13. The height of the adaptive fin 130 is less than the stability edge 103. At the side edge of disc 13, the stability edge 103 serves as the stability fin. The inside curvature 1030 is much larger that the flow will not generate the stagnation point as the stability 103 does. Therefore, the air drag force of disc 13 is reduced. At the front edge, without the adaptive fin 130, the flow becomes the turbulent flow. The turbulent flow increases the drag force a lot. With the adaptive fin 130, the flow becomes laminar flow. The air drag force of the laminar flow reduces a lot.

[0125] As shown in FIG. 13A, FIG. 13B and FIG. 13C, the propeller 141 of the discopter 14 is mounted on the triangle shaped rim of the super lit Adaptive discopter Tarng golfdisc 14. The super-lift Adaptive discopter Tarng discgolf 14 can wear on head that the super-lift Adaptive discopter Tarng golfdisc 14 can take off from the head. With the adaptive fin 130, the super-lift Adaptive discopter Tarng golfdisc 14 can wear on head.

[0126] As shown in FIG. 14A1, FIG. 14A2, FIG. 14B1, FIG. 14B2, FIG. 15A1, FIG. 15A2, 15B1 and FIG. 15B2, the remote surveillance super-lift Adaptive discopter Tarng golfdisc 15 has the smart phone and remote surveillance video camera 151. The smart phone and remote surveillance video camera 151 takes the video. The video signal is transmitted to the wrist monitor 3. As shown in FIG. 15A2 and FIG. 15B2, the solar cell golfdisc 15s provides the electricity to the smart camera 151 and discopter 152.

[0127] The earphone and microphone 152 is one curved bracket can hide in the space between the adaptor 130 and stability edge 103. The disc golfer wears the golfdisc 15 on his head. As the disc golfer wants to speak, the curved bracket pivotally rotates down and the microphone 152 is close to the disc golfer's mouth to speak.

[0128] As shown in FIG. 16A1, FIG. 16A2, FIG. 16B1, FIG. 16B2, FIG. 16C1 and FIG. 16C2, the remote surveillance super-lift Adaptive discopter Tarng golfring 16 has the smart phone and remote surveillance video camera 151. The remote surveillance super-lift Adaptive discopter Tarng golfing 16 can wear on head. As shown in FIG. 16A2 and FIG. 16B2, the solar cell golfdisc 16s provides the electricity to the smart camera 151 and discopter 152.

[0129] As shown in FIG. 17A1, FIG. 17A2, FIG. 17B1 and FIG. 17B2, the remote surveillance super-lift adjustable Adaptive discopter Thing golfring 17 has the adjustable adaptive ring 170 to fit the different size head. The adjustable adaptive ring 170 has an opening to adapt the different size of the heads and offering the spring force to clamp the head. As shown in FIG. 17A2 and FIG. 17B2, the solar cell golfdisc 17s provides the electricity to the smart camera 151 and discopter 152.

[0130] As shown in FIG. 18A1, FIG. 18A2, FIG. 18B1 and FIG. 18B2, the remote surveillance super-lift elastic adjustable Adaptive discopter Tarng golfdisc 18 has the top cover 181 to be elastic in the disc form.

[0131] As shown in FIG. 18B2 and FIG. 19B2, the adaptor 181b of gliding golfdisc 18 has an opening that the adaptor 181b is able to adapt the different size of head. As shown in FIG. 18A2 and FIG. 18B2, the solar cell golfdisc 18s provides the electricity to the smart camera 151 and discopter 152.

[0132] As shown in FIG. 19A1, FIG. 19A2, FIG. 19B1 and FIG. 19B2, the remote surveillance super-lift elastic adjustable Adaptive discopter Tarng golfdisc 18 has the top cover 181 to be elastic in the hat form. As shown in FIG. 19A2 and FIG. 19B2, the solar cell golfdisc 18s provides the electricity to the smart camera 151 and discopter 152.

[0133] As shown in FIG. 20A and FIG. 4D, the super-lift disc 10 has the bottom edge 101 to be flat in the horizontal direction. At the trail edge of the bottom edge 101, the flap 102 is in the right triangle shape with fitting curvatures. The flap 102 makes the super-lift disc 10 having the super-lift.

[0134] The gliding golfdisc as shown in FIG. 4A2 comprises a closed rim airfoil 10 as shown in FIG. 20A. The rim airfoil 10 has a substantially right angle triangular cross-section with the longer right-angle side being a bottom airfoil edge 101 as shown in FIG. 20C. An outer rounded corner and curved hypotenuse being upper airfoil edge 100 of the closed rim airfoil 10. At the rear portion of the bottom edge 101, the closed rim airfoil 10 further comprises a substantially right triangle flap 102. As shown in FIG. 20C, the triangle flap 102 has a longer right-angle side connecting with the bottom airfoil edge 101. The shorter right-angle side of the rim airfoil 10 and the shorter right-angle side of the triangle flap 102 being in alignment to be one nearly vertical curve 103 of the closed rim airfoil 10.

[0135] As shown in FIG. 20B and FIG. 4E, the discap 105 has the bottom edge 101 to be flat. The stability edge 103 is a nearly vertical curve as the conventional disc does. As shown in FIG. 20C and FIG. 4F, to reduce the air drag force, the discap 105 has the plateau 1055. The plateau 1055 fills up the cavity of the discap 105. The plateau 1055 prevents the air flowing into the cavity of discap 105. In the middle of the plateau 1055, there is a rectangle slot 1050. During the plastic injection process, the rectangle slot 1050 is to hold the discap 105 to the wall of the plastic module. The screw 1056 is to engage with the screw 2056 of the disclub head 205 as shown in FIG. 26B.

[0136] As shown in FIG. 21A, FIG. 21B, FIG. 21C1, FIG. 21C2 and FIG. 6C1, is super-lift Tarng golfdisc 11 has the trail triangle flap 102, curved dome 104 and the dimples 110. The trail triangle flap 102, curved dome 104 and the dimples 110 makes the super-lift Tarng golfdisc 11 having the superior flying capability. The anti-thrust stubs 1057 are on the top of discap 105. As shown in FIG. 21B, to reduce the air drag to have the long-range drift and glide capability, the curved dome 104 eliminates the stagnation point of the stability edge 103 as shown in FIG. 20B and FIG. 41E. However, the bottom edge of the curved dome 104 is still nearly vertical that it still has the stability function for the golfdisc 11.

[0137] As shown in FIG. 22A FIG. 22B, FIG. 22C and FIG. 12C, the stability edge 103 is lower than the adaptive fin 130. The stability edge 103 is to stabilize the disc 13 at the right side and left side of golfdisc 13. At the rear edge of the golfdisc 13, the adaptive fin 130 is to reduce the drag force of the stagnation point of stability edge 103. At the front edge of the disc 13, the adaptive fin 130 is to reduce the turbulent flow of the stability edge 103.

[0138] As shown in FIG. 21A and FIG. 22A, the upper surface of the airfoil rim 13 of the gliding golfdisc has dimples.

[0139] As shown in FIG. 21C2, the closed rim airfoil of the gliding golfdisc comprises a central section 106 and an annular shoulder 104. The shoulder 104 decreases in thickness from the rim to the central section 106.

[0140] As shown in FIG. 22C, FIG. 12C and FIG. 16C1, the closed rim airfoil 13 of the gliding golfdisc comprises an adaptor 130. The adaptor 130 is parallel to the vertical edge 103 of the closed rim airfoil 13 Between the adaptor 130 and the vertical edge 103, there is an open space.

[0141] As shown in FIG. 23A and FIG. 17A1, they show the isometric section view of the discopter 17 in the disc-ring shape. As shown in FIG. 23B and FIG. 15A1, they show the isometric section view of the smart phone and camera means 151 of the remote surveillance super-lift Adaptive discopter Tarng golfdisc 15. As shown in FIG. 23C and FIG. 15A1, they show the isometric section view of the propeller 141 of the discopter for the remote surveillance super-lift Adaptive discopter Tarng golfdisc 15. The motor 1410 drives the blade 1411 to rotate.

[0142] As shown in FIG. 23B the gliding means further comprises a smart phone and camera means 151. The smart phone and camera, means 151 is pivotally mounted on said rim airfoil 15.

[0143] As shown in FIG. 23C, the gliding golfdisc further comprises the propellers 141 to be the discopter. The rim airfoil 15 has multiple cavities. The discopter 141 is embedded in the cavity of the rim airfoil 15. The discopter 141 has a propeller 1411 mounted on a motor 1410. The motor 1410 drives the propeller 1411 to rotate.

[0144] To have the long drive for the disc, being similar to the golf ball hit by the club head, the golfdisc 1 is hit with the disclub head 205. However, as the disc 1 is launched, the disc 1 is moving. To keep the disc 1 to be fixed on the disclub head 205, as shown in FIG. 24A, the cam-locking click point 1051 of the discap 105 is held against the cam-locking click point 2051 of the disclub head 205.

[0145] As shown in FIG. 24B, the discap 105 is clamped between the cam-locking click force of the cam-locking click points 1051 and 2051 and the wedge force of screw tighten between the discap 105 and the club head 205. The disc 1 and discap 105 are held to the disclub head 205. The wedge force of the screw tighten force is the tighten force between the discap 105 and the head 205 of disclub, The rotation angle of the discap 105 on the disclub head 205 is about 165.

[0146] As shown in FIG. 25A and FIG. 25B, the click point 1051 is located at the rim of the plateau 1055. The plateau 1055 eliminates the big hole space of the discap 105. The rectangle hole 1050 is at the center of the plateau 1055. It is to hold the discap 105 to the wall of the module for the plastic injection. As shown in FIG. 25B, between the screw 1056 and the plateau 1050, there is a rim-type space to fit for the screw 2056 of the disclub head 205 as shown in FIG. 26A. As shown in FIG. 25C, the anti-thrust stubs 1057 are on the top of the discap 105. They absorb the thrust force as the snapping force applied to the discap 105. The holes 1058 are for the bonding between the disc 1 and the discap 105.

[0147] As shown in FIG. 26A, FIG. 26B and FIG. 26C, the slope 2058 of disclub head 205 is adapted to the triangle flap 102 of discap 105 as shown in FIG. 20A. As the disc 1 rotates about 165 the bottom edge of the discap 105 engages with the flat step 2059 and the triangle flap 102 fits with the slope 2058. The bottom edge 101 of the discap 105 engages with the fiat step 2059 generates the wedge force as shown in FIG. 24B. The solar cell 205s provides the electricity to the smart camera 151 and discopter 152.

[0148] As shown in FIG. 27B and FIG. 29D, the discap and disclub head have a plurality of cam locking clicking point to hold the discap 105 to the disclub head 205. The cam locking clicking point 1051 is attached to inner wall of the discap 105. The cam locking clicking point 2053 is attached to the outer wall of the disclub head 205.

[0149] As shown in FIG. 27A and FIG. 27B, they show the single cam-locking clicking point structure. FIG. 27A shows the single cam-locking clicking point 1051 and cam-locking clicking point 2051 being in the lock position. FIG. 27B shows the single cam-locking clicking point 1051 and cam-locking clicking point 2051 being in the release position. The solar cell 205s provides the electricity to the smart camera 151 and discopter 152.

[0150] To adjust the flying distance of the disc, we can adjust the snapping force with the multiple cam-locking clicking points. As shown in FIG. 28A1 and FIG. 28B1, they show the discap 105 having the multiple cam-locking click points, 1051, 1052 and 1053. As shown in FIG. 28A2 and FIG. 28B2, they show the disclub head 205 having the multiple cam-locking click points, 2051, 2052 and 2053. As shown in FIG. 29A and FIG. 29B, they show the cam-locking clicking point structure. FIG. 29A shows the cam-locking triple clicking point in the release position. FIG. 29B shows the cam-locking triple clicking point at the single lock position having one click point in the lock position. FIG. 29C shows the cam-locking triple clicking point at the double lock position having two click points in the lock position. FIG. 29D shows the cam-locking triple clicking point at the triple lock position having three click points in the lock position.

[0151] As shown in FIG. 30A and FIG. 30B, the smart phone 151 comprises the versatile vision facilities 1512 and 1513 such as camera, holographic projector light, laser, speaker, antenna and infrared, etc. As shown in FIG. 23B, the smart phone 151 is mounted on the golfdisc 1 with the pivotal axis 1511.

[0152] As shown in FIG. 31A and FIG. 31B, the discopter 141 has the propeller 1411 mounted on the motor 1410. As shown in FIG. 23C and FIG. 30A, the propeller 141 of discopter 15 is mounted in the frame of golfdisc rim.

[0153] As shown in FIG. 32A, FIG. 32B, FIG. 1E1 and FIG. 1E2, the golfdisc 12 and disclub 26 can serve as the self-portrait with the camera of smart phone 151. As shown in FIG. 32D1 and FIG. 32D2, the disclub head 205 is mounted a pivotal joint 206. As shown in FIG. 32C1, FIG. 32C2, FIG. 32D1, FIG. 32D2, FIG. 32E1, FIG. 32E2 and FIG. 32F, pulling the cam handle 2632 to rotate on the pixel 26311 to release the lock axle 2631. Pushing the cam handle 2632 to rotate on the pixel 26311, the cam 26310 engages with the fork 2630 to pull the lock axle 2631. As shown in FIG. 32F, the slope 26313 of the lock axle 2631 pushes the slope 20603 of the club head block 2060 to engage the club head block 2060 with the fork 2630.

[0154] As shown in FIG. 33A and FIG. 33B, the disclub 20 has the grip 208 and the club bead 205. The disclub head 205 is mounted on the disclub head tube 203. As shown in FIG. 38A1 and FIG. 38A2, the grip 208 has the clamping ring 2082 and the cam handle 2081. Pushing the cam handle 2081, the cam at the top of the cam handle 2081 will push the 2082 to lock the handle 2081 to the club 20.

[0155] As shown in FIG. 34A and FIG. 34B, the golf-club style disclub 21 has the handle 208 and the club head 205. The disclub head 205 is mounted on the disclub head tube 203. As shown in FIG. 35A, FIG. 36A1, FIG. 36A2 and FIG. 36A3, the telescopic disclub 22, 22e and 22f are in the elongation position. As shown in the FIG. 35A and FIG. 36A1, the callouts show the cross sections of the extendable disclub 22e. The disclub tube 221e and disclub pole 222e have the smooth transition between the circle and elliptical or non-circular cross sections. The elliptical or non-circular section of the disclub tube 221e and disclub pole 222e at the joint portions can resist the twist torque during the swivel of the disclub. The long/major axis of the elliptical or non circular cross section is transverse the swivel direction of the extendable disclub 22e. As shown in FIG. 35A and FIG. 36A1, the bulk 2212e is optional. The bulk 2212e can strengthen the joint to resist the twist torque during the swivel of the disclub 22e. As shown in FIG. 38B3 and FIG. 38B4, the extended pole 222e and tube 221e have the elliptical and non-circular section The tube 221e has one cavity 221c. The pole 222e has one bump 222b. The bump 222b fits in the cavity 221c to lock the pole 222e with the tube 221e. The knotch 222k is to increase the elasticity of the operation of the hump 222b and the cavity 221c. As shown in FIG. 35B, FIG. 36B1, FIG. 36B2 and FIG. 36B3, the telescopic disclub 22, 22e and 22f are in the shortened position. As shown in FIG. 36A2 and FIG. 38B2, the screw 2212 is screwed on the tube 221 to tighten the pole 222. As shown in FIG. 36A2, all the callouts have the circle sections. To resist the twist torque, the friction craw 2215 is adopted. As shown in FIG. 36A2, all the callouts of disclub 22 are circular cross sections view. It needs the self-tighten mechanism of friction craw 2215 to resist the twist torque. The length of disclub 22 can be adjusted freely. As shown in FIG. 36A3 and FIG. 36B3, the torque free disclub 22f has no torque during the swivel of disclub 22. The extend pole 222f has one bend that the disclub head 205 is aligned with the centerline 22fc of the torque free disclub 22f. Since the disclub head 205 is aligned with the centerline 22fc of the torque free disclub 22f, the torque is very small during the swivel of the torque free disclub 22f.

[0156] As shown in FIG. 38C1, FIG. 38C2, FIG. 38D1, FIG. 38D2, FIG. 38E1, FIG. 38E2, FIG. 38F and FIG. 38G, the friction craw 2215 is constituted of the craw 22152 and the driving screw 22151. The driving screw 22151 drives the claw 22152. The friction craw 2215 biases against the internal wall of the tube 221, Rotating the pole 222 to disengage the lock between the pole 222 and the tube 221, the pole 222 can slide inside the tube 221. Rotating the pole in the reverse direction to engage the lock between the pole 222 and the tube 221, the pole 222 is locked with the tube 221. This is the internal lock. Furthermore, there is the external lock. As shown in FIG. 38B1, FIG. 38B2 and FIG. 36A2, the screw 2212 locks the internal sliding pole 222 with the external tube 221. This is the external lock. With both the internal lock and external lock, the sliding pole 222 can be locked to the tube 221 firmly to be the discgolf stick.

[0157] Referring to FIG. 38C1, FIG. 38C2 and FIG. 37A, due to the twisting moment, the telescopic disclub 22 has the self-tighten feature to be the right-hand telescopic disclub 22R as shown in FIG. 37A and left-hand telescopic disclub 22L as shown in FIG. 37B.

[0158] As shown in FIG. 37A, the extendable disclub 22R is right-hand disclub having the left-hand locking screw 2212L and 2215L. All the callouts have the circular cross sections. The disclub head 205R is right-hand screw.

[0159] As shown in FIG. 37A, swiveling the right-hand telescopic disclub 22R, the twisting momentum is left-hand momentum. The friction screw 2215L and the screw 2212L are left-hand screw to have the self-tighten effect.

[0160] As shown in FIG. 37B, the extendable disclub is left-band disclub having the right-hand locking screw 2212R and 2215R. All the callouts have the circular cross sections. The disclub head 205L is left-hand screw.

[0161] As shown in FIG. 37B, swiveling the left-hand telescopic disclub 22R, the twisting momentum is right-hand momentum. The friction screw 2215R and the screw 2212R are right-hand screw to have the self-tighten effect.

[0162] Being similar to FIG. 32A and FIG. 32B, the U-joint 2312 is made of the U-fork 263J and pivotal head 205J as shown in FIG. 38H. As the cam handle 2632J is pushed down to lock the U-joint 2312, the pivotal block 2060J biases against the wall of U-fork 263J. As shown in FIG. 1D2A, FIG. 38H and FIG. 38I, the end bar 232 is mounted on the joint end 205J.

[0163] As shown in FIG. 39A and FIG. 14A1, the wrist-wearing video monitor 3 has the video 31 displayed on the flexible film 30. As shown in FIG. 39B and FIG. 23B, the architecture of the head wearing smart phone wireless camera 151 and the video monitor 3 has the DropLess Voltage regulator DLVR, DropLess Current Regulator DLIR, Frequency Phase Lock Loop FPLL, Radio Front RF, Analog Front AF and Inductor Capacitor Oscillator LCO, etc. As shown in FIG. 40A1, FIG. 40A2, FIG. 40B and FIG. 40C, it is the operation of the LC oscillator LCO. The inductor L1 in FIG. 40A2 might be implemented with the inductor as shown in FIG. 42A. As shown in FIG. 41A1, FIG. 41A2, FIG. 41B, FIG. 41C and FIG. 41D, it is the operation of the FPLL.

[0164] The conventional concept of the phase noise is completely wrong. The clock oscillation is

fclk(t)=B+Asin(t+(t))

[0165] Assuming no phase noise, (t)=0

fclk(t)=B+Asin(t)

=2/(LC.sub.TUNE).sup.1/2

[0166] To completely specify the sinusoidal oscillation of the clock, we need one set having tour parameters, [L, C, A B],

[0167] However, the conventional LCO design has only [L, C] two parameters.

[0168] From the following equations, they show the variance of the amplitude AA and the wandering variance of the baseline/center line B will generate the phase noise (t).

[00001]$\begin{array}{c}\mathrm{fclk}\left(t\right)=.Math.B+A.Math..Math.\sin \left(.Math..Math.t+\left(t\right)\right)\\ =.Math.\left(B+.Math..Math.B\right)+\left(A+.Math..Math.A\right).Math.\sin .Math..Math..Math..Math.t\end{array}$

[0169] The variance of [A, ] becomes the phase noise.

(t)=sin.sup.1{[B+A sin t]/A}

[0170] From the above equation, as A=0 and B=0, the phase noise (t)=0. In other words, to clean out the phase noises, we need to specify the four parameters, [L, C, A, B] to have the A=0 and B=0.

[0171] The amplitude A and baseline B can also be measured with the [0172] A.sub.PEAK: maximum value of A [0173] A.sub.VALLEY: minimum value of A

A=(A.sub.PEAKA.sub.VALLEY)/2

B=(A.sub.PEAK+A.sub.VALLEY)/2

[0174] As shown in FIG. 40A1 and FIG. 40A2, the oscillator has the Common Mode FeedBack CMFB, B=const, feedback B to cancel the B noise. The oscillator has the Constant Amplitude FeedBack CAFB, A=const, feedback A to cancel the A noise.

[0175] As shown in FIG. 40B, it is the mathematical model of the noiseless LCO. The LCO generates f.sub.osc as shown in the curve of f.sub.oscf in FIG. 40C. The local oscillator generates frequency (f.sub.o). The local oscillator frequency (f.sub.o) mixes with the LCO output f.sub.osc. As shown by the curve f.sub.noisef in FIG. 40C, the mixture of the output passes the low pass filter LPF to get the f.sub.noise. The f.sub.noise feedbacks to cancel the f.sub.noise.

[0176] As shown in FIG. 41A1 and FIG. 41A2, they show the waveforms of the operation of the FPLL Frequency-Phase Lock Loop. FIG. 41B shows the architecture of the controller of the FPLL Frequency-Phase Lock Loop. As shown in FIG. 41D, the complete FPLL is constituted of the FPLL controller and the OSC oscillator as shown in FIG. 40A.

[0177] As shown in FIG. 41C, the dotted line is the output frequency of the conventional PLL phase lock loop. The solid line is the output frequency of FPLL. The settling time of the FPLL frequency phase lock is much faster than the conventional PLL. As shown in FIG. 41D, the counter is served as the FLL frequency detector. As shown in FIG. 41B, as the counter finishes count N, the CLK.sub.FB is generated. The phase detector is only serves as the PLL phase detector.

[0178] As the counter is counted to the preset value N, the counter is reset for the next cycle of frequency count. At beginning of the count, the oscillator has the injection lock synchronization to synchronize the input reference clock with the oscillator. As shown in FIG. 41A1, the oscillation conies earlier than the reference clock; the Inject Lock Synchronization makes the synchronization of the reference clock and the oscillator immediately. As shown in FIG. 41A2, the oscillation comes later than the reference clock; the Inject Lock Synchronization makes the synchronization of the reference clock and the oscillator in the next cycle of the reference clock. As shown in FIG. 41B, FIG. 41A1 and FIG. 41A2, the SyncGate is to control the synchronization of the reference clock and the oscillator.

[0179] As shown in FIG. 42A, the planar magnet 40 has the magnet conductor loop 41 and magnet sensor 401. As shown in FIG. 42B1, it is the TubeFET having the gate G, source S and drain D. The conducting channel between the source S and gate D is completely surrounding and embedded in the gate G. Being similar to the TubeFET, as shown in FIG. 42B2, the SmartCoil has the magnet coil completely surrounds and driving the magnet sensor 401. The magnet sensor 401 has the structure of TubeFET. FIG. 43A shows the smart capless LDVR Low Drop Voltage Regulator having the transient & static loop and the dynamic switch loop. As the output voltage Vo is less than the specified voltage, the input terminals of the linear amplifier is short. The transient & static Loop is equivalent to the nonlinear amplifier as shown in FIG. 43B. For the switching current of the digital circuit, the dynamic switch loop has the fast closed loop. During the voltage sink of the digital circuit switching, the capacitor C.sub.SWITCH switches on the P-type switch to pull down the gate of PFET to charge the output.

[0180] As shown in FIG. 43C, the output voltage Vout of the conventional LDVR has the ripple. The in-rush current is very high. The voltage sink of the digital circuit switching is very large.

[0181] As shown in FIG. 43D, the output voltage Vout of the smart LDVR rises slowly and smoothly. The in-rush current is very small. The voltage sink of the digital circuit switching is very small.

[0182] As shown in FIG. 39B and FIG. 44A1, the gliding golfdisc has smart phone and camera means comprises the general green power architecture made of dropless voltage regulator DLVR and dropless current regulator DLIR. A capacitor C.sub.SW connects between the input of the dropless current regulator DLIR and the input of dropless voltage regulator DLVR.

[0183] As shown in FIG. 44A2, the chip level green P&G architecture is constitute of the DLVR DropLess Voltage Regulator and DLIR DropLess Current Regulator.

[0184] As shown in FIG. 39B, FIG. 44A1 and FIG. 441A2, the gliding golfdisc wherein smart phone and camera comprises green power architecture made of dropless voltage regulator DLVR and dropless current regulator DLIR. A passive charging capacitor connected between an input of said dropless current regulator DLIR and an input of said dropless voltage regulator DLVR. The dropless current regulator DLIR filters out the switching circuit noise in ground to be current noises I. The passive charging capacitor C.sub.SW converts the current noises I in the ground node to be the voltage noises V in power node. Instead of the conventional active voltage charge pumping process, this is the passive current charge pumping process. The voltage noises V.sub.DD filtering with said dropless voltage regulator DLVR to be voltage potential energy of clean power supply.

[0185] As shown in FIG. 44A1, FIG. 44B1 and FIG. 44B2, the DLVR DropLess Voltage Regulator has the output voltage to be the constant voltage V.sub.CC. This is the real DC/DC process. The DLIR DropLess Current Regulator has the output current to be the constant current I.sub.SS. The CKT circuit generates the current I.sub.SS+I. Due to the DLIR, the I.sub.SS flows through the ground inductor. From L(dI/dt)=L(dI.sub.SS/dt)=0, the Gnd voltage is the same voltage as PAD_Gnd to be 0V. Due to the buck converter type DLIR Dropless effect caused by the ground inductor, the VSS is 0V.

[0186] Comparing FIG. 44A2 with FIG. 44E, FIG. 44A2 is the chip version of Green Power P&G architecture and system. FIG. 44E is the board version of Green Power P&G architecture and system.

[0187] As shown in FIG. 44A2, it is the detailed design of the chip version green power P&G architecture and system. The Analog circuit and digital circuit are separated. The switching current noise I generated by the digital circuit injects into the switching capacitor C.sub.SW. The switching current I of ground node is converted to the switching voltage V of the power node. This behavior is similar to the charge pump circuit. Instead of using the voltage mode as the active drive circuit of charge pump does, the passive circuit switching circuit use the current mode I to do the current charge pump.

[0188] The switching current I injects into the switch capacitor C.sub.SW to be V. All the switching noise energy injecting into V.sub.DD to store in the power inductor L_V.sub.DD. The switching mode power and the switching noise power add up to be the switch power. The switch power going through the DropLess Voltage Regulator DLVR to be the clean power having the constant voltage V.sub.CC. The switch noise energy is recycled to be the useful power. The parametric inductor L_V.sub.DD serves as the switching energy storage in the dynamic oscillatory form.

[0189] As shown in FIG. 43A, FIG. 44C1, FIG. 44C2 and FIG. 44B2, the Low Drop Voltage Regulator LDVR has the voltage drop. The DropLess Voltage Regulator DLVR does not have the voltage drop due to the DLVR has the hybrid operation of the buck-boost-LDVR type inductor operation.

[0190] The DropLess Voltage Regulator DLVR has the average of the switch mode power voltage due to the extra inductor as shown in FIG. 44C1. The DLVR Drop Less VoltageRegulator is the active RC filter to be rippless and capless.

[0191] As shown in FIG. 44B2 and FIG. 44C2, the waveform of the input of the saw-tooth voltage output of the switch mode power supply is converted to the constant potential voltage of the output power with the active RC filter rippless and capless DLVR Low Drop Buck converter Voltage Regulator.

[0192] As shown in FIG. 44B1, FIG. 44D1 and FIG. 44D2, the chip version DLIR DropLess Current Regulator uses the parametric inductor L_Gnd to be the current sensor. The capacitor CJ is to keep the V.sub.GS of output NMOS type device to be constant to regulate the current to be constant. The differential amplifier senses the voltage variance V caused by the variance of the current I.

[0193] As shown in FIG. 44E, the active Common Mode Choke CM choke is implemented with the DropLess Voltage Regulator DLVR and DropLess Current Regulator DLIR. It is the board version of the green power architecture. It is the merge of the DLVR in FIG. 44C1 with the DLIR in FIG. 44D1.

[0194] As shown in FIG. 44F, the Power Supply Rejection Ratio PSRR of the LDVR has the band-limited frequency in low frequency. The PSRR of conventional Common Mode choke, CM choke, has the band-limited frequency in the high frequency. The PSRR of the Active Common Mode choke, ACM-Choke, has no band limited. The ACM-Choke combines the PSRR of both LDVR and CM Choke to be the flat curve which has no band-limited. The noisy input power VDD is connected to the DLVR as input power. The output of the DLVR is the clean power VCC. The noisy input ground GND is connected to the DLIR. The output of the DLIR is the clean ground VSS.

[0195] As shown in FIG. 44A1, FIG. 44A2 and FIG. 44E, the Green Power Architecture and System has the voltage waveforms of V.sub.DD, V.sub.CC, V.sub.SS and Gnd as shown in FIG. 44G.

[0196] As shown in FIG. 44H1, the SPICE simulation result of the conventional circuit has the waveforms of power VDD and ground GND oscillate violently having the amplitude +/93 mv.

[0197] As shown in FIG. 44A1, FIG. 44A2, FIG. 44E and FIG. 44H2, with the green power architecture and system of recycling energy, the SPICE simulation result shows the noise amplitudes of VCC, VSS and GND are reduced to be +/0.05 mV. The noise reduction is 32.7 dB. However, the amplitude of VDD is almost double, +/160 mV. All the noises in the ground GND is injected and stored in the power VDD. Then the noisy power VDD is filtered to be clean power VCC with the DLVR DropLess Voltage Regulator.

[0198] FIG. 45A shows the analog front of the high frequency wireless cellular phone. FIG. 45B shows the high-speed analog front of the digital communication system. It shows the high frequency wireless system and the high-speed digital circuit. The high-frequency wireless system uses the root-mean-square RMS detector to detect the power to adjust the Variable Gain Amplifier VGA. The high-speed digital circuit uses the peak detector to detect the amplitude to adjust the Variable Gain Amplifier VGA. The comparator of the high-speed digital circuit can be considered as the 1-bit ADC of the high-frequency wireless system.

[0199] As shown in FIG. 46A and FIG. 46B, the gliding golfdisc comprises the smart phone and camera means haying bandgap generator BG. The bandgap generator BG further comprises a voltage bandgap generator V.sub.BG and current bandgap generator I.sub.BG. The voltage bandgap generator V.sub.BG generates I.sub.PTAT current and V.sub.BG bandgap voltage and feeding them into the current bandgap generator I.sub.BG. The current band generator I.sub.BG generates the bandgap current I.sub.BG and feeding it into the voltage bandgap generator V.sub.BG.

[0200] As shown in FIG. 46A and FIG. 46B, the bandgap voltage V.sub.BG is generated by the bandgap generator BG. The BG Bandgap Generator is constituted of the voltage bandgap generator V.sub.BG Gen and the current bandgap generator I.sub.BG Gen. The voltage bandgap generator V.sub.BG Gen sends the voltage V.sub.BG and the current I.sub.PTAT to current bandgap generator I.sub.BG. The current bandgap generator I.sub.BG Gen sends the bandgap current to the voltage bandgap generator V.sub.BG Gen.

[0201] As shown in FIG. 47, the Separation/Parting line of disc determines the performance of disc. The lower the Separation/Parting line is, the more lift is and the less stability is. The higher the Separation/Parting line is, the less lift is and the more stability is. To break the rule, the golfdisc adopts the flat bottom with the tail flap. It has the maximum lift and the maximum stability.

[0202] As shown in FIG. 48, the solid line is the flow trajectory of the golfdisc. The dotted line is the conventional disc. At the front portion, the tail flap has the higher lift. For the golfdisc, the flow hits the rear portion of the dome area. For the conventional disc, the flow hits the front, portion of the dome area. Therefore, the Center of Pressure CP of the golfdisc is located after the Center of Pressure CP of conventional disc. Therefore, the stability of the golfdisc is more stable than the conventional disc does. At the rear portion, for the golfdisc, due to the tail flap, the airflow bypasses the flat bottom and the cavity of the discap 105. For the conventional disc, the air blows into the cavity of discap 105. Therefore, the drag of golfdisc is much less than the conventional disc. At the side of disc 10, the golfdisc flap has more stability than the conventional disc without the flap. Therefore, the disc with the flap is the biggest innovation in the disc golf.

[0203] The camera, video display and monitor have the green power architecture made of the DLVR DropLess Voltage Regulator, DLIR DropLess Current Regulator and Switch Noise Power Charging Capacitor to convert the noise energy to be the useful power. The camera, video display and monitor further have the Bandgap Generator being constituted of the Voltage Bandgap Generator and Current Generator. The Frequency-Phase Lock Loop comprises the frequency lock and phase lock two stages and the frequency lock is implemented with the counter. The DropLess Voltage Regulator DLVR is implemented with the hybrid combination of the LDVR and P-side buck type inductor. The DropLess Current Regulator DLIR is implemented with the sense of voltage difference of the parasitic inductor induced by the variance of the current. The active common mode choke ACM is made of the common mode choke, the DLVR DropLess Voltage Regulator, DLIR DropLess Current Regulator and Switch Noise Power Charging Capacitor.

[0204] While the invention has been particularly shown and described with reference to the preferred embodiments thereof, it will be understood by those skilled in the art that various changes in form and details may be made therein without departing from the spirit and scope of the invention. It is noted that this disclub golf design can be easily modified to be the left-handed ultra-long-drive disc and disclub with the right-hand screws changing to be the left-hand screws. Furthermore, it is noted that the discap and head positions can be interchangeable for disclub and golfdisc. In other words, even in the previous description, all the discussion is based on the alignment of the disclub head 10 being on disclub 1 and the discap 20 is on golfdisc 2. However, the alignment of the fitting discap is on disclub and the head is on golfdisc is also workable. The same principles and methodologies, etc are applicable to both cases. All the innovations made for the golfdisc of disclub golf can be applied to the conventional disc of disc golf, too.