Motorized hydrofoil device
10486771 ยท 2019-11-26
Assignee
Inventors
Cpc classification
B63B32/64
PERFORMING OPERATIONS; TRANSPORTING
B63B32/10
PERFORMING OPERATIONS; TRANSPORTING
International classification
Abstract
A motorized hydrofoil apparatus may include a sailboard having a top surface and a bottom surface; a first hydrofoil assembly; a pivotable second hydrofoil attached to a second support unit; and a propulsion system. The hydrofoil apparatus may also include one or more sensing units disposed on predetermined locations on the first support unit to operatively communicate to the second hydrofoil to automatically generate corrective responses to various destabilizing hydrodynamic effects to stabilize the hydrofoil apparatus.
Claims
1. A motorized hydrofoil apparatus comprising: a sailboard having a top surface and a bottom surface; a first hydrofoil assembly coupled to the sailboard, said assembly having a first hydrofoil, a first support unit coupling said sailboard to said first hydrofoil, and a second hydrofoil hingedly coupled to the first hydrofoil via a second support unit; a propulsion system coupled to the sailboard to provide power to the hydrofoil apparatus; a sensing unit to detect deviation movement of the hydrofoil apparatus; and a control unit to control the second hydrofoil to generate corrective movements to increase stability of the hydrofoil apparatus.
2. The motorized hydrofoil apparatus of claim 1, wherein when the sensing unit detects a pitch deviation movement that may cause the hydrofoil apparatus to tilt in either a forward or a backward manner, the control unit is configured to respond to the pitch deviation movement by triggering the second hydrofoil to make an appropriate corrective pivoting movement to stabilize the hydrofoil apparatus.
3. The motorized hydrofoil apparatus of claim 2, wherein the second support unit extends from a front end of the first hydrofoil, and said second hydrofoil is disposed ahead of the first hydrofoil.
4. The motorized hydrofoil apparatus of claim 3, wherein the entire second hydrofoil pivots relative to the second support unit.
5. The motorized hydrofoil apparatus of claim 4, wherein the second hydrofoil has no aileron and has no flaps.
6. The motorized hydrofoil apparatus of claim 4, wherein the propulsion system is electric and is disposed on the top surface of the sailboard.
7. The motorized hydrofoil apparatus of claim 4, wherein the propulsion system is electric and is disposed below the bottom surface of the sailboard.
8. The motorized hydrofoil apparatus of claim 2, wherein the second support unit extends from a rear end of the first hydrofoil, and said second hydrofoil is disposed behind the first hydrofoil.
9. The motorized hydrofoil apparatus of claim 8, wherein the entire second hydrofoil pivots relative to the second support unit.
10. The motorized hydrofoil apparatus of claim 9, wherein the second hydrofoil has no aileron and has no flaps.
11. The motorized hydrofoil apparatus of claim 9, wherein the propulsion system is electric and is disposed on the top surface of the sailboard.
12. The motorized hydrofoil apparatus of claim 9, wherein the propulsion system is electric and is disposed below the bottom surface of the sailboard.
13. The motorized hydrofoil apparatus of claim 2, wherein the first hydrofoil has a wider wingspan than the second hydrofoil.
14. The motorized hydrofoil apparatus of claim 13, wherein one end of the first support unit is attached to a predetermined location at the bottom surface of the sailboard between a center portion and a rear end of the sailboard; and the other end of the first support unit is attached to nearly a center portion of the first hydrofoil.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1)
(2)
(3)
(4)
(5)
(6)
(7)
(8)
(9)
(10)
(11)
(12)
(13)
(14)
(15)
(16)
(17)
(18)
DETAILED DESCRIPTION OF THE INVENTION
(19) The detailed description set forth below is intended as a description of the presently exemplary device provided in accordance with aspects of the present invention and is not intended to represent the only forms in which the present invention may be prepared or utilized. It is to be understood, rather, that the same or equivalent functions and components may be accomplished by different embodiments that are also intended to be encompassed within the spirit and scope of the invention.
(20) Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood to one of ordinary skill in the art to which this invention belongs. Although any methods, devices and materials similar or equivalent to those described can be used in the practice or testing of the invention, the exemplary methods, devices and materials are now described.
(21) All publication s mentioned are incorporated by reference for the purpose of describing and disclosing, for example, the designs and methodologies that are described in the publications that might be used in connection with the presently described invention. The publications listed or discussed above, below and throughout the text are provided solely for their disclosure prior to the filing date of the present application. Nothing herein is to be construed as an admission that the inventors are not entitled to antedate such disclosure by virtue of prior invention.
(22) As used in the description herein and throughout the claims that follow, the meaning of a, an, and the includes reference to the plural unless the context clearly dictates otherwise. Also, as used in the description herein and throughout the claims that follow, the terms comprise or comprising, include or including, have or having, contain or containing and the like are to be understood to be open-ended, i.e., to mean including but not limited to. As used in the description herein and throughout the claims that follow, the meaning of in includes in and on unless the context clearly dictates otherwise.
(23) It will be understood that, although the terms first, second, etc. may be used herein to describe various elements, these elements should not be limited by these terms. These terms are only used to distinguish one element from another. For example, a first element could be termed a second element, and, similarly, a second element could be termed a first element, without departing from the scope of the embodiments. As used herein, the term and/or includes any and all combinations of one or more of the associated listed items.
(24) In one aspect, as shown in
(25) As discussed above, while conventional hydrofoil devices may be equipped with some control means, conventional hydrofoil devices cannot automatically control the stability of the hydrofoil devices to generate corrective response to various destabilizing hydrodynamic effects. In a further embodiment, the hydrofoil device 100 may include one or more sensing units 150 disposed on predetermined locations on first supporting unit 122 of the first hydrofoil assembly 120.
(26) In an exemplary embodiment, the first hydrofoil assembly 120 has a pair of first actuating units (123, 124) hingedly located on a trailing edge on both sides of the first hydrofoil 121. Similar to ailerons on each wing of the airplane to control the airplane's roll movement, namely movement around the airplane's longitudinal axis, the first actuating units (123, 124) of the first hydrofoil assembly 120 are configured to stabilize the hydrofoil device 100 around its longitudinal axis, or roll axis. The first actuating units (123, 124) may operatively communicate with the sensing unit 150 through a control unit 160, so when a deviation of the hydrofoil device 100 around its longitudinal axis is detected by the sensing unit 150, a deviation signal will be transmitted to the control unit 160 that is configured to control the movement of the first actuating units (123, 124) to correct the deviation. For example, as shown in
(27) As discussed above, the first actuating units (123, 124) are hingedly located on both sides of the first hydrofoil 121 and each of the first actuating units 123 and 124 can move up or down to control the movement of hydrofoil device 100 around its longitudinal axis. More specifically, when the control unit 160 receives the deviation signal regarding deviation D1 from the sensing unit 150, the actuating unit 123 is triggered by the control unit 160 to move up while the actuating unit 124 is triggered to move down to generate a corrective clockwise torque with the corrective movement C1 to eliminate the effect generated by counterclockwise deviation D1 to further stabilize the hydrofoil 100.
(28) Likewise, as shown in
(29) In addition to the first hydrofoil assembly 120, the second hydrofoil assembly 130 can also generate corrective movement to eliminate deviation of the hydrofoil device 100 around its lateral axis. Similar to elevators hingedly located on both sides of the tailplane to control the airplane's pitch, namely increasing or decreasing the lift generated by the wings when it pitches the airplane's nose up or down by increasing or decreasing the angle of attack, the second actuating units (133, 134) of the second hydrofoil assembly 130 are configured to stabilize the hydrofoil device 100 around its lateral axis, or pitch axis.
(30) In another embodiment, the second actuating units (133, 134) may also operatively communicate with the sensing unit 150, so when a deviation of the hydrofoil device 100 around its lateral axis is detected by the sensing unit 150, a deviation signal will be first transmitted to the control unit 160, which will then trigger the second actuating units (133, 134) to correct the deviation. For example, as shown in
(31) More specifically, when the control unit 160 receives the deviation signal regarding deviation D3 from the sensing unit 150, both the second actuating units 133 and 134 are triggered to move up to generate a corrective torque with the corrective movement C3 to eliminate the effect of deviation D3 to further stabilize the hydrofoil 100.
(32) Likewise, as shown in
(33) The hydrofoil device 100 may include an inertial measurement unit (IMU) at a predetermined position thereof. It is noted that the IMUs are often incorporated into Inertial Navigation System which utilize the raw IMU measurements to calculate attitude, angular rates, linear velocity and position relative to a global reference frame.
(34) In one embodiment, the user can stand on the top surface 112 of the sailboard 110 to control the hydrofoil device 100 by shifting his/her own centre of gravity (CG). More specifically, the hydrofoil device 100 may include one or more sensing devices to detect the user's centre of gravity or the change thereof to enable the user to control the hydrofoil by steering, accelerating and braking. In another embodiment, the control of the hydrofoil can be done by a hand-held device on the user's hand. In a further embodiment, the user can sit on the sailboard to control the hydrofoil device 100 as shown in
(35) In another aspect, as shown in
(36) For example, as shown in
(37) More specifically, when the control unit 160 receives the deviation signal regarding deviation D5 from the sensing unit 150, the second actuating units 133 and 134 are triggered to both move up to generate a corrective torque with the corrective movement C5 to eliminate the effect of deviation D5 to further stabilize the hydrofoil 100.
(38) Likewise, as shown in
(39) In addition to the second hydrofoil assembly 130, the first hydrofoil assembly 120 can also generate corrective movement to eliminate deviation of the hydrofoil device 100 around its longitudinal axis as discussed above. For example, as shown in
(40) As discussed above, the first actuating units (123, 124) are hingedly located on both sides of the first hydrofoil 121 and each of the first actuating units 123 and 124 can move up or down to control the movement of hydrofoil device 100 around its longitudinal axis. More specifically, when the control unit 160 receives the deviation signal regarding deviation D7 from the sensing unit, the actuating unit 123 is triggered to move up while the actuating unit 124 is moving down to generate a corrective clockwise torque with the corrective movement C7 to eliminate the effect generated by counterclockwise deviation D7 to further stabilize the hydrofoil 100.
(41) Likewise, as shown in
(42) In a further aspect, as shown in
(43) In an exemplary embodiment, the first hydrofoil assembly 120 has a pair of first actuating units (123, 124) hingedly located on a trailing edge on both sides of the first hydrofoil 121, which are configured to stabilize the hydrofoil device 100 around its longitudinal axis, or roll axis. The first actuating units (123, 124) may operatively communicate with the sensing unit 150, so when a deviation of the hydrofoil device 100 around its longitudinal axis is detected by the sensing unit 150, a deviation signal will be transmitted to the control unit 160 to trigger first actuating units (123, 124) to correct the deviation. For example, as shown in
(44) More specifically, when the first actuating units 123 and 124 receive the deviation signal regarding deviation D9 from the sensing unit, actuating unit 123 is configured to move up while the actuating unit 124 is moving down to generate a corrective clockwise torque with the corrective movement C9 to eliminate the effect generated by counterclockwise deviation D9 to further stabilize the hydrofoil 100.
(45) Likewise, as shown in
(46) In addition to generating corrective movement around the longitudinal axis of the hydrofoil device 100, the first hydrofoil assembly 120 can also generate corrective movement to eliminate deviation of the hydrofoil device 100 around its lateral axis. Similar to elevators hingedly located on both sides of the tailplane to control the airplane's pitch, namely increasing or decreasing the lift generated by the wings when it pitches the airplane's nose up or down by increasing or decreasing the angle of attack, the first actuating units (123, 124) of the first hydrofoil assembly 120 are also configured to stabilize the hydrofoil device 100 around its lateral axis, or pitch axis.
(47) In one embodiment, when a deviation of the hydrofoil device 100 around its lateral axis is detected by the sensing unit 150, a deviation signal will be transmitted to the control unit 160 to trigger the first actuating units (123, 124) to correct the deviation. For example, as shown in
(48) Likewise, as shown in
(49) As shown in
(50)
(51) Referring now to
(52) In a further contemplated embodiment, the propulsion system can be located not under water, but above the water line. As shown in
(53) Having described the invention by the description and illustrations above, it should be understood that these are exemplary of the invention and are not to be considered as limiting. Accordingly, the invention is not to be considered as limited by the foregoing description, but includes any equivalent.