Variable performance axial flow ducted fan with high efficiency and reduced current drawn

Abstract

The ideal design for a fan with variable performance that can replace a family of current axial flow ducted, un-ducted, and centrifugal fan designs by meeting air flow and pressure requirements while drawing less electric current to rotate and thus produce the required flow not only would reduce cost of operation over the life of the fan but opens new possibilities for direct connection to solar collection systems by greatly extending the life of the battery charge employed by the designer of the collection system. In addition the entry of flying machines using pairs of lifting fans such as hover bikes and quadcopters, manned or unmanned is driving a need to re-examine the application of force applied to rotate these fans to achieve a reduction in aircraft weight and increase flying time for a given battery charge or load of fuel.

Claims

1. A fan system comprising: a housing for mounting fan components and comprising of an airflow inlet, airflow outlet, a means to control field reversal, stator mounting apparatus and main axle mounting apparatus; an electric motor rotor and fan assembly mounted in the housing comprising of a main axle, a blade mounting hub, a plurality of fan blades, a rotating duct, a plurality of magnets; a main axle extending along an axis defined between the airflow inlet and airflow outlet; a blade mounting hub coaxially disposed along the main axle within the fan duct; the blade mounting hub supporting the plurality of fan blades evenly spaced around the blade mounting hub; a rotating duct mounted on an end tip of each fan blade; the rotating duct supporting a plurality of evenly spaced electromagnets on an outer wall; a stator fixed on the stator mounting apparatus in the housing; the stator having a plurality of evenly spaced permanent magnets; the stator mounted such that the rotor assembly rotates freely within the housing; a field reversal control means configured to reverse current to the electric motor rotor and thus reverse a magnetic field generated so as to apply force to the outer duct wall and the electromagnets mounted thereto in relation to the stator to drive fan rotation; an axial flux permanent magnet motor to drive fan rotation.

2. The fan system of claim 1 wherein the fan blades are mounted on a plurality of fan blade mounting axles fixed on the fan blade mounting hub and extend outward laterally from and perpendicular to the main axle.

3. The fan system of claim 2 wherein the rotating duct fixed upon the end tip of each fan blade encircles the rotor assembly.

4. A fan system comprising: a housing for mounting fan components and comprising of an airflow inlet, airflow outlet, means to control field reversal, stator mounting apparatus and main axle mounting apparatus; an electric motor rotor and fan assembly mounted in the housing, comprising a main axle, a blade mounting hub, a plurality of variable pitch fan blades, a rotating duct, a plurality of magnets; the main axle extending along an axis defined between the airflow inlet and airflow outlet; a blade mounting hub coaxially disposed along the main axle within the fan duct; the blade mounting hub supported by at least one first inner bearing and race; the blade mounting hub supporting the plurality of fan blades evenly spaced around the blade mounting hub; the plurality of fan blades forming an axial flow fan; a rotating duct mounted on an end tip of each fan blade; the rotating duct supporting a plurality of evenly spaced excitation windings; a stator fixed in the mounting housing; the stator having a plurality of evenly spaced permanent magnets; the stator mounted such that the rotor assembly rotates freely within; a means to reverse current responsive to the field reversal control means and thus reverse a magnetic field so as to apply force to the outer duct wall and electromagnets mounted thereto in relation to the stator to drive fan rotation; a permanent magnet motor to drive fan rotation.

5. The fan system of claim 4 wherein the fan blades are mounted on a plurality of axles fixed in the fan blade mounting hub and extend outward laterally from and perpendicular to the main axle.

6. The fan system of claim 5, wherein the blade axles are matched as pairs, the blades of each pair mounted on opposite sides of the main axle.

7. The fan system of claim 4 further comprising an actuator hub located on the main axle adjacent to the blade mounting hub free to travel linearly along the main axle.

8. The fan system of claim 7 further comprising a return spring located on the main axle between the blade mounting hub and the actuator hub contacting the two hubs at the face of respective inner bearing races.

9. The fan system of claim 7 wherein at least one variable pitch fan blade is mounted on each of a plurality of fan blade mounting axles.

10. The fan system of claim 9, further comprising pitch change horns mounted on the base of each blade closest to the main axle configured to actuate changes to pitch in the blades.

11. The fan system of claim 10 further comprising a plurality of pitch change links each with one end fastened to the actuator hub at equally spaced points around the actuator hub and in the same number as the variable pitch fan blades and the opposite end of each link connected to the pitch change horns on the adjustable fan blades.

12. The fan system of claim 11 further comprising an actuator tube configured to deliver control inputs through the actuator hub and pitch change links thereby applying changes to the pitch of each blade simultaneously.

13. The fan system of claim 12 wherein the actuator horns are connectable to the actuator tube apparatus to slide the actuator tube toward a return spring to mechanically change the pitch of the blades.

14. The fan system of claim 13 wherein the permanent magnet motor is an axial flux permanent magnet motor.

15. The fan system of claim 14 further comprising a sinusoidal pulse width modulation control system configured to control the permanent magnet motor.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 is a cut away side view of a circular mounting housing embodiment employed with a fixed pitch fan or propeller.

(2) FIG. 2 is a cut away side view of a variable pitch fan or propeller with demonstration of bolt on scalability to achieve multiple stages.

(3) FIG. 3 is a cut away side view of the pitch change mechanism.

(4) FIG. 4 is a profile view of an agricultural box fan embodiment.

DETAILED DESCRIPTION OF EXEMPLARY EMBODIMENTS

(5) Integrated Fan Rotor Assembly

(6) Referring to FIGS. 1 and 2, through a center line drawn from the air inlet through the air outlet is a main axle 1 and 8. This axle is retained in that position by sufficient support as determined by the designer. This support can be a front and rear bearing 9 if the fan is mounted vertically or top and bottom bearing 9.

(7) The main axle 1 and 8 needs to be stiff enough to resist unbalanced rotational forces applied during continuous operation. If the environment in which the fan operates is subject to foreign object damage the designer will have to balance increased structure to account for such risk against the safety issues involved, cost of manufacture, and cost of operation.

(8) Fixed linearly on the main axle 1 and 8 and located at the center point of the stator assembly 7, is a fan blade axle mounting hub 2 and 14 (FIG. 3). This hub is so named as the axles on which the fan blades 4 and 22 are mounted are themselves mounted on this hub. Weight is of primary concern and modern precision manufacturing techniques should be employed to obtain a light weight perfectly balanced hub.

(9) The fan blade axle mounting hub 2 and 14 rides on at least one bearing 9. The positioning of this bearing linearly on the axle is fixed. The bearing enables rotation of the hub about the axle and provides for mounting of the fan blade axles 3 on which the fan blades 4 and 22 are mounted.

(10) The fan blade mounting axles 3 are rigidly fixed in pairs to the fan blade axle mounting hub 2 and 14, extending laterally outward perpendicular to the main axle 1 and 8. Each fan blade axle 3 in the pair is mounted on opposing sides of the main axle 1 and 8.

(11) Upon these axles are mounted fan blades 4 and 22. The aerodynamic properties are selected by the designer so as to achieve the flow and pressure production required by the application at a specified speed of rotation and angle of attack. The blades are reversible for ease of scalability. As such a symmetrical shape is desirable. Weight is of primary concern and modern precision manufacturing techniques should be employed to obtain a light weight perfectly balanced set of fan blades.

(12) The variable pitch fan blades 4 and 22 rotate about the fan blade mounting axle 3, and are not turned by the axle. Changes in the angle of attack are delivered to the blade through a pitch change horn mounted at the base of the blade nearest the mounting hub 2.

(13) The fan blades are connected at the pitch change horn 12, through pitch change links 11 and 21 to a pitch change actuator hub 13 and 18. The pitch change links 11, 21 are mounted evenly around the circumference of the pitch change actuator hub 13 and 18 and extend toward the pitch change horn 12 parallel or nearly parallel to the main axle 1 and 8.

(14) The pitch change actuator hub 13 and 18 is mounted on the main axle 1 and 8 riding on at least one bearing 17. The bearing is free to move linearly along the main axle 1 and 8 so as to deliver the desired pitch control inputs through the pitch change links 11 and 21 to the pitch change horns 12 on the blades.

(15) Riding on the main axle 1 and 8 in between and contacting the outside surface of the inner race of both the fan blade axle hub 2 and 14 and the pitch change hub 13 and 18 is a spring acting as a return device 15.

(16) On the opposite side of the pitch change hub 13 and 18 from fan blade axle mounting hub 2 and 14 and also riding on the main axle 1 and 8 is an actuator tube 16 and 19. This tube contacts the inner race of the pitch change hub bearing 17 and can be moved linearly along the main axle 1 and 8.

(17) On this tube 16, are horizontally mounted horns 19 extending laterally outward perpendicular to the main axle 1 and 8. This provides for connection to an actuator mechanism such as a bell crank mounted as the designer selects such as a mounting horn 20 or an electromechanical connection. Through this mechanism physical inputs are delivered from a separate mechanical or electromechanical apparatus to the fan thereby controlling blade pitch.

(18) Affixed to the ends of the fan blade mounting axles is a duct 5 that encircles the whole assembly.

(19) The fan blade tips should touch the inner wall of the duct 5 but be shaped to allow rotational movement of the blade 4 and 22 about the blade mounting axle 3 as pitch adjustments are applied to the blade 4 and 22.

(20) The duct 5 can be constructed of metal, plastic, or composite materials as selected by the designer. However weight is of primary concern and modern precision manufacturing technics should be employed to obtain a light weight and perfectly balanced duct that also provides structural support to resist deformation under high loads.

(21) Construction of the fan rotor assembly requires the designer to select appropriately sized electromagnets or permanent magnets 6 crafted with provision to be mounted to the end of each fan blade mounting axle and or evenly spaced about the duct 5 as the designer selects, with attachment outside the duct wall to the wall or an extension.

(22) Weight is of primary concern and modern precision manufacturing technics should be employed to obtain a light weight perfectly balanced set of permanent magnets or coils 6 as selected and must be evenly spaced about the duct outer wall.

(23) The designer must make provision for pulling any wiring through the mounting axles 3 or along those axles to the control system as applicable.

(24) The whole assembly described is the fan electric motor rotor assembly.

(25) Mounting Housing

(26) The designer can employ mounting housing 10 and 23 as a means for mounting fan components to provide sufficient structure that takes a box, or cylindrical form factor. This mounting housing 10 and 23 has provision for the stator 7 and main axle 1 and 8. This mounting housing provides a structure on which all necessary componentry is mounted 10 and 23.

(27) It likewise provides for mounting points on which the entire fan can be mounted upon in its operational environment.

(28) The housing 10 and 23 can be open with mounting supports for a lifting embodiment attached to an aircraft like a quadcopter such as FIG. 1 or a box fan or a cylinder as in FIG. 2. The sidewalls can be formed with flanges that add stiffness, strength and logical fastening points.

(29) The housing in both FIG. 2 and FIG. 4, could have a structural rear flange oriented outward not interrupting flow, which provides structural support and provides potential for mounting points for internal componentry, mounting points of the unit in its operational environment, and or connection to a subsequent units when multiple units are mounted inline as system requirements dictate.

(30) The housing 10 and 23 open or box style including faceplate, sidewalls, main axle supports front and rear, and rear flange can be easily fabricated from sheet stock or composite material by one accomplished and knowledgeable in the field using common tooling and materials.

(31) The sidewalls may be designed with flanges to attach to the faceplate or the designer might decide to employ welding if the material selected is metallic in nature. If plastic or composite materials are selected the entire housing could be molded as one unit or joined chemically if molded as two parts as the designer deems the application warrants.

(32) Mounted within the modular housing 10 and 23 is the stator assembly 7. The stator needs to be circular in shape so as to encircle the fan blade rotor assembly with a close enough tolerance to function per design yet allowing rotation of the assembly within.

(33) The designer can select the use of electromagnets or permanent magnets 6 to integrate into the stator assembly. The final design must allow the rotation of the fan blade rotor assembly while obtaining the performance specified to meet system requirements.

(34) The housing 10 and 23 will support the main axle 1 and 8 using a single support or combination of supports as deemed necessary by the designer.

(35) The designer can also employ the supports to mount actuators 20 such as bell cranks to deliver mechanical or electromechanical inputs to adjust fan blade angle of attack.

(36) The housing itself could include provision for bolt on scalability as illustrated in FIG. 2 meaning that multiple housing units could be easily fastened together inline inlet to outlet. Thus fan units now become stages in a turbo machine.

(37) The wiring harness for the rotor and stator should be reversible with one switch or plug that can be reversed to change the direction current flows through the motor as assembled. This will rotate the entire rotor assembly within the stator 7 in the opposite direction from the proceeding unit allowing counter rotation of each successive unit or stage.