System and method for vertical take-off in an autogyro

Patent metadata

Field	Value
Publication number	US-11001374-B2
Application number	US-201715705099-A
Country	US
Kind code	B2
Filing date	Sep 14, 2017
Priority date	Sep 14, 2017
Publication date	May 11, 2021
Grant date	May 11, 2021

Abstract

An autogyro includes a frame and a rotor hub coupled to the frame. The autogyro also includes a connector coupled to the rotor hub and configured to couple the rotor hub to a ground-based pre-rotator device to rotate the rotor hub during a vertical take-off operation. The autogyro further includes a plurality of rotor blades coupled to the rotor hub, each rotor blade configured such that rotation of the rotor hub, during the vertical take-off operation, results in twisting the rotor blade from a first blade pitch distribution to a second blade pitch distribution.

First claim

What is claimed is:

1. An autogyro comprising:
a frame;
a rotor hub coupled to the frame;
a connector coupled to the rotor hub, the connector configured to couple the rotor hub to
a ground-based pre-rotator device to rotate the rotor hub during a vertical take-off operation; and

a plurality of rotor blades coupled to the rotor hub, each rotor blade configured such that a speed of rotation of the rotor hub, during the vertical take-off operation, results in twisting a shape of each rotor blade of the plurality of rotor blades from a first shape with a first blade pitch distribution to a second shape with a second blade pitch distribution, wherein the shape of the plurality of rotor blades remains in the second shape during the vertical take-off operation.

2. The autogyro of claim 1 , wherein the second blade pitch distribution is greater than the first blade pitch distribution, and wherein the plurality of rotor blades are configured to generate more lift at the second blade pitch distribution.

3. The autogyro of claim 1 , wherein each of the plurality of rotor blades includes a link configured to twist a corresponding rotor blade based on centrifugal forces.

4. The autogyro of claim 3 , wherein the links comprise composite materials having an anti-symmetrical fiber orientation.

5. The autogyro of claim 3 , wherein each of the links comprise a passive link device including a shaft and a spring, the shaft configured to move and twist responsive to rotation of the rotor hub and the spring configured to bias the rotor blade towards the first blade pitch distribution.

6. The autogyro of claim 1 , wherein each of the plurality of rotor blades includes a blade spar configured to twist a corresponding rotor blade based on centrifugal forces wherein the blade spars comprise composite materials having an anti-symmetrical fiber orientation.

7. The autogyro of claim 1 , further comprising a propeller and an engine coupled to the frame, the propeller configured to generate thrust and move the frame, wherein movement of the frame induces a rotor including the rotor hub and the plurality of rotor blades to autorotate, and wherein autorotation of the rotor results in each of the plurality of rotor blades twisting to a third shape with a third blade pitch distribution.

8. The autogyro of claim 7 , wherein the engine is configured to direct heat to the plurality of rotor blades to increase a temperature of the plurality of rotor blades, and wherein the increase in the temperature of the plurality of rotor blades results in each of the rotor blades twisting to a fourth shape with a fourth blade pitch distribution.

9. The autogyro of claim 1 , further comprising a heating device configured to increase a temperature of the plurality of rotor blades.

10. The autogyro of claim 1 , further comprising at least one of an electric motor, a pneumatic motor, or a hydraulic motor coupled to the connector and the rotor hub and configured to receive energy from the ground-based pre-rotator device and to rotate the rotor hub based on the energy.

11. The autogyro of claim 1 , wherein the connector comprises at least one of a rotor shaft or a gear, and wherein the connector includes a quick disconnect fitting configured to decouple from the ground-based pre-rotator device under tension generated during vertical take-off of the autogyro.

12. A system comprising:
an autogyro comprising:
a frame;
a rotor hub coupled to the frame;
a connector coupled to the rotor hub, the connector configured to couple the rotor hub to a ground-based pre-rotator device to rotate the rotor hub during a vertical take-off operation; and
a plurality of rotor blades coupled to the rotor hub, each rotor blade configured such that a speed of rotation of the rotor hub, during a vertical take-off operation, results in twisting a shape of each rotor blade of the plurality of rotor blades from a first shape with a first blade pitch distribution to a second shape with a second blade pitch distribution, wherein the shape of the plurality of rotor blades remains in the second shape during the vertical take-off operation; and

a ground-based station comprising:
the ground-based pre-rotator device configured to rotate the rotor hub; and
an energy source configured to provide energy to the ground-based pre-rotator device.

13. The system of claim 12 , wherein the ground-based pre-rotator device comprises at least one of an electric motor, a pneumatic motor, a hydraulic motor, or a mechanical engine.

14. The system of claim 12 , further comprising a decoupling device configured to decouple the autogyro from the ground-based station.

15. The system of claim 12 , wherein the shape of the plurality of rotor blades reverts to the first shape responsive to the speed of rotation reducing after the vertical take-off operation is complete.

16. The system of claim 12 , wherein the ground-based pre-rotator device further comprises:
an output shaft;
a second connector configured to couple to the connector of the autogyro; and
a universal joint coupled to the output shaft and to the second connector, the universal joint configured to transmit power from the output shaft to the second connector at different angles.

17. A method of performing a vertical take-off operation of an autogyro, the method comprising:
while an autogyro is coupled to a ground-based station, initiating rotation of a rotor hub of the autogyro;
responsive to a speed of rotation of the rotor hub, twisting a shape of each of a plurality of rotor blades coupled to the rotor hub from a first shape with a first blade pitch distribution to a second shape with a second blade pitch distribution;
decoupling the autogyro from the ground-based station;
vertically taking-off, by the autogyro, while the plurality of rotor blades have the second shape; and
transitioning to forward flight after vertically taking-off.

18. The method of claim 17 , further comprising, flying the autogyro, wherein the rotor hub rotates at a first speed at vertical take-off and rotates at a second speed during the forward flight, and wherein the first speed is greater than the second speed.

19. The method of claim 18 , wherein during the forward flight each of the plurality of rotor blades is twisted, by a link, to a third shape with a third blade pitch distribution based on centrifugal forces generated from rotation of the rotor hub, and wherein the third blade pitch distribution is greater than the first blade pitch distribution and is less than the second blade pitch distribution.

20. The method of claim 17 , further comprising performing a landing operation of the autogyro, the landing operation comprising:
providing heat from a heat generation device to the plurality of rotor blades;
responsive to rotation of the rotor hub and the heat, twisting each of the plurality of rotor blades coupled to the rotor hub to a fourth shape with a fourth blade pitch distribution; and
vertically landing the autogyro while the plurality of rotor blades are oriented at the fourth blade pitch distribution.

Assignees

• Boeing Co

Inventors

• Kawiecki Grzegorz Marian

Classifications

• B64F1/34

  for starting propulsion plant · CPC title

• B64C27/022

  Devices for folding or adjusting the blades · CPC title

• B64C27/023

  Construction of the blades; Coating of the blades · CPC title

• B64C27/025 Primary

  Rotor drives, in particular for taking off; Combination of autorotation rotors and driven rotors · CPC title

• B64C27/021

  Rotor or rotor head construction (for helicopters B64C27/32) · CPC title