Tilting mechanism with telescoping actuator

Patent metadata

Field	Value
Publication number	US-11639218-B2
Application number	US-202117211225-A
Country	US
Kind code	B2
Filing date	Mar 24, 2021
Priority date	Oct 9, 2019
Publication date	May 2, 2023
Grant date	May 2, 2023

Abstract

A tiltrotor has a range of motion between a forward flight position and a hovering position, where a pylon and the tiltrotor are coupled via a telescoping actuator, a rigid bottom bar, and a fixed hinge that is attached between the rigid bottom bar and the tiltrotor. The tiltrotor moves from the forward flight position to the hovering position includes extending the telescoping actuator so that the tilt rotor rotates about the fixed hinge.

First claim

What is claimed is:

1. A system, comprising:
a pylon; and
a tiltrotor that has a range of motion between a forward flight position and a hovering position, wherein:
the pylon and the tiltrotor are coupled via a tilting mechanism, the tilting mechanism including a telescoping actuator and a four bar linkage, the four bar linkage including:
a telescoping top bar,
a fixed-length aft bar,
a fixed-length bottom bar, and
a fixed hinge that is attached between the bottom bar and the tiltrotor,

moving the tiltrotor from the forward flight position to the hovering position includes operating the tilting mechanism including by:
extending the telescoping actuator to cause the telescoping top bar to be diagonal, the fixed-length aft bar to be level with the fixed-length bottom bar, and
rotating the fixed-length bottom bar about the fixed hinge so that the tiltrotor rotates about the fixed hinge, and

in the forward flight position the pylon has reduced length compared with the hovering position.

2. The system recited in claim 1 , wherein the system is included in an electric vertical takeoff and landing (eVTOL) tiltrotor vehicle.

3. The system recited in claim 1 , wherein the pylon is coupled to a trailing edge of a forward-swept main wing.

4. The system recited in claim 1 , wherein the pylon is coupled to a canard.

5. The system recited in claim 1 , further including a telescoping top bar, wherein moving the tiltrotor from the forward flight position to the hovering position includes extending the telescoping top bar.

6. The system recited in claim 1 , wherein the fixed hinge is coupled to the tiltrotor via a bar that is coupled to a surface of the tiltrotor.

7. The system recited in claim 1 , further including a drag chain cable carrier that encloses a cable coupled to the tiltrotor.

8. The system recited in claim 1 , wherein the telescoping actuator includes a passive actuator.

9. The system recited in claim 1 , wherein the telescoping actuator includes a passive actuator, including one or more of the following: a compressed spring or pneumatic piston.

10. A method, comprising:
providing a pylon; and
providing a tiltrotor that has a range of motion between a forward flight position and a hovering position, wherein:
the pylon and the tiltrotor are coupled via a tilting mechanism, the tilting mechanism including a telescoping actuator and a four bar linkage, the four bar linkage including:
a telescoping top bar,
a fixed-length aft bar,
a fixed-length bottom bar, and
a fixed hinge that is attached between the bottom bar and the tiltrotor,

moving the tiltrotor from the forward flight position to the hovering position includes operating the tilting mechanism including by:
extending the telescoping actuator to cause the telescoping top bar to be diagonal, the fixed-length aft bar to be level with the fixed-length bottom bar, and
rotating the fixed-length bottom bar about the fixed hinge so that the

tiltrotor rotates about the fixed hinge, and
in the forward flight position the pylon has reduced length compared with the hovering position.

11. The method recited in claim 10 , wherein the pylon and the tiltrotor are included in an electric vertical takeoff and landing (eVTOL) tiltrotor vehicle.

12. The method recited in claim 10 , wherein the pylon is coupled to a trailing edge of a forward-swept main wing.

13. The method recited in claim 10 , wherein the pylon is coupled to a canard.

14. The method recited in claim 10 , wherein:
the pylon and the tiltrotor are included a vehicle that further includes a telescoping top bar; and
moving the tiltrotor from the forward flight position to the hovering position includes extending the telescoping top bar.

15. The method recited in claim 10 , wherein the fixed hinge is coupled to the tiltrotor via a bar that is coupled to a surface of the tiltrotor.

16. The method recited in claim 10 , wherein the pylon and the tiltrotor are included a vehicle that further includes a drag chain cable carrier that encloses a cable coupled to the tiltrotor.

17. The method recited in claim 10 , wherein the telescoping actuator includes a passive actuator.

18. The method recited in claim 10 , wherein the telescoping actuator includes a passive actuator, including one or more of the following: a compressed spring or pneumatic piston.

Assignees

• Kitty Hawk Corp

Inventors

• Sinha Pranay
• Vander Lind Damon

Classifications

• B64D27/357

  using batteries · CPC title

• B64C27/26

  characterised by provision of fixed wings · CPC title

• B64C29/00

  Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft (rotorcraft B64C27/00) · CPC title

• B64D27/33 Primary

  Hybrid electric aircraft · CPC title

• B64D27/34

  All-electric aircraft · CPC title