Tail-sitter aircraft with legged undercarriage foldable to form rear fuselage

• US 10,272,999 B2
• Filed: 12/08/2016
• Issued: 04/30/2019
• Est. Priority Date: 12/15/2015
• Status: Active Grant

• Current Assignee: Aerovel Corporation
• Original Assignee: Aerovel Corporation
• Inventors: Engbersen, Rutger, McGeer, Brian T., Baxter, Michael
• Primary Examiner(s): Ellis, Christopher P
• Application Number:
  US15/373,085
• Publication Number:
  US 20170166306A1
• Time in Patent Office: 873 Days
• Field of Search: 244109
• CPC Class Codes: B64C 25/52 Skis or runners
• CPC Class Codes: B64C 29/02 having its flight directional axis vertical when grounded
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64U 30/10 Wings
• CPC Class Codes: B64U 50/13 using external fans or propellers
• CPC Class Codes: B64U 70/00 Launching, take-off or landing arrangements

Abstract

Various embodiments of the present disclosure provide a tail-sitter aircraft having a leg assembly convertible from landing gear into a rear fuselage and empennage (or a tail assembly) of the aircraft. Generally, the leg assembly includes multiple legs movable from a closed configuration in which the legs form the tail assembly of the tail-sitter aircraft to an open configuration in which the legs form the landing gear of the tail-sitter aircraft (and vice-versa).

Claims

1. An aircraft comprising:

a fuselage;

multiple wings each attached to and extending transversely from the fuselage; and

multiple legs movable from a closed configuration in which legs form a tail assembly to an open configuration in which the legs at least partially form landing gear.

2. The aircraft of claim 1, wherein the tail assembly includes a rear fuselage and empennage.

3. The aircraft of claim 1, wherein each leg is pivotable relative to the fuselage.

4. The aircraft of claim 3, wherein each leg terminates in a free end.

5. The aircraft of claim 4, wherein the free ends of the legs move radially-outward relative to the fuselage when moving from the closed configuration to the open configuration.

6. The aircraft of claim 5, wherein the free ends of the legs move radially-inward relative to the fuselage when moving from the open configuration to the closed configuration.

7. The aircraft of claim 6, wherein the free ends of the legs move toward a front end of the fuselage when moving from the closed configuration to the open configuration and away from the front end of the fuselage when moving from the open configuration to the closed configuration.

8. The aircraft of claim 4, which includes a motor operably coupled to the legs to move the legs between the closed configuration and the open configuration.

9. The aircraft of claim 8, wherein the motor is operable in a first rotational direction to move the legs from the closed configuration to the open configuration and in a second opposite rotational direction to move the legs from the open configuration to the closed configuration.

10. The aircraft of claim 1, which includes a locking device movable to lock at least two of the legs together when in the closed configuration.

11. The aircraft of claim 10, wherein at least two of the legs include aerodynamic aircraft control surfaces.

12. The aircraft of claim 11, wherein the locking device is movable to lock the at least two of the legs including stabilizing surfaces together when the at least two of the legs are in the closed configuration.

13. The aircraft of claim 1, which includes a flexible stabilizer connecting one of the legs to the fuselage.

14. A method of launching an aircraft, said method comprising:

after multiple legs of the aircraft are in an open configuration and at least partially support the aircraft, controlling the aircraft to climb in thrust-borne flight; and

afterwards, controlling the legs to move to a closed configuration to form a tail assembly of the aircraft.

15. The method of claim 14, which includes controlling the aircraft to transition to wing-borne flight after the legs reach the closed configuration.

16. The method of claim 14, which includes locking at least two of the legs together after reaching the closed configuration.

17. The method of claim 14, which includes controlling the legs to move to the closed configuration after the aircraft reaches a designated altitude.

18. A method of landing an aircraft, said method comprising:

controlling the aircraft to descend in thrust-borne flight;

afterward, controlling multiple legs of the aircraft to move from a closed configuration in which the legs form a tail assembly of the aircraft to an open configuration; and

controlling the aircraft to descend until the legs contact a landing surface.

19. The method of claim 18, which includes unlocking at least two of the legs from one another before moving the legs to the open configuration.

20. The method of claim 18, which includes controlling the legs to move from the closed configuration to the open configuration after the aircraft descends below a designated altitude.