Methods and apparatuses for launching unmanned aircraft, including methods and apparatuses for launching aircraft with a wedge action

• US 7,128,294 B2
• Filed: 01/16/2004
• Issued: 10/31/2006
• Est. Priority Date: 01/17/2003
• Status: Expired due to Term

• Current Assignee: Insitu Incorporated (The Boeing Co.)
• Original Assignee: Insitu Group Inc (The Boeing Co.)
• Inventors: von Flotow, Andreas H., Roeseler, Cory
• Primary Examiner(s): DINH, TIEN QUANG
• Application Number:
  US10/760,150
• Publication Number:
  US 20050151009A1
• Time in Patent Office: 1,019 Days
• Field of Search: 244/63, 244/49, 244/131, 244/101, 244/3.27, 446/62, 446/61
• US Class Current: 244/49
• CPC Class Codes: B63B 35/50 Vessels or floating structures for aircraft aircraft carriers B63G11/00; flying-boat hulls, other flotation means for aircraft B64
• CPC Class Codes: B64F 1/06 using catapults
• CPC Class Codes: B64U 2201/20 Remote controls
• CPC Class Codes: B64U 30/12 Variable or detachable wings, e.g. wings with adjustable sweep
• CPC Class Codes: B64U 50/11 using internal combustion piston engines
• CPC Class Codes: B64U 50/12 using turbine engines, e.g. turbojets or turbofans
• CPC Class Codes: B64U 50/13 using external fans or propellers
• CPC Class Codes: B64U 50/19 using electrically powered motors
• CPC Class Codes: B64U 70/30 for capturing UAVs in flight by ground or sea-based arresting gear, e.g. by a cable or a net
• CPC Class Codes: B64U 70/50 Launching from storage containers, e.g. from submarine missile tubes
• CPC Class Codes: B64U 70/70 Launching or landing using catapults, tracks or rails launching from storage containers B64U70/50
• CPC Class Codes: B64U 80/70 in containers B64U80/60 takes precedence
• CPC Class Codes: B64U 80/84 Waterborne vehicles

Abstract

Methods and apparatuses for launching unmanned aircraft and other flight devices or projectiles are described. In one embodiment, the aircraft can be launched from an apparatus that operates with a wedge action. A launch carriage carrying an unmanned aircraft is positioned on first and second launch members. At least one of the launch members moves relative to the other from a first position to a second position, causing the launch carriage to move from a first launch carriage position to a second launch carriage position. As the launch carriage moves, it accelerates the aircraft and releases the aircraft for takeoff.

Claims

1. An apparatus for launching an unmanned aircraft, comprising:

a first launch member;

a second launch member positioned at least proximate to the first launch member, at least one of the first and second launch members being movable relative to the other between a first position and a second position; and

a launch carriage having an aircraft support positioned to releasably carry an unmanned aircraft during a takeoff operation, the launch carriage touching the launch members and being movable relative to the launch members between a first launch carriage location and a second launch carriage location as the at least one of the first and second launch members moves from the first position to the second position, wherein the launch carriage moves in a first direction between the first launch carriage location and the second launch carriage location, and wherein the at least one launch member moves in a second direction transverse to the first direction between the first position and the second position.

2. The apparatus of claim 1, further comprising a support structure, and wherein the first and second launch members are carried by the support structure.

3. The apparatus of claim 1, further comprising an actuator coupled to the at least one launch member to move the at least one launch member relative to the other.

4. The apparatus of claim 1, further comprising an actuator coupled to the at least one launch member to move the at least one launch member relative to the other, and wherein the actuator includes at least one of a hydraulic cylinder, a spring, a pneumatic cylinder, an electric motor, a flywheel, a steam-powered apparatus, an explosive charge, and a weight.

5. The apparatus of claim 1, further comprising an energy reservoir coupled to the at least one launch member to move the at least one launch member.

6. The apparatus of claim 1, further comprising:

an actuator; and

a transmission coupled between the actuator and the second launch member, wherein the transmission includes a first portion coupled to the actuator to receive a first force from the actuator and accelerate with a first acceleration, the transmission further including a second portion coupled to the second launch member to impart a second force and a second acceleration to the launch carriage, wherein the second force is different than the first force and the second acceleration is different than the first acceleration.

7. The apparatus of claim 1 wherein at least one of the first and second launch members includes a braking portion, and wherein the braking portion is positioned to contact and decelerate the launch carriage as the launch carriage moves from the first launch carriage location to the second launch carriage location.

8. The apparatus of claim 1 wherein at least one of the first and second launch members includes a curved portion, and wherein the curved portion is shaped to provide constant acceleration to the launch carriage as the at least one of the first and second launch members moves relative to the other.

9. The apparatus of claim 1 wherein:

the first launch member includes a first roller surface and the second launch member includes a second roller surface non-parallel to the first roller surface; and

the launch carriage includes a first wheel in rolling contact with the first roller surface and a second wheel in rolling contact with the second roller surface.

10. The apparatus of claim 1 wherein the first launch member includes a first surface in contact with the launch carriage, and wherein the second launch member includes a second surface in contact with the launch carriage, the second surface having a first portion oriented at a first angle relative to the first surface to accelerate the launch carriage, the second surface having a second portion oriented at a second angle relative to the first surface to decelerate the launch carriage, the second angle being different than the first angle.

11. The apparatus of claim 1 wherein the second launch member translates and pivots relative to the first launch member from the first position to the second position.

12. The apparatus of claim 1 wherein the second launch member includes a guide pin, and wherein the apparatus further comprises a guide having an elongated guide slot positioned between the first and second launch members, the guide pin being received in the guide slot to allow the guide pin to translate along the guide slot while the second launch member rotates relative to the first launch member.

13. The apparatus of claim 1, further comprising a carriage return coupled to the launch carriage, the carriage return being positioned to reset the launch carriage to the first launch carriage location after takeoff of the aircraft.

14. The apparatus of claim 1 wherein the at least one launch member moves in a generally vertical plane between the first position and the second position.

15. The apparatus of claim 1 wherein the at least one launch member moves in a generally horizontal plane between the first position and the second position.

16. The apparatus of claim 1 wherein the first and second launch members are coupled to each other with a cable and an arrangement of pulleys.

17. The apparatus of claim 1 wherein the first and second launch members are coupled to each other with a four-bar linkage.

18. The apparatus of claim 1 wherein the first and second launch members are pivotable relative to each other.

19. The apparatus of claim 1 wherein the first launch member includes a first roller surface and the second launch member includes a second roller surface non-parallel to the first roller surface, and wherein the angle between the first and second roller surfaces is greater when the launch carriage is in the second launch carriage location than when the launch carriage is in the first launch carriage location.

20. The apparatus of claim 1, further comprising the unmanned aircraft.

21. An apparatus for launching an unmanned aircraft, comprising:

a support structure;

a first launch member fixed relative to the support structure;

a second launch member coupled to the support structure, the second launch member being movable relative to the support structure and the first launch member;

an actuator coupled to the second launch member and positioned to move the second launch member relative to the first launch member from a first position to a second position; and

a launch carriage having an aircraft support positioned to releasably carry an unmanned aircraft during a takeoff operation, the launch carriage being in direct contact with the first and second launch members and being movable relative to the first and second launch members between a first launch carriage location and a second launch carriage location as the second launch member moves from the first position to the second position, wherein the first launch member includes a first surface in contact with the launch carriage, and wherein the second launch member includes a second surface in contact with the launch carriage, the second surface having a first portion oriented at a first angle relative to the first surface to accelerate the launch carriage, the second surface having a second portion oriented at a second angle relative to the first surface to decelerate the launch carriage, the second angle being different than the first angle.

22. The apparatus of claim 21 wherein the actuator includes at least one of a hydraulic cylinder, a spring, a pneumatic cylinder, an electric motor, a flywheel, a steam-powered apparatus, an explosive charge, and a weight.

23. The apparatus of claim 21, further comprising a transmission coupled between the actuator and the second launch member, wherein the transmission includes a first portion coupled to the actuator to receive a first force from the actuator and accelerate with a first acceleration, the transmission further including a second portion coupled to the second launch member to impart a second force and a second acceleration to the launch carriage, wherein the second force is different than the first force and the second acceleration is different than the first acceleration.

24. The apparatus of claim 21 wherein:

the first launch member includes a first roller surface and the second launch member includes a second roller surface non-parallel to the first roller surface; and

the launch carriage includes a first wheel in rolling contact with the first roller surface and a second wheel in rolling contact with the second roller surface.

25. The apparatus of claim 21 wherein the second launch member translates and pivots relative to the first launch member as the second launch member moves from the first position to the second position.

26. The apparatus of claim 21, further comprising a carriage return coupled to the launch carriage, the carriage return being positioned to reset the launch carriage to the first launch carriage location after takeoff of the aircraft.

27. An apparatus for launching an unmanned aircraft, comprising:

a first launch member;

a second launch member pivotally coupled to the first launch member, at least one of the first and second launch members being pivotable relative to the other between a first position and a second position;

an actuator coupled to the at least one launch member and positioned to pivot the at least one launch member from the first position to the second position; and

a launch carriage having an aircraft support positioned to releasably carry an unmanned aircraft during a takeoff operation, the launch carriage being in contact with the first and second launch members, the launch carriage being forced to move relative to the launch members between a first launch carriage location and a second launch carriage location as the at least one launch member moves from the first position to the second position.

28. The apparatus of claim 27 wherein the first launch member includes a first surface in contact with the launch carriage, and wherein the second launch member includes a second surface in contact with the launch carriage, the second surface having a first portion oriented at a first angle relative to the first surface to accelerate the launch carriage, the second surface having a second portion oriented at a second angle relative to the first surface to decelerate the launch carriage, the second angle being different than the first angle.

29. The apparatus of claim 27 wherein:

the first launch member includes a first roller surface and the second launch member includes a second roller surface non-parallel to the first roller surface; and

the launch carriage includes a first wheel in rolling contact with the first roller surface and a second wheel in rolling contact with the second roller surface.

30. The apparatus of claim 27 wherein the at least one launch member moves in a generally lateral plane.

31. The apparatus of claim 27 wherein each of the first and second launch members pivots relative to the other.

32. The apparatus of claim 27 wherein the actuator includes at least one of a hydraulic cylinder, a spring, a pneumatic cylinder, an electric motor, a flywheel, a steam-powered apparatus, an explosive charge, and a weight.

33. The apparatus of claim 27 wherein:

the first and second launch members each include a first end portion and a second end portion spaced apart from the first end portion;

the first end portions of the first and the second launch member are pivotally coupled together; and

the second end portions of the first and the second launch members are coupled to the actuator, and wherein the actuator is positioned to move the second end portions of the first and the second launch member apart from each other.

34. The apparatus of claim 27, further comprising a carriage return coupled to the launch carriage, the carriage return being positioned to reset the launch carriage to the first launch carriage location after takeoff of the aircraft.

35. An apparatus for launching an unmanned aircraft, comprising:

a first launch member;

a second launch member positioned at least proximate to the first launch member, at least one of the first and second launch members being movable relative to the other between a first position and a second position; and

a launch carriage having an aircraft support positioned to releasably carry an unmanned aircraft during a takeoff operation, the launch carriage being in contact with the first and second launch members, the launch carriage being movable relative to the launch members in a first direction between a first launch carriage location and a second launch carriage location as the at least one of the first and second launch members moves from the first position to the second position in a second direction transverse to the first direction.