IP Library Granted Patent US 11,008,102
Granted Patent B2
US 11,008,102 · App. 16/161,455 · Granted May 18, 2021

Maneuverable capture apparatus for airborne deployment and retrieval of parasite aircraft

Inventors: Michael John Ryan (Colleyville, TX); Carlos Alexander Fenny (Fort Worth, TX); Joseph Scott Drennan (Dallas, TX); John Richard McCullough (Weatherford, TX); Brett Rodney Zimmerman (Hurst, TX)
Assignee: Bell Textron Inc.
B64D5/00B64C3/56B64C39/024B64C2201/027B64C2201/082B64C2201/206
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Quick Facts
Patent No.
US 11,008,102
App. No.
16/161,455
Granted
May 18, 2021
Kind
B2
Abstract

In an embodiment, a maneuverable capture device includes a frame, a plurality of rotors secured to the frame, an attachment point disposed on the frame for securing a cable of a carrier aircraft to the frame, and an attachment feature configured to secure maneuverable capture device to a dock of a parasite aircraft. In an embodiment, a method of docking a maneuverable capture device with a parasite aircraft includes positioning a carrier aircraft above a parasite aircraft, releasing the maneuverable capture device attached to the carrier aircraft by a cable from the carrier aircraft, flying the maneuverable capture device to a dock of the parasite aircraft, and securing the maneuverable capture device to the dock of the parasite aircraft.

Claims (34)

1. A maneuverable capture device comprising:

a frame;

a plurality of rotors secured to the frame;

an attachment point disposed on the frame for securing a cable of a carrier aircraft to the frame; and

an attachment feature configured to secure the frame to a dock of a parasite aircraft, the attachment feature comprising a rod that extends from the frame such that at least a portion of the rod is forward of the plurality of rotors, the rod configured to mate with a housing of the dock.

2. The maneuverable capture device of claim 1 , wherein the rod is configured to enter an opening in the housing of the dock.

3. The maneuverable capture device of claim 1 , wherein the rod comprises a groove configured to interact with a ball-lock disposed within the housing to secure the rod to the dock.

4. The maneuverable capture device of claim 1 , wherein the attachment feature comprises a hook that extends from the frame, the hook configured to mate with a pin of the dock.

5. The maneuverable capture device of claim 1 , further comprising:

a pair of cross-supports attached to the frame; and

wherein the plurality of rotors comprises four rotors and each cross-support of the pair of cross-supports includes one rotor disposed at each end of the cross-support.

6. The maneuverable capture device of claim 1 , wherein each rotor of the plurality of rotors is configured to pivot relative to the frame to allow a direction of thrust of each rotor to be controlled.

7. The maneuverable capture device of claim 1 , further comprising a housing disposed on the frame.

8. The maneuverable capture device of claim 1 , further comprising a second attachment point for securing a cable of the carrier aircraft to the frame.

9. The maneuverable capture device of claim 1 , wherein the attachment feature comprises a hook that extends from the frame substantially perpendicularly to the rod, the hook configured to mate with a pin of the dock.

10. A method of docking a maneuverable capture device with a parasite aircraft, the method comprising:

positioning a carrier aircraft above the parasite aircraft;

releasing the maneuverable capture device from the carrier aircraft;

flying the maneuverable capture device to a dock of the parasite aircraft;

securing the maneuverable capture device to the dock of the parasite aircraft, wherein the securing comprising positioning a rod of the maneuverable capture device into a housing of the dock, and wherein the rod extends forward of a plurality of rotors of the maneuverable capture device; and

wherein the maneuverable capture device is attached to the carrier aircraft by a cable.

11. The method of claim 10 , further comprising letting out the cable from the carrier aircraft as the maneuverable capture device flies toward to the parasite aircraft.

12. The method of claim 10 , wherein the securing comprises positioning the rod of the maneuverable capture device into an opening in the housing of the dock.

13. The method of claim 10 , wherein the rod includes a groove that is configured to mate with a ball-lock disposed within the housing.

14. The method of claim 10 , wherein the securing comprises positioning a hook of the maneuverable capture device around a pin of the dock.

15. The method of claim 10 , wherein, during the positioning the carrier aircraft above the parasite aircraft, the parasite aircraft is positioned on a loading surface.

16. The method of claim 10 , wherein, during the positioning the carrier aircraft above the parasite aircraft, the parasite aircraft is in flight.

17. The method of claim 10 , wherein the flying the maneuverable capture device comprises pivoting the plurality of rotors of the maneuverable capture device to control a direction of thrust of the plurality of rotors.

18. A method of undocking a maneuverable capture device from a parasite aircraft, the method comprising:

releasing the maneuverable capture device from a dock of the parasite aircraft, the releasing comprising unlocking a rod of the maneuverable capture device, the rod extending forward of a plurality of rotors of the maneuverable capture device;

flying the maneuverable capture device away from the parasite aircraft; and

reeling in a cable secured between the maneuverable capture device and a carrier aircraft.

19. The method of claim 18 , wherein the releasing comprises unlocking a ball-lock from the rod of the maneuverable capture device.

20. The method of claim 18 , wherein the flying comprises pivoting the plurality of rotors of the maneuverable capture device to control a direction of thrust of the plurality of rotors.

Assignments (6)
CORRECTIVE ASSIGNMENT TO CORRECT THE THE NAME OF THE RECEIVING PARTY PREVIOUSLY RECORDED AT REEL: 059970 FRAME: 0231. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT. Recorded Jul 29, 2022
From: BELL HELICOPTER TEXTRON INC.
To: BELL HELICOPTER RHODE ISLAND INC.
Reel/Frame 061003/0869 →
CORRECTIVE ASSIGNMENT TO CORRECT THE THE SPELLING IN THE ASSIGONR'S NAME PREVIOUSLY RECORDED AT REEL: 059758 FRAME: 0819. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT. Recorded May 12, 2022
From: BELL HELICOPTER TEXTRON INC.
To: BELL TEXTRON RHODE ISLAND INC.
Reel/Frame 059970/0231 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 28, 2022
From: BELL HELICOTPTER TEXTRON INC.
To: BELL TEXTRON RHODE ISLAND INC.
Reel/Frame 059758/0819 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 28, 2022
From: BELL HELICOPTER RHODE ISLAND INC.
To: TEXTRON INNOVATIONS INC.
Reel/Frame 059765/0361 →
CHANGE OF NAME Recorded Mar 23, 2021
From: BELL HELICOPTER TEXTRON INC.
To: BELL TEXTRON INC.
Reel/Frame 055681/0622 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 19, 2018
From: RYAN, MICHAEL JOHN; FENNY, CARLOS ALEXANDER; DRENNAN, JOSEPH SCOTT; MCCULLOUGH, JOHN RICHARD; ZIMMERMAN, BRETT RODNEY
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 047233/0801 →
Continuity (1)
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