Apparatus for restraining an aircraft

Patent metadata

Field	Value
Publication number	US-11858658-B2
Application number	US-202217687356-A
Country	US
Kind code	B2
Filing date	Mar 4, 2022
Priority date	Jun 10, 2021
Publication date	Jan 2, 2024
Grant date	Jan 2, 2024

Abstract

Examples include an apparatus for restraining an aircraft during engine acceleration, the apparatus including: a collet shaft that is configured to attach to the aircraft, a rod that is configured to attach to a runway, and a release mechanism that is configured to restrain the collet shaft to the release mechanism and configured to release the collet shaft in response to the release mechanism receiving an electric current.

First claim

What is claimed is:

1. An apparatus for restraining an aircraft during engine acceleration, the apparatus comprising:
a collet shaft that is configured to attach to the aircraft;
a rod that is configured to attach to a runway; and
a release mechanism comprising:
an electrical terminal;
a clamshell;
a fuse wire; and
a coil of wire disposed around the clamshell and anchored to the electrical terminal by the fuse wire, wherein the clamshell is configured to restrain the collet shaft and configured to release the collet shaft in response to an electric current flowing through the fuse wire and thermally deforming the fuse wire.

2. The apparatus of claim 1 , wherein the collet shaft is free to move away from the rod upon release of the collet shaft from the release mechanism.

3. The apparatus of claim 1 , further comprising a housing, wherein the collet shaft is configured to move away from the rod within the housing upon release of the collet shaft from the release mechanism.

4. The apparatus of claim 1 , wherein the rod comprises a clevis pin configured to attach to a clevis that is mounted to the runway.

5. The apparatus of claim 1 , wherein the collet shaft comprises keyed receiving surfaces configured to engage with keyed hooks of an attachment component of the aircraft.

6. The apparatus of claim 5 , the apparatus further comprising a housing configured to receive the keyed hooks and hold the keyed hooks against the keyed receiving surfaces.

7. The apparatus of claim 1 , further comprising a housing configured to contain the release mechanism and the collet shaft.

8. The apparatus of claim 1 , further comprising a wireless communication interface, wherein the release mechanism is configured to release the collet shaft in response to receiving a command via the wireless communication interface.

9. The apparatus of claim 1 , further comprising a wired communication interface, wherein the release mechanism is configured to release the collet shaft in response to receiving a command via the wired communication interface.

10. The apparatus of claim 1 , further comprising a power supply, wherein the power supply is configured to cause the release mechanism to release the collet shaft in response to enabling the power supply.

11. The apparatus of claim 1 , the collet shaft comprising a main body and a release pin attached to the main body, wherein the clamshell is configured to restrain the release pin, and wherein a first end of the main body is configured to attach to the aircraft and a second end of the main body is attached to the release pin.

12. A method for restraining an aircraft during engine acceleration, the method comprising:
attaching a collet shaft of an apparatus to the aircraft;
attaching a rod of the apparatus to a runway; and
causing an electric current to flow through a fuse wire of the apparatus, thereby thermally deforming the fuse wire, releasing from an electrical terminal of the apparatus a coil of wire that is disposed around a clamshell, and causing the clamshell to release the collet shaft.

13. The method of claim 12 , wherein causing the clamshell to release the collet shaft comprises causing the collet shaft to move away from the rod such that an attachment component of the aircraft exits a housing of the apparatus and disconnects from the collet shaft.

14. The method of claim 12 , wherein causing the electric current to flow through the fuse wire comprises causing the electric current to flow through the fuse wire in response to a wired communication interface or a wireless communication interface of the apparatus receiving a command to release the aircraft.

15. The method of claim 12 , wherein causing the clamshell to release the collet shaft comprises causing the clamshell to release a release pin of the collet shaft while a main body of the collet shaft is attached to the aircraft and attached to the release pin.

16. The method of claim 12 , further comprising:
accelerating an engine of the aircraft while the aircraft is restrained to the runway by the apparatus.

17. The method of claim 16 , wherein accelerating the engine comprises accelerating the engine before causing the electric current to flow through the fuse wire.

18. The method of claim 16 , wherein causing the clamshell to release the collet shaft comprises releasing the collet shaft such that an attachment component of the aircraft exits a housing of the apparatus and disconnects from the collet shaft.

19. The method of claim 16 , wherein causing the electric current to flow through the fuse wire comprises causing the electric current to flow through the fuse wire in response to a wired communication interface or a wireless communication interface of the apparatus receiving a command to release the aircraft.

20. An apparatus for restraining an aircraft during engine acceleration, the apparatus comprising:
a collet shaft that is configured to attach to the aircraft;
a rod that is configured to attach to a runway; and
a release mechanism that is configured to restrain the collet shaft to the release mechanism and configured to release the collet shaft in response to the release mechanism receiving an electric current,
the collet shaft comprising a main body and a release pin attached to the main body, wherein the release mechanism comprises a clamshell configured to restrain the release pin, and wherein a first end of the main body is configured to attach to the aircraft and a second end of the main body is attached to the release pin,
wherein the release mechanism further comprises:
a coil of wire around the clamshell;
an electrical terminal; and
a fuse wire that anchors the coil of wire to the electrical terminal, wherein the clamshell is configured to release the collet shaft in response to the electric current deforming the fuse wire.

Assignees

• Boeing Co

Inventors

• Bower Tim
• Burns Donald R
• Mulero Mellyssa
• Schnieders John P
• Bedell Roger W

Classifications

• B64F1/223

  for towing aircraft · CPC title

• B64F1/04 Primary

  for launching aircraft · CPC title

• B64F1/06 Primary

  using catapults · CPC title

• B64F1/16

  Pickets or ground anchors; Wheel chocks · CPC title