Electronic release systems and methods for ejection seats

Patent metadata

Field	Value
Publication number	US-11655041-B2
Application number	US-202117461559-A
Country	US
Kind code	B2
Filing date	Aug 30, 2021
Priority date	Aug 30, 2021
Publication date	May 23, 2023
Grant date	May 23, 2023

Abstract

An electronic release system for an aircraft ejection system may comprise: a controller; a plurality of release devices in operable communication with the controller; a plurality of pins, each pin in the plurality of pins operably coupled to a release device in the plurality of release devices, the controller configured to: receive an indication that an ejection event from an aircraft has been initiated, command activation of the plurality of release devices, and in response to commanding the activation, releasing the plurality of pins from an ejection seat.

First claim

What is claimed is:

1. An electronic release system for an aircraft ejection system, comprising:
a controller;
a plurality of release devices in operable communication with the controller;
a plurality of pins, each pin in the plurality of pins operably coupled to a release device in the plurality of release devices, the controller configured to:
receive an indication that an ejection event from an aircraft has been initiated,
command activation of the plurality of release devices, and
in response to commanding the activation, releasing the plurality of pins from an ejection seat.

2. The electronic release system of claim 1 , further comprising the ejection seat.

3. The electronic release system of claim 1 , wherein the plurality of pins includes a first pin configured to release a lap belt during releasing the plurality of pins.

4. The electronic release system of claim 3 , wherein the plurality of pins include a second pin configured to release a leg restraint during releasing the plurality of pins.

5. The electronic release system of claim 1 , wherein releasing each pin in the plurality of pins occurs within one second of each other.

6. The electronic release system of claim 1 , wherein the controller is further configured to receive a second indication a predetermined time has elapsed since the ejection event was initiated.

7. The electronic release system of claim 1 , further comprising a lap belt, a first pin in the plurality of pins configured to secure the lap belt during operation of the aircraft.

8. The aircraft comprising the electronic release system of claim 1 .

9. An electronic release system for an aircraft ejection system, comprising:
a controller;
a maintenance electrical port in electrical communication with the controller;
a plurality of pins configured to be released during an ejection event;
a plurality of release devices in electronic communication with the controller, each release device in the plurality of release devices in operable communication with a pin in the plurality of pins, the controller configured to:
receive a command to release a first release device in the plurality of release devices; and
command release of the first release device in the plurality of release devices, a remainder plurality of release devices remaining un-released.

10. The electronic release system of claim 9 , wherein the controller is further configured to:
receive an indication that the ejection event from an aircraft has been initiated,
command activation of the plurality of release devices, and
in response to commanding the activation, releasing the plurality of pins from an ejection seat.

11. The electronic release system of claim 10 , wherein releasing each pin in the plurality of pins occurs within one second of each other.

12. The electronic release system of claim 9 , further comprising an ejection seat, the controller disposed within the ejection seat.

13. The electronic release system of claim 9 , wherein the plurality of pins includes a first pin configured to release a lap belt during releasing the plurality of pins.

14. The electronic release system of claim 9 , wherein the controller is further configured to:
receive a second command to close the first release device; and
command the first release device to close in response to receiving the second command.

15. A method, comprising:
receiving, via a processor, an indication that an ejection event from an aircraft is initiated;
commanding, via the processor, activation of a plurality of release devices to supply a retraction force to a plurality of pins; and
in response to activation of the plurality of release devices, releasing the plurality of pins from an ejection seat of the aircraft.

16. The method of claim 15 , wherein an occupant is released from the ejection seat in response to releasing the plurality of pins.

17. The method of claim 15 , wherein releasing each pin in the plurality of pins occurs within one second of a remainder of pins in the plurality of pins being released.

18. The method of claim 15 , further comprising receiving, via the processor, a predetermined time has elapsed since the ejection event was initiated.

19. The method of claim 18 , wherein commanding activation of the plurality of release devices is in response to the predetermined time elapsing.

20. The method of claim 15 , wherein releasing the plurality of pins includes releasing a lap belt, a leg restraint, and a shoulder harness.

Assignees

• Ami Ind Inc

Inventors

• Stribrny Casey
• Bharucha Nicholas
• Holstine Steven
• Fulcher Jackson

Classifications

• B64F5/40

  Maintaining or repairing aircraft · CPC title

• B64D25/10 Primary

  Ejector seats · CPC title

• B64D25/06

  Harnessing · CPC title