Hydraulic thrust vector yaw control for rocket catapult motor assembly

Patent metadata

Field	Value
Publication number	US-11338924-B2
Application number	US-202016892972-A
Country	US
Kind code	B2
Filing date	Jun 4, 2020
Priority date	Jul 12, 2019
Publication date	May 24, 2022
Grant date	May 24, 2022

Abstract

A motor cap assembly for an ejection seat may comprise a servo valve assembly, a reservoir a cylinder, a motor cap manifold housing comprising a monolithic body having an internal manifold structure integral to the body configured to communicate a gas between a pressure source and a gas block, and configured to communicate a hydraulic fluid between, the reservoir, the servo valve assembly, and the cylinder, a rack piston disposed within the cylinder and configured to translate axially therein between a base end and a head end of the cylinder, and a motor cap outer housing coupled circumferentially about the motor cap manifold housing, wherein the motor cap outer housing is configured to rotate circumferentially about the motor cap manifold housing in response to an axial translation of the rack piston.

First claim

What is claimed is:

1. A motor cap assembly, comprising:
a servo valve assembly;
a reservoir;
a gas block;
a motor cap manifold housing comprising a monolithic body having an internal manifold structure integral to the monolithic body configured to communicate a gas between a pressure source and the gas block;
a rack piston disposed within a cylinder defined by the motor cap manifold housing, the rack piston being configured to translate axially between a base end and a head end of the cylinder, wherein the internal manifold structure of the motor cap manifold housing is configured to communicate a hydraulic fluid between the reservoir, the servo valve assembly, and the cylinder; and
a motor cap outer housing coupled circumferentially about the motor cap manifold housing, wherein the motor cap outer housing includes a toothed drive ring at an inner diameter surface of the motor cap outer housing, the inner diameter surface being oriented toward an axis about which the motor cap outer housing rotates, and wherein the motor cap outer housing is configured to rotate circumferentially about the motor cap manifold housing in response to an axial translation of the rack piston.

2. The motor cap assembly of claim 1 , wherein the gas block includes a gas nipple piston configured to translate within the gas block in response to a rotation of the motor cap outer housing.

3. The motor cap assembly of claim 2 , wherein the motor cap outer housing comprises a gas tap selectively in fluid communication with the gas block via the gas nipple piston.

4. The motor cap assembly of claim 3 , wherein the cylinder is integral to the motor cap manifold housing.

5. The motor cap assembly of claim 4 , further comprising a pinion gear intermeshed with the rack pinion, and wherein the pinion gear is located through a pinion window defined by the motor cap manifold housing.

6. The motor cap assembly of claim 5 , wherein the rack piston comprises a toothed rack coupled to the pinion gear via the pinion window.

7. The motor cap assembly of claim 6 , further comprising a drive ring gear, wherein rotation of the pinion gear drives a rotation of the drive ring gear.

8. The motor cap assembly of claim 7 , wherein the drive ring gear is intermeshed with the drive ring of the motor cap outer housing.

9. The motor cap assembly of claim 1 , further comprising a tangible, non-transitory memory configured to communicate with a controller, the tangible, non-transitory memory having instructions stored thereon that, in response to execution by the controller, cause the controller to perform operations comprising:
determining, by the controller, a current yaw angle;
determining, by the controller, a desired yaw angle;
calculating, by the controller, a yaw command angle based on the desired yaw angle; and
sending, by the controller, a command to the servo valve assembly, the command being configured to rotate the motor cap outer housing to the yaw command angle.

10. An ejection seat, comprising:
a seat pan;
a seat back coupled to the seat pan; and
a rocket catapult assembly coupled to the seat back, the rocket catapult assembly including:
a motor assembly configured to generate a high pressure gas,
a nozzle assembly coupled to the motor assembly and configured to receive the high pressure gas, and
a motor cap assembly coupled to the motor assembly distal of the nozzle assembly and configured to receive the high pressure gas, the motor cap assembly comprising:
a servo valve assembly;
a reservoir;
a gas block;
a motor cap manifold housing comprising a monolithic body having an internal manifold structure integral to the monolithic body configured to communicate the high pressure gas between the motor assembly and the gas block;
a rack piston disposed within a cylinder defined by the motor cap manifold housing, the rack piston being configured to translate axially within the cylinder, wherein the internal manifold structure of the motor cap manifold housing is configured to communicate a hydraulic fluid between, the reservoir, the servo valve assembly, and the cylinder; and
a motor cap outer housing coupled circumferentially about the motor cap manifold housing, wherein the motor cap outer housing includes a toothed drive ring at an inner diameter surface of the motor cap outer housing, the inner diameter surface being oriented toward an axis about which the motor cap outer housing rotates, and wherein the motor cap outer housing is configured to rotate circumferentially about the motor cap manifold housing in response to an axial translation of the rack piston.

11. The ejection seat of claim 10 , wherein the gas block includes a gas nipple piston configured to translate within the gas block in response to a rotation of the motor cap outer housing.

12. The ejection seat of claim 11 , wherein the motor cap outer housing comprises a gas tap selectively in fluid communication with the gas block via the gas nipple piston.

13. The ejection seat of claim 12 , wherein the cylinder is integral to the motor cap manifold housing.

14. The ejection seat of claim 13 , wherein the rocket catapult assembly further comprises a pinion gear intermeshed with the rack pinion, and wherein the pinion gear is located through a pinion window defined by the motor cap manifold housing.

15. The ejection seat of claim 14 , wherein the rack piston comprises a toothed rack coupled to the pinion gear via the pinion window.

16. The ejection seat of claim 15 , wherein the rocket catapult assembly further comprises a drive ring gear, and wherein rotation of the pinion gear drives a rotation of the drive ring gear.

17. The ejection seat of claim 16 , wherein the drive ring gear is intermeshed with the drive ring.

18. The ejection seat of claim 10 , further comprising a tangible, non-transitory memory configured to communicate with a controller, the tangible, non-transitory memory having instructions stored thereon that, in response to execution by the controller, cause the controller to perform operations comprising:
determining, by the controller, a current yaw angle;
determining, by the controller, a desired yaw angle;
calculating, by the controller, a yaw command angle based on the desired yaw angle; and
sending, by the controller, a command to the servo valve assembly, the command being configured to rotate the motor cap outer housing to the yaw command angle.

19. An article of manufacture including a tangible, non-transitory computer-readable storage medium having instructions stored thereon that, in response to execution by a processor, cause the processor to perform operations comprising:
transitioning, by the processor, a rocket catapult assembly from an inactive to an active state;
retracting, by the processor, a gas nipple piston and breaking a fluid communication between a gas cylinder and a gas port;
determining, by the processor, a current yaw angle based on a yaw rate signal;
determining, by the processor, a desired yaw angle based on a first pressure signal;
calculating, by the processor, a yaw command angle based on the desired yaw angle; and
commanding, by the processor, a motor cap assembly to rotate to the yaw command angle,
wherein commanding, by the processor, the motor cap assembly to rotate to the yaw command angle includes sending, by the processor, a command to a servo valve of the motor cap assembly, and wherein the command is configured to cause an axial translation of a rack piston, and wherein a motor cap outer housing of the motor cap assembly rot

Assignees

• Ami Ind Inc

Inventors

• Mastrolia Bradley

Classifications

• B64D25/10 Primary

  Ejector seats · CPC title

• F02K9/84

  using movable nozzles · CPC title