Passively jettisoned control surface restraint and cover for tactical flight vehicles

Patent metadata

Field	Value
Publication number	US-12044513-B2
Application number	US-202217829799-A
Country	US
Kind code	B2
Filing date	Jun 14, 2022
Priority date	Jun 14, 2022
Publication date	Jul 23, 2024
Grant date	Jul 23, 2024

Abstract

A system for restraining one or more control surfaces of a tactical flight vehicle includes a retaining frame secured at an aft end of the tactical flight vehicle and a cover plate releasably coupled to the retaining frame with a resilient lock ring. The resilient lock ring is disposed between the retaining frame and the cover plate and is deformable between a locking configuration and an unlocking configuration. A control surface restraining ring is releasably coupled to the cover plate and has control surface restraints configured to engage respective control surfaces. The resilient lock ring is configured to deform from the locking configuration to the unlocking configuration upon a launch of the tactical flight vehicle such that the cover plate becomes uncoupled from the retaining frame and may be jettisoned from the tactical flight vehicle after the launch.

First claim

What is claimed is:

1. A control surface restraining system for restraining one or more control surfaces of a tactical flight vehicle, the control surface restraining system comprising:
a retaining frame secured at an aft end of the tactical flight vehicle;
a cover plate releasably coupled to the retaining frame with a resilient lock ring, the cover plate covering the aft end of the tactical vehicle during the launch of the tactical vehicle, and the resilient lock ring being disposed between the retaining frame and the cover plate, wherein the resilient lock ring is deformable between a locking configuration for coupling the cover plate to the retaining frame, and an unlocking configuration for uncoupling the cover plate from the retaining frame; and
a control surface restraining ring releasably coupled to the cover plate and having one or more control surface restraints configured to engage a respective one of the one or more control surfaces of the tactical flight vehicle when the control surface restraining ring is coupled to the cover plate and the cover plate is coupled to the retaining frame;
wherein the resilient lock ring is configured to deform from the locking configuration to the unlocking configuration upon a launch of the tactical flight vehicle such that the cover plate becomes uncoupled from the retaining frame and may be jettisoned from the tactical flight vehicle after the launch.

2. The control surface restraining system according to claim 1 , wherein the retaining frame is annular and is secured around a periphery of the aft end of the tactical flight vehicle.

3. The control surface restraining system according to claim 1 , wherein the retaining frame is secured to the aft end of the tactical flight vehicle with one or more frame fasteners.

4. The control surface restraining system according to claim 1 , wherein the cover plate includes a retaining frame coupling groove arranged concentrically within a periphery of the cover plate on a first face of the cover plate, the first face of the cover plate opposing the aft end of the tactical flight vehicle, for receiving the retaining frame when the cover plate is coupled to the retaining frame.

5. The control surface restraining system according to claim 4 , wherein the resilient lock ring is disposed between a radially inner surface of the retaining frame and a first opposing wall of the retaining frame coupling groove of the cover plate.

6. The control surface restraining system according to claim 5 , wherein the resilient lock ring is disposed at least partially in a lock ring groove on the first opposing wall of the retaining frame coupling groove of the cover plate.

7. The control surface restraining system according to claim 4 , further comprising a seal disposed between a radially outer surface of the retaining frame and a second opposing wall of the retaining frame coupling groove of the cover plate.

8. The control surface restraining system according to claim 7 , wherein the seal is disposed at least partially in a seal groove on the radially outer surface of the retaining frame.

9. The control surface restraining system according to claim 1 , wherein the control surface restraining ring is releasably coupled to the cover plate with one or more restraining ring fasteners.

10. The control surface restraining system according to claim 9 , wherein the one or more restraining ring fasteners includes a quick release pull-pin fastener.

11. The control surface restraining system according to claim 1 , wherein each of the one or more control surface restraints includes a control surface notch for engaging the respective one of the one or more control surfaces of the tactical flight vehicle.

12. The control surface restraining system according to claim 11 , wherein a width of the control surface notch of each of the one or more control surface restraints is greater than a thickness of the one or more control surfaces.

13. The control surface restraining system of claim 1 , wherein the tactical vehicle lies along a longitudinal axis, and wherein the cover plate is jettisoned from the tactical vehicle along said longitudinal axis after the tactical vehicle's launch.

14. The control surface restraining system of claim 1 , wherein the resilient lock ring has a hoop shape.

Assignees

• Raytheon Co

Inventors

• Dixon Jason Allan
• Kehl Kenyon
• Melkers Edgar R
• Firor Randall S

Classifications

• F42B10/00

  Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding (F42B6/00 takes precedence) · CPC title

• F41F3/06

  from aircraft {(F41F3/0406 takes precedence; arrangements of rocket launchers on aircraft B64D7/08; bomb releasing in flight B64D1/06)} · CPC title

• F42B39/00

  Packaging or storage of ammunition or explosive charges; Safety features thereof; Cartridge belts or bags · CPC title

• F42B10/64 Primary

  of fins · CPC title