Joule-Thompson cooler actuation systems

Patent metadata

Field	Value
Publication number	US-12007212-B2
Application number	US-202117450449-A
Country	US
Kind code	B2
Filing date	Oct 8, 2021
Priority date	Oct 8, 2021
Publication date	Jun 11, 2024
Grant date	Jun 11, 2024

Abstract

In accordance with at least one aspect of this disclosure, an actuation system for a guided munition, includes a reservoir disposed in a guided munition body housing a compressible fluid in a compressed state, a fluid path connecting the reservoir in fluid communication with a heat exchange volume, a throttling orifice disposed in the fluid path configured to expand the compressible fluid, and an actuation path connecting the heat exchange volume in fluid communication with a moveable component. The actuation path can be configured to supply pneumatic pressure to the moveable components.

First claim

What is claimed is:

1. An actuation system for a guided munition, comprising:
a reservoir disposed in a guided munition body housing a compressible fluid in a compressed state;
a fluid path connecting the reservoir in fluid communication with a heat exchange volume;
a throttling orifice disposed in the fluid path configured to expand the compressible fluid; and
an actuation path connecting the heat exchange volume in fluid communication with a moveable component, wherein the actuation path is configured to supply pneumatic pressure to the moveable component, wherein the moveable component includes a nose cone segment mounted to the guided munition body.

2. The system as recited in claim 1 , wherein the fluid path is configured to cool the heat exchange volume in the fluid path prior to entering the actuation path.

3. The system as recited in claim 1 , wherein the actuation system is included in the guided munition body, wherein the fluid path is configured to direct the compressible fluid from the throttling orifice outlet to the heat exchange volume and the actuation path is configured to direct the compressible fluid from the heat exchange volume toward a respective nose cone segment to move the nose cone segment from a stowed position to a deployed position.

4. The system as recited in claim 1 , wherein the actuation system is included in a nose cone mounted the guided munition body, wherein the fluid path is configured to direct the compressible fluid from the throttling orifice outlet to the heat exchange volume and the actuation path is configured to direct the compressible fluid from the heat exchange volume away from a respective nose cone segment to move the respective nose cone segment from a stowed position to a deployed position.

5. The system as recited in claim 4 , wherein the actuation system is configured to be ejected from the guided munition body with the respective nose cone segment upon deployment of the respective nose cone segment.

6. The system as recited in claim 1 , wherein the reservoir further includes an actuated discharge valve, and further comprising a controller operatively connected to control the discharge valve to discharge the compressible fluid at a predetermined time.

7. A guided munition comprising:
a guided munition body;
a moveable component mounted for movement relative to the guided munition body; and
an actuation system configured to move the moveable component, the actuation system comprising:
a reservoir disposed in the guided munition body housing a compressible fluid in a compressed state;
a fluid path connecting the reservoir in fluid communication with a heat exchange volume;
a throttling orifice disposed in the fluid path configured to expand the compressible fluid; and
an actuation path connecting the heat exchange volume in fluid communication with the moveable component, wherein the actuation path is configured to supply pneumatic pressure to the moveable component, wherein the moveable component includes a nose cone segment mounted to the guided munition housing.

8. The system as recited in claim 7 , wherein the fluid path is configured to direct the compressible fluid from the throttling orifice outlet to the heat exchange volume and the actuation path is configured to direct the compressible fluid from the heat exchange volume toward a respective nose cone segment to move the nose cone segment from a stowed position to a deployed position.

9. The system as recited in claim 7 , wherein the actuation system is included in a nose cone mounted the guided munition body, wherein the fluid path is configured to direct the compressible fluid from the throttling orifice outlet to the heat exchange volume and the actuation path is configured to direct the compressible fluid from the heat exchange volume away from a respective nose cone segment to move the respective nose cone segment from a stowed position to a deployed position.

10. The system as recited in claim 9 , wherein the actuation system is configured to be ejected from the guided munition body with the respective nose cone segment upon actuation of the actuation system.

Assignees

• Simmonds Precision Products

Inventors

• Graham Jason
• Bibeau Craig R

Classifications

• F42B10/52

  Nose cones · CPC title

• F42B10/20

  deployed by combustion gas pressure, or by pneumatic or hydraulic forces · CPC title

• F25B2309/02

  using the Joule-Thompson effect · CPC title

• F25B9/02

  using Joule-Thompson effect; using vortex effect · CPC title

• F42B10/64

  of fins · CPC title