Pressure activated release for deployment of surface, aerial and subsea payloads

Patent metadata

Field	Value
Publication number	US-10287022-B2
Application number	US-201615250418-A
Country	US
Kind code	B2
Filing date	Aug 29, 2016
Priority date	Aug 29, 2016
Publication date	May 14, 2019
Grant date	May 14, 2019

Abstract

A pressure activated release system and method are disclosed for deployment of surface, aerial and subsea payloads. The system and method include a payload release switch that is activated, without human intervention, by a pressure differential. The system and method also includes a payload release mechanism having an unreleased configuration at pressures below a specified pressure. The release mechanism has a released configuration at pressures above the specified pressure. The switch causes the release mechanism to move from the unreleased configuration to the released configuration.

First claim

We claim:

1. A pressure activated release system for deployment of a payload assembly, comprising:
an aerial deployment subsystem comprising:
an aerial payload release mechanism having an unreleased configuration at pressures below a first specified pressure, the aerial payload release mechanism having a released configuration at pressures above the first specified pressure; and
an aerial payload release switch configured to be activated, without human intervention, by a first pressure differential, wherein the aerial payload release switch is configured to cause the aerial payload release mechanism to move from the unreleased configuration to the released configuration to deploy a first part of the payload assembly;

a surface deployment subsystem comprising:
a surface payload release mechanism having an unreleased configuration at pressures below a second specified pressure, the second payload release mechanism having a released configuration at pressures above the second specified pressure; and
a surface payload release switch configured to be activated, without human intervention, by a second pressure differential, wherein the surface payload release switch is configured to cause the surface payload release mechanism to move from the unreleased configuration to the released configuration to deploy a second part of the payload assembly; and

a subsea deployment subsystem comprising:
a subsea payload release mechanism having an unreleased configuration at pressures below a third specified pressure, the subsea payload release mechanism having a released configuration at pressures above the third specified pressure; and
a subsea payload release switch configured to be activated, without human intervention, by a third pressure differential, wherein the subsea payload release switch is configured to cause the subsea payload release mechanism to move from the unreleased configuration to the released configuration to deploy a third part of the payload assembly; and

wherein the payload assembly includes a payload.

2. The release system of claim 1 , further comprising:
a relay that is operably coupled to a power source and at least one of the aerial payload release switch, the surface payload release switch, and the subsea payload release switch, the relay being configured to carry power to at least one of the aerial payload release mechanism, the surface payload release mechanism, and the subsea release mechanism.

3. The release system of claim 1 , further comprising:
a power source that is operably coupled to a relay, the power source being configured to activate the relay.

4. The release system of claim 1 , wherein the aerial payload deployment subsystem includes:
an aerial drag device configured to delay a descent of an aerial payload;
wherein the aerial payload release mechanism is configured to permit release of the aerial drag device from a vehicle or vessel; and
wherein the aerial payload release switch is configured to release the aerial drag device from the aerial payload.

5. The release system of claim 1 , further comprising:
a timer device configured to permit a timed release of the payload from a shock tube.

6. The release system of claim 1 , wherein the third pressure differential activates the subsea payload release switch at a specified subsea depth; and
wherein the subsea payload release mechanism is configured to release the payload at the specified subsea depth.

7. The release system of claim 1 , wherein at least one of the aerial payload release mechanism, the surface payload release mechanism, and the subsea payload release mechanism is passively powered, and at least one of the aerial release mechanism, the surface release mechanism, and the subsea release mechanism is electrically triggered.

8. The release system of claim 1 , wherein at least one of the aerial payload release mechanism, the surface payload release mechanism, and the subsea surface payload release mechanism is a pin that pulls from a slot.

9. The release system of claim 1 , further comprising:
a containment device that contains the payload, and wherein the containment device is configured to protect the payload until the payload is released from the containment device.

10. The release system of claim 1 , wherein at least one of the aerial payload release switch, the surface payload release switch, and the subsea payload release switch is selected from the group consisting of a shear plate switch, a resettable spring plunger switch, a resettable moving diaphragm switch and a multiple contact switch.

11. The release system of claim 1 , wherein at least one of the aerial payload release mechanism, the surface payload release mechanism, and the subsea payload release mechanism is a resettable spring plunger or a resettable moving diaphragm.

12. The release system of claim 1 , wherein the payload is an active sensor.

13. A release method for deployment of a payload assembly, the method comprising the steps of:
activating, without human intervention, an aerial payload release switch by a first pressure differential;
in response to activating the aerial payload release switch, releasing a first part of the payload assembly by an aerial payload release mechanism having an unreleased configuration at pressures below a first specified pressure, the aerial payload release mechanism having a released configuration at pressures above the first specified pressure;
activating, without human intervention, a surface payload release switch by a second pressure differential;
in response to activating the surface payload release switch, releasing a second part of the payload assembly by a surface payload release mechanism having an unreleased configuration at pressures below a second specified pressure, the surface payload release mechanism having a released configuration at pressures above the second specified pressure;
activating, without human intervention, a subsea payload release switch by a third pressure differential; and
in response to activating the subsea payload release switch, releasing a third part of the payload assembly by a surface payload release mechanism having an unreleased configuration at pressures below a third specified pressure, the subsea payload release mechanism having a released configuration at pressures above the third specified pressure.

14. The release method of claim 13 , further comprising:
providing a relay that is operably coupled to a power source and at least one of the aerial payload release switch, the surface payload release switch, and the subsea payload release switch, the relay being configured to carry power to at least one of the aerial payload release mechanism, the surface payload release mechanism, and the subsea payload release mechanism.

15. The release method of claim 13 , further comprising:
releasing an aerial drag device from a vehicle or vessel;
delaying a descent of an aerial payload with the aerial drag device; and
releasing the aerial drag device from the aerial payload by activating, without human intervention, the aerial payload release switch.

16. The release method of claim 15 , further comprising:
after the step of releasing the aerial drag device, permitting the descent of the aerial payload to a subsea depth, therefore converting the aerial payload to a subsea payload.

17. A pressure activated release system for deployment of payload assembly, comprising:
an aerial deployment subsystem comprising:
an aerial payload release mechanism having an unreleased configuration at pressures below a first specified pres

Assignees

• Spawar Systems Ct Pacific
• Us Navy

Inventors

• Lloyd Jeffrey M
• Wiedemeier Brandon J

Classifications

• B64D17/38 Primary

  Releasable fastening devices between parachute and load or pack · CPC title

• H01H35/26

  Details · CPC title