Payload activation device

Patent metadata

Field	Value
Publication number	US-11565812-B2
Application number	US-201917049377-A
Country	US
Kind code	B2
Filing date	May 1, 2019
Priority date	May 17, 2018
Publication date	Jan 31, 2023
Grant date	Jan 31, 2023

Abstract

When the tension across the cord's 24 length reaches a predetermined threshold, an activation mechanism within the payload 16 and coupled to one of the cord's 24 ends is actuated in order to activate the payload 16 . Activating the payload 16 may include deactivating a SAFU, activating a motor 32 disposed within the housing, or causing flight controls to extend from a housed position. Here, “within the payload 16 ” may mean part of the activation mechanism is disposed on the outer surface or housing of the payload 16.

First claim

The invention claimed is:

1. A deployable payload for an aircraft, the deployable payload comprising:
a payload activation device comprising:
a housing;
a cord disposed within the housing and arranged to be coupled, at a first end, to an activation mechanism within a payload; and
a retardation device coupled to a second end of the cord,
wherein, in a first configuration, the retardation device is retained within or adjacent to the housing, and, in a second configuration, the retardation device is released from the housing to tauten the cord, and
wherein, at a first predetermined tension, the cord is configured to actuate the activation mechanism,

wherein the deployable payload comprises the activation mechanism for activating the payload, the activation mechanism being releasably coupled to the first end of the cord,
wherein, when released, the retardation device is arranged to tauten the cord to actuate the activation mechanism when the cord is at the first predetermined tension between the first end and second end, and
wherein the cord is configured to separate from the activation mechanism when the cord is at a second predetermined tension between the first end and second end, the second tension being greater than the first tension.

2. The deployable payload according to claim 1 , wherein the cord is configured to break when the cord is at the second predetermined tension between the first end and second end, the second tension being greater than the first tension.

3. The deployable payload according to claim 1 , wherein the payload activation device is coupled to the outside of the payload.

4. The deployable payload according to claim 1 , further comprising an engine, wherein the activation mechanism is arranged to activate the engine when actuated.

5. The deployable payload according to claim 1 , further comprising a safety, arming and fusing unit for preventing a warhead from being armed, wherein the activation mechanism is arranged to deactivate the safety, arming and fusing unit when actuated.

6. The deployable payload according to claim 1 , wherein the deployable payload is an air-launched weapon.

Assignees

• Bae Systems Plc

Inventors

• Mcarthur Gordon John Victor

Classifications

• B64D1/06 Primary

  Bomb releasing; Bomb doors · CPC title

• F42B10/56

  of parachute {or paraglider} type · CPC title

• F42C13/006

  for non-guided, spinning, braked or gravity-driven weapons, e.g. parachute-braked sub-munitions · CPC title

• B64D1/12 Primary

  Releasing · CPC title

• B64D17/38

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