Patent · US Active

Aircraft device deployment system with spring-driven mechanical linkage

US8869671B2 · kind B2 · utility

3Cited by
34References
19Claims
0Family size

Assignee

Inventors

Key dates

Filing dateAug 14, 2012
Grant dateOct 28, 2014
Priority date
Expiry dateSep 21, 2032

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64D1/12
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A deployment system includes a spring-driven linkage for deploying one or more kicker feet, to push a device to be deployed away from the deployment system. The kicker feet may include fore and aft kicker feet that push the deployed device to obtain a desire pitch in the launch, an example being a minimal or substantially zero pitch. The release of the kicker feet may be controlled by a pair of actuator, such as electrical solenoid actuators, both of which must be actuated to deploy the device. An electrical connection may allow positional float to account for tolerances in the positioning of the device relative to the deployment system.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.