A parachute system includes a release that detachably couples a self-propelled projectile and parachute canopy to each other. The release detaches the two from each other in response to a triggering of the release. There is also a first path between the release and a payload where the first path includes the parachute canopy and a suspension line between the parachute canopy and the payload. At least part of the suspension line is bound such that the first path is effectively shorter than a second path. In response to the first path being drawn taut, the suspension line becomes unbound so that the first path becomes effectively longer than the second path. In response to the second path being drawn taut after the suspension line becomes unbound, the release is triggered.
PARACHUTE DEPLOYMENT SYSTEM USING DECOUPLED TOW AND RELEASE LINES
2019-04-18
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Parachute deployment system using decoupled tow and release lines
Europäisches Patentamt | 2018
|Parachute deployment system using decoupled tow and release lines
Europäisches Patentamt | 2018
|Parachute deployment system using decoupled tow and release lines
Europäisches Patentamt | 2019
|