A chute-deployment-seat-release system (120) for an ejection seat (106) may be configured to deploy a parachute (112) from the ejection seat (106) and release an occupant restraint (114) of the ejection seat (106). The chute-deployment-seat-release system (120) may comprise an auto-deployment assembly (140), including a first power supply (146), and a manual deployment assembly (150), including a second power supply (158) and a handle (152). The first power supply (146) may be configured to activate in response to expulsion of the ejection seat (106) from an aircraft (102). The second power supply (158) may be configured to activate in response to an actuation of the handle (152).
EMERGENCY MANUAL PARACHUTE OPERATION SYSTEM
MANUELLES FALLSCHIRMBETÄTIGUNGSSYSTEM FÜR DEN NOTFALL
SYSTÈME DE FONCTIONNEMENT DE PARACHUTE MANUEL D'URGENCE
2020-05-06
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
TIBKAT | 1977
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