发明名称 Aircraft with escape system for passengers and crew has upper fuselage that separates from lower fuselage, braking rockets and chute, main chute for soft landing of upper fuselage
摘要 The system has upper fuselage cladding that ejects on detection of a hazard, deployable emergency wings and rear braking parachute and forward pivotable braking rockets; when the speed is reduced a main parachute is deployed, the braking chute is erected, the braking rockets are deployed to the braking position and ignited, then the upper fuselage separates from the lower fuselage and a soft landing of the upper fuselage takes place. The system has a part of the upper fuselage cladding (1) that ejects on detection of a hazard, emergency wings and a rear braking parachute that deploy and forward pivotable braking rockets that are brought into the braking position. When the speed is reduced a main parachute is deployed, the braking chute is erected, the braking rockets are deployed to the braking position and ignited, then the upper fuselage (2) separates from the lower fuselage (3) and a soft landing of the upper fuselage takes place. Independent claims are also included for the following: an escape system for aircraft passengers and crew.
申请公布号 DE10056890(A1) 申请公布日期 2002.05.23
申请号 DE20001056890 申请日期 2000.11.13
申请人 EHRLICH, HORST 发明人 EHRLICH, HORST
分类号 B64C3/56;B64D17/78;B64D17/80;B64D25/00;(IPC1-7):B64D25/12 主分类号 B64C3/56
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