首页> 外国专利> 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

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

机译:带有乘客和机组人员逃生系统的飞机具有与下机身分离的上机身,制动火箭和溜槽,主溜槽用于上机身的软着陆

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.
机译:该系统具有上机身包层,可在检测到危险时弹出,可展开应急机翼,后制动降落伞和可向前旋转的制动火箭;当速度降低时,将部署主降落伞,竖起制动斜槽,将制动火箭部署到制动位置并点火,然后上部机身与下部机身分离,并发生上部机身的软着陆。该系统具有一部分上部机身包层(1),该部分在检测到危险时弹出,并带有应急机翼和后部降落伞,后降落伞部署并向前移动可旋转的制动火箭,将其置于制动位置。当速度降低时,将部署主降落伞,竖起制动斜槽,将制动火箭部署到制动位置并点火,然后上部机身(2)与下部机身(3)分离,并软着陆。上机身发生。独立索赔还包括以下内容:飞机乘客和机组人员的逃生系统。

著录项

  • 公开/公告号DE10056890A1

    专利类型

  • 公开/公告日2002-05-23

    原文格式PDF

  • 申请/专利权人 EHRLICH HORST;

    申请/专利号DE2000156890

  • 发明设计人 EHRLICH HORST;

    申请日2000-11-13

  • 分类号B64D25/12;

  • 国家 DE

  • 入库时间 2022-08-22 00:27:21

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