发明授权
- 专利标题： Extendable nozzle for rocket engine
- 专利标题（中）： 火箭发动机可扩展喷嘴
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申请号： US13572809申请日： 2012-08-13
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公开(公告)号： US09200597B1公开(公告)日： 2015-12-01
- 发明人: Alex Pinera
- 申请人： Alex Pinera
- 申请人地址： US FL Jupiter
- 专利权人： Florida Turbine Technologies, Inc.
- 当前专利权人： Florida Turbine Technologies, Inc.
- 当前专利权人地址： US FL Jupiter
- 代理商 John Ryznic
- 主分类号： F02K9/97
- IPC分类号： F02K9/97 ; F02K9/80
摘要：
An extendable nozzle for a rocket engine includes a chamber with a main combustion chamber and a throat and a main nozzle formed within a guide tube, where a nozzle extension slides over the guide tube from a stowed position to an extendable position. A locking O-ring secures the nozzle extension in a stowed position, and a locking split ring holds the nozzle extension in the extended position.
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