发明名称 |
SEALING PLUG FOR A ROCKET ENGINE CHAMBER |
摘要 |
PURPOSE: A sealing plug for a combustor of a rocket engine is provided to prevent structural damages to a wall of a combustor caused by the sealing plug because the sealing plug is made of rubber. CONSTITUTION: A sealing plug for a combustor of a rocket engine(200) comprises a rubber tube, a pipe(203), a limiter(211), a first cap, a second cap and a pressure gauge(209). The rubber tube has a gas injection port(202) with a third cap. A check valve with a spring is attached to the pipe. The limiter is connected to the check valve by a supporter. The first and second caps seal the both ends of the pipe. The pressure gauge checks the internal pressure of the tube.
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申请公布号 |
KR20120045736(A) |
申请公布日期 |
2012.05.09 |
申请号 |
KR20100107481 |
申请日期 |
2010.11.01 |
申请人 |
KOREA AEROSPACE RESEARCH INSTITUTE |
发明人 |
KIM, CHEUL WOONG;CHUNG, YONG HYUN;SEOL, WOO SEOK |
分类号 |
F02K9/96;B64G1/40;F02K9/60;F02K9/97 |
主分类号 |
F02K9/96 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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