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.
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
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