发明名称 Rocket engine nozzle throat plug engine recovery system
摘要 An expandable throat plug for use in the recovery of a rocket engine nozzle in an engine assembly is disclosed herein having a deployment device carried on the exterior of the engine assembly including an actuator for advancing an extendable column and an arm normal thereto so that the expandable throat plug can be deployed into and inside the nozzle. A telescoping extension shaft deploys the plug interiorly of the nozzle whereby a pressurized medium expands the plug into conformal engagement with the inner surface of the nozzle to seal and close the throat opening.
申请公布号 US5083728(A) 申请公布日期 1992.01.28
申请号 US19900608175 申请日期 1990.10.31
申请人 HECK, GORDON 发明人 HECK, GORDON
分类号 B64G1/62 主分类号 B64G1/62
代理机构 代理人
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