发明名称 REVERSE MECHANISM FOR A JET SYSTEM
摘要 A jet propulsion system includes an inlet receiving a fluid, and a housing defining a discharge nozzle through which fluid is discharged to provide propulsion of a vehicle in a first direction. The jet propulsion system also includes a reverse mechanism movable between a deployed position redirecting fluid from the discharge nozzle toward the first direction and providing propulsion of the vehicle in a second direction substantially opposite the first direction and a non-deployed position allowing fluid to exit the discharge nozzle and provide propulsion of the vehicle in the first direction. The reverse mechanism produces a flow entrainment that enhances forward thrust while the reverse mechanism is in the non-deployed position which results in a net thrust gain over the thrust attributed to the discharge nozzle alone.
申请公布号 US2009203270(A1) 申请公布日期 2009.08.13
申请号 US20090367923 申请日期 2009.02.09
申请人 MARINE 1, LLC 发明人 SNOW SCOTT
分类号 B63H11/11 主分类号 B63H11/11
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