发明名称 Pusher propeller installation for turboprop engines
摘要 A pusher turboprop engine is provided with an interior exhaust duct structure which directs the hot turbine gases through and out of the engine nacelle and around the rear spinner which surrounds the propeller hub. The spinner supports blade-shaped shields which protect the roots of the propeller blades from the hot exhaust gasses.
申请公布号 US4930725(A) 申请公布日期 1990.06.05
申请号 US19880285822 申请日期 1988.12.16
申请人 ALLIED-SIGNAL INC. 发明人 THOMPSON, CRAIG E.;ROWSE, JACK H.
分类号 B64C11/14;F02C6/20;F02C7/12 主分类号 B64C11/14
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