发明名称 Deflectable blade assembly for a prop-jet engine and associated method
摘要 A propeller for a prop-jet engine having a propellor blade formed as a hollow shell member whose outer surface has an aerodynamic blade profile, the propellor blade being secured to a rotor via an adjustment pin. The hollow shell member is internally braced partly along its radial length by a flexible spar secured to the pin and made of thermoplastic material. The flexible spar is hollow and receives a metal spar hich is fixed to the pin and is given flexibility in bending by the provision of a slot therein.
申请公布号 US4884948(A) 申请公布日期 1989.12.05
申请号 US19880174781 申请日期 1988.03.29
申请人 MTU MOTOREN-UND TURBINEN UNION MUNCHEN GMBH 发明人 SIKORSKI, SIEGFRIED
分类号 B64C11/20;B64C11/26;F01D5/28;F04D29/36;F04D29/38 主分类号 B64C11/20
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