发明名称 SYSTEME DE COMMANDE DE L'HELICE D'UN TURBOPROPULSEUR
摘要 <p>The blades are lockable in reduced pitch, with hydraulic channels as well as mechanical connections linking engine and airscrew. The constant-speed controller has three multi-way valves, each communicating with one of the linking channels. The first provides pitch-increase high-pressure fluid, the second connects the airscrew to a drain in the 'blades locked' setting, the third provides pitch-reduction fluid. A servo-valve (24) is hydraulically linked (23) with the first multi-way valve (21) and a reverse-thrust meter (94). The second valve (36) is connected with the second multi-way valve (34) and the torque meter (82), the third valve (75) with the first (24) and the thrust meter (94).</p>
申请公布号 FR2498253(A1) 申请公布日期 1982.07.23
申请号 FR19810000872 申请日期 1981.01.19
申请人 ALEXEEV IVAN 发明人
分类号 B64C11/38;(IPC1-7):02C7/36;05B11/60;64C11/40 主分类号 B64C11/38
代理机构 代理人
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