发明名称 Arrangement for adjusting the rotor blades of a propfan turboprop engine
摘要 An arrangement for the adjusting of rotor blades of a propfan turboprop engine equipped with two counter-rotating propfan rotors has a number of double-toothed planet wheels which are fastened in a rotatably disposed web. The web is supported on the side of the housing by planet members disposed on one of the propfan rotors. The two toothings of the planet wheels are in operative connection with ball spindle adjusting rings. Using an adjusting motor, a relative movement of the web can be achieved with respect to the housing, whereby the blades of two counter-rotating rotor blade rings can be swivelled. According to the invention, an adjustment of rotor blades will also be possible when no stationary housing parts are available for the support.
申请公布号 US5028207(A) 申请公布日期 1991.07.02
申请号 US19890433543 申请日期 1989.11.08
申请人 MTU MUNCHEN GMBH 发明人 ROHRA, ALOIS;GEIDEL, HELMUT-ARND
分类号 B64C11/32;B64C11/30;F02C3/067 主分类号 B64C11/32
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