发明名称 GAS TURBINE GEARBOX
摘要 A method of manufacturing and/or providing a gearbox for rotating a propeller in a selected single one of a first and second direction is disclosed. The gearbox includes a many common components, selected irrespective of desired propeller direction, and a few unique components selected based on desired propeller direction. In one aspect the method includes casting a casing of the gearbox and machining the casing according to a selected configuration of the gear stages of the gearbox used to achieve direction of the propeller in the selected direction.
申请公布号 US2007049454(A1) 申请公布日期 2007.03.01
申请号 US20060553692 申请日期 2006.10.27
申请人 MITROVIC LAZAR 发明人 MITROVIC LAZAR
分类号 F16H57/08;B64D35/00;B64D41/00;F01D15/12;F02C6/20;F02C7/36;F16H1/06;F16H1/28;F16H57/02 主分类号 F16H57/08
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