发明名称 Accessory gearbox device for a jet engine
摘要 The present invention proposes an accessory gearbox for an engine with a drive shaft operatively connectable to a main shaft of the engine, with an extension shaft being provided which can be put into a detachable operative connection to the drive shaft substantially coaxially to said drive shaft of the accessory gearbox At least one auxiliary unit can be detachably arranged on the extension shaft.
申请公布号 US8955403(B2) 申请公布日期 2015.02.17
申请号 US201213593042 申请日期 2012.08.23
申请人 Rolls-Royce Deutschland Ltd & Co KG 发明人 Beier Juergen;Venter Gideon
分类号 F16H37/00;F02C7/32;F16H35/00 主分类号 F16H37/00
代理机构 Shuttleworth & Ingersoll, PLC 代理人 Klima Timothy J.;Shuttleworth & Ingersoll, PLC
主权项 1. An accessory gearbox for an engine including: a drive shaft operatively connectable to a main shaft of the engine, an extension shaft movable between a detachable operative connection to the drive shaft substantially coaxially to said drive shaft and a detached position operatively disconnected from the drive shaft, wherein, in the detached position, at least one auxiliary unit can be detachably arranged for operative connection on the extension shaft; wherein the extension shaft is operatively disconnected from the drive shaft by a translational movement relative to the drive shaft and the at least one auxiliary unit is detached from the extension shaft by a translational movement relative to the extension shaft.
地址 DE