发明名称 Method and device for changing a front seal plate in an aircraft engine
摘要 Method for removing a front seal plate from an aircraft engine, the method comprising at least the following steps: a) separating a part engine unit from the aircraft engine, the part engine unit comprising the core engine and the low-pressure turbine of the aircraft engine,b) removing a front seal plate nut from the part engine unit,c) removing the front seal plate from the part engine unit.
申请公布号 US9409266(B2) 申请公布日期 2016.08.09
申请号 US201213982445 申请日期 2012.01.24
申请人 LUFTHANSA TECHNIK AG 发明人 Buldtmann Markus;Hinz Alexander;Roppelt Eugen;Fitter Jens
分类号 B23P19/04;B23P6/00;F01D25/28 主分类号 B23P19/04
代理机构 Saliwanchik, Lloyd & Eisenschenk 代理人 Saliwanchik, Lloyd & Eisenschenk
主权项 1. A method for removing a front seal plate from an aircraft engine, comprising at least the following steps: a) separating a part engine unit from an aircraft engine, wherein the aircraft engine comprises: an N1 shaft;an N2 shaft,wherein the N1 shaft is surrounded coaxially by the N2 shaft;a front seal plate nut;a front seal plate; andan engine shroud,wherein the N2 shaft is mounted in the engine shroud via a bearing unit,wherein the part engine unit comprises: a core engine; anda low-pressure turbine of the aircraft engine,wherein the N1 shaft, the N2 shaft, the front seal plate nut, and the front seal plate remain in the part engine unit while the part engine unit is separated from the aircraft engine; b) removing the front seal plate nut from the part engine unit, wherein the N1 shaft and the N2 shaft remain in the part engine unit while the front seal plate nut is removed; and c) removing the front seal plate from the part engine unit, wherein the N1 shaft and the N2 shaft remain in the part engine unit while the front seal plate is removed.
地址 Hamburg DE