发明申请
- 专利标题: GAS TURBINE ENGINE FRONT ARCHITECTURE MODULARITY
- 专利标题(中): 气体涡轮发动机前架构模块化
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申请号: US11860719申请日: 2007-09-25
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公开(公告)号: US20090081039A1公开(公告)日: 2009-03-26
- 发明人: Michael E. McCune , Brian D. Merry , Gabriel L. Suciu
- 申请人: Michael E. McCune , Brian D. Merry , Gabriel L. Suciu
- 主分类号: F01D25/24
- IPC分类号: F01D25/24
摘要:
A gas turbine engine is disclosed that includes a spool having a compressor section. An inlet case is arranged axially upstream from the compressor section. A gearbox is secured to the inlet case. The gearbox couples the spool and a fan. A sealing assembly is arranged between the inlet case and the gearbox to provide a sealed bearing compartment. The inlet case, gearbox and seal assembly provide a module. A fastening element removably secures the module to the spool. The gas turbine engine can be serviced by disconnecting the fastening element from the engine core. The gearbox and inlet case can be removed as a module from the engine core without disassembling the gearbox.
公开/授权文献
- US07955046B2 Gas turbine engine front architecture modularity 公开/授权日:2011-06-07
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