Invention Grant
US09133729B1 Flexible support structure for a geared architecture gas turbine engine
有权
适用于齿轮架构燃气涡轮发动机的柔性支撑结构
- Patent Title: Flexible support structure for a geared architecture gas turbine engine
- Patent Title (中): 适用于齿轮架构燃气涡轮发动机的柔性支撑结构
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Application No.: US13623309Application Date: 2012-09-20
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Publication No.: US09133729B1Publication Date: 2015-09-15
- Inventor: Michael E. McCune , Jason Husband
- Applicant: United Technologies Corporation
- Applicant Address: US CT Hartford
- Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Hartford
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: F01D25/16
- IPC: F01D25/16 ; F02C7/20
Abstract:
A gas turbine engine includes a flex mount for a Fan Drive Gear System defined by a lateral and transverse stiffness relatonship.
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