Invention Grant
- Patent Title: Engine mount system for a turbofan gas turbine engine
- Patent Title (中): 用于涡轮风扇燃气涡轮发动机的发动机支架系统
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Application No.: US13336140Application Date: 2011-12-23
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Publication No.: US08267349B2Publication Date: 2012-09-18
- Inventor: Gabriel L. Suciu , Brian D. Merry , Christopher M. Dye , Steven B. Johnson
- Applicant: Gabriel L. Suciu , Brian D. Merry , Christopher M. Dye , Steven B. Johnson
- 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: B64D27/00
- IPC: B64D27/00
Abstract:
A gas turbine engine according to an exemplary aspect of the present invention includes a gear train defined along an engine centerline axis, and a spool along the engine centerline axis which drives the gear train, the spool includes a low stage count low pressure turbine.
Public/Granted literature
- US20120099963A1 ENGINE MOUNT SYSTEM FOR A TURBOFAN GAS TURBINE ENGINE Public/Granted day:2012-04-26
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