Invention Grant
- Patent Title: Gas turbine engine compressor arrangement
- Patent Title (中): 燃气涡轮发动机压缩机布置
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Application No.: US13340940Application Date: 2011-12-30
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Publication No.: US08684303B2Publication Date: 2014-04-01
- 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: B64D29/00
- IPC: B64D29/00
Abstract:
A gas turbine engine includes a spool along an engine centerline axis which drives a gear train, said spool includes a low pressure compressor with four (4) stages.
Public/Granted literature
- US20120121390A1 GAS TURBINE ENGINE COMPRESSOR ARRANGEMENT Public/Granted day:2012-05-17
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