发明授权
- 专利标题： Gas turbine engine compressor arrangement
- 专利标题（中）： 燃气涡轮发动机压缩机布置
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申请号： US13340969申请日： 2011-12-30
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公开(公告)号： US08807477B2公开(公告)日： 2014-08-19
- 发明人: Gabriel L. Suciu , Brian D. Merry , Christopher M. Dye , Steven B. Johnson , Frederick M. Schwarz
- 申请人： Gabriel L. Suciu , Brian D. Merry , Christopher M. Dye , Steven B. Johnson , Frederick M. Schwarz
- 申请人地址： US CT Hartford
- 专利权人： United Technologies Corporation
- 当前专利权人： United Technologies Corporation
- 当前专利权人地址： US CT Hartford
- 代理机构： Carlson, Gaskey & Olds, P.C.
- 主分类号： B64D29/00
- IPC分类号： B64D29/00
摘要：
A gas turbine engine includes a fan section and a low spool that includes a low pressure compressor section. The low pressure compressor section includes eight (8) or less stages. A high spool includes a high pressure compressor section that has between eight to fifteen (8-15) stages. An overall compressor pressure ratio is provided by the combination of the low pressure compressor section and the high pressure compressor. A gear train is defined along an engine centerline axis. The low spool is operable to drive the fan section through the gear train.
公开/授权文献
- US20120198816A1 GAS TURBINE ENGINE COMPRESSOR ARRANGEMENT 公开/授权日：2012-08-09
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