发明名称 |
Gearless / oilless gas turbine engine |
摘要 |
The complex mechanical gear trains and lubrication systems of conventional engine configurations are eliminated by using combinations of hydrodynamic air foil bearings, hydrodynamic solid geometry carbon seals/bearings, magnetic bearings, and electrical starter/generators that can also act as bearings to support the high speed shafts of gas turbine engines. The various bearing types and the starter/generators are arranged in such a way as to share peak loads experienced by the engine shaft during maximum aircraft maneuvers. This results in a minimal bearing and engine size.
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申请公布号 |
US2004161333(A1) |
申请公布日期 |
2004.08.19 |
申请号 |
US20030631946 |
申请日期 |
2003.07.30 |
申请人 |
HONEYWELL INTERNATIONAL INC. |
发明人 |
KLAASS REINHARD M.;TAKEUCHI DONALD I.;SCHENK BJOERN |
分类号 |
F01D25/16;F01D25/22;F16C17/10;F16C17/12;F16C27/02;F16C33/16;(IPC1-7):F03D11/00 |
主分类号 |
F01D25/16 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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