- 专利标题: Method of defining gas turbine engine control ratings
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申请号: US15899486申请日: 2018-02-20
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公开(公告)号: US10808629B2公开(公告)日: 2020-10-20
- 发明人: Stefan M. Poth, Jr.
- 申请人: Raytheon Technologies Corporation
- 申请人地址: US CT Farmington
- 专利权人: Raytheon Technologies Corporation
- 当前专利权人: Raytheon Technologies Corporation
- 当前专利权人地址: US CT Farmington
- 代理机构: Carlson, Gaskey & Olds, P.C.
- 主分类号: F02C9/48
- IPC分类号: F02C9/48 ; F02C9/16 ; F02C9/26 ; G05B19/02 ; G05B17/02 ; F02C9/00 ; G05B15/02
摘要:
A disclosed control system and method of controlling a gas turbine engine utilizes a thrust rating schedule generated from airframe selected requirements. The system utilizes a generic logic structure for ratings combined with simple selection logic to customize rating schedules for multiple airframe customers. The use of a common generic logic structure to generate rating schedules for different airframe manufacturers reduces software design effort, memory consumption, and processor throughput requirements.
公开/授权文献
- US20180238243A1 METHOD OF DEFINING GAS TURBINE ENGINE CONTROL RATINGS 公开/授权日:2018-08-23
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