Invention Grant
- Patent Title: Method of defining gas turbine engine control ratings
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Application No.: US14430589Application Date: 2013-03-15
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Publication No.: US09909510B2Publication Date: 2018-03-06
- Inventor: Stefan M. Poth, Jr.
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: Carlson, Gaskey & Olds, P.C.
- International Application: PCT/US2013/032047 WO 20130315
- International Announcement: WO2014/055124 WO 20140410
- Main IPC: F02C9/48
- IPC: F02C9/48 ; G05B19/02 ; G05B17/02 ; F02C9/16 ; G05B15/02 ; F02C9/00 ; F02C9/26 ; G06Q10/06 ; G06Q10/00

Abstract:
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.
Public/Granted literature
- US20150275767A1 METHOD OF DEFINING GAS TURBINE ENGINE CONTROL RATINGS Public/Granted day:2015-10-01
Information query
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