Invention Grant
- Patent Title: Gas turbine engine failure detection
- Patent Title (中): 燃气轮机发动机故障检测
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Application No.: US12618060Application Date: 2009-11-13
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Publication No.: US08954228B2Publication Date: 2015-02-10
- Inventor: Ronald Alan Falkmann , Michael T. Elliott , Edward A. Lheureau
- Applicant: Ronald Alan Falkmann , Michael T. Elliott , Edward A. Lheureau
- Applicant Address: US IN Indianapolis
- Assignee: Rolls-Royce Corporation
- Current Assignee: Rolls-Royce Corporation
- Current Assignee Address: US IN Indianapolis
- Agency: Krieg DeVault LLP
- Main IPC: G06F7/00
- IPC: G06F7/00 ; G06F19/00 ; F02K9/66 ; F02C9/00

Abstract:
A gas turbine engine control system is disclosed having a fault detection system capable of detecting a high N1 condition. N1 rotational speed is measured and, in two different locations, subtracted from a target N1 value and a requested N1 value. The resultant error values are scaled by a gain that is scheduled as a function of N2 rotational rate. Each error value is accumulated with separate integrators that have independent maximum and minimum limits. The integrators are reset based upon a number of conditions. A number of additional conditions must also be satisfied for the fault detection system to trigger a fault condition. If the additional conditions are satisfied and the integrators are accumulating values, then a fault condition is set if either or both integrators accumulate a value that reaches a selected limit.
Public/Granted literature
- US20100168952A1 GAS TURBINE ENGINE FAILURE DETECTION Public/Granted day:2010-07-01
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