Invention Grant
- Patent Title: Gas turbine engine rotor lock prevention system and method
- Patent Title (中): 燃气轮机发动机转子锁定防止系统及方法
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Application No.: US12105835Application Date: 2008-04-18
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Publication No.: US07902999B2Publication Date: 2011-03-08
- Inventor: Chris D. Eick
- Applicant: Chris D. Eick
- Applicant Address: US NJ Morristown
- Assignee: Honeywell International Inc.
- Current Assignee: Honeywell International Inc.
- Current Assignee Address: US NJ Morristown
- Agency: Ingrassia Fisher & Lorenz, P.C.
- Main IPC: G08B23/00
- IPC: G08B23/00
Abstract:
A system and method of at least reducing the likelihood of a rotor lock in an aircraft gas turbine engine is provided. A determination is made that each propulsion gas turbine engine on an aircraft has experienced a flameout. The rotational speed of each propulsion gas turbine engine is compared to a predetermined threshold rotational speed and, if the rotational speed of each propulsion gas turbine engine is below the predetermined threshold rotational speed, a warning is supplied to a flight crew.
Public/Granted literature
- US20090261989A1 GAS TURBINE ENGINE ROTOR LOCK PREVENTION SYSTEM AND METHOD Public/Granted day:2009-10-22
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