Invention Grant
- Patent Title: Method and apparatus for gas turbine engine temperature management
- Patent Title (中): 燃气轮机发动机温度管理方法和装置
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Application No.: US13951907Application Date: 2013-07-26
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Publication No.: US08714906B2Publication Date: 2014-05-06
- Inventor: Rex Allen Morgan , Michael Alan Davi , Clement Gazzillo , Harold Lamar Jordan
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Cantor Colburn LLP
- Main IPC: F02C7/18
- IPC: F02C7/18

Abstract:
A turbine engine includes a turbine, a compressor for compressing air and a combustor for receiving the compressed air through an inlet passage and operable to burn fuel therewith to deliver hot exhaust gas to the turbine. Also included is a wheel space defined proximate to the combustor. Further included is a cooling air passage extending between the compressor and the wheel space. Yet further included is a valve assembly having a valve member disposed in the cooling air passage and operable to admit a cooling air to the wheel space in response to a condition therein.
Public/Granted literature
- US20130305740A1 METHOD AND APPARATUS FOR GAS TURBINE ENGINE TEMPERATURE MANAGEMENT Public/Granted day:2013-11-21
Information query
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