Invention Grant
US09261022B2 System for controlling a cooling flow from a compressor section of a gas turbine
有权
用于控制来自燃气轮机的压缩机部分的冷却流的系统
- Patent Title: System for controlling a cooling flow from a compressor section of a gas turbine
- Patent Title (中): 用于控制来自燃气轮机的压缩机部分的冷却流的系统
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Application No.: US13708092Application Date: 2012-12-07
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Publication No.: US09261022B2Publication Date: 2016-02-16
- Inventor: Rajarshi Saha , Santhosh Donkada , Indrajit Mazumder , Bhaskar Pemmi
- 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: Dority & Manning, PA
- Main IPC: F02C9/18
- IPC: F02C9/18 ; F02C7/12 ; F01D17/14 ; F01D25/12 ; G05D23/02
Abstract:
A system for controlling a flow rate of a compressed cooling medium between a compressor section and a turbine section of a gas turbine includes a flow path that is defined between the compressor section and the turbine section of the gas turbine and a thermally actuated variable flow valve disposed within the flow path. The variable flow valve defines an opening that changes in size based on a temperature of the compressed cooling medium flowing therethrough.
Public/Granted literature
- US20140157791A1 SYSTEM FOR CONTROLLING A COOLING FLOW FROM A COMPRESSOR SECTION OF A GAS TURBINE Public/Granted day:2014-06-12
Information query
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