Invention Grant
US09429072B2 Return fluid air cooler system for turbine cooling with optional power extraction
有权
返回流体空气冷却器系统，用于涡轮冷却，可选择功率提取
- Patent Title: Return fluid air cooler system for turbine cooling with optional power extraction
- Patent Title (中): 返回流体空气冷却器系统，用于涡轮冷却，可选择功率提取
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Application No.: US13900189Application Date: 2013-05-22
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Publication No.: US09429072B2Publication Date: 2016-08-30
- Inventor: Carlos Enrique Diaz , Jorge Alejandro Carretero Benignos
- Applicant: GENERAL ELECTRIC COMPANY
- Applicant Address: US NY Niskayuna
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Niskayuna
- Agent John P. Darling
- Main IPC: B64D15/00
- IPC: B64D15/00 ; F02C7/18 ; F02C7/047
Abstract:
In an aircraft including a gas turbine engine, a system for cooling the gas turbine engine includes a tank provided in a wing of the aircraft, the tank being configured to store a cooling fluid supply; and a heat exchanger provided in the gas turbine engine configured to exchange heat from the compressor discharge air to the cooling fluid.
Public/Granted literature
- US20140345292A1 RETURN FLUID AIR COOLER SYSTEM FOR TURBINE COOLING WITH OPTIONAL POWER EXTRACTION Public/Granted day:2014-11-27
Information query
