Invention Application
- Patent Title: TURBINE ENGINE ASSEMBLY AND METHOD OF OPERATING THEREOF
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Application No.: US14879470Application Date: 2015-10-09
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Publication No.: US20170101933A1Publication Date: 2017-04-13
- Inventor: Debabrata Mukhopadhyay , Pugalenthi Nandagopal , James Adaickalasamy
- Applicant: General Electric Company
- Main IPC: F02C7/18
- IPC: F02C7/18 ; F01K23/10 ; F02C3/04

Abstract:
A turbine engine assembly is provided. The assembly includes a compressor, and an air duct coupled in flow communication with the compressor. The air duct is configured to channel a flow of bleed air from the compressor therethrough. The assembly also includes a fluid supply system coupled in flow communication with the air duct, wherein the fluid supply system is configured to channel a flow of fluid towards the air duct to modify a temperature of the bleed air based on an operating condition of the turbine engine assembly.
Public/Granted literature
- US10119471B2 Turbine engine assembly and method of operating thereof Public/Granted day:2018-11-06
Information query
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