Invention Grant
- Patent Title: System and method for combining compressor bleed flow and ventilation flow of gas turbine engine
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Application No.: US16875989Application Date: 2020-05-16
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Publication No.: US11572829B2Publication Date: 2023-02-07
- Inventor: Ravinder Yerram , Quoc Hoai Nguyen , Mohammad Mahabub , Tho V. Nguyen
- 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: Fletcher Yoder, P.C.
- Main IPC: F02C6/08
- IPC: F02C6/08 ; F02C9/18

Abstract:
A flow combiner is provided for a gas turbine engine. The flow combiner includes an outlet duct, a compressor bleed inlet duct coupled to the outlet duct, and a ventilation inlet duct coupled to the outlet duct. The compressor bleed inlet duct is configured to receive a bleed flow from a compressor of the gas turbine engine. The ventilation inlet duct is configured to receive a ventilation flow from an enclosure surrounding the gas turbine engine. The bleed flow and the ventilation flow are combined as an outlet flow through the outlet duct.
Public/Granted literature
- US20210355868A1 SYSTEM AND METHOD FOR COMBINING COMPRESSOR BLEED FLOW AND VENTILATION FLOW OF GAS TURBINE ENGINE Public/Granted day:2021-11-18
Information query
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