Invention Grant
- Patent Title: Combustor cooling system
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Application No.: US14835775Application Date: 2015-08-26
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Publication No.: US10436114B2Publication Date: 2019-10-08
- Inventor: Bhawan B. Patel , Oleg Morenko
- Applicant: PRATT & WHITNEY CANADA CORP.
- Applicant Address: CA Longueuil, QC
- Assignee: PRATT & WHITNEY CANADA CORP.
- Current Assignee: PRATT & WHITNEY CANADA CORP.
- Current Assignee Address: CA Longueuil, QC
- Agency: Norton Rose Fulbright Canada LLP
- Main IPC: F23R3/60
- IPC: F23R3/60 ; F02C7/18 ; F02C3/14 ; F23R3/00 ; F23R3/50 ; F23R3/04 ; F23R3/06

Abstract:
A gas turbine engine has a combustor supported in a gas generator case. A baffle apparatus is attached to the gas generator case, surrounding an upstream section of the combustor to create at least one passage for directing an air flow discharged from a compressor diffuser to pass therethrough for cooling the combustor. The at least one passage extends from an upstream end of the combustor and has a passage exit immediately upstream of a dilution hole in the combustor. The baffle apparatus is configured to increase a velocity of the air flow entering the at least one passage and passing over the combustor.
Public/Granted literature
- US20170058775A1 COMBUSTOR COOLING SYSTEM Public/Granted day:2017-03-02
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