Invention Grant
- Patent Title: Gas turbine engine combustor and method of forming same
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Application No.: US14808456Application Date: 2015-07-24
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Publication No.: US10337736B2Publication Date: 2019-07-02
- Inventor: Sri Sreekanth , Douglas Maccaul , Eduardo Hawie , Ion Dinu
- Applicant: Pratt & Whitney Canada Corp.
- Applicant Address: CA Longueuil
- Assignee: PRATT & WHITNEY CANADA CORP.
- Current Assignee: PRATT & WHITNEY CANADA CORP.
- Current Assignee Address: CA Longueuil
- Agency: Norton Rose Fulbright Canada LLP
- Main IPC: F23R3/00
- IPC: F23R3/00 ; F23R3/54 ; F23R3/60 ; F23R3/02 ; F01D9/04 ; F01D9/02

Abstract:
A gas turbine engine combustor is described which includes outer and inner annular combustor liners formed of sheet metal. The exit duct circumscribes an annular combustor exit and defines a combustion gas path. The exit duct includes a large exit duct having an annular forged metal section which is butt welded at an upstream end to the outer combustor liner to form a first annular joint. The annular forged metal section is fixed at a downstream end to an annular sheet metal wall to form a second annular joint. Methods of forming and of repairing a gas turbine engine combustor are also disclosed.
Public/Granted literature
- US20170023249A1 GAS TURBINE ENGINE COMBUSTOR AND METHOD OF FORMING SAME Public/Granted day:2017-01-26
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