Invention Grant
- Patent Title: Two-stage combustor for gas turbine engine
- Patent Title (中): 燃气轮机二级燃烧器
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Application No.: US13313321Application Date: 2011-12-07
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Publication No.: US09243802B2Publication Date: 2016-01-26
- Inventor: Eduardo Hawie , Nigel Davenport
- Applicant: Eduardo Hawie , Nigel Davenport
- 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: F23R3/06
- IPC: F23R3/06 ; F23R3/16 ; F23R3/44 ; F23R3/26 ; F23R3/34

Abstract:
A combustor for a gas turbine engine comprises an inner annular liner and an outer annular liner. A first and a second combustion stages are defined between the liners, each said combustion stage having a plurality of fuel injection bores distributed in a liner wall defining the respective stage. Valves at the fuel injection bores of one of the combustion stages, the valves each defining an air passage from an exterior to an interior of the combustion stage, the valves each having an actuatable member for adjusting a size of a respective air passage for air staging the combustor.
Public/Granted literature
- US20130145741A1 TWO-STAGE COMBUSTOR FOR GAS TURBINE ENGINE Public/Granted day:2013-06-13
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