Invention Grant
- Patent Title: Counter swirl doublet combustor
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Application No.: US14137391Application Date: 2013-12-20
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Publication No.: US09765969B2Publication Date: 2017-09-19
- Inventor: Charles B. Graves , Donald M. Wicksall , Thomas F. Richardson, Jr.
- Applicant: Rolls-Royce Corporation
- Applicant Address: US IN Indianapolis
- Assignee: Rolls-Royce Corporation
- Current Assignee: Rolls-Royce Corporation
- Current Assignee Address: US IN Indianapolis
- Agency: Fishman Stewart PLLC
- Main IPC: F23R3/04
- IPC: F23R3/04 ; F23R3/28 ; F23R3/06 ; F02C3/00 ; F23R3/00
Abstract:
An improved combustor for a gas turbine is operable to provide high combustion efficiency in a compact combustion chamber. The combustor includes a counter swirl doublet for improved fuel/air mixing. The enhanced combustor assembly and method of operation improves operation of the turbine.
Public/Granted literature
- US20150040576A1 COUNTER SWIRL DOUBLET COMBUSTOR Public/Granted day:2015-02-12
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