Invention Application
- Patent Title: FUEL INJECTOR
- Patent Title (中): 喷油器
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Application No.: US15179495Application Date: 2016-06-10
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Publication No.: US20170009991A1Publication Date: 2017-01-12
- Inventor: Jonathan F. CARROTTE , Stephen C. HARDING , Ashley G. BARKER
- Applicant: ROLLS-ROYCE plc
- Applicant Address: GB London
- Assignee: ROLLS-ROYCE plc
- Current Assignee: ROLLS-ROYCE plc
- Current Assignee Address: GB London
- Priority: GB1512000.9 20150709
- Main IPC: F23R3/20
- IPC: F23R3/20 ; F23R3/34 ; F02C7/22

Abstract:
A fuel injection system for a gas turbine engine (10) comprises; a pilot fuel injector section (22, 23) and a main airblast fuel injector section (25, 26, 27, 28, 29), the main airblast fuel injector section having an aft end (29) facing a combustion chamber (30). A surface of the injection system exposed to air flow through an injection system is non-axisymmetric or non-planar in a reference circumferential plane and/or is configured to generate controlled and varying acoustic impedance at or adjacent the aft end where, in use, the air flow collides with an oncoming acoustic wave.
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