Invention Grant
- Patent Title: Cooled fuel injector system for a gas turbine engine
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Application No.: US15029503Application Date: 2014-10-31
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Publication No.: US10400672B2Publication Date: 2019-09-03
- Inventor: John D. Frish , Alexander W. Williams , Sean D. Bradshaw
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: O'Shea Getz P.C.
- International Application: PCT/US2014/063419 WO 20141031
- International Announcement: WO2015/112215 WO 20150730
- Main IPC: F23R3/28
- IPC: F23R3/28 ; F02C7/22 ; F02C7/14

Abstract:
A cooling system for a fuel injector system of a gas turbine engine has a heat exchanger for cooling a portion of diffuser case air and then routing the cooled diffuser case air through a sleeve that surrounds a fuel injector conduit located in at least the diffuser case plenum for minimizing fuel heat-up rates in the conduit. By minimizing fuel temperatures within the injector conduit, coking accumulation is thereby eliminated or reduced.
Public/Granted literature
- US20160273453A1 COOLED FUEL INJECTOR SYSTEM FOR A GAS TURBINE ENGINE Public/Granted day:2016-09-22
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