Invention Grant
- Patent Title: Particle extraction system for a gas turbine engine
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Application No.: US15194944Application Date: 2016-06-28
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Publication No.: US10774788B2Publication Date: 2020-09-15
- Inventor: Matthew R. Feulner
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: Raytheon Technologies Corporation
- Current Assignee: Raytheon Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: F02C7/052
- IPC: F02C7/052 ; F02K3/06 ; F02C3/045 ; F02C6/08

Abstract:
A gas turbine engine includes an engine core includes at least one compressor, a combustor downstream of the compressor, and at least one turbine downstream of the combustor. A primary flowpath fluidly connects each of the compressor, the combustor, and the turbine. At least one particle extraction duct has an extraction duct inlet connected to the primary flowpath fore of the compressor and an extraction duct outlet connected to a bypass flowpath.
Public/Granted literature
- US20170370326A1 PARTICLE EXTRACTION SYSTEM FOR A GAS TURBINE ENGINE Public/Granted day:2017-12-28
Information query
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