Invention Grant
- Patent Title: Axial compressor with inter-stage centrifugal compressor
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Application No.: US15851285Application Date: 2017-12-21
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Publication No.: US10415465B2Publication Date: 2019-09-17
- Inventor: Matthew E Bintz , Enzo DiBenedetto
- 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: Snell & Wilmer, L.L.P.
- Main IPC: F02C3/08
- IPC: F02C3/08 ; F02C7/28 ; F02C9/18
Abstract:
An auxiliary compressor for a gas turbine engine is disclosed. The auxiliary compressor includes a first axial rotor, a second axial rotor positioned downstream of the first axial rotor, and a centrifugal impeller positioned intermediate the first axial rotor and the second axial rotor and operably coupled to the first axial rotor.
Public/Granted literature
- US20190195127A1 AXIAL COMPRESSOR WITH INTER-STAGE CENTRIFUGAL COMPRESSOR Public/Granted day:2019-06-27
Information query
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