Invention Grant
- Patent Title: Turbine engine with a turbo-compressor
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Application No.: US14622523Application Date: 2015-02-13
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Publication No.: US10337401B2Publication Date: 2019-07-02
- Inventor: Daniel B. Kupratis , William G. Sheridan
- 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.
- Main IPC: F02C3/34
- IPC: F02C3/34 ; F01D13/00 ; F02C3/073 ; F02C7/08 ; F02C7/36 ; F02C3/14 ; F02K3/115

Abstract:
A turbine engine is provided that includes a turbo-compressor, a combustor section, a flow path and a recuperator. The turbo-compressor includes a compressor section and a turbine section. The combustor section includes a combustor and a plenum adjacent the combustor. The flow path extends through the compressor section, the combustor section and the turbine section. The recuperator is configured with the flowpath between the combustor section and the turbine section. An inlet duct to the recuperator is fluidly coupled with the flow path upstream of the plenum. An outlet duct from the recuperator is fluidly coupled with the plenum.
Public/Granted literature
- US20160237894A1 TURBINE ENGINE WITH A TURBO-COMPRESSOR Public/Granted day:2016-08-18
Information query
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