Invention Grant
- Patent Title: Recuperator for gas turbine engine
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Application No.: US15843260Application Date: 2017-12-15
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Publication No.: US10830141B2Publication Date: 2020-11-10
- Inventor: William Dwight Gerstler , Daniel Jason Erno , Brian Lewis Devendorf , Kevin Kenneth Pruzinsky
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Armstrong Teasdale LLP
- Main IPC: F02C7/10
- IPC: F02C7/10 ; F02C7/08 ; F02C3/04 ; F28D21/00

Abstract:
A recuperator includes a monolithic heat exchanger core having a first side proximal to a combustor inlet and a turbine outlet, and a second side that includes an exhaust outlet. A compressed air inlet is located on the second side, and a compressed air outlet is located on the first side. The compressed air outlet supplies air to a combustor. A first plurality of passageways connects the compressed air inlet to the compressed air outlet. A turbine exhaust inlet is located on the first side, and a turbine exhaust outlet is located on the second side. A second plurality of passageways connects the turbine exhaust inlet to the turbine exhaust outlet. The first and second plurality of passageways are defined by parting plates that extend radially outward in a spiral pattern that maintains a substantially equal distance between adjacent parting plates.
Public/Granted literature
- US20190186361A1 RECUPERATOR FOR GAS TURBINE ENGINE Public/Granted day:2019-06-20
Information query
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