Invention Grant
- Patent Title: Recuperated bypass turbine engine
- Patent Title (中): 回流旁路涡轮发动机
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Application No.: US12189908Application Date: 2008-08-12
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Publication No.: US08387357B2Publication Date: 2013-03-05
- Inventor: Gordon F Jewess , Charles Travelbee
- Applicant: Gordon F Jewess , Charles Travelbee
- Applicant Address: US CT East Hartford
- Assignee: Pratt & Whitney
- Current Assignee: Pratt & Whitney
- Current Assignee Address: US CT East Hartford
- Agent Stephen G. Mican
- Main IPC: F02C7/10
- IPC: F02C7/10 ; F02K3/02

Abstract:
A by-pass turbofan gas turbine engine, has a by-pass fan, a generally annular core engine duct, a generally annular by-pass duct situated in a generally coaxial relationship with the core engine duct coupled to the by-pass fan, an upstream axial compressor coupled to the core engine duct, a downstream radial compressor coupled to the upstream compressor, a generally annular recuperator with a cool side inlet coupled to the downstream compressor, a generally annular combustor coupled to a cool side outlet of the recuperator, a radial turbine coupled to the combustor and a warm side inlet of the recuperator coupled to the radial turbine, at least one exhaust nozzle coupled to a warm side outlet of the recuperator that discharges into the by-pass duct and a propelling nozzle coupled to the by-pass duct.
Public/Granted literature
- US20100037623A1 High Efficiency Turbine Engine Public/Granted day:2010-02-18
Information query
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