Invention Grant
- Patent Title: Combustion engine including turbomachine
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Application No.: US17362124Application Date: 2021-06-29
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Publication No.: US11619177B2Publication Date: 2023-04-04
- Inventor: Kevin P. Hallisey , Dominique Patrick Sautron
- Applicant: GE Aviation Systems LLC
- Applicant Address: US MI Grand Rapids
- Assignee: GE Aviation Systems LLC
- Current Assignee: GE Aviation Systems LLC
- Current Assignee Address: US MI Grand Rapids
- Agency: McGarry Bair PC
- Main IPC: F02C9/18
- IPC: F02C9/18 ; B64D27/10 ; B64D29/00 ; F04D27/02 ; B64D13/06

Abstract:
A combustion engine including at least one combustion chamber, a first bleed air supply fluidly coupled to a portion of the combustion engine upstream the combustion chamber, a second bleed air supply fluidly coupled to a portion of the combustion engine downstream the combustion chamber, a first thermal bus, and a turbomachine including a compressor, a rotary pump, and a first turbine, with the compressor and rotary pump in serial flow arrangement and the rotary pump being fluidly coupled to the first thermal bus.
Public/Granted literature
- US20220145809A1 COMBUSTION ENGINE INCLUDING TURBOMACHINE Public/Granted day:2022-05-12
Information query
IPC分类: