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1.
公开(公告)号:US11807381B2
公开(公告)日:2023-11-07
申请号:US17203324
申请日:2021-03-16
Applicant: Krishnamoorthi Sivalingam , Chandana J. Gajanayake , Jeyaraman Kumaravel , Palanisamy Mohan Kumar , Govind Pandey , Yunzhe Zhai , Divya Bharathi Perumal
Inventor: Krishnamoorthi Sivalingam , Chandana J. Gajanayake , Jeyaraman Kumaravel , Palanisamy Mohan Kumar , Govind Pandey , Yunzhe Zhai , Divya Bharathi Perumal
CPC classification number: B64D33/08 , B64D27/02 , B64D27/10 , B64D27/24 , B64D2027/026
Abstract: A hybrid propulsion system for use with an aircraft includes a gas turbine engine, at least one propulsor, and an electric power system. The electric power system is coupled to the gas turbine engine to generate electrical energy and the propulsor to provide electrical energy to drive the propulsor. The electric power system includes a thermal management system configured to cool a heat load generated by the electric power system.
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公开(公告)号:US20220297848A1
公开(公告)日:2022-09-22
申请号:US17203324
申请日:2021-03-16
Applicant: Krishnamoorthi Sivalingam , Chandana J. Gajanayake , Jeyaraman Kumaravel , Palanisamy Mohan Kumar , Govind Pandey , Yunzhe Zhai , Divya Bharathi Perumal
Inventor: Krishnamoorthi Sivalingam , Chandana J. Gajanayake , Jeyaraman Kumaravel , Palanisamy Mohan Kumar , Govind Pandey , Yunzhe Zhai , Divya Bharathi Perumal
Abstract: A hybrid propulsion system for use with an aircraft includes a gas turbine engine, at least one propulsor, and an electric power system. The electric power system is coupled to the gas turbine engine to generate electrical energy and the propulsor to provide electrical energy to drive the propulsor. The electric power system includes a thermal management system configured to cool a heat load generated by the electric power system.
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