Invention Grant
- Patent Title: Aircraft hybrid propulsion system including cold plate for a high density power converter
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Application No.: US17203324Application Date: 2021-03-16
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Publication No.: US11807381B2Publication Date: 2023-11-07
- Inventor: Krishnamoorthi Sivalingam , Chandana J. Gajanayake , Jeyaraman Kumaravel , Palanisamy Mohan Kumar , Govind Pandey , Yunzhe Zhai , Divya Bharathi Perumal
- Applicant: Krishnamoorthi Sivalingam , Chandana J. Gajanayake , Jeyaraman Kumaravel , Palanisamy Mohan Kumar , Govind Pandey , Yunzhe Zhai , Divya Bharathi Perumal
- Applicant Address: SG Seletar
- Assignee: Rolls-Royce Corporation
- Current Assignee: Rolls-Royce Corporation
- Current Assignee Address: US IN Indianapolis
- Agency: Barnes & Thornburg LLP
- Main IPC: B64D33/08
- IPC: B64D33/08 ; B64D27/02 ; B64D27/24 ; B64D27/10
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.
Public/Granted literature
- US20220297848A1 COLD PLATE FOR HIGH DENSITY POWER CONVERTER Public/Granted day:2022-09-22
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