Invention Grant
- Patent Title: Dual drive electro-aero-thermal turbine engine
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Application No.: US16900199Application Date: 2020-06-12
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Publication No.: US11326467B2Publication Date: 2022-05-10
- Inventor: Daniel Bernard Kupratis , Zubair Ahmed Baig , Gary Collopy , Coy Bruce Wood
- Applicant: Raytheon Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: Raytheon Technologies Corporation
- Current Assignee: Raytheon Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: F01D15/10
- IPC: F01D15/10 ; F01D25/24 ; F02C7/32 ; F02C7/36 ; F02K3/06 ; B64D27/02
Abstract:
A turbine engine includes integrated electric machines in the compressor section and the turbine section to supplement power produced from fuel with electric power. The compressor section includes a compressor electric motor that is electrically coupled to a compressor generator. The example turbine section includes a turbine electric motor that is coupled to a geared architecture to supplement power driving the fan section. A turbine generator driven by a portion of the turbine section provides electric power to the turbine electric motor.
Information query
