Invention Grant
- Patent Title: Hybrid power system architecture for an aircraft
- Patent Title (中): 飞机混合动力系统架构
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Application No.: US13953164Application Date: 2013-07-29
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Publication No.: US08662445B2Publication Date: 2014-03-04
- Inventor: Louis J. Bruno , Anthony C. Jones , Todd A. Spierling , Gregory L. DeFrancesco
- Applicant: Hamilton Sundstrand Corporation
- Applicant Address: US CT Windsor Locks
- Assignee: Hamilton Sundstrand Corporation
- Current Assignee: Hamilton Sundstrand Corporation
- Current Assignee Address: US CT Windsor Locks
- Agency: Kinney & Lange, P.A.
- Main IPC: B64D13/08
- IPC: B64D13/08 ; B64C13/40 ; B64D41/00
Abstract:
A hybrid power distribution system for an aircraft generates hydraulic power from one of a plurality of power sources based on which power source provides energy most efficiently. Power sources includes an electric power distribution bus that distributes electrical energy onboard the aircraft, a pneumatic distribution channel that distributes pneumatic energy onboard the aircraft, and mechanical power provided by one or more engines associated with the aircraft.
Public/Granted literature
- US20130306790A1 HYBRID POWER SYSTEM ARCHITECTURE FOR AN AIRCRAFT Public/Granted day:2013-11-21
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