NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Cooling of Electric Motors Used for Propulsion on SCEPTORBenefits of Electric Power: Reduced energy consumption, Lower emissions, Less noise. Traction motors: Permanent magnet, Synchronous, High torque at low rotational speeds, High power density, (High concentration of heat). Annular inlet: Very compatible with PM motors, (Provides cooling where needed, No need for complicated ducting, Leads to a larger motor diameter which is beneficial for motor torque) Effect of prop wash on heat transfer coefficients: Assumed propeller induced turbulence would increase heat transfer coefficients, Holmes, Obara Yip reported 'propeller slipstream showed little if any apparent effect of the slip stream', Derlaga @ LaRC also found little change in heat transfer in the wake of the propeller.
Document ID
20170001724
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Christie, Robert
(NASA Glenn Research Center Cleveland, OH United States)
Dubois, Authur
(Joby Aviation, Inc. Santa Cruz, CA, United States)
Derlaga, Joseph
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
February 22, 2017
Publication Date
June 13, 2016
Subject Category
Aircraft Design, Testing And Performance
Aircraft Propulsion And Power
Report/Patent Number
GRC-E-DAA-TN32571
Meeting Information
Meeting: AIAA Aviation and Aeronautics Forum and Exposition
Location: Washington, DC
Country: United States
Start Date: June 13, 2016
End Date: June 17, 2016
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 533127.02.15.03.02
CONTRACT_GRANT: NND15SA42C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Aircraft
Power
Propulsion
No Preview Available