Hybrid electric
Hybrid electric
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An airplane is provided. The airplane includes a vapor cycle air conditioning system that receives outside air, a bleed system with at least one port, and an electric fan. A source of outside air when the airplane is on ground is forced air from the electric fan. The source of the outside air when the airplane is at cruise is bleed air from the at least one port.
Document information
Title
:
Hybrid electric
Contributors:
BRUNO LOUIS J
(author)
/
ZYWIAK THOMAS M
(author)
/
ANDERSON DAVID W
(author)
/
SPIERLING TODD A
(author)
Publication date
:
2019-05-21
Type of media
:
Patent
Type of material
:
Electronic Resource
Language
:
English
Classification
:
| IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |