A cross flow fan to be incorporated into an aircraft comprises a cross flow fan rotor to be positioned in an aircraft, a drive arrangement for the cross flow fan rotor, and a plurality of vanes positioned downstream of the cross flow fan rotor. An aircraft is also disclosed.
CROSS FLOW FAN WITH EXIT GUIDE VANES
2017-09-21
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Performance of Advanced Fan Exit Guide Vanes with a Forward Swept Fan
British Library Conference Proceedings | 2003
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