Abstract A rotating propeller or fan motor, ducted or un-ducted, with two or more self-contained aerofoils connected with side supports, the aerofoils are placed within the engine slipstream so that lift is achieved as a by-product of the forward thrust, the motor is fixed to the outer side support on a rotating bracket to allow the angle of attack between the propeller slipstream and aerofoils to be adjusted. Figure 2. Side View of Lifting Engine with Self Contained Aerofoils AMI M ts bal4. . - #~nWg P43r A~enrAd iqw r4 M9e *
LIFTING ENGINE WITH SELF CONTAINED AEROFOILS
2017-06-15
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
European Patent Office | 2017
|Engineering Index Backfile | 1934
|Engineering Index Backfile | 1934
|TIBKAT | 1922
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