An improved efficiency propeller for aircraft includes a blade structure mounted onto a propeller hub, a servo unit, and a cantilevered base. A distinctive feature of the invention is that the blade structure includes a main mast, which is mounted onto a propeller hub and forms the spine of the leading edge of the blade structure, and at least one secondary mast aligned with the main mast, and turning spacers with struts fitted with a strut are mounted onto the main mast, and the struts are covered by lateral pieces of a skin module, and the overlapping and flexible lateral piece of the skin module form a skin.
HIGH-EFFICIENCY PROPELLER FOR AIRCRAFT
2022-12-22
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
A High Efficiency Fuselage Propeller ("Fusefan") for Subsonic Aircraft
British Library Conference Proceedings | 1999
|A High Efficiency Fuselage Propeller (”Fusefan”) for Subsonic Aircraft
SAE Technical Papers | 1999
|