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Chinook / Osprey hybrid design

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manolis

Well-Known Member
Joined
Jul 2, 2007
Messages
313
Here is the Chinook (Boeing CH-47):

chinook-helicopter.jpg


here is the Osprey (Bell-Boeing V-22):

Ossprey.jpg


and here is a hybrid design, something eliminating some weaknesses / drawbacks of both:

PatOsp_Front.png


PatOsp_Back.png


Instead of supporting “tilting” engines and transmissions at the ends of the wings (as the Osprey does) the engines / transmissions are secured on the fuselage and the only that is tilting is a rotor / propeller at the nose of the airplane and another “pusher” rotor / propeller at the tail of the airplane (counter-rotating at takeoff, and rotating at the same direction at cruising).


The red spheres are CVJ’s (constant velocity joints) characterised by:
100% constant velocity joint,
low friction,
over +/-60 degrees operating angles,
high torque capacity,
heavy axial load capacity,
and vibration-free operation,

say,

as the following PatDan CVJ (stereoscopic animation):

PatDAN_M1.gif


a plastic prototype (3D-printed) of which is shown at operation in the following two youtube videos:

[video=youtube_share;6w9vOgXtngk]https://youtu.be/6w9vOgXtngk[/video]

https://youtu.be/gxAHSrZqABQ

Imagine a small home-built airplane capable for vertical take-off / landing (as a helicopter) and capable for cruising at high speed / high mileage as an airplane.

Thanks
Manolis Pattakos
 
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