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Old 1st March 2008 | 02:16
  #27 (permalink)  
Dave_Jackson
 
Joined: Apr 2003
Posts: 1,635
Likes: 1
From: Vancouver, BC, Canada
Mart,
The concept definitely has pros and cons, but so far - so good.

Some quick replies.
the machine magically appears from hover to cruise state.
Yes, transition is currently the primary concern. Here are Seven preliminary ideas for effecting the transition.

I still think that if you want the best transition performance you need a low front rotor and high rear rotor, to avoid interference effects. .... Even so, the penalty of carrying those wings around in hover will be high.
The V-22 looses 10% of its thrust in hover due to its downwash on the wings (Leishman and one other). This 2x4 PropRotor only places a downwash on the wings during transition and the downwash will not be normal to the flat-plate surface of the wings.

Keeping the rotor/prop hubs at the same position in space will also simplify the drive-train.
The drive-train consists of four independant PropRotor+Motor, with a liberal sprinkling of electronic SAS.


Theoretically the 2x4 Effective Aerodynamic Disk Area should give a better hover AND a faster cruise than the current V-22.

A testimonial; "This is actually a very good idea. It is one of the most cleaver solutions I have seen yet. You have actually had me looking at your idea for about 20 minutes now." ~ Dennis Fetters.

Mart, Any ideas for a good transition mechanism?

Dave
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