PPRuNe Forums - View Single Post - Why are Helicopters with the Flettner-System so slow?
Old 7th Dec 2006, 00:04
  #30 (permalink)  
Dave_Jackson
 
Join Date: Apr 2003
Location: Vancouver, BC, Canada
Posts: 1,635
Likes: 0
Received 0 Likes on 0 Posts
Opps!
Post #22 on http://www.pprune.org/forums/showthr...=252205&page=2 and most of the following posts on that thread should have been posted on this thread.

________________________________________________________



It was mentioned by IMFU, in a different thread, that Sikorsky's new X2 coaxial ABC will have multiple-speed rotors, as did its predecessor, the XH-59A ABC.

However, the possibility of using single-speed, low-rpm rotors with wide chord blades (large solidity ratio) for tomorrow's high speed rotorcraft appears to have significant advantages.

Two bits of information have come to light while digging deeper into this subject.

1/ A cursory review of the technical papers on the XH-59A ABC show that the 'solidity ratio' is much used in the evaluation of many variables. However, I cannot find any place where the solidity ratio, itself, was evaluated as a variable.

2/ Stepniewski considers the rpm of the rotors as a variable in his conceptual Intermeshing ABC, but it appears that this evaluation was only to pick the optimum single-speed RPM.


Can anyone suggest one or more potentially viable reasons for using multiple-speed main rotors?

__________________

Another bit of uncovered trivia, from the Spring 2001 AHS publication of Vertiflite;
"I [Glidden Doman] committed office and shop space to him [Anton Flettner ".. at a relatively advanced age"] for the construction of a unique intermesher with no hinges. When the project did not go ahead I hired his top engineer and lost contact."

Apparently, Kellett was not the only person at that time to consider an intermeshing configuration with rigid rotors.


Dave

Last edited by Dave_Jackson; 8th Dec 2006 at 20:03. Reason: Opps! added. Then later spelling corrected.
Dave_Jackson is offline