Thread View: sci.aeronautics
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Started by Trevor German
Tue, 15 Dec 1992 14:19
TAIL ROTORS
Author: Trevor German
Date: Tue, 15 Dec 1992 14:19
Date: Tue, 15 Dec 1992 14:19
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I am an engineer and think I understand all the reasons why helos
have tail rotors, however, it seems to me that they may not be
as nessecary as they appear.
I remember seeing a real low speed film of a dragonfly in flight
and watching with fascination how the beast uses a pair or weighted
pendulums behind the wings that swing in anti-phase to the main wings
counteracting the up and down forces on the critters body caused by
the wing beats. Why can't a similar thing be done in helocopters.
The problem, as I understand it, is that the torque of the engine
driving the rotor is balanced by the tail rotor pushing the other
way. By adjusting the pitch of this rotor the balance is modified
to swing the tail in either direction.
My question is why not put the torque adjusting in line with the
main rotor. Granted there are counter-rotating rotor machines but
these are complicated and expensive. Why not have a higher RPM
ducted vertical fan driven through a gearbox on the main shaft
pumping air down under the craft. The design of the fan should be
done in a way that makes it very viscous, that is, a lot of torque
required to move air. The speed of the fan would
obviosly be greater than that of the main rotor. The pitch of the
fan would again be adjustable, or maybe just a damper in the airflow
could suffice.
This may have already been tried, or maybe I am missing something
fundemental, but I am intrested in any comments or knowledge of
similar schemes that have been tried.
--
>| "Only average people | Trevor J German BSc |<
>| never make mistakes." | NCR, Waterloo, Ontario |<
>| tjgerman@53iss6.Waterloo.NCR.COM | Canada. |<
Re: TAIL ROTORS
Author: Teresa Kline
Date: Tue, 15 Dec 1992 18:09
Date: Tue, 15 Dec 1992 18:09
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In article <10299@ncrwat.Waterloo.NCR.COM>, tjgerman@53iss6.Waterloo.NCR.COM (Trevor German) writes... > > Why not have a higher RPM > ducted vertical fan driven through a gearbox on the main shaft > pumping air down under the craft. The design of the fan should be > done in a way that makes it very viscous, that is, a lot of torque > required to move air. The speed of the fan would > obviosly be greater than that of the main rotor. The pitch of the > fan would again be adjustable, or maybe just a damper in the airflow > could suffice. > > This may have already been tried, or maybe I am missing something > fundemental, but I am intrested in any comments or knowledge of > similar schemes that have been tried. > It has been tried. See any AvWeek or similar journal and look for the NOTAR (no tail rotor). -- Teresa Life -- just for the FUN of it!!!!
Re: TAIL ROTORS
Author: Peter Gale
Date: Thu, 17 Dec 1992 04:32
Date: Thu, 17 Dec 1992 04:32
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tjgerman@53iss6.Waterloo.NCR.COM (Trevor German) writes: > I am an engineer and think I understand all the reasons why helos > have tail rotors, however, it seems to me that they may not be > as nessecary as they appear. Try the Sikorsky ABC aircraft, Kaman's, Russian machines, MDHC's MDX Explorer (1st flight this week?)... > these are complicated and expensive. Why not have a higher RPM > ducted vertical fan driven through a gearbox on the main shaft > pumping air down under the craft. The design of the fan should be > done in a way that makes it very viscous, that is, a lot of torque > required to move air. In otherwords a power plant just to generate drag?... > This may have already been tried, or maybe I am missing something Then again maybe just hold the aircraft up with a skyhook. :-) -- Peter Gale | Ph: 61 2 330-1686 | Sydney Senior Systems Programmer | gale@socs.uts.edu.au | Australia School of Computing Sciences | Fax: 61 2 330-1807 | --------- University of Technology, Sydney | --------------------------------
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