For now I'm dreaming of a 70% scale carbon fiber CL-84 Dynavert with
  twin quad rotor turbo compounded 26Bs. The best design to date,
  better than the difficult to fly and deadly Osprey. In my opinion
  anyway. http://www.aviastar.org/helicopters_eng/canadair_dynavert.php


  https://youtu.be/iCd2FqTJKs0 <https://youtu.be/iCd2FqTJKs0>https://youtu.be/tzsAuSyEOl0
  https://youtu.be/dKcmjuoPQfs <https://youtu.be/dKcmjuoPQfs>Really cool vtol/stol mix including
  CL-84 and vertical take off design like Paul's.
  https://youtu.be/tzsAuSyEOl0 <https://youtu.be/tzsAuSyEOl0>Best Regards, Kurt Emerson

  I would hardly say the Osprey is difficult to fly or deadly.  It has
  a fly by wire control system which is probably universally now used
  in expensive aircraft. The F16 is inherently unstable with out it.
  One must avoid the ring vortex state but all helicopters have that
  problem more or less.  Yes they had some fatal crashes in the Osprey
  development period when the ring vortex state was not fully
  understood. Now the Marines love them.

  The idea of making an adiabatic internal combustion engine has been
  around for years. Several have been built regardless of the
  difficulty or ease of fabricating the parts. No positive BSFC
  results have been reported so far. BSFC is so critical to the
  function of an internal combustion engine if it had worked the
  ceramic parts would have now  been common.

  Some claims for ceramic coatings on piston tops have been mentioned
  but I don't thing that is common on production pistons either. The
  risk factor is high because  if it comes off the engine is toast.

  AIXRO does not recommend ceramic rotor bearings for that reason. In
  addition there is the initial increased cost of the ceramic bearing
  itself.

  Ceramic turbines in turbo charger have also been successfully tried.
  However they do not dominate turbo charger turbine material. Inconel
  is still preferred.

  As far as turbines in turbo jets or turbo fans I have no idea if
  ceramic version are widely used or not. Cost of course is less of an
  issue.

  Paul Lamar


  Definitely the KOOL factor, but horribly complex mechanically, and
  to operate !

  Steve Carlisle


  Steve are you talking about the CL-84 or the Osprey? The articles on
  the CL-84 say it flew just like a plane. The control box was a piece
  of genius. I'm sure it could be duplicated and mimicked using fly by
  wire.

  Kurt Emerson

  It was a 2 engine copy of the  LTV XC-142
  https://en.wikipedia.org/wiki/LTV_XC-142


  Or the  Vertol VZ-2 (Model 76)

https://commons.wikimedia.org/wiki/File:Vertol_VZ-2_%28Model_76%29_NASA_GPN-2000-001732.jpg

The problem was they had too high of a disk loading for taking off
  vertically with a low payload to power ratio.

  They solved that  problem in the Osprey. The Osprey solved that
  problem with much larger diameter rotors.


  Paul Lamar

  I would think in the early 80,s the CL-84 was mechanical, and the
  newer Osprey, similar bird, would be fly by wire, You say the control
  box was a piece of genius. 2 main wing rotors and a tail rotor to
  make all this act like a helicopter, and a plane. Impressive !

  Steve Carlisle



Paul,
Don't forget the Curtiss X-19.
Dave James


Looks like the uber proposal except they want to lift an additional
1000 pounds of battery :-).

Paul Lamar

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