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new twin concept from Cirrus



 
 
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  #11  
Old May 10th 06, 02:33 AM posted to rec.aviation.piloting
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Default new twin concept from Cirrus

In article .com,
"Kingfish" wrote:

All good points. Probably the best argument against the twin is that
Cirrus' singles are so damn fast already


nah - people seem to wants twins for night over-the-mountains and for hauling
more stuff

--
Bob Noel
Looking for a sig the
lawyers will hate

  #12  
Old May 10th 06, 12:00 PM posted to rec.aviation.piloting
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Default new twin concept from Cirrus

Kingfish,

Ah, a jet and a twin based on the single-engine design - and with
Thielerts. Now where have I heard that idea before? g

Hint: www.diamondaircraft.com

--
Thomas Borchert (EDDH)

  #13  
Old May 10th 06, 12:00 PM posted to rec.aviation.piloting
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Default new twin concept from Cirrus

Kingfish,

I think the next big thing
could be diesels, and a Thielert or SMA might be a nice addition to a
fast airframe.


I may have reported this here already, but I live in Hamburg, Germany,
home of the Thielert group. And at the Hamburg airport, I have seen
what seemed to be a prototype of an SR-22 fitted with the big 350-HP
Thielert. So there's hope, I guess. From what I hear, Cirrus has pretty
much given up on SMA. But I may be wrong...

--
Thomas Borchert (EDDH)

  #14  
Old May 10th 06, 01:57 PM posted to rec.aviation.piloting
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Default new twin concept from Cirrus

Thomas B wrote:

I have seen what seemed to be a prototype of an SR-22 fitted with the big 350-HP Thielert.


I kinda figured that would be the next evolution of that airframe. Did
the cowling look like it was modified?

Now where have I heard that idea before? g


Hint: www.diamondaircraft.com

Reference my second and third posts re the DA-42

  #15  
Old May 10th 06, 02:43 PM posted to rec.aviation.piloting
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Default new twin concept from Cirrus


"john smith" wrote in message
...
I don't see any economic advantage to adding a twin to their product
line. Their singles already offer "twin-like" speeds without the expense
of the second engine and systems. I don't see any evidence that there is
demand for a new piston twin.


The purpose of a twin is load capacity.

The development and certification costs alone would require that the
selling price be in the VLJ range.


And the maintenance $$ on those is a lot higher.


  #16  
Old May 10th 06, 02:44 PM posted to rec.aviation.piloting
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Default new twin concept from Cirrus


"Kingfish" wrote in message
oups.com...
John S. wrote:

I don't see any economic advantage to adding a twin to their product

line. Their singles already offer "twin-like" speeds without the
expense
of the second engine and systems. I don't see any evidence that there
is
demand for a new piston twin.

All good points and tough to argue. It was more of a "what if"
excercise. I'm sure if there was a good business case for a twin
Klapmier would be all over it.


I suspect he's up to his eyeballs already.


  #17  
Old May 10th 06, 02:57 PM posted to rec.aviation.piloting
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Default new twin concept from Cirrus


"Kingfish" wrote in message
oups.com...
All good points. Probably the best argument against the twin is that
Cirrus' singles are so damn fast already. I read recently about a
turbonormalizer STC for the SR22 that boosts the cruise up to 200kts.
Not a cheap mod for an extra 15kt on the top end, but the climb is
probably pretty impressive past 8k feet.


That's the main purpose of turbonormalizing, climb performance; and much
better "high and hot" performance.

There's a significant difference between tubronormalizing and
turbosupercharging and evidently that's what Cirrus is going after.





  #18  
Old May 10th 06, 03:01 PM posted to rec.aviation.piloting
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Default new twin concept from Cirrus


"Mike Schumann" wrote in message
.net...
I would be putting my money on a diesel engine. That would be huge in
Europe. With the price of gas going up in the US, it would be a big hit
here also.

It was my (mis?)understanding that a diesel is, HP/lb, heavier than a
standard aircraft engine, especially when getting into the higher (over 250)
HP models. Correct?
--
Matt
---------------------
Matthew W. Barrow
Site-Fill Homes, LLC.
Montrose, CO


Does it tell you something about our times
when a representative of the Taliban is
welcome on the Yale University campus
but representatives of our own military
forces are not? - Tom Sowell, May 1, 2006


  #19  
Old May 10th 06, 03:16 PM posted to rec.aviation.piloting
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Default new twin concept from Cirrus

Kingfish,

Did
the cowling look like it was modified?


Just a little. Some louver-type ventilation and such. But the engine is
heavier than the TCM.

--
Thomas Borchert (EDDH)

  #20  
Old May 10th 06, 04:11 PM posted to rec.aviation.piloting
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Default new twin concept from Cirrus

Matt,

It was my (mis?)understanding that a diesel is, HP/lb, heavier than a
standard aircraft engine, especially when getting into the higher (over 250)
HP models. Correct?


Not necessarily, but the big Thielert at 350 HP is heavier than an IO-520/550.
60 pounds or so.

--
Thomas Borchert (EDDH)

 




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