![]() |
If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below. |
|
|
Thread Tools | Display Modes |
#11
|
|||
|
|||
![]()
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
|
|||
|
|||
![]()
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
|
|||
|
|||
![]()
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
|
|||
|
|||
![]()
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
|
|||
|
|||
![]() "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
|
|||
|
|||
![]() "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
|
|||
|
|||
![]() "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
|
|||
|
|||
![]() "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
|
|||
|
|||
![]()
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
|
|||
|
|||
![]()
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) |
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
Cirrus demo | Dan Luke | Piloting | 12 | December 4th 05 05:26 AM |
New G-1000 182 & Cirrus SR-22 GTS | Dan Luke | Piloting | 24 | June 27th 05 07:18 PM |
Parachute fails to save SR-22 | Capt.Doug | Piloting | 72 | February 10th 05 05:14 AM |
Cirrus SR22 Purchase advice needed. | C J Campbell | Piloting | 122 | May 10th 04 11:30 PM |
New Cessna panel | C J Campbell | Owning | 48 | October 24th 03 04:43 PM |