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08-02-2016, 10:08 AM
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Join Date: Jan 2005
Location: Tampa, FL
Posts: 2,861
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Quote:
Originally Posted by 1001001
At what altitude does a normally aspirated IO-540 rated at 260 at sea level begin to make only 230 hp?
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Is the diesel turbocharged or normally aspirated--maybe a stupid question but I'm ignorant on diesels? I'm assuming turbo'd which is where it's easy to see, now that you've brought it to my attention, they'd get the performance at altitude to offset the HP reduction. That would be appealing if the cost is not significantly higher than an IO-540. Again I'll reserve judgment until performance figures, reliability figures, installation details, and cost are published.
Of course I'm more concerned about getting off the ground with a fully loaded plane on a hot day than cruise performance at 10K.
__________________
Todd "I drink and know things" Stovall
PP ASEL-IA
RV-10 N728TT - Flying!
WAR EAGLE!
Last edited by Auburntsts : 08-02-2016 at 10:13 AM.
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08-02-2016, 10:12 AM
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Senior Curmudgeon
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Join Date: Sep 2005
Location: Dayton Airpark, NV A34
Posts: 15,408
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Quote:
Originally Posted by Auburntsts
Is the diesel turbocharged ?--
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Yep, the thing hanging below the engine.

__________________
Mike Starkey
VAF 909
Rv-10, N210LM.
Flying as of 12/4/2010
Phase 1 done, 2/4/2011 
Sold after 240+ wonderful hours of flight.
"Flying the airplane is more important than radioing your plight to a person on the ground incapable of understanding or doing anything about it."
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08-02-2016, 10:12 AM
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Join Date: Mar 2005
Location: Calgary, Canada
Posts: 5,744
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Quote:
Originally Posted by 1001001
At what altitude does a normally aspirated IO-540 rated at 260 at sea level begin to make only 230 hp?
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About 4000 feet. I'd also be surprised if you can buy this engine for less than $65K.
Last edited by rv6ejguy : 08-02-2016 at 10:15 AM.
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08-02-2016, 10:14 AM
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Join Date: Jan 2005
Location: Tampa, FL
Posts: 2,861
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Quote:
Originally Posted by Mike S
Yep, the thing hanging below the engine.
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Thanks - I'm at work and the pics are blocked.
__________________
Todd "I drink and know things" Stovall
PP ASEL-IA
RV-10 N728TT - Flying!
WAR EAGLE!
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08-02-2016, 10:53 AM
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Join Date: Jun 2014
Location: Ottawa, ON, Canada
Posts: 353
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__________________
J.F.
Sling 4 empennage kit on order!
Future EAA 245 Member (Hopefully)
Current Piper Warrior PA-28-151 Owner/Pilot
Ottawa, Ontario, Canada
http://www.sling4.ninja
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08-02-2016, 11:02 AM
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Join Date: Sep 2007
Location: Albuquerque, NM
Posts: 659
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Quote:
Originally Posted by Auburntsts
Of course I'm more concerned about getting off the ground with a fully loaded plane on a hot day than cruise performance at 10K.
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Maybe you'd get both with the diesel? Density altitude might put the diesel close to or above the hp of the 540 on the ground. One of my local airports (KMGY, elev 952') is showing a DA of 2905' today, and it's not even really hot yet.
__________________
Andy Compton, PhD EE
RV-10 - #41414 (building)
RV-9A - N643AC (built,flying,sold,missed)
My blood and sweat, the Wifey's tears
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08-02-2016, 11:02 AM
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Join Date: Jun 2014
Location: Ottawa, ON, Canada
Posts: 353
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Quote:
Originally Posted by rv6ejguy
About 4000 feet. I'd also be surprised if you can buy this engine for less than $65K.
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20K more than a Van'S IO-540 new price.
Looking at 100LL.com, there's on average let's say a 80 cents difference in favour of jet-A, per gallon.
Continental claims 10.94 G/Hr on the CD-230, let's use 11.
For an IO-540, let's say 16.
5 * 80 cents = 4$/Hr difference on fuel costs.
5000 hours to break even, based on these very simple calculations ...
So yeah, only truly useful to those without a good 100LL source.
And if someone ends up producing a viable drop in replacement to 100LL, who knows, it could go worldwide ... and kill Diesel in at least some other parts of the world??
Don't see the point at this time ...
__________________
J.F.
Sling 4 empennage kit on order!
Future EAA 245 Member (Hopefully)
Current Piper Warrior PA-28-151 Owner/Pilot
Ottawa, Ontario, Canada
http://www.sling4.ninja
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08-02-2016, 11:11 AM
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Join Date: Jul 2014
Location: Madison, WI
Posts: 683
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Your math is a little off.
CD-230 = 11gph @ $4.19 = $46.09/hr
IO-540 = 16gph @ $5.00 = $80/hr
difference is $33.91/hr
__________________
---
RV-9A - started 01/2015, completed 07/19/2018, 500hrs 03/14/2020
RV-10 - started 04/2020
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08-02-2016, 11:24 AM
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Join Date: Aug 2006
Location: Taylor Texas
Posts: 811
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certification SNAFUs, and more
Well, the diesels are only allowed to fly so high - I think 13000MSL or so? Seems they can't get restarted if someone pulls the power back to where the compression ignition fire goes out. The engine will run up to 18000MSL or so, but I would expect a small throttle reduction - as would be used in any descent - and the fire will go out - until you get to a lower altitude.
So you have to make powered descents? No thanks - I like to keep Mr Vne happy (except at Reno - he has to take what I give him while we are there).
I'm almost sure this basic engine was used by the Flying Frog race team that had a diesel in an NXT. Once they turned the wick up, it really went. So - the HP limit is NOT 230 hp - I would guess closer to 350 (judging from the speed). The plane was totaled in a crash in France later - engine failure, if memory serves...
Carry on!
Mark
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08-02-2016, 12:01 PM
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Join Date: Oct 2005
Location: 08A
Posts: 9,476
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Quote:
Originally Posted by F1Boss
I'm almost sure this basic engine was used by the Flying Frog race team that had a diesel in an NXT. Once they turned the wick up, it really went. So - the HP limit is NOT 230 hp - I would guess closer to 350 (judging from the speed). The plane was totaled in a crash in France later - engine failure, if memory serves...
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That nicely defines the fear I detect when I talk diesel EAB with senior folks at Continental. They figure if left to our own devices, we'll install it wrong and treat it badly, and everyone will start saying their diesels are no good.
__________________
Dan Horton
RV-8 SS
Barrett IO-390
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