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MarkWDavis
Joined: 03 Jan 2007 Posts: 104 Location: Syracuse, KS
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Posted: Wed Nov 28, 2007 3:35 am Post subject: Throttle setting at higher cruising altitudes |
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I recall reading that the carburetor on the M-14P is altitude compensating, but has an auto-rich feature when opened to full throttle. If that's true, how far back does the throttle need to be pulled to get it out of the auto-rich mode and start leaning itself? I was bucking a 50 knot headwind yesterday and needed to reduce the time my beak was pointed into it so I ran at 70% and the throttle just backed off of the forward stop to where it started to reduce manifold pressure a couple of tenths. Once again a GPS sure beats a stopwatch and a sectional to avoid sweating fuel so much.
Mark Davis
N44YK
[quote][b]
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mark.bitterlich(at)navy.m Guest
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Posted: Wed Nov 28, 2007 1:11 pm Post subject: Throttle setting at higher cruising altitudes |
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The answer to that question that I got from Vladimir Yastremski is to
simply pull the throttle back to the point where you sign even the
slightest reduction in manifold pressure and then to leave it right
there.
I've tried it. It works.
Mark Bitterlich
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Mozam
Joined: 24 Nov 2006 Posts: 85
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Posted: Thu Nov 29, 2007 6:39 am Post subject: Re: Throttle setting at higher cruising altitudes |
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I have a Fuel Scan unit in my TW that has proved to be very accurate.
During high altitude cruise (say above 6,000'), I cannot detect any evidence of this full throttle enrichment.
For example, at 9,500' with the prop at 65%, I can place the throttle at the forward stop, note the fuel flow, then retard the throttle until the manifold pressure drops several inches (this is a couple inches of throttle movement), and I see very little change in fuel flow.
It appears to me that if there is any full throttle fuel enrichment, it is "disengaged" at "higher" altitudes.
Also, FWIW, I have found that RPM has a much greater effect on fuel flow than manifold pressure (throttle position). In other words, pulling the prop back from 70% to 65% reduces the fuel flow more than leaving the prop at 70% and reducing the manifold pressure three or four inches.
So at high altitude with a nice tailwind I pull the prop back to 60% and put the throttle at the forward stop. This results in a fuel flow of about 12.8 gal/hr.
Just my opinion (based on my Fuel Scan observations), I think the most fuel efficient M-14 throttle setting for cruise is to set the throttle at the boost limit for any given RPM setting.
Note: Your mileage may vary, past returns are no guarantee of future returns, some assembly required, batteries not included, etc.
Cheers,
Steve Dalton
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napeone
Joined: 10 Jan 2006 Posts: 36 Location: Birmingham, Al.
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Posted: Thu Nov 29, 2007 2:23 pm Post subject: Re: Throttle setting at higher cruising altitudes |
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Concur with Mozam.
David H.
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MarkWDavis
Joined: 03 Jan 2007 Posts: 104 Location: Syracuse, KS
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Posted: Thu Nov 29, 2007 2:25 pm Post subject: Throttle setting at higher cruising altitudes |
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Steve and Mark,
Thanks for the replies. I have noticed it appears to be a bit leaner
when running at 65% vs. 70%. So, I've been running at 70% into headwinds
and 65% with tailwinds.
Mark Davis
N44YK
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mark.bitterlich(at)navy.m Guest
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Posted: Thu Nov 29, 2007 2:47 pm Post subject: Throttle setting at higher cruising altitudes |
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I did not have the instrumentation that Steve has when I came to the
belief that I stated, and I tend to defer to his testing. However, this
directly contradicts what Vladimir told me and I also trust HIS judgment
beyond others as well!
Makes me wonder if it might not be worthwhile to run the test again at
altitude but with higher RPM settings. I wonder if Steve's test would
duplicate at 10,000 feet and say 85% on the RPM? I would really like to
know the answer to this for sure in case I have somehow managed to
delude myself!
Steve did say: "I think the most fuel efficient M-14 throttle setting
for cruise is to set the throttle at the boost limit for any given RPM
setting.
To the best of my knowledge Steve, there are no "boost limits" to this
engine at ANY RPM.
Mark Bitterlich
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MarkWDavis
Joined: 03 Jan 2007 Posts: 104 Location: Syracuse, KS
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Posted: Thu Nov 29, 2007 3:23 pm Post subject: Throttle setting at higher cruising altitudes |
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I think I'll just stick with backing the throttle off of the stop just
a tad. It doesn't appear to make a noticeable difference in power output
and it might also save a little wear and tear on the engine. Besides, it's
still just natural for me to back it off a bit after 1,700 hours of making
heat with J-52's that we could run all day at MIL minus 3%. I'll be in
black figures all of my life with my taxes after all the JP-4 and JP-5 I
got paid to burn!
Mark Davis
N44YK
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wlannon(at)persona.ca Guest
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Posted: Thu Nov 29, 2007 3:24 pm Post subject: Throttle setting at higher cruising altitudes |
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Mark Bitterlich wrote;
Quote: | To the best of my knowledge Steve, there are no "boost limits" to this
engine at ANY RPM.
Mark Bitterlich
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Mark;
There are varying RPM/manifold pressure limits for every engine with a
variable pitch propellor.
Probably the easiest (but not recommended) way to find the first one is to
attempt a take-off with the prop control at low RPM.
Walt
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mark.bitterlich(at)navy.m Guest
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Posted: Thu Nov 29, 2007 3:51 pm Post subject: Throttle setting at higher cruising altitudes |
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Really. Well Walt, I am not so sure you are right about that, but I am
always ready to stand corrected and learn something that I did not know
before.
My M-14 Manual says that you can operate this engine at full throttle
with the engine reduced to the very minimum RPM setting available at ANY
altitude. And ... I've read every available operating manual on this
engine that I can find.
So what is the limit you are speaking of with the M-14P ???
Mark
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brian-1927(at)lloyd.com Guest
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Posted: Thu Nov 29, 2007 4:12 pm Post subject: Throttle setting at higher cruising altitudes |
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On Nov 29, 2007, at 6:39 AM, Mozam wrote:
Quote: | So at high altitude with a nice tailwind I pull the prop back to
60% and put the throttle at the forward stop. This results in a
fuel flow of about 12.8 gal/hr.
Just my opinion (based on my Fuel Scan observations), I think the
most fuel efficient M-14 throttle setting for cruise is to set the
throttle at the boost limit for any given RPM setting.
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That is true for most recip engines, i.e. run maximum MAP to minimize
pumping losses and modulate RPM to control power output.
Brian Lloyd 3191 Western Drive
brianl AT lloyd DOT com Cameron Park, CA 95682
+1.916.367.2131 (voice) +1.270.912.0788 (fax)
PGP key ID: 12095C52A32A1B6C
PGP key fingerprint: 3B1D BA11 4913 3254 B6E0 CC09 1209 5C52 A32A 1B6C
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Mozam
Joined: 24 Nov 2006 Posts: 85
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Posted: Thu Nov 29, 2007 4:27 pm Post subject: Re: Throttle setting at higher cruising altitudes |
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mark.bitterlich(at)navy.m wrote: | .
To the best of my knowledge Steve, there are no "boost limits" to this
engine at ANY RPM.
Mark Bitterlich
-- |
Hi Mark,
I agree, I have never seen any either.
Perhaps not the best choice of words on my part. What I was trying to say was to use the max manifold pressure that the manual lists for a given power setting. For example, the manual lists "Cruise 1" power as 64% RPM and 735 mmHg (29"). I *think* that using less than 735 mmHg in this case reduces engine efficiency.
But, I do not know if using more throttle would be an actual "over-boost" situation.
Cheers,
Steve
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Mozam
Joined: 24 Nov 2006 Posts: 85
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Posted: Thu Nov 29, 2007 4:33 pm Post subject: Re: Throttle setting at higher cruising altitudes |
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mark.bitterlich(at)navy.m wrote: | I did not have the instrumentation that Steve has when I came to the
belief that I stated, and I tend to defer to his testing. However, this
directly contradicts what Vladimir told me and I also trust HIS judgment
beyond others as well!
Makes me wonder if it might not be worthwhile to run the test again at
altitude but with higher RPM settings. I wonder if Steve's test would
duplicate at 10,000 feet and say 85% on the RPM? I would really like to
know the answer to this for sure in case I have somehow managed to
delude myself!
-- |
Mark,
I agree, Vladimir (and others) have a wealth of knowledge about these engines.
I have only looked (and not found) this "max throttle enrichment" at high altitude. Perhaps the carb only operates this feature at lower altitudes?
I will experiment further and report my findings. Any excuse to go fly is a good one!!
Cheers,
Steve
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mark.bitterlich(at)navy.m Guest
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Posted: Thu Nov 29, 2007 4:47 pm Post subject: Throttle setting at higher cruising altitudes |
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Thanks Steve, I'll sure be interested in your results.
Mark
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brian-1927(at)lloyd.com Guest
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Posted: Thu Nov 29, 2007 4:48 pm Post subject: Throttle setting at higher cruising altitudes |
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On Nov 29, 2007, at 3:49 PM, Bitterlich, Mark G CIV Det Cherry Point,
MALS-14 64E wrote:
Quote: |
Point, MALS-14 64E" <mark.bitterlich(at)navy.mil>
Really. Well Walt, I am not so sure you are right about that, but
I am
always ready to stand corrected and learn something that I did not
know
before.
My M-14 Manual says that you can operate this engine at full throttle
with the engine reduced to the very minimum RPM setting available
at ANY
altitude. And ... I've read every available operating manual on this
engine that I can find.
So what is the limit you are speaking of with the M-14P ???
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I don't think there is one for the M14P or the Huosai. There are RPM
limits but not MAP limits (that one can reach).
But in general, peak cylinder pressures are a function of MAP. At
really low RPMs you can complete combustion at an earlier crank angle
before the combustion chamber volume has changed as much so you can
get higher peak cylinder pressures at high MAP and low RPM. This
translates into higher main bearing pressure due to combustion.
(OTOH, higher RPMs result in higher main bearing pressure due to
accelerating the moving mass.) So I can imagine an engine having a
max MAP spec for a lower RPM. I recall that this is the case for most
of the big radial engines. I suspect Pappy can name these limits for
the 1820 for us.
Regardless, you aren't going to hurt your M14P or Huosai engine by
leaving the throttle all the way forward and changing power by
changing RPM. The only question is whether or not there is an
enrichment circuit in the carb at full throttle. I think that having
a fuel-flow gauge and having it NOT show a noticeable reduction in
fuel flow when the throttle is pulled back a skosh puts this one to
bed also.
Brian Lloyd 3191 Western Drive
brianl AT lloyd DOT com Cameron Park, CA 95682
+1.916.367.2131 (voice) +1.270.912.0788 (fax)
PGP key ID: 12095C52A32A1B6C
PGP key fingerprint: 3B1D BA11 4913 3254 B6E0 CC09 1209 5C52 A32A 1B6C
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mark.bitterlich(at)navy.m Guest
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Posted: Thu Nov 29, 2007 5:03 pm Post subject: Throttle setting at higher cruising altitudes |
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This is not a reply to your posting Brian, but just a reply in general.
In my earlier post, I did not mean to imply that manifold / RPM
relationships were unrestricted on EVERY airplane, just that such
restrictions did not always exist for any engine with a variable pitch
prop as Walt was mentioning. I distinctly remember reading that you can
be at full power on the M-14P, and I mean WFO, and pull the prop back to
ANY RPM setting while leaving the throttle wide open. This surprised me
enough that I questioned it and had it verified by a number of both
written and verbal (all Russian) sources. But if anyone has any written
source that specifies differently, I would be happy to be proven wrong.
This is to me not a matter of who is right and who is wrong, but WHAT is
right and WHAT is wrong.
Mark
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wlannon(at)persona.ca Guest
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Posted: Thu Nov 29, 2007 5:33 pm Post subject: Throttle setting at higher cruising altitudes |
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Hi Mark;
I don't have the M14P manual to refer to but Steve has just posted the
Cruise 1 setting of 64% and 735 mm/hg. This is a recommended limit.
Granted that as altitude increases the throttle must be opened to maintain
the desired MP. Since these engines have a low blower ratio compared to an
"altitude" engine the full throttle altitude will be reached very quickly.
In fact it is actually sea level but only with the power settings given in
the manual.
I absolutely agree with Steve's first post to use max. manifold pressure for
a given RPM. He has revised it a bit to a given power setting rather than
RPM but I think he means the same. The "power setting" is a combination of
RPM and MP.
I'm sure you would agree that at sea level a power setting of full throttle
and 1450 (50%)RPM could be fairly described as over boosted.
Cheers;
Walt
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N13472(at)aol.com Guest
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Posted: Thu Nov 29, 2007 6:58 pm Post subject: Throttle setting at higher cruising altitudes |
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In a message dated 11/29/2007 5:34:25 P.M. Pacific Standard Time, wlannon(at)persona.ca writes:
Quote: | absolutely agree with Steve's first post to use max. manifold pressure for
a given RPM. He has revised it a bit to a given power setting rather than
RPM but I think he means the same. The "power setting" is a combination of
RPM and MP.
I'm sure you would agree that at sea level a power setting of full throttle
and 1450 (50%)RPM could be fairly described as over boosted.
Cheers;
Walt
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Walt, does not the Cj-6A manual say that Max power is 2350 rpm M/P ambient + 85 mm ?
Tom Elliott
CJ-6 NX63727
Sandy Valley NV
3L2
702-723-1223
Check out AOL Money & Finance's list of the hottest products and top money wasters of 2007.
[quote][b]
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wlannon(at)persona.ca Guest
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Posted: Thu Nov 29, 2007 7:18 pm Post subject: Throttle setting at higher cruising altitudes |
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Hi Tom;
Yep. But referring on this thread to the M14P. Trust all is well with you.
Best:
Walt
[quote] ---
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viperdoc(at)mindspring.co Guest
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Posted: Thu Nov 29, 2007 7:38 pm Post subject: Throttle setting at higher cruising altitudes |
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Huh?
Doc
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MarkWDavis
Joined: 03 Jan 2007 Posts: 104 Location: Syracuse, KS
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Posted: Thu Nov 29, 2007 7:55 pm Post subject: Throttle setting at higher cruising altitudes |
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Doc,
I use 65% to take the free ride of the tailwind. 70% to reduce the time
the headwind has to work on me. Navy technique we used. In significant
headwinds we always ran at near military power settings. Max endurance AOA
with a strong tailwind when trying to stretch range.
Mark Davis
N44YK
---
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