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James plenum question

 
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Lenny Iszak



Joined: 23 Mar 2008
Posts: 270

PostPosted: Sun Sep 27, 2009 5:14 pm    Post subject: James plenum question Reply with quote

Those of you who installed the James plenum (Deems, Robin?), how did you get air to the left side heat muff?

Thanks,
Lenny


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recapen(at)earthlink.net
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PostPosted: Sun Sep 27, 2009 5:59 pm    Post subject: James plenum question Reply with quote

Here's how I did the ones on my 6A.....

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robin1(at)mrmoisture.com
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PostPosted: Sun Sep 27, 2009 6:46 pm    Post subject: James plenum question Reply with quote

Lenny,
  Because of high temp issues early on we upgraded and relocated the oil cooler to accept RAM air from the front of the cowl. We sealed the rear hole leaving all the cowl/plenum air for cooling the cylinders. While I hope temps will not be an issue with your build I suspect you will experience similar thermal challenges. Assuming I were using the James Cowl/Plenum again (highly doubtful) I would consider side louvers as the under cowl louvers were beneficial but still not sufficient to keep temps in an acceptable range. I have even toyed with the idea of converting the Plenum back to standard baffles but there are too many unknowns to go that route at this point in time.
  I hate to sound like an RV-List whiner dealing with the Garmin issues and the James Cowl/Plenum cooling but these are real life challenges and I sure hate to have people see my beautiful front end and think it's all rainbows and unicorns. That being said I did display the -10 at SBP Airport Day last Saturday sitting across from a fleet of Cirrus and a bunch of other experimental & certified aircraft and we can be pretty proud of the decision we made to build these airplanes. Once you have a flying -10 there are some planes you no longer have the need to envy.

Robin

Note: Ram Oil Cooler inlet just below Pilots Side Inlet
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Lenny Iszak



Joined: 23 Mar 2008
Posts: 270

PostPosted: Mon Sep 28, 2009 6:04 am    Post subject: Re: James plenum question Reply with quote

Robin,

Thanks for you input. That's a brave idea to cut into the lower cowling and move the oil cooler. How did it work out? By the way, do you have some before and after numbers for oil temps?

I have the stock engine, so I hope I'm not going to have too high temps but everyone reassures me that I will so life is good, i'm assured to have a "hot" airplane Smile

Were your CHTs ok? Did closing off the oil cooler hole in the back help your CHTs at all?

Lenny


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robin1(at)mrmoisture.com
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PostPosted: Mon Sep 28, 2009 8:52 am    Post subject: James plenum question Reply with quote

Lenny,
I no longer have any specific numbers but here is a thumbnail of
our development.
First we worked closely with Airflow Performance who loaned us a
Manometer to test differential pressure (DP) in many different areas on
our set up. We probably relocated and tested DP's in 20+ different
areas. It was immediately obvious that the DP over the oil cooler was
very poor. And in the case of the oil cooler wedge the DP was small and
not evenly distributed meaning that the upper portion of the cooler was
receiving most of the minimal airflow while the lower 1/3 had almost no
airflow so 1/3rd of the cooler was just along for the ride. In rough
numbers we were getting DP's of between 0.7 to 1.5 "W/C. We tried a
bunch of different configurations with the oil cooler temperately
supported in different areas. We also tested DP from the top of the
engine to the bottom and near the outlet area. The DP was just not that
significant in our set up to drive the air through the cylinders and out
the bottom of the cowl. If our thinking was correct and we were not
seeing a large DP over the cylinders than most likely much of the
cooling air was reversing out the inlet holes causing two issues,
minimal cooling and disturbed aerodynamic as the airflow is pouring out
the front of the cowl instead of down & out the underside.. Once we knew
that we first worked on opening up the bottom of the cowl by trimming
back & adding first one set of AFP louvers then a second set of louvers.
This helped substantially but still not enough to drive out CHTs' under
400.
After exhausting all other likely options we decided that the
CHT/EGT issue was one in the same and that we were not going to get the
CHT's lower till we got the oil temps inline. We seem to always have
CHT's two times Oil Temps (215/430, 212/425...). We decided that
pulling hot air off the engine and running it through the largest oil
cooler AFP makes was not enough so we chose to seal up the back end of
the plenum providing more cooling air to the cylinders and cutting a RAM
air inlet for a high volume of cooler air direct to the oil cooler. The
DP results were immediate. We went from 0.7-1.2 "W/C (depending on the
phase of flight) to 7.0-9.0 "W/C. That is a HUGE change over the cooler.
This made the plane flyable and brought our oil temps to about 220-230
in climb and 210 in cruise. CHT's were now 410-420 in cruise. Please
keep in mind this was a brand new engine that tends to run hot for up to
150 hours. I am now at 85 hours and am seeing further settling down of
both CHT's & oil tempts. Again the oil temps are coming down slightly
because the CHT's are a bit lower. Unfortunately they are both still
higher than I would like and probably higher than optimal.
So the major improvements came when we opened up the bottom of
the cowl and when we plumbed RAM air to the oil cooler. Still none of
these numbers are great or even good in my opinion but I can now fly the
plane consistently with numbers that are not detrimental to the engine.
My plan is to get past 150 hours TT and see where the engine settles in
temp wise. Additionally I am working on optimizing for LOP which should
really help the temps all the way around.
I have to say I am a bit surprised that most standard build
-10's still using the wedge and original oil cooler do not have greater
temp problems. I do live in CA with high OAT's but still our numbers are
still too high to be acceptable.
The one option we did not try was to place a louver on the side
of the lower cowl and orient the back side of the oil cooler towards
that louver. Some have added these side louvers (one or both sides) with
some success (I believe). We did not want to ruin the appearance of the
nose area but in retrospect anything that improves functions is probably
better looking than Yellow or Red warning indications on your PFD.
To those that are to follow us down the path of alternate
cowl/plenum I can only say good luck. This mod has cost us significantly
more time & money to develop than we ever thought it could. Add the
potential costs of an engine not going to TBO and the stock Vans cowl is
looking better & better all the time. That Van is a smart guy. Finally
the hassle of having to remove the plenum every time you want to take a
look at something quadruples (or worse) the amount of time it takes to
remove the lid. I can take my top cowl off in 90 seconds. The plenum is
another story even with our simple attachment mechanism It's 5-7 minutes
off and 10 minutes on plus wear & tear.
I have to say that so many of my original ideas in aviation were
wrong. I always thought I wanted retract aircraft till I owned several
of them. I then discovered the retracts can be a pain in the rear by
adding complexity, weight & maintenance costs, plus increase insurance
rates. I hope to never own a retract again (Pilatus excluded). Same goes
for the beauty of the round inlet cowls that have ZERO engineering
behind them. Don't fool yourself, these cowls are originally crafted for
looks. No one did 3D modeling, computer simulations, critical airflow
analysis, probably not even a slide rule or an abacus to generate this
design. Just another pretty face. And hot too! But the wrong type of hot
unfortunately. Throw in the pressure issues trying to run LOP vs. the
standard cowl and you may have more R&D than you were planning to
perform once you plane is past Phase 1.

Again off to the airport for my regular commute.

Robin
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Deems Davis



Joined: 09 Jan 2006
Posts: 925

PostPosted: Mon Sep 28, 2009 12:06 pm    Post subject: James plenum question Reply with quote

Here's a link to some pictures that might help.

http://deemsrv10.com/album/Sec%20FF6%20Exhaust%20System/index.html

However, it should be noted that I have since removed the heat muff on
the left side, in a semi-successful attempt to clean-up the airflow in
this area and to improve cooling.
(Cabin heat is NOT an issue for me currently)

Deems Davis
N519PJ

Lenny Iszak wrote:
Quote:


Those of you who installed the James plenum (Deems, Robin?), how did you get air to the left side heat muff?

Thanks,
Lenny


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Lenny Iszak



Joined: 23 Mar 2008
Posts: 270

PostPosted: Mon Sep 28, 2009 3:05 pm    Post subject: Re: James plenum question Reply with quote

Thanks Deems! That's what I was looking for. Where did you get that Y splitter from?

Lenny


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Deems Davis



Joined: 09 Jan 2006
Posts: 925

PostPosted: Mon Sep 28, 2009 3:48 pm    Post subject: James plenum question Reply with quote

I believe I got it from Aircraft Spruce.
http://www.aircraftspruce.com/menus/ep/engineaccessories_connectors.html

Deems

Lenny Iszak wrote:
Quote:


Thanks Deems! That's what I was looking for. Where did you get that Y splitter from?

Lenny


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http://forums.matronics.com/viewtopic.php?p 65415#265415




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Lenny Iszak



Joined: 23 Mar 2008
Posts: 270

PostPosted: Mon Sep 28, 2009 4:01 pm    Post subject: Re: James plenum question Reply with quote

Duh... should have checked first. Thanks!

Lenny
Deems Davis wrote:
I believe I got it from Aircraft Spruce.
http://www.aircraftspruce.com/menus/ep/engineaccessories_connectors.html

Deems

Lenny Iszak wrote:
Quote:


Thanks Deems! That's what I was looking for. Where did you get that Y splitter from?

Lenny


Read this topic online here:

http://forums.matronics.com/viewtopic.php?p 65415#265415





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rene(at)felker.com
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PostPosted: Mon Sep 28, 2009 4:13 pm    Post subject: James plenum question Reply with quote

Vans sells the y also.

Rene' Felker
RV-10 N423CF Flying
801-721-6080
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