I have a 21 lb cap on
my system for this very purpose. I don’t presently have a coolant recovery
tank and if the cap burps, I could lose coolant overboard. I am rethinking
this and plan to install a coolant recovery tank as
well.
By the way, on the high
coolant pressure, in surfing the web I have found that this problem is most
likely caused by combustion gasses getting into the coolant. That would
mean a busted o-ring. I have been in denial that this is the cause because
I don’t want to tear the engine down. Today I plan to see if I can find
any coolant coming out of a sparkplug hole. Fingers are
crossed!
Bill
B
From:
Rotary motors in aircraft
[mailto:flyrotary@lancaironline.net] On
Behalf Of Ed Anderson
Sent: Friday, March 25, 2011 8:27
AM
To: Rotary motors in aircraft
Subject: [FlyRotary] Radiator Caps
[FlyRotary] Re: On the subject of installations...Coolant
Pressure
One thing to keep in mind about the
pressure rating of the radiator cap you are using. All are rated relative
to a standard sea level ambinent pressure. This means that he air pressure
itself is contributing 14.7 psi at sea level.
So at sea level when your
differential pressure coolant gauge is reading 10 psi - the absolute pressure in
your coolant system is then 14.7 + 10 = 24.7 psi. Now if you are
flying at 8000 MSL your ambient pressure is approx 1/2 at sea level. So
your 14.7 psi CAP now has the lesser capacity of 7.3 + 10 = 17.3 psi absolute
pressure capacity - somewhat less than the 24.7 psi absolute it had at sea
level.
When you increase in altitude this
component naturally decreases. So while a 14.7 psi CAP may work fine at
sea level, more than one person found that at altitude that rating
was insufficient and some coolant was
lost.
I personally would not fly with less
than a 21 psi cap and currently fly with a 24 psi radiator
cap.
There is another factor that
occurred to me. Once a hot coolant system blows the relief valve on
the cap, that lowers the pressure inside the system, superheated (>212F)
coolant can quickly flash to steam and further cause lost of coolant. So a
Higher PSI cap can lessen the chance of that happening.
Sent: Thursday,
March 24, 2011 5:30 PM
Subject:
[FlyRotary] Re: On the subject of installations...Coolant
Pressure
Lynn,
You have hit my
quandary squarely on the head. Assuming that the pressure was zero at room
temp and rose to say 6-7 pounds at 200 degrees, and assume that the flow
restriction in the system caused a pressure rise of about 2 pounds at 2000 rpm
and a pressure rise of, say, 6-7 pounds at 6000 rpm. Under that scenario,
you would have a pressure that ran at between 7-9 pounds at 2000 and rose to
12-14 pounds at 6000. Those pressures would be easily contained with the
stock cap of 14 pounds. And the pressure would be constantly changing with
rpm and possibly temp of the system as you were under power or
not.
I have a 21 pound
cap. My system climbs smartly to the top and stays there. No
fluctuation with rpm, no real fluctuation at temp because it has already hit the
21 pounds before the engine is actually hot. (around
190)
Something is wrong and
I don’t understand what it is.
Bobby
I am going to insert
answers to your questions in your msg below.
Bill
B
From:
Rotary motors in aircraft
[mailto:flyrotary@lancaironline.net] On
Behalf Of Bobby J.
Hughes
Sent:
Thursday, March 24, 2011 1:57 PM
To: Rotary motors
in aircraft
Subject: [FlyRotary] Re: On the subject of
installations...Coolant Pressure
Bill,
This is all I can think
of at the moment.
Are you running a
thermostat or did you plug the hole between the inlets and outlets of the water
pump?
No thermostat. The
Renesis has a thermostat tower which is too tall to fit under my cowl, so I
removed it and fabricated a flat plate with two 1.25 aluminum tubes for the
inlet and outlet of the water pump. That hole you are referencing exists
in the tower, but not in my plate.
If plugged did you
drill a small hole in the plug to allow air a place to escape? I used a #30
drill.
Any air in my system
would have to be carried to the highest point, (radiator cap) then be forced by
pressure to the bottom of the swirl tank where it would be trapped. This
seems to be working because I have found that after I open the system for some
reason, the level in the swirl tank will go down and there is never any air at
the top of the radiator.
After an engine run is
the radiator the same temperature at the inlet / outlet / bottom and top? If I
have trapped air only part of my radiator gets hot to the touch. Dual pass
barrier leaking?
Seems to be. I
have mistakenly laid my arm on the top of the radiator after a run…usually I
manage to get off pretty fast! :>) I can not see into the
radiator tank on the barrier side. It is possible it could be
leaking. I suppose if there was a rag in the thing it could be trapped
here also. I have no way to see in there even if the hose was
removed. I would need some kind of flexible camera or something like
that.
Use an extra CHT
channel and clamp it to the inlet of your radiator to measure Delta
T.
Good idea. I will
have to rig one up. I don’t have an extra
now.
My water pressure does
not vary that much in operation. But it does hold a little pressure for a few
days after shutdown. 1-2 psi.
What is your pressure
during operation? What is the pressure cap rating? Does it vary at
all with temp and/or rpm? Mine is maxed
out..always!
What size hoses? I’m
running 1in.
The RX-8 uses 1.25
hoses. I stuck with that size as well.
Where are you measuring
water pressure?
The hose that comes off
the top of the rear iron goes to the top of the radiator, just below the cap. A
tee in this line has the water pressure sender in it. The radiator cap is
just a cap, not a pressure cap. The outlet in the radiator neck goes to
the bottom of the swirl tank.
Is your pressure cap on
the bleed / swirl tank?
Yes.
Any pictures of the
plumbing?
Not of the current
setup.
Bobby
From:
Rotary motors in aircraft
[mailto:flyrotary@lancaironline.net] On
Behalf Of Bill Bradburry
Sent: Thursday, March 24, 2011 10:23
AM
To: Rotary motors in aircraft
Subject: [FlyRotary] On the subject of
installations...Coolant Pressure
I need some help with
figuring out my cooling problems.
Just so it doesn’t get
lost in the following BS, I need to state that I think the problem is related to
the coolant pressure. It seems to me to be way too high. I am
beginning to think that the coolant is somehow partially
blocked.
Now the rest of the
story….
After I did the flight
described in the attached email, I installed an opening in the bottom of the
cowl that would work something like a cowl flap that is permanently open.
The new opening is 9 inches by 5 inches or 54 sq in.. There is a flare in
front of the opening that is at an angle of 45 degrees and extends down into the
airstream about 4 inches. (it is 6 inches long.) This opening is in
addition to two 6 X 6 openings, one of which has a 3 inch diameter exhaust pipe
in it.
This helped a little,
but nothing like I expected it would. The pressure inside the radiator
inlet dropped from 10 inches of water to 8 inches of water. (by the way,
Steve was right about it being inches of water and not inches of
Hg.)
The pressure after the
radiator and inside the cowl dropped to 8 inches as well. The temperature
of the water dropped to 208 and the oil a couple of degrees. Neither of
these had the result that I expected.
My water pressure cap
is rated at 21 lbs. I have not calibrated the sender that came with my
EM-2 and it shows 3 lbs when the engine is cold. I assume that this is
zero. When in flight the pressure climbs to 24 lbs and stays there.
I assume that at this point, the cap is at 21 lbs and is bleeding off air.
There is about a pint to a quart of air above the coolant in the bleed
tank.
This morning I ran the
engine on the ground for about 10-15 minutes at an rpm of 3000 to 3200.
The OAT was 75 degrees.
I read the temps and
pressures every minute or two during the run. I hope this doesn’t get
jumbled during transmission.
Oil temp –
80
103
130
139
144
155
162
165
Air temp after cooler -
97
109
122
129
133
134
Water temp
-
86 126
161
173
178
190
198
199
Air temp after rad
-
109
133
157
169
179
183
Water pressure
-
2
11
17
20
21
24
I noticed that the
water pressure could be brought from 2 lbs to 9 lbs by changing the rpm while
the engine was still relatively cool
What should I expect
for water pressure at lower temps and how could I go about making a
determination that the water passages are clear?
I am beginning to think
that a rag has been left either in the engine or the radiator. I have
never torn the engine down and I sent the radiator out to have a leak repair a
couple of years ago. It is a double pass radiator. I can look into
the end that has both sides connected thru the radiator cap neck, but not into
the inlet and outlet end.
Suggestions???
Thanks,
Bill
B
From: Bill
Bradburry [mailto:bbradburry@bellsouth.net]
Sent: Sunday, March 20, 2011 5:29
PM
To: 'Rotary motors in
aircraft'
Subject: On the subject of
installations...
My water temp has been
running between 199 and 217, depending on the OAT. The oil is pretty
steady at around 175. Today I finally got to fly with pressure probes
inside the cowling. I was all set to try and enlarge the inlet to the
radiator to solve the problem. It turns out that “in” is not the problem,
it is “out” that is the problem!
I have 10 inches of Hg
pressure in the radiator inlet and 10 inches of Hg on the outlet side as well as
the same pressure everywhere I measured inside the cowl. I need to open up
the cowl some so more air can get out. I had considered a cowl flap but
that would not work in this instance because the problem is at cruise. I
need a permanent opening. I am considering louvers and I am looking for a
source. I know some of you are using them. Where did you get them
and how are they installed so that they look ok?
I am also considering
some kind of flare around the exit area to create a low pressure area to help
suck air out. Do any of you have those and do they seem to
work?
While I look into this,
I also need to do something about my muffler…Thank you,
Bobby!
I wonder about that
spiral muffler some of you are trying??
Bill B 9 hours
and counting…
By the way, I was
considering putting a 1 or 2 inch wide piece of cardboard across the bottom of
the oil cooler to partially block it in the hopes that more air would then flow
through the radiator. Sort of like truckers do with the radiator in cold
weather. What opinions do you have about that idea? I realize it
would make more sense if the oil was really cool, but I think the oil might not
get much hotter if an inch or so was blocked. What do you
think???