X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from fed1rmfepo203.cox.net ([68.230.241.148] verified) by logan.com (CommuniGate Pro SMTP 5.4c2) with ESMTP id 4923558 for flyrotary@lancaironline.net; Sat, 26 Mar 2011 17:54:53 -0400 Received-SPF: none receiver=logan.com; client-ip=68.230.241.148; envelope-from=alventures@cox.net Received: from fed1rmimpo03.cox.net ([70.169.32.75]) by fed1rmfepo203.cox.net (InterMail vM.8.01.04.00 201-2260-137-20101110) with ESMTP id <20110326215416.ETIQ22406.fed1rmfepo203.cox.net@fed1rmimpo03.cox.net> for ; Sat, 26 Mar 2011 17:54:16 -0400 Received: from BigAl ([72.199.216.14]) by fed1rmimpo03.cox.net with bizsmtp id Pxu41g00B0KDB3c04xu4zU; Sat, 26 Mar 2011 17:54:05 -0400 X-VR-Score: 0.00 X-Authority-Analysis: v=1.1 cv=+7g07FftAVK5SzfBDSzY8IJIWiAWL38p2qa3Op/8zMo= c=1 sm=1 a=AApptJGG4TQA:10 a=TPvrVRyicAsl4VeEYn0L5g==:17 a=Ia-xEzejAAAA:8 a=N8B9JuSIAAAA:8 a=ayC55rCoAAAA:8 a=pedpZTtsAAAA:8 a=1nqpRpBh6yjSK8PcCUoA:9 a=YBpVooeyrPFmLFpUaiMA:7 a=iPjx2AU707tqyiGyakai4t__ijwA:4 a=CjuIK1q_8ugA:10 a=EzXvWhQp4_cA:10 a=eJojReuL3h0A:10 a=Wq7D8N-LPGxjwL32:21 a=BQM1Ju_2HHCLj_Cy:21 a=GAYLhCBiSt5kMUfFjAUA:9 a=nY64uV6sGpEipw2spEYA:7 a=KGP7ZFS-j8AxPE4CsAoY_brWJioA:4 a=wq8xTB2XoNAsO-wX:21 a=_lWJ4btIt3tCdAmq:21 a=OWgrx0ofoTpa1dWfHZEA:9 a=ESLshFLKNiAM0oTE0t9TZj1otf0A:4 a=KQqxNPgzF0kA:10 a=Lf7gr0n1KRO0Ajke:18 a=TPvrVRyicAsl4VeEYn0L5g==:117 X-CM-Score: 0.00 Authentication-Results: cox.net; none From: "Al Gietzen" To: "Rotary motors in aircraft" Subject: FW: [FlyRotary] Re: Radiator Caps [FlyRotary] Re: On the subject of installations...Coolant Pressure Date: Sat, 26 Mar 2011 14:54:10 -0800 Message-ID: MIME-Version: 1.0 Content-Type: multipart/mixed; boundary="----=_NextPart_000_0000_01CBEBC5.AA5653A0" X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook, Build 10.0.6863 Importance: Normal Thread-Index: AcvrHcfe6VkWkOmTRKyoqDSg+xPYWgA4ZYPgAAJEyiA= X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.5994 This is a multi-part message in MIME format. ------=_NextPart_000_0000_01CBEBC5.AA5653A0 Content-Type: multipart/alternative; boundary="----=_NextPart_001_0001_01CBEBC5.AA5653A0" ------=_NextPart_001_0001_01CBEBC5.AA5653A0 Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: quoted-printable =20 Bill; =20 Some comments on your coolant pressure issue, pressure caps, etc. Are = you sure you have a problem? Calibration of the pressure readout would be a = good idea. As your engine heats up the coolant will expand, and the pressure will rise until it reaches rated cap pressure. The pressure will not = reduce again until the temperature is decreased; so you shouldn't be alarmed if = the pressure stays high during a constant power run. If you have no air to compress the pressure will reach cap pressure in a minute. It will also drop rapidly with a reduction in temperature. If there is air in your = filler bottle, or whatever, the pressure will rise, or decrease more slowly. =20 On the question of safe pressure, I have frequently pressure tested my system to 40 psi. I have a double cap setup shown in the photo. The = filler neck cap has no air space (after initial fill and bleed). The pressure = in the system rises rapidly to cap pressure. Coolant in released to the = bottom of the neighboring overflow bottle which also has a pressure cap, and = has a volume of air. I have a float switch near the bottom of the overflow = bottle that would alert me if the level got too low. =20 When the engine is at its max temp, the system pressure can reach 37 psi = (16 plus 21), and basically all of the air has been expelled. As the engine cools down, the coolant in the system contracts, the pressure drops, = and coolant is forced back into the filler neck. The idea is to always have positive pressure in the system to reduce the possibility of pump cavitation, increase the boiling point, and to maintain system pressure = at altitude. Typical cruise temps are 20 - 30F less than max power climb, = and the pressure is 6 - 10 psi.=20 =20 The filler neck is connected on the inlet side of the pump - that's = where you want the pressure at high rpm. A double cap system is not required, = and possibly has limited advantage in that we would seldom run at high power until things have heated, and pressurized anyway. =20 It has worked well for me for over 200 hours. I've not had any coolant = loss. I haven't needed to add any coolant except when I drained to take = something apart, or at each annual when I drain, and replace about half the = coolant. I use about 30% EG in distilled water. =20 =20 Al G =20 =20 =20 =20 -----Original Message----- From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Bill Bradburry Sent: Friday, March 25, 2011 10:52 AM To: Rotary motors in aircraft Subject: [FlyRotary] Re: Radiator Caps [FlyRotary] Re: On the subject of installations...Coolant Pressure =20 Dave, =20 What does your water pressure run in normal operation? =20 Bill B =20 _____ =20 From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of David Leonard Sent: Friday, March 25, 2011 1:32 PM To: Rotary motors in aircraft Subject: [FlyRotary] Re: Radiator Caps [FlyRotary] Re: On the subject of installations...Coolant Pressure =20 I wonder how much pressure it would really take to blow out the seals on = the pump. My primary cap is 20# and the cap on the seconday tank is 12#. = So my Max pressure is 32# relative to ambient. I only keep a small amount of coolant in that tank. The air spring takes up all the expansion on most flights so I usually don't reach full pressure. But a few times I have overheated the system (Al can attest) and blown out coolant without any apparent damage to the water pump. =20 --=20 David Leonard Turbo Rotary RV-6 N4VY http://N4VY.RotaryRoster.net http://RotaryRoster.net On Fri, Mar 25, 2011 at 6:10 AM, Ed Anderson wrote: In reading back over my message, I realized that I could mislead some = into thinking that the higher cap radiator capacity - but, there is a limit. = At some point, if the cap did not release pressure, the coolant pressure = could get high enough to start forcing coolant past seals such as the water = pump shaft seal. So don't over do it. =20 =20 Unless you are going to be flying higher than 18,000MSL, 24 psi is = probably the highest capacity perhaps even 21 psi. You may get away with a 14.7 = psi cap provided the absolute coolant pressure does not rise above the = absolute cap pressure at any given altitude. Cooler ambient air at altitude and = less power could permit a 14.7 psi cap to work, but I personally would = hesitate to use less than a 21 psi cap. =20 Ed =20 =20 =20 From: Ed Anderson =20 Sent: Friday, March 25, 2011 8:27 AM To: Rotary motors in aircraft=20 Subject: [FlyRotary] Radiator Caps [FlyRotary] Re: On the subject of installations...Coolant Pressure =20 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. =20 =20 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 = =3D 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 =3D 17.3 psi absolute pressure capacity - somewhat less than the 24.7 = psi absolute it had at sea level. =20 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. =20 I personally would not fly with less than a 21 psi cap and currently fly with a 24 psi radiator cap. =20 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. =20 =20 FWIW =20 Ed =20 From: Bill Bradburry =20 Sent: Thursday, March 24, 2011 5:30 PM To: Rotary motors in aircraft =20 Subject: [FlyRotary] Re: On the subject of installations...Coolant = Pressure =20 Lynn, =20 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. =20 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) =20 Something is wrong and I don't understand what it is. =20 Bobby =20 I am going to insert answers to your questions in your msg below. =20 Bill B =20 _____ =20 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 =20 Bill, =20 This is all I can think of at the moment.=20 =20 Are you running a thermostat or did you plug the hole between the inlets = and outlets of the water pump?=20 =20 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. =20 If plugged did you drill a small hole in the plug to allow air a place = to escape? I used a #30 drill.=20 =20 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. =20 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? =20 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. =20 Use an extra CHT channel and clamp it to the inlet of your radiator to measure Delta T. =20 Good idea. I will have to rig one up. I don't have an extra now. =20 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.=20 =20 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! =20 What size hoses? I'm running 1in.=20 =20 The RX-8 uses 1.25 hoses. I stuck with that size as well. =20 Where are you measuring water pressure? =20 =20 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. =20 Is your pressure cap on the bleed / swirl tank? =20 Yes. =20 Any pictures of the plumbing? =20 Not of the current setup. =20 Bobby _____ =20 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 =20 I need some help with figuring out my cooling problems. =20 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. =20 Now the rest of the story.. =20 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. =20 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. =20 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. =20 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. =20 I read the temps and pressures every minute or two during the run. I = hope this doesn't get jumbled during transmission.=20 =20 Oil temp - 80 103 130 139 144 155 162 165 Air temp after cooler - 97 109 122 129 133 134 =20 Water temp - 86 126 161 173 178 190 198 199 Air temp after rad - 109 133 157 169 179 183 =20 Water pressure - 2 11 17 20 21 24 =20 =20 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 =20 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? =20 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.=20 =20 Suggestions??? =20 Thanks, =20 Bill B =20 _____ =20 From: Bill Bradburry [mailto:bbradburry@bellsouth.net]=20 Sent: Sunday, March 20, 2011 5:29 PM To: 'Rotary motors in aircraft' Subject: On the subject of installations... =20 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! =20 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? =20 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? =20 While I look into this, I also need to do something about my = muffler.Thank you, Bobby! =20 I wonder about that spiral muffler some of you are trying?? =20 Bill B 9 hours and counting. =20 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??? ------=_NextPart_001_0001_01CBEBC5.AA5653A0 Content-Type: text/html; charset="us-ascii" Content-Transfer-Encoding: quoted-printable

 

Bill;

 

Some comments on your coolant = pressure issue, pressure caps, etc. Are you sure you have a problem? Calibration = of the pressure readout would be a good idea.  As your engine heats = up the coolant will expand, and the pressure will rise until it reaches rated = cap pressure.  The pressure will not reduce again until the temperature = is decreased; so you shouldn’t be alarmed if the pressure stays high = during a constant power run.  If you have no air to compress the pressure = will reach cap pressure in a minute.  It will also drop rapidly with a reduction in temperature. If there is air in your filler bottle, or = whatever, the pressure will rise, or decrease more slowly.

 

On the question of safe pressure, = I have frequently pressure tested my system to 40 psi.  I have a double = cap setup shown in the photo. The filler neck cap has no air space (after initial = fill and bleed). The pressure in the system rises rapidly to cap pressure. = Coolant in released to the bottom of the neighboring overflow bottle which also = has a pressure cap, and has a volume of air. I have a float switch near the = bottom of the overflow bottle that would alert me if the level got too = low.

 

When the engine is at its max = temp, the system pressure can reach 37 psi (16 plus 21), and basically all of the = air has been expelled. As the engine cools down, the coolant in the system = contracts, the pressure  drops, and coolant is forced back into the filler neck.  The idea is to always have positive pressure in the system = to reduce the possibility of pump cavitation, increase the boiling point, = and to maintain system pressure at altitude. Typical cruise temps are 20 = – 30F less than max power climb, and the pressure is 6 – 10 psi. =

 

The filler neck is connected on = the inlet side of the pump – that’s where you want the pressure = at high rpm.  A double cap system is not required, and possibly has limited advantage in that we would seldom run at high power until things have = heated, and pressurized anyway.

 

It has worked well for me for = over 200 hours. I’ve not had any coolant loss. I haven’t needed to = add any coolant except when I drained to take something apart, or at each annual = when I drain, and replace about half the coolant.  I use about 30% EG in distilled water. 

 

Al G

 

 

 

 

-----Original = Message-----
From: Rotary motors in = aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Bill Bradburry
Sent: Friday, March 25, 2011 10:52 = AM
To: Rotary motors in = aircraft
Subject: [FlyRotary] Re: = Radiator Caps [FlyRotary] Re: On the subject of installations...Coolant = Pressure

 

Dave,

 

What does your = water pressure run in normal operation?

 

Bill = B

 

From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of David Leonard
Sent: Friday, March 25, 2011 1:32 = PM
To: Rotary motors in = aircraft
Subject: [FlyRotary] Re: = Radiator Caps [FlyRotary] Re: On the subject of installations...Coolant = Pressure

 

I wonder how much pressure it would really = take to blow out the seals on the pump.  My primary cap is 20# and the cap = on the seconday tank is 12#.  So my Max pressure is 32# relative to ambient.  I only keep a small amount of coolant in that = tank.  The air spring takes up all the expansion on most flights so I usually = don't reach full pressure. But a few times I have overheated the system = (Al can attest) and blown out coolant without any apparent damage to the = water pump.

 

--
David Leonard

Turbo Rotary RV-6 N4VY
http://N4VY.RotaryRoster.net http://RotaryRoster.net

On Fri, Mar 25, 2011 at 6:10 = AM, Ed Anderson <eanderson@carolina.rr.com&g= t; wrote:

In reading back over my = message, I realized that I could mislead some into thinking that the higher cap = radiator capacity - but, there is a limit.  At some point, if the cap did = not release pressure, the coolant pressure could get high enough to start = forcing coolant past seals such as the water pump shaft seal.  So don't = over do it. 

 

Unless you are going to be = flying higher than 18,000MSL, 24 psi is probably the highest capacity perhaps = even 21 psi.  You may get away with a 14.7 psi cap provided the absolute = coolant pressure does not rise above the absolute cap pressure at any given altitude.  Cooler ambient air at altitude and less power could = permit a 14.7 psi cap to work, but I personally would hesitate to use less than a = 21 psi cap.

 

Ed

 

 

 

From: Ed Anderson =

Sent: Friday, March 25, 2011 8:27 AM

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 =3D 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 =3D 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.  =

 

FWIW

 

Ed

 

From: Bill Bradburry =

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 –             &= nbsp;        80      103      130           &nbs= p;  139           &nbs= p; 144           155          162         = 165

Air temp after = cooler -             &= nbsp; 97       109           &nbs= p;            = ;        122            129          133         = 134

 

Water temp -            =       86       126      161           &nbs= p;  173           &nbs= p; 178           190          198          = 199

Air temp after = rad -            =         109      133           &nbs= p;            = ;        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???



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