X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from cdptpa-omtalb.mail.rr.com ([75.180.132.122] verified) by logan.com (CommuniGate Pro SMTP 5.4c2) with ESMTP id 4921665 for flyrotary@lancaironline.net; Fri, 25 Mar 2011 10:42:26 -0400 Received-SPF: pass receiver=logan.com; client-ip=75.180.132.122; envelope-from=eanderson@carolina.rr.com Return-Path: X-Authority-Analysis: v=1.1 cv=Nm3SJc7L3wlcojC9snsyzORkYWw1JOu3BeZkTeIwPUk= c=1 sm=0 a=eIaU6C7QCisA:10 a=rPkcCx1H5rrOSfN0dPC7kw==:17 a=Ia-xEzejAAAA:8 a=pedpZTtsAAAA:8 a=hv1z29ixCIz9dNhM2NQA:9 a=CGRH-RleCQ8Ek9It5-sA:7 a=2D-JCAvSY8WmxaSS4UHkhaHSQHkA:4 a=wPNLvfGTeEIA:10 a=EzXvWhQp4_cA:10 a=eJojReuL3h0A:10 a=Hnt0oGelnIqtVlQR:21 a=zRZg7yWA03wY5rmk:21 a=4_5BnYSxaNnzk1_3Lh8A:9 a=n6o_nVMB_fumKvR_xKoA:7 a=JQM7W_JRk_K52GiDoGYV47gz2H8A:4 a=BIJREz9axxgZpW72:21 a=75Qptl2Rd6_vGsd9:21 a=rPkcCx1H5rrOSfN0dPC7kw==:117 X-Cloudmark-Score: 0 X-Originating-IP: 174.110.167.5 Received: from [174.110.167.5] ([174.110.167.5:49413] helo=EdPC) by cdptpa-oedge02.mail.rr.com (envelope-from ) (ecelerity 2.2.3.46 r()) with ESMTP id 29/6D-11439-EA9AC8D4; Fri, 25 Mar 2011 14:41:50 +0000 Message-ID: From: "Ed Anderson" To: "Rotary motors in aircraft" References: In-Reply-To: Subject: Re: [FlyRotary] Re: Radiator Caps [FlyRotary] Re: On the subject of installations...Coolant Pressure Date: Fri, 25 Mar 2011 10:41:36 -0400 MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----=_NextPart_000_000C_01CBEAD9.372D9C90" X-Priority: 3 X-MSMail-Priority: Normal Importance: Normal X-Mailer: Microsoft Windows Live Mail 14.0.8117.416 X-MimeOLE: Produced By Microsoft MimeOLE V14.0.8117.416 This is a multi-part message in MIME format. ------=_NextPart_000_000C_01CBEAD9.372D9C90 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable Bill, One check is if you can, is to remove the cap while the engine is = running and if you can maintain a SAFE distance from the spinning prop = to observe the top of your coolant and see whether: 1. There are any bubbles coming up (stready stream) 2. Any sign of oil slick on top (coming in with combustion gases) My coolant pressure will jump from zero to 21 psi instantly upon start = up because I have no air bubble in my coolant system. Hydrostatic = "lock" (no air bubble to absorb any pressure waves) amplifies any = pressure present - until the engine block and coolant system heat up = and expand a tiny bit - then within a minute or two the coolant drops = back down to a nominal 5-7 psi. Ed From: Bill Bradburry=20 Sent: Friday, March 25, 2011 9:49 AM To: Rotary motors in aircraft=20 Subject: [FlyRotary] Re: Radiator Caps [FlyRotary] Re: On the subject of = installations...Coolant Pressure 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. =20 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! =20 Bill B =20 -------------------------------------------------------------------------= ------- 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 =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 -------------------------------------------------------------------------= ------- 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 -------------------------------------------------------------------------= ------- 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 -------------------------------------------------------------------------= ------- 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_000_000C_01CBEAD9.372D9C90 Content-Type: text/html; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable
Bill,
 
One check is if you can, is to remove the cap = while the=20 engine is running and if you can maintain a SAFE distance from the = spinning prop=20 to observe the top of your coolant and see whether:
 
1.  There are any bubbles coming up = (stready=20 stream)
2.  Any sign of oil slick on top (coming in = with=20 combustion gases)
 
My coolant pressure will jump from zero to 21 = psi=20 instantly upon start up because I have no air bubble in my coolant = system. =20 Hydrostatic "lock" (no air bubble to absorb any pressure waves) = amplifies any=20 pressure present -  until the engine block and coolant system heat = up and=20 expand a tiny bit - then within a minute or two the coolant drops back = down to a=20 nominal 5-7 psi.
 
Ed

From: Bill Bradburry
Sent: Friday, March 25, 2011 9:49 AM
Subject: [FlyRotary] Re: Radiator Caps [FlyRotary] Re: On = the=20 subject of installations...Coolant Pressure

I have a 21 = lb cap on=20 my system for this very purpose.  I don=92t presently have a = coolant recovery=20 tank and if the cap burps, I could lose coolant overboard.  I am = rethinking=20 this and plan to install a coolant recovery tank as=20 well.

 

By the way, = on the high=20 coolant pressure, in surfing the web I have found that this problem is = most=20 likely caused by combustion gasses getting into the coolant.  That = would=20 mean a busted o-ring.  I have been in denial that this is the cause = because=20 I don=92t want to tear the engine down.  Today I plan to see if I = can find=20 any coolant coming out of a sparkplug hole.  Fingers are=20 crossed!

 

Bill=20 B

 

From:=20 Rotary motors in aircraft=20 [mailto:flyrotary@lancaironline.net] On=20 Behalf Of Ed Anderson
Sent: Friday, March 25, 2011 8:27 = AM
To: = Rotary motors in aircraft
Subject: [FlyRotary] Radiator = Caps=20 [FlyRotary] Re: On the subject of installations...Coolant=20 Pressure

 

One thing to keep in mind = about the=20 pressure rating of the radiator cap you are using.  All are rated = relative=20 to a standard sea level ambinent pressure.  This means that he air = pressure=20 itself is contributing 14.7 psi at sea level. =20

 

So at sea level when your=20 differential pressure coolant gauge is reading 10 psi - the absolute = pressure in=20 your coolant system is then  14.7 + 10 =3D 24.7 psi.  Now if = you are=20 flying at 8000 MSL your ambient pressure is approx 1/2 at sea = level.  So=20 your 14.7 psi CAP now has the lesser capacity of 7.3 + 10 =3D 17.3 psi = absolute=20 pressure capacity - somewhat less than the 24.7 psi absolute it had at = sea=20 level.

 

When you increase in = altitude this=20 component naturally decreases.  So while a 14.7 psi CAP may work = fine at=20 sea level, more than one person found that at altitude  that = rating=20 was  insufficient and some coolant was=20 lost.

 

I personally would not fly = with less=20 than a 21 psi cap and currently fly with a 24 psi radiator=20 cap.

 

There is another factor = that=20 occurred to me.  Once a hot coolant system blows the relief = valve on=20 the cap, that lowers the pressure inside the system, superheated = (>212F)=20 coolant can quickly flash to steam and further cause lost of = coolant.  So a=20 Higher PSI cap can lessen the chance of that happening. =20

 

FWIW

 

Ed

 

From: Bill=20 Bradburry

Sent: Thursday,=20 March 24, 2011 5:30 PM

To: Rotary motors in = aircraft=20

Subject:=20 [FlyRotary] Re: On the subject of installations...Coolant=20 Pressure

 

Lynn,

 

You have hit = my=20 quandary squarely on the head.  Assuming that the pressure was zero = at room=20 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=20 and a pressure rise of, say, 6-7 pounds at 6000 rpm.  Under that = scenario,=20 you would have a pressure that ran at between 7-9 pounds at 2000 and = rose to=20 12-14 pounds at 6000.  Those pressures would be easily contained = with the=20 stock cap of 14 pounds.  And the pressure would be constantly = changing with=20 rpm and possibly temp of the system as you were under power or=20 not.

 

I have a 21 = pound=20 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=20 21 pounds before the engine is actually hot.  (around=20 190)

 

Something is = wrong and=20 I don=92t understand what it is.

 

Bobby

 

I am going to = insert=20 answers to your questions in your msg = below.

 

Bill=20 B

 

From:=20 Rotary motors in aircraft=20 [mailto:flyrotary@lancaironline.net] On=20 Behalf Of Bobby J.=20 Hughes
Sent:=20 Thursday, March 24, 2011 1:57 PM
To: Rotary motors=20 in aircraft
Subject: [FlyRotary] Re: On the = subject of=20 installations...Coolant Pressure

 

Bill,

 

This is all I = can think=20 of at the moment.

 

Are you = running a=20 thermostat or did you plug the hole between the inlets and outlets of = the water=20 pump?

 

No = thermostat.  The=20 Renesis has a thermostat tower which is too tall to fit under my cowl, = so I=20 removed it and fabricated a flat plate with two 1.25 aluminum tubes for = the=20 inlet and outlet of the water pump.  That hole you are referencing = exists=20 in the tower, but not in my plate.

 

If plugged = did you=20 drill a small hole in the plug to allow air a place to escape? I used a = #30=20 drill.

 

Any air in my = system=20 would have to be carried to the highest point, (radiator cap) then be = forced by=20 pressure to the bottom of the swirl tank where it would be = trapped.  This=20 seems to be working because I have found that after I open the system = for some=20 reason, the level in the swirl tank will go down and there is never any = air at=20 the top of the radiator.

 

After an = engine run is=20 the radiator the same temperature at the inlet / outlet / bottom and = top? If I=20 have trapped air only part of my radiator gets hot to the touch. Dual = pass=20 barrier leaking?

 

Seems to = be.  I=20 have mistakenly laid my arm on the top of the radiator after a = run=85usually I=20 manage to get off pretty fast!  :>)  I can not see into the = radiator tank on the barrier side.  It is possible it could be=20 leaking.  I suppose if there was a rag in the thing it could be = trapped=20 here also.  I have no way to see in there even if the hose was=20 removed.  I would need some kind of flexible camera or something = like=20 that.

 

Use an extra = CHT=20 channel and clamp it to the inlet of your radiator to measure Delta=20 T.

 

Good = idea.  I will=20 have to rig one up.  I don=92t have an extra=20 now.

 

My water = pressure does=20 not vary that much in operation. But it does hold a little pressure for = a few=20 days after shutdown.  1-2 psi.

 

What is your = pressure=20 during operation?  What is the pressure cap rating?  Does it = vary at=20 all with temp and/or rpm?  Mine is maxed=20 out..always!

 

What size = hoses? I=92m=20 running 1in.

 

The RX-8 uses = 1.25=20 hoses.  I stuck with that size as = well.

 

Where are you = measuring=20 water pressure?  

 

The hose that = comes off=20 the top of the rear iron goes to the top of the radiator, just below the = cap. A=20 tee in this line has the water pressure sender in it.  The radiator = cap is=20 just a cap, not a pressure cap.  The outlet in the radiator neck = goes to=20 the bottom of the swirl tank.

 

Is your = pressure cap on=20 the bleed / swirl tank?

 

Yes.

 

Any pictures = of the=20 plumbing?

 

Not of the = current=20 setup.

 

Bobby

From:=20 Rotary motors in aircraft=20 [mailto:flyrotary@lancaironline.net] On=20 Behalf Of Bill Bradburry
Sent: Thursday, March 24, 2011 = 10:23=20 AM
To: = Rotary motors in aircraft
Subject: [FlyRotary] On the = subject of=20 installations...Coolant Pressure

 

I need some = help with=20 figuring out my cooling problems.

 

Just so it = doesn=92t get=20 lost in the following BS, I need to state that I think the problem is = related to=20 the coolant pressure.  It seems to me to be way too high.  I = am=20 beginning to think that the coolant is somehow partially=20 blocked.

 

Now the rest = of the=20 story=85.

 

After I did = the flight=20 described in the attached email, I installed an opening in the bottom of = the=20 cowl that would work something like a cowl flap that is permanently = open. =20 The new opening is 9 inches by 5 inches or 54 sq in..  There is a = flare in=20 front of the opening that is at an angle of 45 degrees and extends down = into the=20 airstream about 4 inches.  (it is 6 inches long.)  This = opening is in=20 addition to two 6 X 6 openings, one of which has a 3 inch diameter = exhaust pipe=20 in it.

 

This helped a = little,=20 but nothing like I expected it would.  The pressure inside the = radiator=20 inlet dropped from 10 inches of water to 8 inches of water.  (by = the way,=20 Steve was right about it being inches of water and not inches of=20 Hg.)

The pressure = after the=20 radiator and inside the cowl dropped to 8 inches as well.  The = temperature=20 of the water dropped to 208 and the oil a couple of degrees.  = Neither of=20 these had the result that I expected.

 

My water = pressure cap=20 is rated at 21 lbs.  I have not calibrated the sender that came = with my=20 EM-2 and it shows 3 lbs when the engine is cold.  I assume that = this is=20 zero.  When in flight the pressure climbs to 24 lbs and stays = there. =20 I assume that at this point, the cap is at 21 lbs and is bleeding off = air. =20 There is about a pint to a quart of air above the coolant in the bleed=20 tank.

 

This morning = I ran the=20 engine on the ground for about 10-15 minutes at an rpm of 3000 to = 3200. =20 The OAT was 75 degrees.

 

I read the = temps and=20 pressures every minute or two during the run.  I hope this = doesn=92t get=20 jumbled during transmission.

 

Oil temp =96=20             &= nbsp;        80=20      103     =20 130           &nbs= p; =20 139           &nbs= p;=20 144          =20 155         =20 162        =20 165

Air temp = after cooler -=20             &= nbsp; 97      =20 109           &nbs= p;            = ;       =20 122           =20 129         =20 133        =20 134

 

Water temp=20 -            =      =20 86       126      = 161           &nbs= p; =20 173           &nbs= p;=20 178          =20 190         =20 198         =20 199

Air temp = after rad=20 -            =        =20 109     =20 133           &nbs= p;            = ;       =20 157          =20 169         =20 179          =20 183

 

Water = pressure=20 -            = =20 2         =20 11       =20 17       =20        20     = ;         =20 21            = ;            =    =20 24     

 

I noticed = that the=20 water pressure could be brought from 2 lbs to 9 lbs by changing the rpm = while=20 the engine was still relatively cool

 

What should I = expect=20 for water pressure at lower temps and how could I go about making a=20 determination that the water passages are = clear?

 

I am = beginning to think=20 that a rag has been left either in the engine or the radiator.  I = have=20 never torn the engine down and I sent the radiator out to have a leak = repair a=20 couple of years ago.  It is a double pass radiator.  I can = look into=20 the end that has both sides connected thru the radiator cap neck, but = not into=20 the inlet and outlet end.

 

Suggestions???

 

Thanks,

 

Bill=20 B

 

From: Bill=20 Bradburry [mailto:bbradburry@bellsouth.net]
Sent: Sunday, March 20, 2011 5:29 = PM
To: = 'Rotary motors in=20 aircraft'
Subject: On the subject of=20 installations...

 

My water temp = has been=20 running between 199 and 217, depending on the OAT.  The oil is = pretty=20 steady at around 175.  Today I finally got to fly with pressure = probes=20 inside the cowling.  I was all set to try and enlarge the inlet to = the=20 radiator to solve the problem.  It turns out that =93in=94 is not = the problem,=20 it is =93out=94 that is the problem!

 

I have 10 = inches of Hg=20 pressure in the radiator inlet and 10 inches of Hg on the outlet side as = well as=20 the same pressure everywhere I measured inside the cowl.  I need to = open up=20 the cowl some so more air can get out.  I had considered a cowl = flap but=20 that would not work in this instance because the problem is at = cruise.  I=20 need a permanent opening.  I am considering louvers and I am = looking for a=20 source.  I know some of you are using them.  Where did you get = them=20 and how are they installed so that they look = ok?

 

I am also = considering=20 some kind of flare around the exit area to create a low pressure area to = help=20 suck air out.  Do any of you have those and do they seem to=20 work?

 

While I look = into this,=20 I also need to do something about my muffler=85Thank you,=20 Bobby!

 

I wonder = about that=20 spiral muffler some of you are trying??

 

Bill B  = 9 hours=20 and counting=85

 

By the way, I = was=20 considering putting a 1 or 2 inch wide piece of cardboard across the = bottom of=20 the oil cooler to partially block it in the hopes that more air would = then flow=20 through the radiator.  Sort of like truckers do with the radiator = in cold=20 weather.  What opinions do you have about that idea?  I = realize it=20 would make more sense if the oil was really cool, but I think the oil = might not=20 get much hotter if an inch or so was blocked.  What do you=20 think???

=
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