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Thread-Topic: [FlyRotary] 2 pass or not 2 pass... oil cooler? 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The field elevation here is 728= 0 ft. The conditions and results are listed in case they may be of interes= t: Climb from density altitude 9400' to 11600' OAT decreased from 21 to 14 deg C MAP decreased from 22.1 to 20.4 inches Hg Fuel flow decreased from 13.2 to 12.4 gal/hr RPM was 6800 IAS was 70 Kt TAS was 80 Kt Coolant was thermostatically controlled and 89 deg C The air pressure difference across the oil cooler core was 2.5 inches H2O Heat rejected by the coolant and oil cooling systems was 68% by coolant and= 32% by oil. The following temperatures were stabilized at the end of the climb: Oil cooler oil inlet temperature was 114 deg C Oil cooler outlet temperature was 85 deg C Oil inlet side air exiting the core was 78 deg C Oil outlet side air exiting the core was 72 deg C The oil cooler was a single pass DB30618. I don't think I have observed an indication that the oil side of the oil co= oler is limiting when there is sufficient air flow through the core. As a = result, it may be unlikely that converting the cooler to double pass would = improve its performance very much. If you changed from a stock Mazda cool= er to the DB30618, you now have about twice the oil flow rate through the c= ooler. If the temperature of the oil coming out of the cooler is about the= same as you had from the Mazda cooler, the temperature difference of the o= il across the cooler is now about half of what it was originally. In other= words, about the same amount of heat is being removed by the oil but the t= emperature of the oil in the sump is significantly less. Do you measure th= e oil cooler inlet and outlet oil temperatures? I do not have an oil cooler outlet air duct. Under almost all cruise condi= tions, I restrict the air flow through the cooler by partially or fully clo= sing a shutter on the air outlet side of the cooler in order to get oil tem= peratures out of the cooler above 71 degrees C. The shutter does not close= off all the core area due to interference with the engine mount. I cannot produce as much power as you can due to the altitude here and my n= ormally aspirated engine. However as altitude decreases the cooling capaci= ty of the air increases by the same amount as the increase in power. So I = have not observed a change in operating temperatures as a result of changin= g altitude. For what it is worth. Steve Boese RV6A, 1986 13B NA, EC2, RD1C, MT electric CS prop ________________________________ From: Rotary motors in aircraft on behalf of = Todd Bartrim bartrim@gmail.com Sent: Sunday, September 30, 2018 1:55:57 AM To: Rotary motors in aircraft Subject: [FlyRotary] 2 pass or not 2 pass... oil cooler? Hey Rotorheads; This summer I bought the Fluidyne DB30618 but it is only a single pass. = I recently inquired about them with Summit Racing and they say they will pr= ovide a 2-pass as a custom order. The stock oil cooler is a 2-pass but much= more restrictive. The single pass added a longer hose with a 180 swept fit= ting to make it work. I'm seeing higher temps than I'd like to despite my improved duct work. = Actually inlet duct was improved, but outlet duct is new as I didn't have o= ne before and I do wonder if the outlet duct is restrictive but I'm limited= with space and old nose gear mount being in the way (as much as I'd like t= o remove the nose wheel mount it is integral to the engine mount, so I'm st= uck with it), so I wonder if it would be better to remove the exit duct com= pletely and just leave the oil cooler exit air un-ducted? But to the main question for tonight, I'm thinking about converting my c= ooler to a 2-pass. I have been experiencing higher oil temps than expected = at around 110C and considering the OAT has dropped considerably, I would li= ke to reduce these somewhat. I suspect that the flow is not going through t= he entire cooler evenly with a majority of flow channeling through only a f= ew of the tubes as it is not really any different than the temps it used to= see with the Mazda cooler. The larger size and more efficient design shoul= d produce better cooling if oil was flowing evenly through all tubes and sp= ending a longer time in the cooler. So I'm thinking it should be simple enough to convert to a 2-pass cooler = which should ensure a better distribution of flow through all the tubes. Bu= t is it really so simple?? See pic at https://photos.app.goo.gl/TrU99jXjftz4X8h37 It would seem a simple matter to zip-cut a slot where the red line is, slid= e in a baffle plate and weld it up, re-sealing the end tank, drill a hole a= nd weld in the new AN10 fitting and at the other end, zip off the old AN12 = fitting and weld it up. This would also simplify plumbing, as the oil in li= ne would be shorter and go straight in with no 180 bend. But the thing is I can only weld on 3 sides of the baffle plate that I w= ould install. I can ensure that it is tightly seated against the tube end p= late between the tube but it wouldn't be a sealed junction. Do it right and= an insignificant amount of oil may bypass there and not go through the tub= es. Do it wrong and it could be a significant amount with a drastic reducti= on in cooling. Obviously I've already removed the cooler and brought it home with the i= ntent to do this mod, but now I'm second guessing myself. I've considered t= hat if Summit Racing is modifying these as a custom order then they likely = are doing just what I plan to do. Otherwise it would have to be done during= manufacture by Fluidyne. It seems simple, but I lost sleep last night considering all the various= issues. Still didn't do it today, so I figured I'd pose the question to th= e group and go hunting with my kid tomorrow while I wait for the opinions t= o arrive. On another topic, during a take-off roll the other day, the diaphragm in= my old stock wastegate actuator blew. I didn't catch it with the throttle = until I hit 16.5 psi of boost. No damage but I gotta say that's a fun way t= o get off the ground in a hurry! I usually limit myself to 6 psi of boost a= s that was the spring pressure. I do have an electronic controller (TurboSm= art) which allows me to have higher pressures above the spring pressure, bu= t that is intended for high altitude and mountain flying. I've ordered a new adjustable piston type of actuator that comes with a s= election of 6 springs. I intend to use the 3 psi spring as I usually use th= e boost very conservatively and the TurboSmart controller can give me more = if I need it for short mountain strips. Anyways, I look forward to your opinions on the oil cooler. Todd Bartrim ....... 20.6 hours on new RV9 version 2.0..... I had to = cash in beer cans for gas money.... C-FSTB RV9 13Bturbo --_000_MWHPR0501MB3804A563D68CC703003F7385B9EF0MWHPR0501MB3804_ Content-Type: text/html; charset="us-ascii" Content-Transfer-Encoding: quoted-printable

Todd,


This morning I made a short fligh= t designed to challenge my cooling systems as opposed to the way I normally= operate.  The field elevation here is 7280 ft.  The conditions a= nd results are listed in case they may be of interest:


Climb from density altitude 9400'= to 11600'

OAT decreased from 21 to 14 deg C=

MAP decreased from 22.1 to 20.4 i= nches Hg

Fuel flow decreased from 13.2 to = 12.4 gal/hr

RPM was 6800

IAS was 70 Kt

TAS was 80 Kt

Coolant was thermostatically cont= rolled and 89 deg C

The air pressure difference acros= s the oil cooler core was 2.5 inches H2O

Heat rejected by the coolant and = oil cooling systems was 68% by coolant and 32% by oil.


The following temperatures were s= tabilized at the end of the climb:

Oil cooler oil inlet temperature = was 114 deg C

Oil cooler outlet temperature was= 85 deg C

Oil inlet side air exiting the co= re was 78 deg C

Oil outlet side air exiting the c= ore was 72 deg C


The oil cooler was a single pass = DB30618.


I don't think I have observed an = indication that the oil side of the oil cooler is limiting when there is su= fficient air flow through the core.  As a result, it may be unlikely t= hat converting the cooler to double pass would improve its performance very much.   If you changed from a stoc= k Mazda cooler to the DB30618, you now have about twice the oil flow rate t= hrough the cooler.  If the temperature of the oil coming out of the co= oler is about the same as you had from the Mazda cooler, the temperature difference of the oil across the cooler is n= ow about half of what it was originally.  In other words, about the sa= me amount of heat is being removed by the oil but the temperature of the oi= l in the sump is significantly less.  Do you measure the oil cooler inlet and outlet oil temperatures?


I do not have an oil cooler outle= t air duct.  Under almost all cruise conditions, I restrict the air fl= ow through the cooler by partially or fully closing a shutter on the air ou= tlet side of the cooler in order to get oil temperatures out of the cooler above 71 degrees C.  The shutter d= oes not close off all the core area due to interference with the engine mou= nt.


I cannot produce as much power as= you can due to the altitude here and my normally aspirated engine.  H= owever as altitude decreases the cooling capacity of the air increases by t= he same amount as the increase in power.  So I have not observed a change in operating temperatures as a result of c= hanging altitude.


For what it is worth.


Steve Boese

RV6A, 1986 13B NA, EC2, RD1C, MT = electric CS prop



       

From: Rotary motors in airc= raft <flyrotary@lancaironline.net> on behalf of Todd Bartrim bartrim@= gmail.com <flyrotary@lancaironline.net>
Sent: Sunday, September 30, 2018 1:55:57 AM
To: Rotary motors in aircraft
Subject: [FlyRotary] 2 pass or not 2 pass... oil cooler?
 
Hey Rotorheads;
   This summer I bought the Fluidyne DB30618 but it is only = a single pass. I recently inquired about them with Summit Racing and they s= ay they will provide a 2-pass as a custom order. The stock oil cooler is a = 2-pass but much more restrictive. The single pass added a longer hose with a 180 swept fitting to make it work.
   I'm seeing higher temps than I'd like to despite my impro= ved duct work. Actually inlet duct was improved, but outlet duct is new as = I didn't have one before and I do wonder if the outlet duct is restrictive = but I'm limited with space and old nose gear mount being in the way (as much as I'd like to remove the nose wheel mount= it is integral to the engine mount, so I'm stuck with it), so I wonder if = it would be better to remove the exit duct completely and just leave the oi= l cooler exit air un-ducted?
   But to the main question for tonight, I'm thinking about = converting my cooler to a 2-pass. I have been experiencing higher oil temps= than expected at around 110C and considering the OAT has dropped considera= bly, I would like to reduce these somewhat. I suspect that the flow is not going through the entire cooler evenly with= a majority of flow channeling through only a few of the tubes as it is not= really any different than the temps it used to see with the Mazda cooler. = The larger size and more efficient design should produce better cooling if oil was flowing evenly through all= tubes and spending a longer time in the cooler.
  So I'm thinking it should be simple enough to convert to a 2-pa= ss cooler which should ensure a better distribution of flow through all the= tubes. But is it really so simple?? See pic at
It would seem a simple matter to zip-cut a slot where the red line is,= slide in a baffle plate and weld it up, re-sealing the end tank, drill a h= ole and weld in the new AN10 fitting and at the other end, zip off the old = AN12 fitting and weld it up. This would also simplify plumbing, as the oil in line would be shorter and go s= traight in with no 180 bend.
   But the thing is I can only weld on 3 sides of the baffle= plate that I would install. I can ensure that it is tightly seated against= the tube end plate between the tube but it wouldn't be a sealed junction. = Do it right and an insignificant amount of oil may bypass there and not go through the tubes. Do it wrong and it coul= d be a significant amount with a drastic reduction in cooling.
   Obviously I've already removed the cooler and brought it = home with the intent to do this mod, but now I'm second guessing myself. I'= ve considered that if Summit Racing is modifying these as a custom order th= en they likely are doing just what I plan to do. Otherwise it would have to be done during manufacture by Fluidyne.<= /div>
   It seems simple, but I lost sleep last night considering = all the various issues. Still didn't do it today, so I figured I'd pose the= question to the group and go hunting with my kid tomorrow while I wait for= the opinions to arrive.

   On another topic, during a take-off roll the other day, t= he diaphragm in my old stock wastegate actuator blew. I didn't catch it wit= h the throttle until I hit 16.5 psi of boost. No damage but I gotta say tha= t's a fun way to get off the ground in a hurry! I usually limit myself to 6 psi of boost as that was the spring pressure. = I do have an electronic controller (TurboSmart) which allows me to have hig= her pressures above the spring pressure, but that is intended for high alti= tude and mountain flying. 
  I've ordered a new adjustable piston type of actuator that come= s with a selection of 6 springs. I intend to use the 3 psi spring as I usua= lly use the boost very conservatively and the TurboSmart controller can giv= e me more if I need it for short mountain strips.
Anyways, I look forward to your opinions on the oil cooler.

Todd Bartrim     .......  20.6 hours o= n new RV9 version 2.0.....  I had to cash in beer cans for gas money..= ..
C-FSTB
RV9 13Bturbo
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