Mailing List flyrotary@lancaironline.net Message #9037
From: Ed Anderson <eanderson@carolina.rr.com>
Subject: Re: [FlyRotary] Re: Cooling oil
Date: Fri, 11 Jun 2004 11:37:34 -0400
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Well, my figures for 160Hp show fuel burn of 1.58 lbm/min, so a quick sanity check shows 1.58*60 = 94.8 lbsm/hour/6 = 15.8 Gallons/hour which sounds about right for 160HP with a "Best Power" A/F of 12.56
 
So 1.58 lbm/min *19,000 BTU/Lbm = 30020 BTU/Min
 
Taking Al's apportionment we have
 
Power = 28%*30020 = 8405.6 BTU/Min = 198.02 HP (I think this is a bit high on HP for a 15.8 gallon/hr fuel flow, I would expect to
see a fuel flow of around 18.5 gph for close to 200HP)
Coolant = 18%*30020 = 5403.6 BTU/Min
Oil = 7%*30020 = 2101.4 BTU/Min
Exhaust the remainder.
 
So using Al's figures, we are closer to the 1775 BTU figure for the oil cooler.  I use 25% for power and 25% for waste heat and 50% for Exhaust, just to be on the conservative side. Also I allocate 2/3 of waste heat to coolant and 1/3 to oil.
 
Al's percentages may be closer to reality than the ones I use, which are pretty standard for a reciprocating engine.  But, I have never found any similar percentages for the rotary.  If someone could direct me to a credible source, I will revise my allocation of BTUs.
 
Thanks
 
Ed
Ed Anderson
RV-6A N494BW Rotary Powered
Matthews, NC
----- Original Message -----
Sent: Friday, June 11, 2004 10:26 AM
Subject: [FlyRotary] Re: Cooling oil

Al,

   Perchance, did you forget that the 160 HP is *output*,
not the total produced from the fuel burn?

Dale R.
COZY MkIV-R #1254

>
> From: "Al Gietzen" <ALVentures@cox.net>
> Date: 2004/06/11 Fri AM 12:46:45 EDT
> To: "Rotary motors in aircraft" <flyrotary@lancaironline.net>
> Subject: [FlyRotary] Re: Cooling oil
>

>
> Subject: [FlyRotary] Re: Cooling oil
>

>

>
> ----- Original Message -----
>
> From: "Joseph Berki" <joseph.berki@grc.nasa.gov>
>
> To: "Rotary motors in aircraft" <flyrotary@lancaironline.net>
>
> Sent: Thursday, June 10, 2004 12:39 PM
>
> Subject: [FlyRotary] Re: Cooling oil
>

>

>
> > It would be interesting to measure flow in both engines.  I thought that
>
> > both Lycoming and Mazda engines rejected 2/3 heat load through the
>
> > oil  that is why I started going down this road.  If the engines generated
>
> > the same Hp than the heat load should be similar.
>
> >
>
> > Joe Berki
>

>
> Joe, both engines may generate the same heat load, but the proportion
>
> rejected through the coolant in case of the Mazda is 2/3 of its waste heat
>
> while the oil rejects another 1/3 of the waste heat.  Neither engine rejects
>
> anywhere near 2/3 of its waste heat through the oil.
>

>
> Most aircraft engines reject on the order of 300-600 BTU/Min through the
>
> oil, the Mazda at 160HP rejects approx 2446 BTU/Min through the oil.
>

>
> Ed Anderson
>

>
> Ed;
>

>
> That number looked a bit high to me, so I went in to my file to check.  My
> data shows 28% of the fuel burn energy in the rotary gets converted to HP,
> 18% goes to the coolant, and about 7% to the oil. Most of the rest goes out
> the exhaust pipe. For 160 HP output, I think that should be 1725 BTU/Min
> going to the oil cooler.  So about 3 times the comparable powered Lyc.
>

>
> Double check me on this.
>

>
> Al
>

>

>
>
>


 

Subject: [FlyRotary] Re: Cooling oil

 

 

----- Original Message -----

From: "Joseph Berki" <joseph.berki@grc.nasa.gov>

To: "Rotary motors in aircraft" <flyrotary@lancaironline.net>

Sent: Thursday, June 10, 2004 12:39 PM

Subject: [FlyRotary] Re: Cooling oil

 

 

> It would be interesting to measure flow in both engines.  I thought that

> both Lycoming and Mazda engines rejected 2/3 heat load through the

> oil  that is why I started going down this road.  If the engines generated

> the same Hp than the heat load should be similar.

>

> Joe Berki

 

Joe, both engines may generate the same heat load, but the proportion

rejected through the coolant in case of the Mazda is 2/3 of its waste heat

while the oil rejects another 1/3 of the waste heat.  Neither engine rejects

anywhere near 2/3 of its waste heat through the oil.

 

Most aircraft engines reject on the order of 300-600 BTU/Min through the

oil, the Mazda at 160HP rejects approx 2446 BTU/Min through the oil.

 

Ed Anderson

 

Ed;

 

That number looked a bit high to me, so I went in to my file to check.  My data shows 28% of the fuel burn energy in the rotary gets converted to HP, 18% goes to the coolant, and about 7% to the oil. Most of the rest goes out the exhaust pipe. For 160 HP output, I think that should be 1725 BTU/Min going to the oil cooler.  So about 3 times the comparable powered Lyc.

 

Double check me on this.

 

Al

 

 


>>  Homepage:  http://www.flyrotary.com/
>>  Archive:   http://lancaironline.net/lists/flyrotary/List.html
Subscribe (FEED) Subscribe (DIGEST) Subscribe (INDEX) Unsubscribe Mail to Listmaster