Mailing Lijst flyrotary@lancaironline.net Bericht #47192
Van: Jeff Luckey <JLuckey@pacbell.net>
Onderwerp: RE: [FlyRotary] Re: Renesis Cooling Thermodynamics
Datum: Mon, 13 Jul 2009 18:00:23 -0700
Aan: 'Rotary motors in aircraft' <flyrotary@lancaironline.net>

Thanks to all for the kind welcome & info, and especially to Ed Anderson for the spreadsheet.  It will take a few days for me to work thru this info, but I’ll be back soon w/ more questions.

 

 


From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of George Lendich
Sent: Saturday, July 11, 2009 18:06
To: Rotary motors in aircraft
Subject: [FlyRotary] Re: Renesis Cooling Thermodynamics

 

Jeff,

1.Multiply Hp x 42.4 to get BTU/Min.

 Or 2545 BTU/ hr = 1 hp

2.Oil cooler cools 30 % of Rotary heat.

3.?

4. Up to 60 gal a min.

George (down under)

Welcome Jeff,

Have you searched the archives?

Bryan

 


From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Jeff Luckey
Sent: Saturday, July 11, 2009 7:11 PM
To: Rotary motors in aircraft
Subject: [FlyRotary] Renesis Cooling Thermodynamics

 

 

Hello All,

 

I’ve started the tail section of an RV-7A and want to power it w/ a Renesis.  I need information about cooling thermodynamics.

 

Here are my questions:

 

  1. How much heat must be rejected thru the coolant (in BTUs)?
  2. How much heat must be rejected thru the oil?
  3. What is the temp delta between radiator inlet/outlet in a typical installation?
  4. What is the coolant flow (in GPM) for the stock Renesis cooling system?

 

If these questions have already been answered, please direct me to those answers.

 

 

Thanks for the help,

 

 

Jeff Luckey

Costa Mesa, CA

 

 

 

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