Mailing List flyrotary@lancaironline.net Message #14070
From: Russell Duffy <13brv3@bellsouth.net>
Subject: RE: [FlyRotary] Re: cooler thoughts
Date: Sat, 18 Dec 2004 20:08:31 -0600
To: 'Rotary motors in aircraft' <flyrotary@lancaironline.net>
Message
The problem might simply be that the pulses are hitting high pressures and fatiguing the reasonably flimsy evap cores.  There's also the possibility that the pulses hit a resonant vibration at some point, which causes the failure.

 

It would be interesting to see a trace of these pulses, and they may be important; but I am skeptical about them being the primary cause unless your cooler is near the engine outlet, and you have rigid (solid metal) lines.   

 

Hi Al,

 

If I thought a standard pressure sensor could catch the pulses, I'd be tempted to put a scope on it. I just don't think it would be a conclusive test though.  Leon has told me some interesting stories that lead me to believe in the pressure pulse theory.  I also can't think of a better explanation.  I don't quite buy the cycling pressure theory, because I'm only running about 80 psi at the cooler.  I think the evap core probably sees close to an 80 psi cycle between static, and operating pressure.  Also, I believe the leak started after a good 20 minutes of flight, not on initial pressure at startup, which wouldn't indicate that it failed on the pressure cycle.  

 

Fortunately, I think the only point we need to prove is that evap cores are a bad idea for oil coolers.

 

Cheers,

Rusty

 

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