Mailing List flyrotary@lancaironline.net Message #21207
From: Barnhart <dsbarno@vbe.com>
Subject: Re: [FlyRotary] Home again, home again!
Date: Sun, 1 May 2005 15:37:29 -0500
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Ed,
 
Good to hear your back "home".  How did you put the engine on the plane from the back of a van?
 
Barny
MGDQ 20bt (removing engine and engine mount to take care of some Murphy tail related problems)
----- Original Message -----
Sent: Sunday, May 01, 2005 12:41 PM
Subject: [FlyRotary] Home again, home again!

Wife, drove me and my flight gear to aircraft getting there around 1100.  By time finished loading, reinstalling the avionics - the @$#%^ transponder wouldn't slide all the way back in an engage the pins it was 1130 and the wind was picking up.  - I figured I'd stay low enough and out of class B airspace anyway. 
 
I told her that she could pick me up back at the home airport in NC if I didn't have any problem - she said I wouldn't have any problem.  Curious, I asked how did she know I wouldn't have any problem - "Headwind" she said.  Women, got to love em.
 
Cranked up the engine and let oil and coolant temp rise to 120F and taxied to runup at end or runway.  Everything looking good, I restricted takeoff rpm to 5400 (6000 ft long runway), still accelerated rapidly and lifted off.  Kept it low until hitting 140 mph hoping to maintain good cooling.  However, coolant temp rose to 220F during the circuits of the airport as I slowly climbed.  I pulled the power back to 4500 rpm and the temps stabilized at 210F.  Oil temp was around 185F.  Normally coolant is in syn with the oil or perhaps 5F higher.  After flying for approx 20 minutes coolant temps were at 200F, so slowly coming down.
 
This is pretty much what Tracy reported when first flying with the Renesis engine - tight engine, more power, more heat.  So it appears that this engine is much tighter.  I can now maintain level flight burning 4 gph when it used to take 5.5 gph.  Can't wait until its broken in a bit more to see what the top end is.  Overhaul kit from Real World Solutions and parts from Bruce T appear to have come together in a tight nit engine.
 
But, it does appear the  small cooling inlets (which I had planned to open up a bit) are too small for the new HP being produced (are you listening, AL {:>)?. Also, several people mentioned after I arrived back at GooseCreek that the exhaust was  deeper and louder.  Even my wife mentioned it no longer had that "whinny" sound.
 
So thanks for all the well wishes from everyone, advice, and engineering consultation on the cause.  I have mailed seals to Tracy and Bob Perkinson, so that should provide some "harder" data on the status of the seals.
 
 
Ed Anderson
Rv-6A N494BW Rotary Powered
Matthews, NC
eanderson@carolina.rr.com
 

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