Mailing List flyrotary@lancaironline.net Message #19840
From: Ed Anderson <eanderson@carolina.rr.com>
Subject: Re: [FlyRotary] Re: New manifold on engine
Date: Tue, 5 Apr 2005 23:15:55 -0400
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Jack, I'm certain your are right - that is probably why my wife insists on grilling our steaks {:>)
 
Ed
----- Original Message -----
From: Jack Ford
Sent: Tuesday, April 05, 2005 10:31 PM
Subject: [FlyRotary] Re: New manifold on engine

Ed,
 
1650F is way way too hot for grilled steaks.
 
Jack
----- Original Message -----
Sent: Tuesday, April 05, 2005 4:42 PM
Subject: [FlyRotary] New manifold on engine

Here are a couple of photos of the old and new manifold on the aircraft.  The new one has a much wider range of adjustment tube length of from 6 1/2" of tubes to 11".  The old one had a max of 9".  However, I can only use about 9 3/4" before I bump into the cowl with the air inlet elbow.  So I will reshape that to lower its profile and see If I can't get at least 10".
 
 
Went out around noon and fired it up with an OAT of 85F got 5800 rpm static with the old manifold.  Flew the old manifold and got 6400 rpm at 2000 MSL and 6400 at 7000 msl.  Landed and proceeded to take off old manifold and put on new.  Discovered I had failed to remove a boss on the new one that interfered with the motor mount and had to take it home and grind that off.  Back out in the late afternoon and got the new one installed.   I tried several lengths of adjustment,  but this was just a quick and dirty and will need more testing to confirm.  But for what its worth these were the results
 
Length             Static         Fuel Flow                    Calculated HP based on fuel burn
6 1/2"          5800            14.5 GPH    OAT 87F      164.77
9"                6000            15.25 GPH  OAT 87F       173.29
10"              6100            16.50 GPH  OAT 88F       187.50
 
As Al pointed out, that fuel burn may  not quite as reliable a measure of HP for the rotary as it may be for a piston engine  The reason -  you can keep cranking up (enriching) the mixture once past a certain point and the fuel burn rate will increase but you may not really be converting all of that increase into power - it could simply be blown through the chamber and burnt in the exhaust manifold.
 
  I know when I continuing enrichment, my EGTs come down after a certain point of enrichment - that leads me to believe that excess fuel in the exhaust actually results in lesser temps - cools the exhaust as counterintuitive as that seems.  If this supposition is correct, then by monitoring your EGTs you may be able to detect when that "excess" point is reach.  The end result may be a better estimate based on your observed fuel burn rate. 
 
I should have recorded the EGTs, but didn't think of it at the time.  Was in a hurry to get home so as not to miss grilled steaks.  Both were up in their normal range around 1650F.
 
In any case, at 6 lbs 3 0z this intake is lighter by 4 lbs than the old one and I believe esthetically more pleasing to the eye.
 
Couple of photos attached.
 
Will report flight results later.
 
Ed
 
 
Ed Anderson
Rv-6A N494BW Rotary Powered
Matthews, NC
eanderson@carolina.rr.com


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