Mailing List flyrotary@lancaironline.net Message #7140
From: Russell Duffy <13brv3@bellsouth.net>
Subject: RE: [FlyRotary] Dave's pump problems and Rotor Poll
Date: Fri, 9 Apr 2004 12:18:23 -0500
To: 'Rotary motors in aircraft' <flyrotary@lancaironline.net>
Message
From the discussion so far, it sounds like I need some more continuous flow through the vent system so I have attached a drawing of my proposed changes, submitted for your [dis]approval. 
 
Hi Dave.  The proposed scheme is much better.  In fact, it's EXACTLY what I had in rev-1 (big low mounted rad, same vent port, etc), and also the way it's done in a 3rd gen car.   Mazda refers to the pressurized can as an AST (air separator tank).  Mine flowed just dandy with and without a thermostat.  The only problem was that it was a pain to fill, since my pressure cap wasn't the high point.  
 
During my rev-2 upgrade, I simplified the system further, and got rid of the AST.  I was able to mount a pressurized cap at the high point where the water outlet is, and only have a plastic jug for overflow now.   So far, this is working even better.   

 

 

 Lastly, I want to take a poll.  I know there is no right answer so I am looking for everybody’s opinion.  While I have the engine apart I am considering replacing the 9.0:1 turbo rotors with the higher compression 9.7:1 n.a. rotors, even thought I still plan to run the turbo.   

 

I ran as much as 10 psi on mine, with 9.7 rotors, but I was using 100LL fuel, and had the timing retarded a bit.  From everything I've heard, you won't really be able to tell the diff between 9.0, and 9.7.  That being said, when I upgraded my 8.5 rotors, I insisted on 9.7, rather than the 9.4 rotors.  The 8.5's are still in the attic.  They only have Mazda's test run time on them.  I'll make you a good deal :-)

 

Cheers,

Rusty (off to test a pitch setting that's probably too low)

 

 

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