Mailing List flyrotary@lancaironline.net Message #9632
From: Bob Perkinson <bobperk@bellsouth.net>
Subject: RE: [FlyRotary] BOV more/less air flow
Date: Fri, 9 Jul 2004 21:10:25 -0500
To: Rotary motors in aircraft <flyrotary@lancaironline.net>

So what happens when the BOV opens. The pressure on the intake manifold side starts immediately venting to the atmosphere reducing the pressure inside the manifold – this is of course what the BOV is designed to do. The compressor wheel has been spinning at 90,000 rpm with 1.5 boost pressure ratio. Now the boost pressure ratio may be 1.2 or less in a very short duration of time (milliseconds). This immediately reduces the backpressure on the compressor wheel caused by the manifold pressure being less than it before the venting. . The engine has not yet reacted to this change, as it is still combusting the boost density air it had ingested into the combustion chamber before the BOV opened. Neither has the exhaust gas flow been affected - yet.

 

Ed,

In the situation that you describe what would prevent the BOV from alternately opening and closing causing noticeable power surges?

IMHO  I would also think that the turbine that had the larger compressor would be the one whose shaft would suffer from the sudden attempt to accelerate and the increase in vibration as the speed increases when the back pressure is lost.

I would also like to take this opportunity to thank you and all the others on this list for all the information that is freely imparted.

Bob Perkinson
Hendersonville, TN.
RV9A
If nothing changes
Nothing changes
 

 
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