Mailing List lml@lancaironline.net Message #23075
From: Brent Regan <brent@regandesigns.com>
Sender: Marvin Kaye <marv@lancaironline.net>
Subject: Re: First Legacy with an IO-520 and tuned exhaust
Date: Wed, 17 Mar 2004 11:50:13 -0500
To: <lml@lancaironline.net>
Chuck writes:
<<Horse Power rating = ALLOT!>>

Beautiful installation. Lots of nice work.

Two comments come to mind from the pictures.

The ignition cables should be grommeted where they pass through the baffle and  should be positively retained to prevent disconnection at the plug. (you probably already considered this).

Are you sure the air filter is big enough?  I know the K&Ns have the best flow rating but your engine needs about 430 CFM at 2700 RPM (assuming a volumetric efficiency of 1.0). Any pressure drop translates to a loss of horsepower. Most filters are flow (SCFM)  rated at 1" H2O pressure drop. A 400 SCFM rated filter would therefore cost about 1 horsepower, no big deal. The pressure drop varies as the square of the flow so a 200 SCFM rated filter will cost you about 4 horsepower. This is significant if you consider what those high compression pistons  cost per horsepower. Also consider that those flow ratings are for CLEAN filters. Remember how much suction you shop vac had when it was new compared to now, even though you cleaned the filter? After spending so much care and $$s on those last few ponies I would hate to see you send some to the air filter knackers.

The air filter flow problem is worse in turbocharged planes because the flow increases with altitude and the pressure drop is a larger percentage of the available pressure. For the same power setting, the airflow  through the filter will be 2.5 times greater at FL270 than at sea level. I use 800 SCFM worth of filter in my IV-P.

You may want to measure the inlet temperature and pressure to be sure you are not getting radiated or conducted heating (from the engine) of the inlet air. Use the local pressure, ambient temperature and pressure altitude  to calculate the adiabatic temperature rise of the air in the plenum. Compare this to the actual temperature rise to see if some shielding is needed.

For what it is worth, some free advice. You have built a high compression engine with a custom ignition, cam and exhaust. Before I flew behind it I would want to have it run at full power on a test stand to be sure all the bits play well together. Detonation would be my first concern. Get the temps up to red line (oil & cylinder) and verify that you do not have too much advance, that your mixture is correct and balanced and there are no leaks.  I would hate to see the first flight  terminate badly. You also want to do a flow and pressure test on the airframe's fuel system. Be sure you can get the GPH's that big boy needs.

Keep up the good work!

Regards
Brent Regan
Subscribe (FEED) Subscribe (DIGEST) Subscribe (INDEX) Unsubscribe Mail to Listmaster