Mailing List lml@lancaironline.net Message #37842
From: Gary Casey <glcasey@adelphia.net>
Sender: <marv@lancaironline.net>
Subject: Re: Boost pump switching
Date: Sun, 24 Sep 2006 23:07:32 -0400
To: <lml@lancaironline.net>
There are at least 3 fundamental types of fuel injection systems in production, whether for automotive applications or aircraft.  A "Speed-Density" essentially multiplies engine speed times manifold air density to get a desired fuel flow.  A "Speed-Theta" system multiplies engine speed times a function of throttle position.  And finally a "Mass Air Flow" system measure air flow directly.  In present-day automotive applications air-flow systems are most common, but there are a lot of speed-density systems used, primarily by Honda and Chrysler.  The Continental system is a speed-theta system, also used by Harley Davidson and some Italian cars.  (hmm....)  The speed function is provided by the constant-displacement gear pump and the "theta" function is provided by the barrel valve linked to the throttle.  Note that there is nothing in the system that is related in any way to air flow - the assumption is that an engine of a given displacement running at a given throttle opening will want a given amount of fuel.  Maybe, but a lot of conditions affect it and that is why there are so many final adjustments and tweaking required.  And since fuel flow is the result of a balance of flow through various orifices operation of the boost pump can upset the system, since it essentially bypasses the engine-driven pump.  The engine-driven pump is not just a fuel supply - it is an essential metering element in the system.

The "Bendix" Precision Airmotive system used by Lycoming is an air flow system.  It uses a venturi to measure air flow and controls fuel flow in proportion.  It does this by regulating fuel flow so that the pressure drop across the metering orifice is the same as the venturi throat vacuum.  Idle air flow is too low to accurately measure so there is a separate "theta" control system for idle and that is the only normal adjustment in the system.  The system is completely insensitive to supply pressure as long as the pressure is within an acceptable range of typically 15 to 40 psi.  One big advantage of this type of system is that the system can be accurately calibrated on the bench.  If you order a replacement system you can just bolt it on and go.  Another advantage is that the orifice size of the injectors doesn't affect the fuel flow (orifice balance does affect the fuel distribution, though).  These advantages are the main reason I went to the trouble to put a Lycoming engine in my ES.  The only other option in my mind was to adapt a Precision Airmotive  fuel system to a Continental engine - probably less work.  What are the disadvantages of the "Bendix" system?  One is that the venturi causes and unavoidable pressure drop in the system and therefore the engine will produce slightly less power.  Another is that there is no return path that can separate vapor, notwithstanding the "purge" valve that Air Flow Performance sells.

The comment about altitude compensation is partly true.  Some Continental systems have an aneroid bellows that adjusts for altitude, but I have no idea as to whether it works well.  A standard Precision system has not altitude compensation, but there are units available that have altitude compensation.  Even without it the Precision system has an advantage since the venturi system inherently compensates by the square root of air density - it essentially takes out half of the altitude effect.

I've suggested to Various Lancair people the possibility of offering a Lycoming option, but I don't think there is much interest in doing so.

Gary Casey


"The TCM System varies greatly from its Lycoming counterpart, the Bendix Fuel Servo.  Perhaps most noticeable is the absence of a venturi to schedule fuel flow proportionate to air flow. The Bendix  system regulates fuel flow by means of a delta pressure across an air diaphragm. Comparatively, the  Continental System has no way to sense airflow. It does not compensate for altitude or density changes, nor does it correct for MAP unless turbocharged. "

http://www.kellyaerospace.com/articles/ContinuousFlow.pdf#search=%22io550%20fuel%20pump%22

 

Bob Belshe


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