Subject: Icing and waste spark.
From: rotaryeng
Date: 4/26/2012, 8:34 AM
To: AAAA Put this in the To box


Hi  Paul.

  1)  Aside  from   perceived  poor  fuel  economy  of  rotary
    engines, what  are  its  disadvantages ?

  2)  You  advised  carbs  and  magnetos.Why  are  they  not
 discussed here? Are  they  not  suitable  for  rotaries ?   If
  suitable,   Let's have  more  discussions.

  3)  Can  there  be  carb  icing  in  tropical  countries  below  3,
  000 feet ?

  Best regards.
  Ben

  Fuel economy is only 5% higher than an aircraft piston engine.
  This is more than made  up for by the 25% lower cost of auto gas.

  Magnetos are suitable. They will work fine.  They are just too costly.
    $2000 each new
  and $400 to $800 re manufactured plus cores. People don't want to
  pay as much for two  aircraft magnetos as they pay for the rest of
  the engine. In some cases much more than  they payed for the
engine.  RX8 ignition coils are $25 each for a total of $100. One
coil per plug.

  However if I were certifying a rotary I would use aircraft magnetos
  and an aircraft carb. The FAA is much more comfortable with that
 they   they are with EFI and electronic ignition. In that case the
 rotary engine would pass   certification in a heart beat.

  The best carb (cost verses power) to use is a two barrel 500 CFM Holley
    with a
  leaning kit.

  The FAA will not sign off on your carb engine unless it has carb heat.

  Paul Lamar

    Thanks  Paul.

    I'm  glad  there  is  someone  like  you  who
    has  the  knowledge  and  patience  to  answer
    our  questions.

    Can  there  be  carb  icing  in  tropical  countries  at  an
  altitude  up  to 4,000 feet ?

  Best regards.
  Ben

    At the higher altitudes for sure. The evaporation of the fuel in
  the carb venturi causes a cooling effect.

    Paul Lamar

  Paul,
  My Continental IO 520D has fuel injection- but it is a very basic system
  indeed. One inj per cyl, a regulator, and a mechanical "TPS". It
  looks like it all related back to the manual leaning valve and
quite  possibly the manifold pressure. This system seems remarkably like
  the old FI on the corvettes in the early 60s. Regulators and manual
  flow metering.

  Why would this be a difficult system for the rotary? Before I sell
 my Connie, I might inventory the system and see about maybe a prototype.

  Kevin Alderman

  http://www.vette-vues.com/parts_for_sale.html

  Early Power Sport used mech fuel injection.
  It is still sold for aircraft.
  http://www.airflowperformance.com/html/site_html.html

  Paul Lamar

    These early Rochester FI systems were not received well due to a
 couple of things. The dual quad made more power the next year and
 the injection was very sensitive to atmospheric conditions. It
 required almost daily tuning unless someone really knowledgeable
 worked on it.   Att 1.  The "throttle" in the center is not the
 throttle. It is the choke plate.  The throttle can be more easily
 seen in Att 4.   This works similar to the Bosch/Volkswagon FI and
 the Mazda MCES systems, that use a special volute and flapper to
 measure air flow. The Rochester used the cone in the intake to
 create a pressure drop like a venturi. This was fed over to the
 diaphragm to lift the metering "rod" to add fuel. At idle there
 would be no "vacuum" on the sensing line. As the throttle is
 depressed, the air flow causes a vacuum at the venturi and lifts the
 diaphragm. Different air densities and humidity affected the fuel
 required which was not well compensated for. The Mazda MCES works
 fairly well as the sensor is a form of mass flow and is compensated
 with the computer. The Bosch also works as a basic mass meter, but
 did not have a computer (Rabbit system. different from K-jetronic).
  Any AC system will have compensation for atmospheric condition as a
 requirement for altitude changes.

  Dale Davies

  Hi   Paul,
   No FI system I have ever flown with has allowance for
  temperature or density, only have experience with Cont and Lyc. My
 understanding is they are both a engine speed/throttle/mixture
 position, ie if you have the mixture,prop,throttle to the wall you
 will always get the same fuel flow, regardless of temperature and,or
 altitude. But I love 'em, no carby icing!! BUT if you have clogged
 injectors your fuel flow gauge will tell you you have say 36 gallons
 pre hour at take-off, you will have something less than that,
  because it is not a fuel flow meter but purely a pressure gauge!
 calibrated to indicate fuel flow in gallons per hour. Where it
 become bad is if you have only one injector, you may not notice the
 fuel flow is lower than it should be for that engine, unless you
 have  EGT probes in each exhaust outlet. John Burey

  Hi  Paul,   I was half asleep last missive I think, I had said "if
  you have only one injector", I really wanted to say was that if you
 had

  (one injector partly clogged), you would have a lower fuel flow to
that  cylinder, which you can pick up with a EGT in each exhaust
outlet. Fuel  injection is much better than carbys every time, as
for the spark, I  cannot see why one could not use a electronic
ignition as a previous  writer described (B&S), one for each
cylinder with wasted spark, ie two plug wires on each coil, then if
one coil failed you would be only drop out one plug on opposing
cylinders, plus you would have a very hot spark with about .040" gap
not the pillidy .015" to .020" with a magneto, just the correct size
gap to catch a bit of carbon,  I am surprised that the FAA still
allow magneto's to be used, I have had more failures with magnetos
in engines than any other single thing. I know all the reasons they
are used (no external power) ect., ect.. John Burey

  Be careful with wasted spark. Only the bottom plugs will tolerate that.

  Paul Lamar

    Hi   Paul, what is the reason for not tolerating wasted spark on
the  top plugs? as you know I nothing, nothing, (in a high pitched
 voice),about Rotarys.   John Burey

  Waste spark fires two plugs at the same time.

  The problem is rotor 2 is always 180 degrees out of phase with
 rotor 1 so when rotor 1 is on the firing stroke rotor 2 is on the
 compressing stroke with a combustible fuel air mixture that might
 pre ignite causing a negative torque on the e-shaft. You can see
 that with this picture of a transparent model engine.

  In a 2 cylinder or more piston engine, the firing stroke is 180 our
 of phase with an exhaust stroke so the waste spark has no effect on
 the spent exhaust mixture.

  Paul Lamar back from China.

 What if you hooked the waste spark return to the 2nd plug on the
 same rotor?  Is there enough power to fire both?

 We are running Klaus' Lightspeed on the little Continental and it
 works like a charm.

 Chris Cosman

 That should work. Is Klaus using waste spark coils? I think that is
 a CD system.

 Paul Lamar

 The only problem I see is that the plug gap resistance is doubled.
This could lead to misfires. A normal waste spark has a very low
resistance on the plug that is firing across the exhaust gap.

Dale Davies

Does not seem to bother them as waste spark is widely used on auto engines.

Paul Lamar



 Yes they work fine when the one plug is firing in the exhaust on the running
mate of the cylinder you expect to ignite. Of course 360 degrees later the
plug firing in the exhaust is reversed. If you use one waste spark coil to
fire both plugs in one rotor, the plug resistance may be too high. Remember
that this is a circuit and total resistance has to be considered. Also one of
the plugs will always be firing in reverse polarity (backwards) which it does
not want to do as well. If someone wants to experiment with this, I would
recommend putting the reverse polarity side on the trailing plugs. If the coil
can create enough energy this could be used. I have not tried this. Also a
supercharged engine will require higher spark energy. Turbo normalized engines
are like naturally aspirated in that the air molecules in the plug gap are the
same as at low altitude when at higher altitude.

Dale Davies

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