ELECTRONIC IGNITION

Forums: 

From: DON & PAT RYAN <djpryan [at] ruralnet.net>
Subject: ELECTRONIC IGNITION
Date: Sat, 11 Dec 1999 08:23:43 -0700
To: LML <lancair.list [at] olsusa.com>

         <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>>

          <<  Lancair Builders' Mail List  >>

          <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>>

>>

Does anyone know what has happened to Jeff Rose, "ELECTOAIR"??



I have recently tried to contact him and found that the phone number I have

has been disconnected.  I have his DIS ignition system on an IO360 and find

that the strobe lights cause the DIS timing display to bounce severely.

There doesn't seem to be any interference with the actual ignition.  The

manual does indicate that the signal lead to the display should maybe

shielded, but since I didn't build this one I don't know whether it is

shielded.  I wonder now about support for the system.



>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>

LML website:   http://www.olsusa.com/Users/Mkaye/maillist.html

Builders' Bookstore:   http://www.buildersbooks.com/lancair

>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>

Electronic Ignition

From: <Sky2high [at] aol.com>
Sender: <marv [at] lancaironline.net>
Subject: Re: [LML] Re: Electronic Ignition
Date: Fri, 19 Nov 2010 16:53:13 -0500
To: <lml [at] lancaironline.net>

Doug,
 
Your worries are over.  At takeoff power with my 9:1 CR I see
about 22 DBTDC at a MAP of 29.9" and 2740 RPM.  My home airport is at
700 MSL.  Cruise (180 KIAS) at about 5000 MSL, MAP about 26", RPM 2500
and 10.3 gph I see 24-25 DBTDC (still not running LOP as the power is too
high).  Higher up and at pretty low power, ROP/LOP with a KTAS of 187 to
195 I see timing reaching 29-30 DBTDC. LOP down to 5.5 gph (I only lose
about 6-8 Knots running LOP, but save about 2 gph to extend my
range). 
 
While LSE doesn't publish timing data, one can determine that from the
optional display and various flight regimes.  Even P-Mag displays its model
mapping on its web site and has announced that a display is (or will be)
available.  Only LASAR's peculiar system keeps its maps as a trade
secret.  I have no idea about the existing FADEC systems.
 
The only problem with GAMI's opinion is that they tout a competing
vaporware system.  I respect the engine knowledge that they have
and communicate and I utilize the engine management procedures they
propound.  I hope their no-lead fuel formulation becomes the standard
of the future. 
 
I have drunk from the EI Koolaid pitcher with the smiley face and
demonstrated to myself its value, even after struggling with LASAR. 
 
Another difference I have with GAMI relates to the method one might utilize
to reach A/F ratio happiness betwixt cylinders.  A first approach for a NA
injected engine might be to balance the air reaching last century injectors to
equalize the atomization first.  Before dickering with nozzle size,
one can use a plenum, along with shrouded injectors, to even out the air
supply.  If one flies fast enough and uses ram air induction that can raise
the MAP 1.5 or more inches above ambient, it is even more argument to use
the same shrouded injectors that turbo charged engines use to make sure the deck
pressure supplying air to the injectors is a match to the MAP.  I use ram
air to supply the plenum and am insured of equally distributed atomization air
at or above MAP.  If that doesn't work with a GAMI lean test, one should
consider further tuning the nozzle sizes.
 
Let's go fly,
 
Scott
In a message dated 11/19/2010 7:03:21 A.M. Central Standard Time,
douglasbrunner [at] earthlink.net writes:

Scott,

You said:
 
Remember that magneto systems
don't measure any factor yet the engine manufacturer has no problem with LOP
or ROP operations with some restrictions (see below).  Indeed, there are
no timing adjustments for CR while EIs provide fjor such.  As I have
said, EIs don't provide much timing change from the base timing (dependent on
CR) for power settings over 75% as inferred by a combination of RPM and MAP -
a typical way of expressing power.  At lower power settings there is a
benefit of advancing the spark to get more work done by the combustion event
occurring in the cylinder.  At low power settings it is hard to get bad
events to occur, including damaging peak cylinder pressures.

 
Finally, please stop using ROP
settings where the EGT is -50F from peak as that is outside the good operating
range of my engine (that's info from both Lyc and GAMI, worst peak pressures)
- Of course, if you are running a Continental engine, well, uh, you have to
find your own info.

 
Scott
Krueger

 

Scott,

As a graduate of the AP
Seminars, I have drunk the GAMI Koolaid.  What they said about Electronic
Ignition makes sense to me - the advance curves are proprietary and do not
take into account the effect of mixture on timing.

Several quick
comments:

  • Does your abbreviation "CR" mean compression ratio?  My engine has
    a 10:1 compression and the timing has been retarded to account for this.
  • "please stop using ROP settings where the EGT is -50F from peak"  I
    do not use this setting although I think it is acceptable to use this power
    setting at low enough power settings - <70%.  If I am at a low power
    setting I am typically LOP.
  • You say: "EIs don't
    provide much timing change from the base timing (dependent on CR) for power
    settings over 75%
    "   What is the timing change that EI
    uses?  Do you have data on this that you can share?


I think
we would all like an electronic ignition system that provides a hot consistent
spark, easy starting and does not have the maintenance and arcing problems of
magnetos.  We would also like one that kept the effective timing at 16
deg ATDC.  The problem with current electronic ignition systems is that
since they don't take mixture into account, they can't maintain the same
effective timing with different mixtures.

I would actually like to be
able to advance my spark during certain flight regimes (LOP at less than 70%
power) in which I am fairly certain nothing bad will happen and advanced
timing will give better power/economy.  It is the rest of the flight
regime (like takeoff at 2700 RPM, 30" MAP and 10:1 compression) that I am
worried about


-----Original
Message-----
From: Sky2high [at] aol.com
Sent: Nov 18, 2010 7:52 PM

To: lml [at] lancaironline.net
Subject: [LML] Re: Electronic Ignition


Doug,
 
You said:
===My
point was that electronic ignition systems measure only 2 of the 3 factors
that influence timing.  Mixture can have a significant effect on when
Peak Intracylinder Pressure (= effective timing) occurs.  Hence the
effective timing at a best power mixture (50 to 100 deg ROP) would be
significantly advanced compared to the effective timing at best economy
mixture (approx 50 LOP).  This is not accounted for by electronic
ignition systems and could lead to excessive spark
advance.

===
 
Remember that magneto systems don't measure any factor yet the engine
manufacturer has no problem with LOP or ROP operations with some
restrictions (see below).  Indeed, there are no timing adjustments
for CR while EIs provide fjor such.  As I have said, EIs don't provide
much timing change from the base timing (dependent on CR) for power
settings over 75% as inferred by a combination of RPM and MAP - a typical
way of expressing power.  At lower power settings there is a benefit of
advancing the spark to get more work done by the combustion event occurring
in the cylinder.  At low power settings it is hard to get bad events to
occur, including damaging peak cylinder pressures.
 
Finally, please stop using ROP settings where the EGT is -50F from
peak as that is outside the good operating range of my engine (that's info
from both Lyc and GAMI, worst peak pressures) - Of course, if you are
running a Continental engine, well, uh, you have to find your own
info.
 
Scott Krueger
 
PS If you are talking about supercharged/turbocharged engines always
running at high power then the benefits of EIs are simply a better, more
reliable spark without worrying about esoteric things such as that the
magneto is properly pressurized so no sparking occurs in the mag. 
 
/files/LML/56756-02-R/X.MA1.1290103540 [at] aol.com" sandbox="" width="654" height="997" comp_state="quality" datasize="141380">
 
In a message dated 11/16/2010 6:11:46 P.M. Central Standard Time,
douglasbrunner [at] earthlink.net writes:

Scott,

 

I
will concede your point about the hotter, longer and more consistent
spark, although in most flight regimes (no extreme of F/A mixture) it
probably doesn’t make much difference.

 

With
respect to your comment:

 

“your
argument of moving timing by messing with the mixture is, uh, not good
operational practice”

 

I
think you misunderstood my point.  I certainly do not advocate
“messing with the mixture” – especially at power levels above 70%. 

 

My
point was that electronic ignition systems measure only 2 of the 3 factors
that influence timing.  Mixture can have a significant effect on when
Peak Intracylinder Pressure (= effective timing) occurs.  Hence the
effective timing at a best power mixture (50 to 100 deg ROP) would be
significantly advanced compared to the effective timing at best economy
mixture (approx 50 LOP).  This is not accounted for by electronic
ignition systems and could lead to excessive spark
advance.

 

D.
Brunner

 

 

From: Lancair
Mailing List [lml [at] lancaironline.net
]">mailto:lml [at] lancaironline.net] On Behalf Of
Sky2high [at] aol.com
Sent: Tuesday, November 16, 2010 9:25
AM
To: lml [at] lancaironline.net
Subject: [LML] Re:
Electronic Ignition

 

Doug,

 

I
have a problem with your argument.  It seems to be upside down. 
In reference I refer you to my 11/2/2010 email entitled "NA Injected
Engine Performance LOP".  In any event, for any given
proper fuel/air ratio (mixture), there is a narrow timing range
that produces efficient cylinder pressures at the correct crank angle
range.  The Lycoming engine manual (for my 320) displays the
acceptable range for the EGT for best power as 100F to 180F
ROP, and best economy as 0F to 80F LOP.  Running 50F ROP is very bad
for cylinder pressures as stated by GAMI - thus your argument of moving
timing by messing with the mixture is, uh, not good operational
practice.

 

Secondly,
you imply that the only function of an electronic ignition is to advance
the timing.  Au contraire mon ami!  An electronic ignition
provides for a hotter, longer, more consistent spark over a greater plug
gap that better insures the reliable and timely ignition of the
combustible mixture even though the F/A may be at some extreme.  This
results in greater efficiency/HP depending on the way one looks at
it.  See the pamphlet on the benefits of the LASAR electronic
ignition that shows speed increases for the same fuel burn or reduced fuel
burn at the same speed of a magneto driven
engine.

 

The
fixed timing of a magneto (i.e. 25 DBTDC) is a compromise. 
Generally speaking, EIs advance the base spark timing minimally
until the power, as measured by RPM and MAP, is reduced below
75%.  Bad events, such as pre-ignition, detonation and incorrectly
timed cyl pressure, are less likely in this regime (that is why the GAMI
lean test is done at less than 75% power).  Furthermore, EGTs
(representing F/A ratios) are still maintained in the engine
manufacturer's recommended ranges and the timing is a better match
for the combustion event pressures.

 

Note
that during my best power cruises at middle altitudes (2500 RPM, MAP
> 22", EGT > 120F ROP), the EI timing is about 25 DBTDC plus or
minus a degree. 

 

Yes,
more HP.  Better speed for the same fuel burn holding other
conditions equal.

Yes,
in all the modes you mentioned.

 

I
haven't reached TBO yet, I go too fast to accumulate that much
time.

 

Scott
Krueger

IO
320 Dual Lightspeed Plasma III EI

 

In
a message dated 11/15/2010 8:21:27 P.M. Central Standard Time,
douglasbrunner [at] earthlink.net writes:

At
the risk of starting a “theological” controversy, I would like to raise
some reservations about electronic ignition systems (other than
reliability and loss of electrical power)

 

Peak
intracylinder pressure (the point in the combustion cycle at which
pressure in the cylinder is highest = effective timing) is related to 3
things; spark timing, rpm and MIXTURE. 

 

Why
mixture? Because air and fuel mixtures burn at different rates depending
on how rich or lean they are.  So at a given RPM, MAP and spark
advance you can vary your effective timing by changing the
mixture. 

 

·        
Want
to advance your timing? Change your mixture to a 50 deg ROP mixture –
which is the fastest burning.

·        
Want
to retard your timing?  Make your mixture richer or leaner from 50
deg ROP.

 

And
since optimal power is achieved at an effective timing of 16 deg ATDC,
advancing the spark timing may or MAY NOT increase
horsepower depending on the mixture.  But advancing the timing will
likely increase the magnitude of peak intracylinder pressure leading to
higher intracylinder pressures, higher cylinder head temperatures and
greater stress = shorter enging life.

 

For
those of you who are using electronic ignition (I am
not):

·        
Are
you sure you are getting more horsepower?  How do you
know?

·        
If
you are getting more horsepower, are you getting it during all modes of
engine operation?  Rich of peak, lean of peak, high MAP, low MAP,
etc

·        
What
is happening to your TBO?

 

D.
Brunner

 

The
biggest advantage of any of the electronic systems (in my opinon) is
that they provide a spark advance that is a function of at least
manifold pressure, giving an advantage any time the manifold pressure is
much lower than maybe 25 inches.  But there is very little
combustion taking place in the exhaust system regardless.  The
reason the exhaust temperature rises is that more of the combustion
occurs after TDC and that means less of the energy is being converted to
work.  The down side of advancing the spark is that since more
combustion occurs at the highest cylinder pressure, more heat is
transferred to the cylinder head and piston. 

 

--

For archives and unsub http://mail.lancaironline.net:81/lists/lml/List.html

Electronic Ignition

From: Gary Casey <casey.gary [at] yahoo.com>
Sender: <marv [at] lancaironline.net>
Subject: Re: Electronic Ignition
Date: Sun, 21 Nov 2010 22:17:43 -0500
To: <lml [at] lancaironline.net>
Okay, now you've got me confused (not that it takes a lot for that to happen :-), which part of my discussion is incorrect?
Gary



From Scott:
Balderdash
 
In a message dated 11/18/2010 6:56:18 P.M. Central Standard Time, casey.gary [at] yahoo.com writes:


Scott,
I have a problem with your problem with Doug's argument :-).  Well, not much of a problem, but it does make for an interesting discussion.  True, for any condition there is a range of timing that produces the most effective pressure profile - I wouldn't call it "efficient cylinder pressures".  That profile has been stated by the GAMI guys as the timing that produces a peak cylinder pressure at 16 ATC.  But it's not like you're falling off a cliff on either side of this timing.  And this peak pressure point does move with mixture changes - it's unavoidable.  So one of the things you
do with mixture is to try to put the peak cylinder pressure at the right angle.  Indirectly, because there is no instrumentation to go by.

Yes, there are other characteristics of "electronic" ignition that have an effect.  Usually, a battery-power system that is electronically switched (Is that "electronic"?  I suppose) provides more spark energy than with a magneto.  And all magnetos (and some
electronic systems) use shield spark plug wires and they "suck" some of the energy out of the spark.  What's the energy good for?  To get more a combination of time and current in the spark that exceeds what would otherwise be available.  There the approaches of different suppliers diverge.  The Lightspeed system uses a capacitor-discharge (CD) method that charges a capacitor to something over 100 volts and then discharges this into a coil.  This produces a very high current, low duration spark.  The duration is perhaps 1 or 2 microseconds(very, very short).  The other suppliers typically use an inductive system just like in a magneto.  This produces a much lower current spark that lasts a "long" time maybe 2 milliseconds.  Each method works, but they have different limitations.  A short duration spark has one chance to light the fire and if it misses that, there is no second chance.  A long
duration spark might have less of a chance to light the fire in the first microsecond (less current means less "intensity"), but it keeps trying.  So Klaus built the "III" that double-fires the spark.  Problem is that the second spark can't come immediately after the first one.  I don't know the delay, but is suspect it might be 1 millisecond, maybe half that.  At 2500 rpm the the crank turns 15 degrees per millisecond, so the second spark would be 15 degrees "late".  Better late than never, I suppose.  The biggest advantage of the double strike comes in starting and idling, when finding a combustible mixture near the plug at any given instant is not likely.  When attempting to run lean mixtures, automotive OEM's tried everything and finally gave up on CD technology.  The inductive system lights a lean mixture better.  And either technology can fire a larger plug gap, but the CD system can take advantage of
it better.

Another advantage of higher-energy sparks is that they reduce the "initial combustion time".  They can light more fuel molecules and that speeds up the initial portion of the fire.  Imagine a bonfire where you light more kindling.  The fire reaches its peak faster, but once the end result is the same.  Now imagine the pressure in the cylinder immediately after ignition - there is almost no change initially, but once a substantial portion is burning the pressure goes up rapidly and then there is no difference.  So, what I'm getting at is that a higher powered spark results in combustion that behaves exactly like that lit with a low-power spark, but with a little more advance (maybe 2 degrees or so).  That change shouldn't be
construed as an advantage - you can get the same result by advancing the magneto timing.


Pages

Post a Reply

Filtered HTML

  • Web page addresses and e-mail addresses turn into links automatically.
  • Each email address will be obfuscated in a human readable fashion or, if JavaScript is enabled, replaced with a spam resistent clickable link. Email addresses will get the default web form unless specified. If replacement text (a persons name) is required a webform is also required. Separate each part with the "|" pipe symbol. Replace spaces in names with "_".
  • Allowed HTML tags: <a> <em> <strong> <cite> <blockquote> <code> <ul> <ol> <li> <dl> <dt> <dd> <h1> <h2> <h3>
  • Lines and paragraphs break automatically.

Plain text

  • No HTML tags allowed.
  • Each email address will be obfuscated in a human readable fashion or, if JavaScript is enabled, replaced with a spam resistent clickable link. Email addresses will get the default web form unless specified. If replacement text (a persons name) is required a webform is also required. Separate each part with the "|" pipe symbol. Replace spaces in names with "_".
  • Web page addresses and e-mail addresses turn into links automatically.
  • Lines and paragraphs break automatically.
Attachments
Files must be less than 512 MB.
Allowed file types: jpg jpeg gif png txt doc docx xls xlsx pdf ppt pptx pps ppsx odt ods odp mp3 mov mp4 m4a m4v mpeg avi ogg oga ogv weba webp webm.