> I think the safest and best trade is still one magneto and one electronic system.
Ross, et al -
How about 2 magnetos and a dual electronic ignition. The Lasar (Unison)
System can use your installed harness with its 2 new mags wired to their
electronic ignition box. Any failure of any part of the electronic ignition
(including total electric system failure), causes a reversion to using both mags as mags. The usual pre-flight "mag test" is just that,the electronics are turned off for 20 seconds while the mags are function tested. Timing advance is dependent on RPM and Manifold Pressure. If you put the power breaker in the cockpit, you can turn off the electronic ignition in flightjust for the fun of it.A single electronic ignition is a hopeless arrangement since the mag is not advanced whilst the electronic ignition should be --figure what that flame front looks like.
I have an IO360 with the combined dual magnetos and would very much like to turn it over to full electronic ignition. Full makes the most sense in this situation I believe as I cannot remove one magneto only.
Light Speed have a system that appears to fit and it would appear sensible to use the direct crank triggering and keep the magneto drive for a possible small alternator, later. A separate isolated battery would provde back up. In all the discussions on electronic ignition the question of back up is well to the fore as it should be. However I note from the Light Speed specifications that current draw for a 4 cylinder engine is 1.2amps at 13.8volts. This amperage would increase as standby battery voltage falls if it is not being charged. If we consider a draw of 2.5amps at 6.9 volts which is still above the minimum operating voltage of the ignition system (4volts) then a battery of 10AH capacity would give a theoretical 4 hours with two hours being well within its capacity. Plenty of time to find an airport and even enough power for limited use of radios and nav.
So I have three questions at least,
1. Is my theory and calculation wrong?
2. Why are people quoting pucker up experiences when using a standby battery to get home after the main system failed? Are their batteries too small? Do their electronic ignition systems draw a lot more power than the Light Speed I have quoted?
3. What do other users of electronic ignition recommend as a system/manufacturer.
I looked at the Wag-Aero catalog. This is a recommended dealer. I also looked at Aircraft Spruce. Couldn't find the Lasar System there either. Where did you buy your system? How much did it cost? Could you buy it without the new mags?
I have a mag that's due for overhaul and would rather spend the dough on a suitable electronic replacement. Can anyone out there recommend an "excellent" electronic ignition replacement for a magneto?
In a message dated 12/18/2004 6:05:45 P.M. Central Standard Time, farnsworth [at] charter.net writes:
Lee
Behel had Light Speed ignition on his Legacy for a while. He started having
problems and put mags back on. He had his control boxes on the engine side
of the firewall too. My understanding is that the heat from the engine did
bad things to the control boxes.
Lynn, Skip, Et Al,
Hmmmmm, I have been moving towards the dual Lightspeeds but I don't
want to install the controllers under my seats. I was considering mounting
them on the firewall with aluminum shields and blast tubes. This would be
a conversion from LASAR.
I've gone with dual Light Speed Laser III ignitions on my Super ES. I'm mounting them in the cabin side of the firewall on the copilot side, above the horizontal shelf. One mounts vertically to the firewall, and the second is above the first on standoffs. I had to plumb the manifold pressure into the cabin for the sensor anyway so this was not a concern. The wires from the crank sensors I'm running through the firewall on a multipin connector, and I mounted 6 BNC bulkhead feedthru connectors in the firewall. These are for the connection to the coils which is made using RG-400 coaxial cables.
I do have dual batteries and alternators, without which I would not go dual electronic ignition. The big drawback compared to a magneto is the need for DC power to run them. I have split the systems between the two buses.
I second the concerns expressed on the need to install the system properly. I had the ignition system installed by Performance Engines when they built the engine, and it was tested and timed before the engine was delivered.
Lynn: I have a dual Light Speed Ignition set up on my LIV and put the
control boxes on the back side of the firewall in front of the rudder
pedals--one on each side of the tunnel. They really don't require much
room as they are quite thin. Now I realize my IV is different than your
Super Legacy, but having flown with Light Speed ignitions for about 15 years (on
a LongEZ, the Lancair IV is scheduled for a first flight sometime this spring,
hopefully...), I think it is worth the effort to find a way to squeeze them
in--and outside of the engine compartment is best. regards, paul
Do you know what kind of electronic
emissions are/might be generated by the control box that might harm/
interfere with other electronic equipment?
Maybe you could ask Klaus?
I really want it but Andy says there is no
room behind the instrument panel.
Lynn: I have a dual Light Speed Ignition set up on my LIV and put
the control boxes on the back side of the firewall in front of the rudder
pedals--one on each side of the tunnel. They really don't require much
room as they are quite thin. Now I realize my IV is different than your
Super Legacy, but having flown with Light Speed ignitions for about 15 years
(on a LongEZ, the Lancair IV is scheduled for a first flight sometime this
spring, hopefully...), I think it is worth the effort to find a way to squeeze
them in--and outside of the engine compartment is best. regards, paul
Features (PRISM): â¢Optimized Spark Timing to
achieve maximum brake torque â¢Simple, fewer moving parts, fiber optic
design â¢Increased horsepower at all power settings â¢Smoother engine
operation- reduces coefficient of variation of combustion- even on lean
mixtures â¢More efficient engine operation-CDI produces larger spark at
optimized time BTDC â¢Replaces both magnetos- no overhaul required prior to
TBO â¢Fully redundant design- proven electronic durability with quad redundant
ignition â¢Includes GAMI's Supplenatorâ¢
Supplemental Alternator- back-up power to primary alternator and battery and
GAMI's PDUâ¢
Panel Display Unit â¢Automatic detection/prevention of detonation
â¢Maintains lower peak cylinder pressures- reduced loads on power train
components, longer engine life â¢Allows for the future use of lower octane,
unleaded fuels. This is the only system on the millennial horizon that is
inherently compatible with lower octane, unleaded fuels. â¢Champion® ignition
components (spark plugs, wires, coils) â¢Optional panel display of actual
real-time horsepower and torque â¢Optional digital tachometer â¢Optional
extensive on-board engine diagnostic capability â¢Improved fuel economy- lower
BSFCs than previously possible â¢Significantly lower EGTs/TITs for reduced
exhaust system maintenance FAA STC certification expected
soon!
E-Mag is a next-generation electronic
ignition, designed to serve as an upgrade or replacement for traditional
aircraft engine magnetos. The idea behind a next-generation "anything" is
that it 1) builds on what came before, and 2) gives more of what the customer
wants. Â
What Does The Customer Want?Â
Reliability, performance, economy, and convenience is a short and familiar
list. The challenge for designers is getting all these features into a
single package. It's rare when a single modification can:
Benefit so many areas (reliability, performance, economy, convenience).
Require so little investment.
Require so little time. Â
What Came Before?Â
Automobiles have used electronic ignitions for decades. Most of us have
experienced worn-out car tires, batteries, brakes, etc. But have you ever
worn out you car's electronic ignition? Likely not. Alternatively,
when did you last pull your mags for inspection/repair/replacement? How
many hours until your next mag appointment? Even so, the automotive
analogy has its limits. Auto ignitions evolved to serve different types of
engines.  Fortunately, aircraft ignitions are undergoing a similar
evolution, one that's oriented to their environment and engine-specific
needs. Â
The basic advantages of electronic ignition are very straight forward, and
"first-generation" aircraft ignitions perform them well. Â
Stronger Spark - Electronic ignitions deliver greater energy,
allowing spark plug gaps to be set much wider. The result is a hotter,
longer length, and longer duration spark.   Â
Variable Timing -Â Variable spark timing improves efficiency
over a wider range of operating speeds and conditions. Smoother idle,
efficient cruise, etc.
Multi-Strike Start - High-energy multi-strike start mode helps
overcome a variety of start-up challenges (cold engine, low battery, poor
mixture, oily plugs, etc.). Â
Fewer Moving Parts - Parts that donât exist don't wear out.Â
Light
Speed Engineering has introduced a new ignition system to its line of
products. The new Plasma III
Capacitor Discharge System is the latest high performance ignition for all 4-cyl
and 6-cyl aircraft engines. Its
long duration spark and optimized timing curve makes more horsepower and
improves fuel efficiency- at all altitudes. Other benefits include quick starts,
reduced maintenance, light weight, lower EGTâs and up to 20% more range. As with all LSE ignitions, RPM and
manifold pressure inputs are used for our proprietary timing curves. The Plasma
III is also capable of displaying the current timing advance, manifold pressure
and rpm on an optional lightweight LCD display.
Â
Scott Krueger
AKA Grayhawk N92EX IO320 Aurora, IL (KARR)
Lynn again: Re Light Speed EI EMI: I talked to Klaus and he sez
the Plasma IIIs (the ones you want to use on a turbo 550; the ones I am using)
have had no EMI problems when wired correctly. They can be wired
incorrectly by not properly connecting the shielding on the power wires to
provide continuity, but when done right the EI can be operated even with storm
scopes which are reputed to be very sensitive to EMI. He recommends
about six inches between his control box(s) and any other electronic
devices--but here too builders have mounted the box(s) on the radio stack and
not had problems. So I would think an aft firewall position would be no
problem for your Chelton, stack or panel--at least I hope not 'cause that
is the way mine is built! Any remaining tech questions, give Klaus a call
(best after 9am pacific so he has had time for a couple cups of tea).
don't settle, paul
Yes, that is true, but only if you are running from a single power source. This is true of my whole AC, as it is all electric with no vacuum system.
Part of my background as an engineer was development of missile tracking and Range Safety systems for the Navy testing of submarine launched ballistic missile. The systems we designed had two critical characteristics. 1. No single point failure could jeopardize the mission, property or life, and 2. No critical failure could go un-monitored.
If you power the ignition systems from two independent power sources (alternator and batteries sets), size them to run your critical minimum power need and monitor the health of these sources you should be business. I've a 60A and 20A alternator, each driving independent 28vdc batteries and buses, with voltage/current monitors with alarms on each bus. I have redundant minimum IFR instrumentation split between the buses. My minimum "fly to an airport in hard IFR" load I calculate at 17.4A, which I can source with a worst case single point failure.
When I test fly the AC I'll test the power system, but I believe I sufficiently redundant and monitored to cover the 'possible" situations. (remember, nothing is 100%.) BTW- one thing I do not have is an Avionics Master. It is a designed in single point failure. Just turn the units on/off individually.
I recently replaced my left mag with a Lightspeed Engineering electronic
unit. What a difference! Anyone having problems with a mag sould
look into it.
Forgot to mention in my previous posting some of the benefits of my
Lightspeed Engineering Plasma III electronic ignition which replaced a Bendix
mag:
Quicker starting...
Smoother idle...
Higher static RPM by 50...
Better takeoff & climb performance - especially out of higher density
altitude airports (SEZ & FLG for example)...
Leaner mixture in climb and cruise...
No fixed timing - is automatically variable between 20 to 40
degrees...
No points to wear out and no negative implications of high altitude flight
(at least up to17,500')... I suspect this type ignition system that even
the guys who fly up into the mid-to high 20's that their problems might be over
as well...
With the extreme rain we've had here in Southern California lately, I've
had occation to fly in moderate to heavy rain with no problems...
Hi Pete, I've only flown behind mags..can you enlighten me a little about
electronic ignition. What are the immediate benefits? Is the Bendix unit
replaced and therefore does it solve problems with a "stuck" Bendix o
starting. What happens if you're battery dies? Do you still have a
mag?
Thanks mate,
-- Gerard O Connell Melbourne,
Australia VH-LPD (LNC2)
I recently replaced my left mag with a Lightspeed Engineering
electronic unit. What a difference! Anyone having problems with
a mag sould look into it.
Some of the benefits of my Lightspeed Engineering Plasma III electronic
ignition which replaced a Bendix mag:
Quicker starting...
Smoother idle...
Higher static RPM by 50...
Better takeoff & climb performance - especially out of higher density
altitude airports (SEZ & FLG for example)...
Leaner mixture in climb and cruise...
No fixed timing - is automatically variable between 20 to 40
degrees...
No points to wear out and no negative implications of high altitude flight
(at least up to17,500')... I suspect this type ignition system that even
the guys who fly up into the mid-to high 20's that their problems might be over
as well...
With the extreme rain we've had here in Southern California lately, I've
had occation to fly in moderate to heavy rain with no problems...
I would be reluctant to replace both mags with electronic units. It's
reassuring to know the mag is there if one has a complete electrical
failure...
Pete Cavitt - N320PL
L-235/320 Kit No.077
7.5 years & 1,200 hours
619-701-0784
In a message dated 3/10/2005 4:53:16 PM Pacific Standard Time, goconnell [at] dodo.com.au writes:
Hi Pete,
I've only flown behind mags..can you enlighten me a little about electronic
ignition. What are the immediate benefits? Is the Bendix unit replaced and
therefore does it solve problems with a "stuck" Bendix o starting. What
happens if you're battery dies? Do you still have a mag?
Thanks
mate,
-- Gerard O Connell Melbourne, Australia VH-LPD
(LNC2)
Forgot to mention in my previous posting some of the benefits of
my Lightspeed Engineering Plasma III electronic ignition which replaced
a Bendix mag:
Quicker starting...
Smoother idle...
Higher static RPM by 50...
Better takeoff & climb performance - especially out of
higher density altitude airports (SEZ & FLG for example)...
Leaner mixture in climb and cruise...
No fixed timing - is automatically variable between 20 to 40
degrees...
No points to wear out and no negative implications of high
altitude flight (at least up to17,500')... I suspect this type
ignition system that even the guys who fly up into the mid-to high 20's
that their problems might be over as well...
With the extreme rain we've had here in Southern California
lately, I've had occation to fly in moderate to heavy rain with no
problems...
In a message dated 3/13/2005 8:38:30 A.M. Central Standard Time, glcasey [at] adelphia.net writes:
<<The decreased fuel flow in cruise will cover their cost in
about 300 hrs.>>
I would certainly like to see real data on
this, for both single electronic and dual electronic systems. How
much BSFC improvement is there to be had by advancing only one of the
sparks? Both of the sparks? I'm thinking of manifold pressures
of 20 inches or lower. Has anyone done a real dyno test to get this
data? How about a timing sweep under these
conditions?
Gary,
Let's see, saving .66 gph for the same performance over 300
hours would use 200 gallons less fuel and, @ $3/gal that is a
savings of merely $600. Of course, if you used the gph savings to extend
range you may save yourself a stop. Gee, if you boost the fuel burn back
to the previous level you will have increased the power - there is never too
much power for a low-drag Lancair.
Take a look at the way Unison presented its' data for a fixed pitch
prop on a carbureted C172 (I think).
Remember that this may be the worse performing electronic system, but with
a comfortable backup - mags.
==================
Advancing one spark may be better than none, but the flame fronts start at
different times - It is best to fire both plugs at the same time. But,
some people settle for 1/2 a system as it makes them comfortable with the
apparent risk/reward.
No Dyno test is a replacement for a flight test. Best is two planes
side by side in a race.
What's a timing sweep? Unison and E-Mag keep their timing secret,
Lightspeed has an optional display so you can monitor the timing (change it if
you dare, too).
In a message dated 3/14/2005 10:08:50 A.M. Central Standard Time, hapgoodm94 [at] alum.darden.edu writes:
I am running a non- aviation EFI
system. I'd love to see what the Lightspeed system shows for advance at
various power settings...
Anyone care to provide me with some of the
numbers you are seeing on the display?
Matt,
OK, expect to see some numbers from me in mid-April. If it
really works well, expect me to lie until after the Air Venture Cup Race.
Klaus wants those with compression ratios greater than 8.7:1 to retard
everything by 5 degrees. I have 9:1 right now, and I will have to do an
estimate after putting in the smaller automotive plugs - that may drop the
ratio.
Scott Krueger
AKA Grayhawk Lancair N92EX IO320 SB 89/96 Aurora, IL (KARR)
Fair
and Balanced Opinions at No Charge! Metaphysical Monologues used at your own
Risk.
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