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EFI Injection Strategies/ Injector Placement

rv6ejguy

Well Known Member
We’ve had some questions this week about injection strategies and mountings used in aircraft EFI systems since there seems to be some confusion about these topics.

At SDS, we’ve always been focused on performance and reliability. For the last 25 years, we’ve used the non-sequential strategy on all our aviation and automotive systems because it’s simple and reliable and provides the same power potential as sequential. We’ll continue to use the same injection strategy on the new EM-6 currently under development.

What’s the difference?

Non-sequential strategies vary, injectors may be fired in ones, twos, threes or most commonly, all at once which is usually called batch fired. On our 4 cylinder, aviation systems with individual cylinder trim, injectors fire one at a time, in sequence, so there is some confusion as to what to call this strategy but SDS aviation systems are technically not batch fired as some have erroneously stated. Injectors are not timed to valve opening however and don’t require a cam sensor.

Sequential injection is an unfortunate misnomer (should be called timed IMO) but generally means that injectors are triggered in relation to valve opening on that port. This strategy was developed in the 1990s by auto OEMs to aid emissions and part throttle driveability, especially when cold. Sequential injection requires a cam sensor and one drive transistor per injector.

Semi-sequential or bank fire is another strategy which is more like batch firing because no cam sensor is fitted, so injector firing cannot be timed to occur while the valve is open and port air flow is established. Part of the fuel may be injected on a closed valve and part on an open valve.

In dyno testing at high throttle and rpm, there is no difference in power between any of the 3 basic strategies. We had one of our race engine builder clients in Okinawa put the same Nissan SR20DET engine on his engine dyno with SDS and Motec EMSs on the same day since he was a dealer/ tuner for both brands. The result was that the engine pulled the same power, ± 2hp in each instance on this 500hp engine. Other people have found the same result in their dyno testing.

Sequential is superior for low rpm/ low load emissions- which is what it was developed for. Since aircraft engines don’t spend much time at low rpm and MAP and emissions are not a concern. We don’t consider that sequential is of benefit here, given the extra complexity.

Sequential, in most instances, becomes not timed to the valve open period at high MAP/ RPM anyway because there is not enough time to get all the fuel into the port during that time span. Under these conditions, the system must start spraying fuel on a closed valve. This is the main reason why there are no power gains at high rpm over batch or semi sequential firing.

To realize the full potential of sequential injection, you'd have to dyno the engine to determine when to start and stop the injector open period. You can’t really guess at this. This adds another layer of complexity.

For best power, all that has to happen is that the air/ fuel ratio is optimal and the spark timing is in the right place for peak cylinder pressure to occur at the most advantageous crankpin angle.

Interestingly, one of our Reno race clients was told by the Motec dealer (he was considering both SDS and Motec on advice of his engine builder) that you couldn’t trim the fuel amount to each cylinder individually without a cam sensor. That’s interesting, but not true with SDS, since we’ve been doing it since 2016… All you need is one drive transistor per injector. He went with SDS after seeing Andy Findlay win Sport class last year with the EM-5 system. Motec could be forgiven for this erroneous advice since they don't know SDS any more than I know their system.

In the end, the intake valve lets the fuel/air mixture into the cylinder to be ignited at the right time and injection strategies don’t matter much on aircraft applications.
 
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Thank you for taking the time to provide these educational insights, Ross. While I don't fly your injection or ignition products I very much appreciate your generous sharing of knowledge.
 
Part 2, Injector Mounting

So that now we understand a bit more about how the injectors are pulsed, how should they be mounted?

On aircraft engines, we mount injectors both in the induction tubes and cylinder ports depending on the engine type and application. Both locations work fine. Port mounting improves cold starting and cold throttle response slightly on Lycoming engines. In all cases, we face the injector nozzle towards the port as all OEMs do. Tube mounting may show some hp gains at very high fuel flow rates or when using methanol fuels due to less charge stratification since there is more time to mix the fuel and air prior to the charge entering the chamber.

Some other EFI systems mounted the injectors in the induction tubes but faced the nozzles away from the port. As you’d expect, this resulted in degraded cold start and throttle response since the fuel traveled the wrong way down the tube for some distance before reversing direction- especially so on a Lycoming with updraft induction tubes. Gravity wasn’t friendly here, especially during cold starting, pulling liquid fuel down the runner rather than towards the valve.

Now we see people switching this system over to one with the injector port mounted, claiming improved starting and low rpm running. No magic here, the injector is just pointed where it should be and we’d expect that result.



SDS induction tube mounted injector

Where in the port is the best place to have that injector installed?

We see 2 possibilities on Lycoming engines-

1. In the OEM injector port on the top of the cylinder
2. In the primer port on the bottom of the cylinder

Both locations point the injector spray at the back of the valve. That’s good.

Top mounting has the advantage of gravity aiding fuel movement during cranking when airflow is low with closed throttle.

Top mounting allows the injector to run cooler on downdraft cooling systems like RVs use since the air in the upper plenum is essentially ambient. That’s good to minimize the chances of fuel boiling. We also found in testing by Dave Anders, that the injectors stayed cooler after hot shutdown than lower mounted ones. His testing with thermocouples on the injector housings showed a max temp of 174F after 10 minutes with the heads at about 280F on shutdown so the injectors didn't get anywhere near as hot as the heads. With the lower mounted ones, he was seeing about 260F which is right at the published limit for the injectors.

In flight, where the engine spends most of its time, injector temps were 150-200F cooler with the top mount injectors compared to lower head mounting as they're bathed in ambient air rather than air passing through the head finning and adjacent to the 1200F+ exhaust stacks.



Top mount placement on an AV cylinder

Most of our systems since 2016, use top mount, narrow spray pattern injectors given the advantages demonstrated above although at least one user did mount them in the primer ports and they work fine in that location too. In all cases of downdraft cooling though, be aware that the injectors will operate at higher temperatures when mounted on the bottom of the engine.



1/8 NPT angle valve mount

For updraft cooling as some canard designs use, we prefer to tube mount or bottom mount to keep the injectors as cool as possible in flight which is most important in our view. Some race applications must use high flow, wide spray pattern injectors and these are not suitable for use with thread-in 1/8NPT injector mounts as the spray pattern impinges on the small ID adapter bore. For all out race applications, we can supply a 1/4 NPT mount which allows the use of a high flow, wide pattern injector however, you'd have to enlarge the injector port from 1/8 NPT to 1/4 NPT.



1/4 NPT AV race injector mount

All our thread-in mounts use a proprietary material with 190,000 psi tensile strength for the lower portion. We don't feel traditional 304/316 SS or 7075-T6 has adequate strength or fatigue resistance to be used here.
 
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Ross;
My question does have the word "injector" in it, but couldn't find a different thread to resurrect.

Does the injector relay box run hot? I was looking where to mount it, and my number one choice right now is right to the top of the ECU box. I will use standoffs if heat is an issue.
 
No, the relays are in the relaxed position in normal or primary modes, no current flow through them.

In activated backup mode, no noticeable heat either so fine to mount them on top of the ECU.

BTW, the ECU doesn't generate any significant heat either so does not need any form of cooling air past it. Ambient cockpit air is fine. I wouldn't mount it to the back side of an uninsulated firewall however.
 
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