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Direct Injected UAV Diesel Engine

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Old 11-09-2006 | 08:28 AM
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Default Direct Injected UAV Diesel Engine

http://www.cosworth.com/news_detail.php?id=66
http://www.gizmag.com/go/5917/

Cool. I wonder what the government pays for one of these.

Old 11-09-2006 | 09:24 AM
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Default RE: Direct Injected UAV Diesel Engine

This is a remarkable achievement amd most likely the price will be too, Bottom line however is our current engines do well at a very reasonable prices the current fuel miixes when you figure economy of running them is not a major issue and as we know we have all given running and set up issues with compression and needle settings to help out the converts. I have my doubts with a lot of modlelers dealing with the possible complexity of this engine, and a hard landing would be curtains down, this does not in any way
degrade what they have done as I said remarkable. One a different note we have all seen the profusion on nice built up arfs that are great for converson to glow and small diesels
Even with the inroads of electric flight with its pros, cons, expense, it appears there is more intrest in diesel
Davis is cranking out more head conversions

I am still trying to upload his new head pix for the OS 10 anular ringed nice thumb screw compression adjustment
this is my next one martin
Old 01-10-2007 | 09:07 PM
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Default RE: Direct Injected UAV Diesel Engine

I have seen and held this engine. Having looked at the specifications I believe they still have qute a way to go. It is a beautiful engine, the machining is not as good as a DA and the weight is a bit more than what I hoped for before we recieved them. I see a couple of issues but I am not an engineer so what do I know. The head is held on by 4 bolts they apear to be about 3/16" and the RPM range is very limited. In order to effectivly use this engine a variable pitch prop will need to be developed.
They are headed in the right direction and as a first engine it is fine.
Steve
Old 01-10-2007 | 09:40 PM
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Default RE: Direct Injected UAV Diesel Engine

I wouldn't be concerned about the head bolts. If the RPM range is limited, that is typical of injected diesels. Can you share any of the specs on this engine?
Old 01-10-2007 | 10:15 PM
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Default RE: Direct Injected UAV Diesel Engine

I miss spoke the bolts which secure the head also hold down the cylinder.
I do not remember the rpm range but it has a huge prop, 20"+ and the rpm spread is about 3,000 min to max.
Steve
Old 01-11-2007 | 12:04 PM
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Default RE: Direct Injected UAV Diesel Engine

Steve, what is seen at left of the injector is a spark/glow plug?
ugo
Old 01-11-2007 | 03:35 PM
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Default RE: Direct Injected UAV Diesel Engine

The article didn't call this a Diesel. So I have to wonder about the direct injected part.
Old 01-11-2007 | 03:48 PM
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Default RE: Direct Injected UAV Diesel Engine

The article says "direct injection, compression ignition".
Old 01-16-2007 | 10:33 AM
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Default RE: Direct Injected UAV Diesel Engine

So why is it not a diesel. Could be the fuel is injected during the intake stroke? That is the part I was wondering about.
Old 01-16-2007 | 11:08 AM
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Default RE: Direct Injected UAV Diesel Engine

The definition of a "diesel" is: direct injection, compression ignition. It doesn't matter if they call it a diesel or not. Sometimes they choose not to call them diesel not to imply that it will only operate on "diesel fuel". Direct injection compression ignition engines can be deisgned to burn anything from bunker oil to kerosene to waste vegetable oil. Many will burn a range of those fuels. There is no such thing as a manifold fuel injected or carburated diesel in the full size world. Those types of engine are called HCCI.

http://en.wikipedia.org/wiki/Diesel_engine
http://en.wikipedia.org/wiki/HCCI
Old 01-16-2007 | 01:45 PM
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Default RE: Direct Injected UAV Diesel Engine

The definition of a "diesel" is: direct injection, compression ignition
No it must have near constant pressure. To do that fuel must be injected through most of its power stroke. There have been direct injected spark ignition, not sure of non diesel compression ignition. The compression may also have to be higher. To not use the Diesel name tells me somthing is amiss.
Old 01-16-2007 | 04:49 PM
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Default RE: Direct Injected UAV Diesel Engine

No it must have near constant pressure. To do that fuel must be injected through most of its power stroke.
The diesel cycle which you refer to is a theoretical thing. Most high speed diesels are not as near the ideal cycle as the huge low speed engines. What duration in crank angle degrees do you suppose fuel is injected into the cylinder? Do you have an example of a direct injection, compression ignition engine that is NOT a diesel? I have never seen such a thing. I would be curious. Direct injection always refers to injecting fuel into the combustion chamber.

http://www.answers.com/topic/diesel-engine
Old 01-16-2007 | 09:35 PM
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Default RE: Direct Injected UAV Diesel Engine

Yup - all direct injection or IDI compression ignition engines are diesels no matter whay they burn or what you call them..

I don't think there is any diesel that is constant pressure. I know people have tryed to do it.. There is no reason for that now days anyway. I'd say that all modern diesels ignite the fuel before top dead center and that causes a pressure spike that works well with the power stroke. The knock you hear in a diesel is a pressure spike.

There are plenty of IDI (inderect injection as in a pre chamber ) diesels out there as well.

Our little engines don't fit any catagory perfectly except internal combustion. But the compression ingnition part makes it fit the diesel catagory best in my opinoion.
Old 01-17-2007 | 03:06 PM
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Default RE: Direct Injected UAV Diesel Engine

Treven,
very few engines work approximating Diesel cycle, since it can performed only partly without very particular arrangements. The Diesel cycle can work with a glow plug, a simple hot head previously heated with ...a blacksmith forge, or simply ignite on the rise of temperature caused by adiabatic compression.
NO commercial engine work following true Diesel cycle, so their efficiency is lower than the exceptional one of Diesel cycle. In practice they all differ from the original idea by approximating the isothermal combustion-expansion phase of the original cycle by means of tricks, more or less efficient and simple.
Model engines, apart from remarkable exceptions to be counted on the fingers of one hand, are the roughest approximation of diesel cycle. They are HCCI engines, (Homogeneus Charge Compression Ignition) The combustion-expansion is in practice left to nature, renouncing to the control of the injection of the fuel DURING the combustion, that is THE ONLY peculiar characteristic of the diesel cycle.
It is a common practice to name "diesel" every engine with compression ignition, as you understand this is only an approximation, but this can lead to considerable disguise when using too far the similitude. WHAT IS THE COMBUSTION OF A TRUE DIESEL WILL NEVER HAPPEN IN A MODEL "DIESEL", so the best thing is to forgot verbal similitudes.
Old 01-17-2007 | 03:17 PM
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Default RE: Direct Injected UAV Diesel Engine

I don't think there is any diesel that is constant pressure.
Well they are. But not perfectly. Yes the modern high speed diesel is further from perfect than the large marine engines, but then they are even further from it when the injectors shorten their duration. But when the engine is at maximum power they are close enough to call it constant pressure. I think there have been some direct injection engines which were not Diesels in the past, but probably not presently. I think the old hot bulb oil engines used indirect injection or similar, but were injected during the intake cycle. There are also indirect injection Diesel engines which confuses the issue.
Old 01-17-2007 | 03:24 PM
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Default RE: Direct Injected UAV Diesel Engine


ORIGINAL: merugo

Treven,
very few engines work approximating Diesel cycle, since it can performed only partly without very particular arrangements. The Diesel cycle can work with a glow plug, a simple hot head previously heated with ...a blacksmith forge, or simply ignite on the rise of temperature caused by adiabatic compression.
NO commercial engine work following true Diesel cycle, so their efficiency is lower than the exceptional one of Diesel cycle. In practice they all differ from the original idea by approximating the isothermal combustion-expansion phase of the original cycle by means of tricks, more or less efficient and simple.
Model engines, apart from remarkable exceptions to be counted on the fingers of one hand, are the roughest approximation of diesel cycle. They are HCCI engines, (Homogeneus Charge Compression Ignition) The combustion-expansion is in practice left to nature, renouncing to the control of the injection of the fuel DURING the combustion, that is THE ONLY peculiar characteristic of the diesel cycle.
It is a common practice to name "diesel" every engine with compression ignition, as you understand this is only an approximation, but this can lead to considerable disguise when using too far the similitude. WHAT IS THE COMBUSTION OF A TRUE DIESEL WILL NEVER HAPPEN IN A MODEL "DIESEL", so the best thing is to forgot verbal similitudes.

Model Diesel engines are actually Otto cycle engines without the spark. The thermodynamics is the same near constant volume. They are constant volume only because the fuel burns extremely quick. While a Diesel engine is not truely 100% constant pressure, they are reasonably close, with the pressure staying fairly constant and winding down near the end. The injection is also usually delayed a bit, but most are near constant volume while the injector is injecting fuel. However modern engines will change the timing of the injector instead of changing the rate of fuel injected, especially near the end of the power stroke.
Old 01-17-2007 | 04:28 PM
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Default RE: Direct Injected UAV Diesel Engine

If it's not a diesel what is it?

We have:

Spark Igntion: carburated, manifold injected, or direct injected, but ignition source is always spark.
Compression Igntion: direct injection or indirect injection(prechamber). Ignition is due to injecting fuel into compressed air hot enough to ignite it. Timing is dependent on injection.
HCCI(homogenous combustion compression ignition): Carburated, manifold injected, direct injected. Ignition is due to compression of fuel/air mixture and timing is dependent on lambda, compression ratio, and a variety of other factors.
There are also mixed mode HCCI engines. that switch between HCCI and spark ignition or HCCI and direct injection compression ignition.

Model engines (glow and diesel) most definitely fall into the HCCI category.

http://en.wikipedia.org/wiki/HCCI
Old 01-17-2007 | 04:45 PM
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Default RE: Direct Injected UAV Diesel Engine

I was just wondering why they didn't use the term Diesel. Seems to me it would have been a plus.
Old 01-17-2007 | 04:56 PM
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Default RE: Direct Injected UAV Diesel Engine

I think it's to make it clear that it will run on fuels other than DF2.
Old 01-17-2007 | 07:52 PM
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Default RE: Direct Injected UAV Diesel Engine

This is a compression ignition diesel. here are some of the specs for the engine.


Weight 3.8 Kg
HP 3.5 HP
RPM range 3500 RPM Min / 5100RPM Max.
Prop specifications 27-10
Max RPM 5000 Max.
This engine is being evaluated in Tazmania with results to follow.
Steve

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