Will Atomized Kerosene Ignite with a Spark in Controlled Conditions?

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Discussion Overview

The discussion centers on whether atomized kerosene can ignite with a spark or plasma arc under controlled conditions, specifically within a stoichiometric ratio at pressures of 1-2 atm and temperatures of 15-45º C. Participants explore various ignition methods and conditions related to kerosene combustion, including comparisons to other fuels and historical applications.

Discussion Character

  • Exploratory
  • Technical explanation
  • Debate/contested
  • Historical

Main Points Raised

  • Some participants suggest that kerosene can ignite without a stoichiometric ratio due to combustion occurring on the surface of atomized droplets, similar to diesel engines.
  • Others argue that ignition methods like electric arcs are commonly used in jet engines, implying that such methods should work for atomized kerosene as well.
  • A participant mentions historical techniques used in tractors to ignite kerosene, indicating that heating the engine can facilitate ignition.
  • One participant proposes that using super-cooled liquid oxygen (LOX) with kerosene could enable ignition without a spark, referencing its use in space missions.
  • Another participant challenges the idea of kerosene being hypergolic with LOX, stating that ignition at cryogenic temperatures requires more powerful ignition sources than standard spark plugs.
  • Concerns are raised about the ignition energy required for kerosene in gas turbine engines, highlighting the need for high-energy spark sources.

Areas of Agreement / Disagreement

Participants express multiple competing views regarding the ignition of atomized kerosene, with no consensus reached on the necessity of a spark or the conditions under which ignition can occur.

Contextual Notes

Some claims depend on specific conditions, such as temperature and pressure, and there are unresolved questions about the effectiveness of different ignition methods and the role of stoichiometric ratios in combustion.

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Will atomized kerosene (that is, kerosene as mist in air), with a proper stoichiometric ratio in an environment of 1-2 atm and 15-45º C, ignite via a spark/plasma arc?

I know kerosene generally has to be in a warm environment to ignite, but I am trying to figure out a way to get around that (if you have any ideas, please let me know).

Thanks a lot!
 
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Yep. Blew up a house that way when I was a kid. Made a great fuel air bomb, but I was too young to understand what one of those was at the time.

You do not need a stoichiometric ratio because burning happens on the surface of each atomized droplet. This is why you can run a diesel engine with fuel/air mixtures far less than stoichiometric, since diesel fuel and kerosene are exactly the same thing for the purposes of this discussion. (Not the same thing for other discussions.)

Since gasoline burns as a vapor and not as an atomized mist, that must be near stoichiometric.
 
Sounds as if your trying to start a jet engine.
 
My thoughts were similar to Jobrag. When I saw the title of the thread I said to myself: Let's hope so, otherwise there are a lot of jet airplanes in trouble. An electric arc is a very very common way to ignite fuel oil.
 
Pkruse said:
Yep. Blew up a house that way when I was a kid. Made a great fuel air bomb, but I was too young to understand what one of those was at the time.

You do not need a stoichiometric ratio because burning happens on the surface of each atomized droplet. This is why you can run a diesel engine with fuel/air mixtures far less than stoichiometric, since diesel fuel and kerosene are exactly the same thing for the purposes of this discussion. (Not the same thing for other discussions.)

Since gasoline burns as a vapor and not as an atomized mist, that must be near stoichiometric.

That's interesting, thanks.
Jobrag said:
Sounds as if your trying to start a jet engine.

Yeah. In model jet turbine engines, fuel is, as far as I can tell, always vaporized through tubes inside the combustion chamber. This makes it so that the engine must be hot to run on kerosene (so it's usually started on propane then switched to kerosene), and I believe it's also less efficient. I'm hoping to use 2 or 3 micro atomizers to get the job done, and hopefully I can get it to work.
 
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i read a post here,

i'm trying to get to the guy that asked a question how to ignite kerosene 40 deg. c .

i'am neither a chemist nor physicist.. i am an ad-hock professor..

the solution is simple, and you don't even need a "spark" the apollo missions did it all the time, insertion into lunar orbit and lunar exit.. but it has to be done without nitrogen (which we breathe 75% +15% oxygen + the others) so we need the vacuum and cold of space to get it done... that's why it works out there.. and it's very cold.

it's LOX(super cold liquid oxygen) and kerosene... mix it correctly, it just works! no spark needed!
we used LOX plus near frozen Hydrogen on the space shuttle missions..
[RIP challenger 86' and Columbia 03']

the great physicist, Michio Kaku once said "..we cannot get off this planet without being a tier 1 hydrogen, society.."

i say lets get it done already!!
 
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guss said:
Will atomized kerosene (that is, kerosene as mist in air), with a proper stoichiometric ratio in an environment of 1-2 atm and 15-45º C, ignite via a spark/plasma arc?
This is an old farmer cost reduction scheme. Kerosene was cheaper than gasoline, so they had an incentive to run tractors on kerosene. The technique was to put a blanket over the radiator, run the tractor hard until the water started to boil, then switch to kerosene. It worked on the low compression engines of early tractors, and as long as the water kept boiling.

This is from my father, who left the farm as soon as he was old enough, and never looked back.
 
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darrinburr said:
i read a post here,

i'm trying to get to the guy that asked a question how to ignite kerosene 40 deg. c .

i'am neither a chemist nor physicist.. i am an ad-hock professor..

the solution is simple, and you don't even need a "spark" the apollo missions did it all the time, insertion into lunar orbit and lunar exit.. but it has to be done without nitrogen (which we breathe 75% +15% oxygen + the others) so we need the vacuum and cold of space to get it done... that's why it works out there.. and it's very cold.

it's LOX(super cold liquid oxygen) and kerosene... mix it correctly, it just works! no spark needed!
we used LOX plus near frozen Hydrogen on the space shuttle missions..
[RIP challenger 86' and Columbia 03']

the great physicist, Michio Kaku once said "..we cannot get off this planet without being a tier 1 hydrogen, society.."

i say lets get it done already!!
… okay, wait…

Are you suggesting that kerosene is hypergolic with liquid oxygen?

That is completely incorrect. You can get it to be hypergolic with high-test hydrogen peroxide, but HTP is hypergolic with pretty much anything even remotely flammable.

At cryogenic temperatures, even spark ignition will not light off kerosene/LOX. That’s why they use tetra ethyl aluminum/tetraethylborane (TEAL/TEB) for ignition on the Merlin engines on the Falcon 9.

At ambient temperatures in a gas turbine engine, the spark required to ignite kerosene during startup is… powerful. The spark plug on your car will not cut it. You need a lot hotter spark than a traditional spark plug can provide. Usually you need a capacitive discharge igniter, and even the small ones run in the single digit joule range. The ones on airliners are easily 20+ joules and will straight up kill you on the spot if you accidentally discharge it through you.

Once you’re lit, though, whether on a gas turbine or a rocket engine, you no longer need an ignition source to maintain combustion. The constant flow nature of the engines means that there is always combustion occurring in the combustion chamber and you’re just adding fresh reactants. Piston engines running on kerosene get around the ignition source requirement by running high enough compression, and by extension high enough temperature, to cause autoignition of the fuel as it gets sprayed into the cylinder.
 
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