Fellow PJ enthusiasts:
This is to announce that I have been successful in converting my Kentfield 4-tube engine to run on liquid fuel; I have operated on both gasoline and Jet-A.
The character of the engine's operation is much more aggressive, with the combustion events having a much sharper individual sound (presumably this is the result of a higher combustion rate).
I'm also getting data on fuel flow now (with a digital fuel-flow meter); I can tell you (Graham) that it appears I'm getting a degree of pressure modulation; even with a supply pressure of 65-70 PSIG the modulation appears to be on the order of 25% of flow rating. Max fuel flow so far is 10.5 gal/hr--not quite up to the max flow quoted by Kentfield. Nozzle rating related to fuel pressure is a big factor here, and I've been through several changes already.
Nozzle location is critical, and I need to further refine my installation.
Start-up procedures also need further refining, but (with a little help) I think the solution is in hand. Further experimentation required.
The whole system is more complex than I had originally envisioned, but not excessively so. For anybody interested in trying to get a more advanced system up-and-running, I can assure you there's a lot of effort involved!
Bill H.
Acoustic Propulsion Concepts, Inc.
liquid-fuel success!
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Bill,
Awesome work. Details and pictures?
Chris
Awesome work. Details and pictures?
This is my main reason for wanting to run our big engines with liquid. More bang!The character of the engine's operation is much more aggressive, with the combustion events having a much sharper individual sound (presumably this is the result of a higher combustion rate).
Chris
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Re: liquid-fuel success!
Your the first person to confirm that level of modulation in the fuel supply line Bill but it does not surprise me (Graham and Nick Too:-)hinote wrote:Fellow PJ enthusiasts:
This is to announce that I have been successful in converting my Kentfield 4-tube engine to run on liquid fuel; I have operated on both gasoline and Jet-A.
The character of the engine's operation is much more aggressive, with the combustion events having a much sharper individual sound (presumably this is the result of a higher combustion rate).
I'm also getting data on fuel flow now (with a digital fuel-flow meter); I can tell you (Graham) that it appears I'm getting a degree of pressure modulation; even with a supply pressure of 65-70 PSIG the modulation appears to be on the order of 25% of flow rating. Max fuel flow so far is 10.5 gal/hr--not quite up to the max flow quoted by Kentfield. Nozzle rating related to fuel pressure is a big factor here, and I've been through several changes already.
Nozzle location is critical, and I need to further refine my installation.
Start-up procedures also need further refining, but (with a little help) I think the solution is in hand. Further experimentation required.
The whole system is more complex than I had originally envisioned, but not excessively so. For anybody interested in trying to get a more advanced system up-and-running, I can assure you there's a lot of effort involved!
Bill H.
Acoustic Propulsion Concepts, Inc.
Viv
"Sometimes the lies you tell are less frightening than the loneliness you might feel if you stopped telling them" Brock Clarke
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Monsieur le commentaire
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