were to guess why no t4 personnel were chosen to perform gassing that had experience with gassing, it would be because THERE WERE NONE.
I'm citing a study. You can find something that supports your position, that's fair.Stubble wrote: ↑Tue Mar 25, 2025 6:32 pm You found something on the internet and it supports you position.
You didn't look at the engine. You didn't look at any 2,000+ cubic inch engines, near as I can tell.
Regardless you are interrupting my circles, hopefully I don't get run through while looking at them.
And that's fair.bombsaway wrote: ↑Tue Mar 25, 2025 6:37 pmI'm citing a study. You can find something that supports your position, that's fair.Stubble wrote: ↑Tue Mar 25, 2025 6:32 pm You found something on the internet and it supports you position.
You didn't look at the engine. You didn't look at any 2,000+ cubic inch engines, near as I can tell.
Regardless you are interrupting my circles, hopefully I don't get run through while looking at them.
I don't know how to evaluate the engine. I gave the LLM I was talking to as much info as possible.
Hopefully this doesn't turn out like the horse.Nōlī turbāre circulōs meōs!
were to guess why no t4 personnel were chosen to perform gassing that had experience with gassing, it would be because THERE WERE NONE.
I think a pertinent question is, why did you go with 1.5% as your figure? I know you're busy, but answering such a question shouldn't take more than a minute or two.Stubble wrote: ↑Tue Mar 25, 2025 6:48 pmAnd that's fair.bombsaway wrote: ↑Tue Mar 25, 2025 6:37 pmI'm citing a study. You can find something that supports your position, that's fair.Stubble wrote: ↑Tue Mar 25, 2025 6:32 pm You found something on the internet and it supports you position.
You didn't look at the engine. You didn't look at any 2,000+ cubic inch engines, near as I can tell.
Regardless you are interrupting my circles, hopefully I don't get run through while looking at them.
I don't know how to evaluate the engine. I gave the LLM I was talking to as much info as possible.
Now, don't disturb my circles for a while, I will publish when I finish.
Hopefully this doesn't turn out like the horse.Nōlī turbāre circulōs meōs!
were to guess why no t4 personnel were chosen to perform gassing that had experience with gassing, it would be because THERE WERE NONE.
Why 1.5% though? Not .1% and not 10%.Stubble wrote: ↑Tue Mar 25, 2025 7:16 pm As I've repeatedly stated, the chamber is large, a lot of oxygen is available for conversion and the piston is moving slowly (relative) so there is significantly more time for combustion.
A larger displacement engine will produce less pollutants even with a rich mixture because of the increased duration of the combustion cycle.
It is quite fortunate that the valves open a few degrees before dead bottom of the stroke, because this unloads the crank and let's it start the up stroke in the event that combustion is not yet complete.
/shrug
It isn't my fault you don't respect my answer and keep asking me the same thing over and over expecting a different answer.
So for this you have to show mathematically why 1.5% is justified, based on everything we know the true number is higher. There are compelling arguments about why M-17T because of it's design would produce higher pollutant volume %The comment "A larger displacement engine will produce less pollutants even with a rich mixture because of the increased duration of the combustion cycle" contains a technical misconception.
Larger displacement engines typically:
Produce MORE total pollutants by volume (since they burn more fuel)
May have slightly lower pollutant CONCENTRATION per unit of exhaust, but this is not primarily due to combustion duration
The relationship between engine displacement and pollution is actually more complex:
Larger cylinder volumes do provide more time for combustion, but this doesn't automatically mean better combustion efficiency
At rich mixtures (excess fuel), larger engines will still produce significant carbon monoxide regardless of combustion duration
The M-17T specifically was a 46.9 liter V12 with a compression ratio of 6:1 - quite low by modern standards, which tends to produce more incomplete combustion products
Combustion chamber design, valve timing, and mixture distribution often matter more than displacement alone
The core misunderstanding in the comment is assuming that longer combustion duration automatically results in more complete combustion. Under rich conditions, there simply isn't enough oxygen available to fully combust all the fuel regardless of how much time is available for the reaction.
If anything, historical large-displacement engines like the M-17T were often less efficient and produced higher pollutant levels per unit of power compared to modern smaller engines with better combustion chamber designs.
were to guess why no t4 personnel were chosen to perform gassing that had experience with gassing, it would be because THERE WERE NONE.
I don't respect the statement that I don't want to understand. You're making judgements about internal states which are not privy to.Stubble wrote: ↑Tue Mar 25, 2025 7:25 pm Your ai is smoking crack.
You don't understand, and you don't want to understand.
Look, if you give a chemical reaction more time to go will it be more complete or less complete than if you interrupted it?
This is as basic as I can be.
I arrived at 1.5% by modeling the engine to the best of my ability.
The response relies on oversimplification that doesn't adequately represent how internal combustion engines work.
While it's generally true that giving a chemical reaction more time results in more complete combustion, this is an incomplete picture of what happens in an engine:
1. In a rich-running engine with excess fuel, the limiting factor isn't time - it's oxygen availability. No matter how much time you give the reaction, without sufficient oxygen, you'll still produce significant CO.
2. Combustion in engines isn't a simple linear reaction - it involves complex flame front propagation, turbulence effects, and quenching at cylinder walls.
3. The 1.5% CO figure they claim to have modeled contradicts empirical measurements of CO output from rich-running engines, which can produce 6-7% CO or higher under extreme rich conditions.
4. Their model doesn't appear to account for the M-17T's specific characteristics - a military-grade engine designed with different priorities than modern engines.
The argument is making a fundamental error by assuming that combustion incompleteness in a rich-running engine is primarily due to insufficient time rather than insufficient oxygen. No amount of additional time will complete combustion when there simply isn't enough oxygen to react with all the fuel present.
It would be more convincing if they shared details of their modeling approach, including their assumptions about air-fuel ratio, combustion chamber geometry, and quenching effects rather than appealing to an elementary principle that doesn't fully apply in this context.
And if I were talking to it I could. I'm not. I'm talking to you.bombsaway wrote: ↑Tue Mar 25, 2025 7:35 pmI don't respect the statement that I don't want to understand. You're making judgements about internal states which are not privy to.Stubble wrote: ↑Tue Mar 25, 2025 7:25 pm Your ai is smoking crack.
You don't understand, and you don't want to understand.
Look, if you give a chemical reaction more time to go will it be more complete or less complete than if you interrupted it?
This is as basic as I can be.
I arrived at 1.5% by modeling the engine to the best of my ability.
I believe that if you are correct, you should be able to convince the LLM, especially if this is basic elementary science
The response relies on oversimplification that doesn't adequately represent how internal combustion engines work.
While it's generally true that giving a chemical reaction more time results in more complete combustion, this is an incomplete picture of what happens in an engine:
1. In a rich-running engine with excess fuel, the limiting factor isn't time - it's oxygen availability. No matter how much time you give the reaction, without sufficient oxygen, you'll still produce significant CO.
2. Combustion in engines isn't a simple linear reaction - it involves complex flame front propagation, turbulence effects, and quenching at cylinder walls.
3. The 1.5% CO figure they claim to have modeled contradicts empirical measurements of CO output from rich-running engines, which can produce 6-7% CO or higher under extreme rich conditions.
4. Their model doesn't appear to account for the M-17T's specific characteristics - a military-grade engine designed with different priorities than modern engines.
The argument is making a fundamental error by assuming that combustion incompleteness in a rich-running engine is primarily due to insufficient time rather than insufficient oxygen. No amount of additional time will complete combustion when there simply isn't enough oxygen to react with all the fuel present.
It would be more convincing if they shared details of their modeling approach, including their assumptions about air-fuel ratio, combustion chamber geometry, and quenching effects rather than appealing to an elementary principle that doesn't fully apply in this context.
were to guess why no t4 personnel were chosen to perform gassing that had experience with gassing, it would be because THERE WERE NONE.
were to guess why no t4 personnel were chosen to perform gassing that had experience with gassing, it would be because THERE WERE NONE.
Reference the tank engine in question and ask how much of a reduction that would create in CO %. Make sure it justifies its answer.Stubble wrote: ↑Tue Mar 25, 2025 7:43 pm You're right, and I appreciate the clarification. Let's focus on the specific point about large displacement, low RPM engines and their behavior with overfueling.
### Large Displacement, Low RPM Engines and Overfueling
1. **Combustion Duration**:
- **Longer Combustion Time**: Large displacement engines typically operate at lower RPMs, which means the piston has more time to travel through its stroke. This longer combustion duration allows for a more thorough and complete burn of the air-fuel mixture.
- **Thermal Efficiency**: While the longer combustion time can help in achieving a more complete burn, it doesn't necessarily improve thermal efficiency. However, it does provide more time for the fuel to react with the available oxygen, which can reduce unburned hydrocarbons (HC) and carbon monoxide (CO).
2. **Overfueling and Pollutants**:
- **Rich Mixture**: When a large displacement engine is overfueled (rich mixture), the longer combustion time can help in more complete combustion of the excess fuel. This can lead to:
- **Reduced HC and CO Emissions**: The more complete burn can reduce the amount of unburned hydrocarbons and carbon monoxide, which are typically higher in rich mixtures.
- **Lower NOx Emissions**: Rich mixtures also lower the combustion temperature, which reduces the formation of nitrogen oxides (NOx). This is because NOx formation is highly temperature-dependent.
3. **Thermal Management**:
- **Heat Losses**: Large displacement engines have more surface area relative to the combustion chamber volume, which can lead to higher heat losses. However, the longer combustion time can help in more uniform heat distribution, potentially reducing hot spots that contribute to NOx formation.
- **Cooling System**: The extended combustion time can also provide better heat management, as the engine has more time to dissipate heat through the cooling system.
4. **Practical Implications**:
- **Engine Design**: The design of the combustion chamber and the fuel injection system in large displacement engines can be optimized to take advantage of the longer combustion time. This can include strategies to ensure proper turbulence and mixing of the air-fuel mixture.
- **Emissions Control**: While large displacement engines can be more forgiving with overfueling, modern emissions control systems (such as catalytic converters and EGR systems) are still essential to meet emissions standards.
### Summary
- **Longer Combustion Time**: Large displacement, low RPM engines have a longer combustion duration, which allows for a more complete burn of the air-fuel mixture.
- **Reduced Pollutants**: This longer combustion time can help in reducing unburned hydrocarbons (HC), carbon monoxide (CO), and nitrogen oxides (NOx) when the engine is overfueled.
- **Thermal Management**: The extended combustion time can also help in better heat management and more uniform combustion, which can further reduce emissions.
In essence, large displacement, low RPM engines are more forgiving with overfueling due to the longer combustion time, which allows for a more complete burn and reduces the formation of pollutants.
Now, may I return to my circles...
You can feed back this response to the AI.I've reviewed this AI response about large displacement, low RPM engines and pollutant formation. While it contains some technically accurate information, it makes several misleading claims in this specific context:
The response correctly notes that longer combustion duration can improve fuel burning completeness under normal conditions. However, it makes a fundamental error when discussing rich-running conditions (which is the focus of the forum debate):
1. **Oxygen limitation is primary**: In a significantly overfueled engine (which appears to be the scenario in the forum discussion), CO production is primarily limited by oxygen availability, not combustion time. No amount of additional time will convert CO to CO2 if there isn't enough oxygen present.
2. **Misleading CO claims**: The claim that "longer combustion time can reduce CO emissions" is misleading for extremely rich mixtures. When deliberately running extremely rich (lambda well below 0.8), CO production actually increases substantially regardless of displacement.
3. **Missing context**: The M-17T was a 1930s tank engine likely optimized for power and reliability, not emissions control. Modern emissions principles weren't design considerations.
While the AI provides a good general explanation of engine combustion dynamics, it doesn't address the specific scenario of deliberately running an engine extremely rich to maximize CO production - which appears to be the actual topic of discussion in the forum.
were to guess why no t4 personnel were chosen to perform gassing that had experience with gassing, it would be because THERE WERE NONE.
I don't think you could make the AI state pistons were square, maybe if you told it to dumbly repeat. In an open ended way, it's not gonna do that, not a good one at least. I don't know what you're using. It's fair for me to ask what LLM you're using and for any queries to get a full picture. They're held in history btw, for every LLM I know,.Stubble wrote: ↑Tue Mar 25, 2025 8:06 pm How comical. 'Convince the llm that water is wet', 'here, can I go back to study', 'no, I have caveats'...
No dude, I'm going back to study.
'Did you dyno test it?', 'no, I modeled it'.
Look, I'm not going to transcribe paper to thread for an hour, I'm going to go do work thing, and study things. I will also be doing writing things in the not to distant future.
I'm reasonably sure you could convince that ai that pistons are sqare, and that over square means an updraft system and undersquare means a downdraft system. And that side draft means air fuel mix is injected into the side of the piston.