Why are engines with carburetors hard to start in cold weather?When is pre-heating a piston engine important, and how does one pre-heat correctly?Why are updraft carburetors standard in aviation?Why are Inline Engines more commonly used than Radial Engines?What may be the cause of hot start problems in a Lycoming fuel injected engine?Why are piston engines for aircraft rarely diesel powered?Why are some fuel-injected engines started with the mixture at idle cut-off?Why isn't the application of “carb heat” in initial piston multi-engine failure emergency procedures?How do carbureted and fuel injected engines compare in high altitude?Why are two-stroke engines nearly unheard of in aviation?
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Why are engines with carburetors hard to start in cold weather?
Why are engines with carburetors hard to start in cold weather?
When is pre-heating a piston engine important, and how does one pre-heat correctly?Why are updraft carburetors standard in aviation?Why are Inline Engines more commonly used than Radial Engines?What may be the cause of hot start problems in a Lycoming fuel injected engine?Why are piston engines for aircraft rarely diesel powered?Why are some fuel-injected engines started with the mixture at idle cut-off?Why isn't the application of “carb heat” in initial piston multi-engine failure emergency procedures?How do carbureted and fuel injected engines compare in high altitude?Why are two-stroke engines nearly unheard of in aviation?
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$begingroup$
Why are engines with carburetors hard to start in cold weather?
And why is there a different procedure for hot start scenarios, after you've just shut down the engine and want to power up again?
piston-engine
$endgroup$
add a comment
|
$begingroup$
Why are engines with carburetors hard to start in cold weather?
And why is there a different procedure for hot start scenarios, after you've just shut down the engine and want to power up again?
piston-engine
$endgroup$
add a comment
|
$begingroup$
Why are engines with carburetors hard to start in cold weather?
And why is there a different procedure for hot start scenarios, after you've just shut down the engine and want to power up again?
piston-engine
$endgroup$
Why are engines with carburetors hard to start in cold weather?
And why is there a different procedure for hot start scenarios, after you've just shut down the engine and want to power up again?
piston-engine
piston-engine
edited 4 hours ago
Pondlife
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54.5k12 gold badges155 silver badges319 bronze badges
asked 11 hours ago
Mike no smith Mike no smith
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3 Answers
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active
oldest
votes
$begingroup$
They are all harder to start in the cold, fuel injected engines included, and need an over-rich mixture for starting. The rich mixture is required because a lean one is harder for a spark to light off if the fuel/air charge is cold.
Now, it's still cold outside after the engine warms up, so the air charge is still cold, initially, but on a warm engine it gets heated as it extracts heat from the intake passage, valve and cylinder head on its way into the combustion chamber (and on Lycomings, the carburetor, which is bolted directly to the oil sump).
Carbureted aircraft engines use primer systems instead of chokes, as mentioned in AEhere's answer, because it's undesirable to have that sort of obstruction device in the intake passage. The primer injects raw fuel at the intake port using a syringe type hand pump, most of which settles on the intake passage walls and runs down the tubes a bit, and sits there slowly evaporating, and when the engine cranks, the vapours add to the fuel normally drawn at the carburetor. It does this for a period of time after the engine starts depending on how much prime you used.
Fuel injected aircraft engines are primed the same way, but since there are injectors already there at the intake port they don't require a separate primer system. You just turn on the fuel pump with the mixture rich for x seconds and it injects raw fuel just like a primer system.
Carbureted aircraft engines also use a slightly richer than necessary setting in the idle circuit to help them run better when cold. That's why you get a little rpm rise when pulling idle cutoff.
You can have too little primer fuel when starting, or too much, and it varies widely depending on the engine, its temperature, and the air temperature, so you have to learn how much is enough on each engine type. A typical protocol is:
- On a cold engine in warm weather, you might use 4 strokes of prime.
- On a cold engine in cold weather, you might use 6 to 8 strokes of prime.
- On a warm engine in cold weather, you might use 1 or 2 strokes of prime.
- On a warm engine in warm weather, or a hot engine you just shut down, you usually don't need any prime, but may use a little half-shot of prime, or, if the carb has an accelerator pump, a short stroke or two of throttle applied while cranking (to avoid fuel running down into the air box since throttle pumping sprays extra fuel from the accelerator pump right at the carb, and if the engine backfires with fuel in the airbox you can have an intake fire).
Different engine models have different starting quirks, and different primers have varying fuel volumes per stroke. It's something you learn on that engine type, along with whatever other unique characteristics of a particular aircraft you have to be aware of.
$endgroup$
$begingroup$
Also fuel injected engines (at least automotive ones - I've never dealt with an aviation one) have electronic systems that supply exactly the right amount of fuel for a given temperature, rather than just a rule of thumb X strokes of prime.
$endgroup$
– jamesqf
5 hours ago
$begingroup$
Yes aircraft engines of the traditional type are basically like 1930s tractor engines, complete with magneto ignition, except for being air cooled and much lighter. However, the "crudeness" of these engines is a plus when your life depends on them, and the theoretical loss of efficiency of not having the latest features is just not that big a deal. For example, to use an EFI system on an airplane using solid state electronics you have to use an architecture with zero single points of failure, which means two of everything all the way up to the power source. Then try to certify it.
$endgroup$
– John K
4 hours ago
add a comment
|
$begingroup$
Carburetors don't work as well in cold conditions because they themselves tend to cool the air as it flows through the Venturi tube, compounding the issue of cold intake air and cold fuel.
From Wikipedia:
When the engine is cold, fuel vaporizes less readily and tends to condense on the walls of the intake manifold, starving the cylinders of fuel and making the engine difficult to start; thus, a richer mixture (more fuel to air) is required to start and run the engine until it warms up. A richer mixture is also easier to ignite.
To provide the extra fuel, a choke is typically used; this is a device that restricts the flow of air at the entrance to the carburetor, before the venturi. With this restriction in place, extra vacuum is developed in the carburetor barrel, which pulls extra fuel through the main metering system to supplement the fuel being pulled from the idle and off-idle circuits. This provides the rich mixture required to sustain operation at low engine temperatures.
To put it in simple terms, carburetors create a combustible fuel air mixture by letting fuel evaporate into a stream of air in more or less controlled conditions. To do this, they reduce the pressure of the air by forcing it through a Venturi tube; this facilitates fuel evaporation.
An undesirable side effect of the process to reduce the air stream pressure is a drop in temperature. A lower temperature makes it harder to vaporize the fuel, and if the intake air and fuel are already colder than usual, the resulting mixture might be too lean to burn.
This is countered via special cold start devices such as chokes, manual mixture control and heaters. Of course if the engine is already hot, having been shut down recently, it might be able to restart without such contrivances. Keep in mind, however, that the carburetors will usually cool much faster than the engine block, being smaller often exposed to more airflow, and all it takes is for them to cool down to impede a restart.
$endgroup$
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$begingroup$
Hot starts are sometimes difficult on fuel injected engines because the engine heat will boil the fuel in the fuel lines, creating a vapor lock. Fuel pumps are designed to pump liquid fuel, not fuel vapor.
Look at your POH hot start procedure. Usually this involves running the fuel pump to move liquid fuel into the lines, flushing out the fuel vapor, and in most cases flooding the engine as well. Then the flooded start procedure must be used.
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3 Answers
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active
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3 Answers
3
active
oldest
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$begingroup$
They are all harder to start in the cold, fuel injected engines included, and need an over-rich mixture for starting. The rich mixture is required because a lean one is harder for a spark to light off if the fuel/air charge is cold.
Now, it's still cold outside after the engine warms up, so the air charge is still cold, initially, but on a warm engine it gets heated as it extracts heat from the intake passage, valve and cylinder head on its way into the combustion chamber (and on Lycomings, the carburetor, which is bolted directly to the oil sump).
Carbureted aircraft engines use primer systems instead of chokes, as mentioned in AEhere's answer, because it's undesirable to have that sort of obstruction device in the intake passage. The primer injects raw fuel at the intake port using a syringe type hand pump, most of which settles on the intake passage walls and runs down the tubes a bit, and sits there slowly evaporating, and when the engine cranks, the vapours add to the fuel normally drawn at the carburetor. It does this for a period of time after the engine starts depending on how much prime you used.
Fuel injected aircraft engines are primed the same way, but since there are injectors already there at the intake port they don't require a separate primer system. You just turn on the fuel pump with the mixture rich for x seconds and it injects raw fuel just like a primer system.
Carbureted aircraft engines also use a slightly richer than necessary setting in the idle circuit to help them run better when cold. That's why you get a little rpm rise when pulling idle cutoff.
You can have too little primer fuel when starting, or too much, and it varies widely depending on the engine, its temperature, and the air temperature, so you have to learn how much is enough on each engine type. A typical protocol is:
- On a cold engine in warm weather, you might use 4 strokes of prime.
- On a cold engine in cold weather, you might use 6 to 8 strokes of prime.
- On a warm engine in cold weather, you might use 1 or 2 strokes of prime.
- On a warm engine in warm weather, or a hot engine you just shut down, you usually don't need any prime, but may use a little half-shot of prime, or, if the carb has an accelerator pump, a short stroke or two of throttle applied while cranking (to avoid fuel running down into the air box since throttle pumping sprays extra fuel from the accelerator pump right at the carb, and if the engine backfires with fuel in the airbox you can have an intake fire).
Different engine models have different starting quirks, and different primers have varying fuel volumes per stroke. It's something you learn on that engine type, along with whatever other unique characteristics of a particular aircraft you have to be aware of.
$endgroup$
$begingroup$
Also fuel injected engines (at least automotive ones - I've never dealt with an aviation one) have electronic systems that supply exactly the right amount of fuel for a given temperature, rather than just a rule of thumb X strokes of prime.
$endgroup$
– jamesqf
5 hours ago
$begingroup$
Yes aircraft engines of the traditional type are basically like 1930s tractor engines, complete with magneto ignition, except for being air cooled and much lighter. However, the "crudeness" of these engines is a plus when your life depends on them, and the theoretical loss of efficiency of not having the latest features is just not that big a deal. For example, to use an EFI system on an airplane using solid state electronics you have to use an architecture with zero single points of failure, which means two of everything all the way up to the power source. Then try to certify it.
$endgroup$
– John K
4 hours ago
add a comment
|
$begingroup$
They are all harder to start in the cold, fuel injected engines included, and need an over-rich mixture for starting. The rich mixture is required because a lean one is harder for a spark to light off if the fuel/air charge is cold.
Now, it's still cold outside after the engine warms up, so the air charge is still cold, initially, but on a warm engine it gets heated as it extracts heat from the intake passage, valve and cylinder head on its way into the combustion chamber (and on Lycomings, the carburetor, which is bolted directly to the oil sump).
Carbureted aircraft engines use primer systems instead of chokes, as mentioned in AEhere's answer, because it's undesirable to have that sort of obstruction device in the intake passage. The primer injects raw fuel at the intake port using a syringe type hand pump, most of which settles on the intake passage walls and runs down the tubes a bit, and sits there slowly evaporating, and when the engine cranks, the vapours add to the fuel normally drawn at the carburetor. It does this for a period of time after the engine starts depending on how much prime you used.
Fuel injected aircraft engines are primed the same way, but since there are injectors already there at the intake port they don't require a separate primer system. You just turn on the fuel pump with the mixture rich for x seconds and it injects raw fuel just like a primer system.
Carbureted aircraft engines also use a slightly richer than necessary setting in the idle circuit to help them run better when cold. That's why you get a little rpm rise when pulling idle cutoff.
You can have too little primer fuel when starting, or too much, and it varies widely depending on the engine, its temperature, and the air temperature, so you have to learn how much is enough on each engine type. A typical protocol is:
- On a cold engine in warm weather, you might use 4 strokes of prime.
- On a cold engine in cold weather, you might use 6 to 8 strokes of prime.
- On a warm engine in cold weather, you might use 1 or 2 strokes of prime.
- On a warm engine in warm weather, or a hot engine you just shut down, you usually don't need any prime, but may use a little half-shot of prime, or, if the carb has an accelerator pump, a short stroke or two of throttle applied while cranking (to avoid fuel running down into the air box since throttle pumping sprays extra fuel from the accelerator pump right at the carb, and if the engine backfires with fuel in the airbox you can have an intake fire).
Different engine models have different starting quirks, and different primers have varying fuel volumes per stroke. It's something you learn on that engine type, along with whatever other unique characteristics of a particular aircraft you have to be aware of.
$endgroup$
$begingroup$
Also fuel injected engines (at least automotive ones - I've never dealt with an aviation one) have electronic systems that supply exactly the right amount of fuel for a given temperature, rather than just a rule of thumb X strokes of prime.
$endgroup$
– jamesqf
5 hours ago
$begingroup$
Yes aircraft engines of the traditional type are basically like 1930s tractor engines, complete with magneto ignition, except for being air cooled and much lighter. However, the "crudeness" of these engines is a plus when your life depends on them, and the theoretical loss of efficiency of not having the latest features is just not that big a deal. For example, to use an EFI system on an airplane using solid state electronics you have to use an architecture with zero single points of failure, which means two of everything all the way up to the power source. Then try to certify it.
$endgroup$
– John K
4 hours ago
add a comment
|
$begingroup$
They are all harder to start in the cold, fuel injected engines included, and need an over-rich mixture for starting. The rich mixture is required because a lean one is harder for a spark to light off if the fuel/air charge is cold.
Now, it's still cold outside after the engine warms up, so the air charge is still cold, initially, but on a warm engine it gets heated as it extracts heat from the intake passage, valve and cylinder head on its way into the combustion chamber (and on Lycomings, the carburetor, which is bolted directly to the oil sump).
Carbureted aircraft engines use primer systems instead of chokes, as mentioned in AEhere's answer, because it's undesirable to have that sort of obstruction device in the intake passage. The primer injects raw fuel at the intake port using a syringe type hand pump, most of which settles on the intake passage walls and runs down the tubes a bit, and sits there slowly evaporating, and when the engine cranks, the vapours add to the fuel normally drawn at the carburetor. It does this for a period of time after the engine starts depending on how much prime you used.
Fuel injected aircraft engines are primed the same way, but since there are injectors already there at the intake port they don't require a separate primer system. You just turn on the fuel pump with the mixture rich for x seconds and it injects raw fuel just like a primer system.
Carbureted aircraft engines also use a slightly richer than necessary setting in the idle circuit to help them run better when cold. That's why you get a little rpm rise when pulling idle cutoff.
You can have too little primer fuel when starting, or too much, and it varies widely depending on the engine, its temperature, and the air temperature, so you have to learn how much is enough on each engine type. A typical protocol is:
- On a cold engine in warm weather, you might use 4 strokes of prime.
- On a cold engine in cold weather, you might use 6 to 8 strokes of prime.
- On a warm engine in cold weather, you might use 1 or 2 strokes of prime.
- On a warm engine in warm weather, or a hot engine you just shut down, you usually don't need any prime, but may use a little half-shot of prime, or, if the carb has an accelerator pump, a short stroke or two of throttle applied while cranking (to avoid fuel running down into the air box since throttle pumping sprays extra fuel from the accelerator pump right at the carb, and if the engine backfires with fuel in the airbox you can have an intake fire).
Different engine models have different starting quirks, and different primers have varying fuel volumes per stroke. It's something you learn on that engine type, along with whatever other unique characteristics of a particular aircraft you have to be aware of.
$endgroup$
They are all harder to start in the cold, fuel injected engines included, and need an over-rich mixture for starting. The rich mixture is required because a lean one is harder for a spark to light off if the fuel/air charge is cold.
Now, it's still cold outside after the engine warms up, so the air charge is still cold, initially, but on a warm engine it gets heated as it extracts heat from the intake passage, valve and cylinder head on its way into the combustion chamber (and on Lycomings, the carburetor, which is bolted directly to the oil sump).
Carbureted aircraft engines use primer systems instead of chokes, as mentioned in AEhere's answer, because it's undesirable to have that sort of obstruction device in the intake passage. The primer injects raw fuel at the intake port using a syringe type hand pump, most of which settles on the intake passage walls and runs down the tubes a bit, and sits there slowly evaporating, and when the engine cranks, the vapours add to the fuel normally drawn at the carburetor. It does this for a period of time after the engine starts depending on how much prime you used.
Fuel injected aircraft engines are primed the same way, but since there are injectors already there at the intake port they don't require a separate primer system. You just turn on the fuel pump with the mixture rich for x seconds and it injects raw fuel just like a primer system.
Carbureted aircraft engines also use a slightly richer than necessary setting in the idle circuit to help them run better when cold. That's why you get a little rpm rise when pulling idle cutoff.
You can have too little primer fuel when starting, or too much, and it varies widely depending on the engine, its temperature, and the air temperature, so you have to learn how much is enough on each engine type. A typical protocol is:
- On a cold engine in warm weather, you might use 4 strokes of prime.
- On a cold engine in cold weather, you might use 6 to 8 strokes of prime.
- On a warm engine in cold weather, you might use 1 or 2 strokes of prime.
- On a warm engine in warm weather, or a hot engine you just shut down, you usually don't need any prime, but may use a little half-shot of prime, or, if the carb has an accelerator pump, a short stroke or two of throttle applied while cranking (to avoid fuel running down into the air box since throttle pumping sprays extra fuel from the accelerator pump right at the carb, and if the engine backfires with fuel in the airbox you can have an intake fire).
Different engine models have different starting quirks, and different primers have varying fuel volumes per stroke. It's something you learn on that engine type, along with whatever other unique characteristics of a particular aircraft you have to be aware of.
answered 9 hours ago
John KJohn K
43.2k1 gold badge78 silver badges149 bronze badges
43.2k1 gold badge78 silver badges149 bronze badges
$begingroup$
Also fuel injected engines (at least automotive ones - I've never dealt with an aviation one) have electronic systems that supply exactly the right amount of fuel for a given temperature, rather than just a rule of thumb X strokes of prime.
$endgroup$
– jamesqf
5 hours ago
$begingroup$
Yes aircraft engines of the traditional type are basically like 1930s tractor engines, complete with magneto ignition, except for being air cooled and much lighter. However, the "crudeness" of these engines is a plus when your life depends on them, and the theoretical loss of efficiency of not having the latest features is just not that big a deal. For example, to use an EFI system on an airplane using solid state electronics you have to use an architecture with zero single points of failure, which means two of everything all the way up to the power source. Then try to certify it.
$endgroup$
– John K
4 hours ago
add a comment
|
$begingroup$
Also fuel injected engines (at least automotive ones - I've never dealt with an aviation one) have electronic systems that supply exactly the right amount of fuel for a given temperature, rather than just a rule of thumb X strokes of prime.
$endgroup$
– jamesqf
5 hours ago
$begingroup$
Yes aircraft engines of the traditional type are basically like 1930s tractor engines, complete with magneto ignition, except for being air cooled and much lighter. However, the "crudeness" of these engines is a plus when your life depends on them, and the theoretical loss of efficiency of not having the latest features is just not that big a deal. For example, to use an EFI system on an airplane using solid state electronics you have to use an architecture with zero single points of failure, which means two of everything all the way up to the power source. Then try to certify it.
$endgroup$
– John K
4 hours ago
$begingroup$
Also fuel injected engines (at least automotive ones - I've never dealt with an aviation one) have electronic systems that supply exactly the right amount of fuel for a given temperature, rather than just a rule of thumb X strokes of prime.
$endgroup$
– jamesqf
5 hours ago
$begingroup$
Also fuel injected engines (at least automotive ones - I've never dealt with an aviation one) have electronic systems that supply exactly the right amount of fuel for a given temperature, rather than just a rule of thumb X strokes of prime.
$endgroup$
– jamesqf
5 hours ago
$begingroup$
Yes aircraft engines of the traditional type are basically like 1930s tractor engines, complete with magneto ignition, except for being air cooled and much lighter. However, the "crudeness" of these engines is a plus when your life depends on them, and the theoretical loss of efficiency of not having the latest features is just not that big a deal. For example, to use an EFI system on an airplane using solid state electronics you have to use an architecture with zero single points of failure, which means two of everything all the way up to the power source. Then try to certify it.
$endgroup$
– John K
4 hours ago
$begingroup$
Yes aircraft engines of the traditional type are basically like 1930s tractor engines, complete with magneto ignition, except for being air cooled and much lighter. However, the "crudeness" of these engines is a plus when your life depends on them, and the theoretical loss of efficiency of not having the latest features is just not that big a deal. For example, to use an EFI system on an airplane using solid state electronics you have to use an architecture with zero single points of failure, which means two of everything all the way up to the power source. Then try to certify it.
$endgroup$
– John K
4 hours ago
add a comment
|
$begingroup$
Carburetors don't work as well in cold conditions because they themselves tend to cool the air as it flows through the Venturi tube, compounding the issue of cold intake air and cold fuel.
From Wikipedia:
When the engine is cold, fuel vaporizes less readily and tends to condense on the walls of the intake manifold, starving the cylinders of fuel and making the engine difficult to start; thus, a richer mixture (more fuel to air) is required to start and run the engine until it warms up. A richer mixture is also easier to ignite.
To provide the extra fuel, a choke is typically used; this is a device that restricts the flow of air at the entrance to the carburetor, before the venturi. With this restriction in place, extra vacuum is developed in the carburetor barrel, which pulls extra fuel through the main metering system to supplement the fuel being pulled from the idle and off-idle circuits. This provides the rich mixture required to sustain operation at low engine temperatures.
To put it in simple terms, carburetors create a combustible fuel air mixture by letting fuel evaporate into a stream of air in more or less controlled conditions. To do this, they reduce the pressure of the air by forcing it through a Venturi tube; this facilitates fuel evaporation.
An undesirable side effect of the process to reduce the air stream pressure is a drop in temperature. A lower temperature makes it harder to vaporize the fuel, and if the intake air and fuel are already colder than usual, the resulting mixture might be too lean to burn.
This is countered via special cold start devices such as chokes, manual mixture control and heaters. Of course if the engine is already hot, having been shut down recently, it might be able to restart without such contrivances. Keep in mind, however, that the carburetors will usually cool much faster than the engine block, being smaller often exposed to more airflow, and all it takes is for them to cool down to impede a restart.
$endgroup$
add a comment
|
$begingroup$
Carburetors don't work as well in cold conditions because they themselves tend to cool the air as it flows through the Venturi tube, compounding the issue of cold intake air and cold fuel.
From Wikipedia:
When the engine is cold, fuel vaporizes less readily and tends to condense on the walls of the intake manifold, starving the cylinders of fuel and making the engine difficult to start; thus, a richer mixture (more fuel to air) is required to start and run the engine until it warms up. A richer mixture is also easier to ignite.
To provide the extra fuel, a choke is typically used; this is a device that restricts the flow of air at the entrance to the carburetor, before the venturi. With this restriction in place, extra vacuum is developed in the carburetor barrel, which pulls extra fuel through the main metering system to supplement the fuel being pulled from the idle and off-idle circuits. This provides the rich mixture required to sustain operation at low engine temperatures.
To put it in simple terms, carburetors create a combustible fuel air mixture by letting fuel evaporate into a stream of air in more or less controlled conditions. To do this, they reduce the pressure of the air by forcing it through a Venturi tube; this facilitates fuel evaporation.
An undesirable side effect of the process to reduce the air stream pressure is a drop in temperature. A lower temperature makes it harder to vaporize the fuel, and if the intake air and fuel are already colder than usual, the resulting mixture might be too lean to burn.
This is countered via special cold start devices such as chokes, manual mixture control and heaters. Of course if the engine is already hot, having been shut down recently, it might be able to restart without such contrivances. Keep in mind, however, that the carburetors will usually cool much faster than the engine block, being smaller often exposed to more airflow, and all it takes is for them to cool down to impede a restart.
$endgroup$
add a comment
|
$begingroup$
Carburetors don't work as well in cold conditions because they themselves tend to cool the air as it flows through the Venturi tube, compounding the issue of cold intake air and cold fuel.
From Wikipedia:
When the engine is cold, fuel vaporizes less readily and tends to condense on the walls of the intake manifold, starving the cylinders of fuel and making the engine difficult to start; thus, a richer mixture (more fuel to air) is required to start and run the engine until it warms up. A richer mixture is also easier to ignite.
To provide the extra fuel, a choke is typically used; this is a device that restricts the flow of air at the entrance to the carburetor, before the venturi. With this restriction in place, extra vacuum is developed in the carburetor barrel, which pulls extra fuel through the main metering system to supplement the fuel being pulled from the idle and off-idle circuits. This provides the rich mixture required to sustain operation at low engine temperatures.
To put it in simple terms, carburetors create a combustible fuel air mixture by letting fuel evaporate into a stream of air in more or less controlled conditions. To do this, they reduce the pressure of the air by forcing it through a Venturi tube; this facilitates fuel evaporation.
An undesirable side effect of the process to reduce the air stream pressure is a drop in temperature. A lower temperature makes it harder to vaporize the fuel, and if the intake air and fuel are already colder than usual, the resulting mixture might be too lean to burn.
This is countered via special cold start devices such as chokes, manual mixture control and heaters. Of course if the engine is already hot, having been shut down recently, it might be able to restart without such contrivances. Keep in mind, however, that the carburetors will usually cool much faster than the engine block, being smaller often exposed to more airflow, and all it takes is for them to cool down to impede a restart.
$endgroup$
Carburetors don't work as well in cold conditions because they themselves tend to cool the air as it flows through the Venturi tube, compounding the issue of cold intake air and cold fuel.
From Wikipedia:
When the engine is cold, fuel vaporizes less readily and tends to condense on the walls of the intake manifold, starving the cylinders of fuel and making the engine difficult to start; thus, a richer mixture (more fuel to air) is required to start and run the engine until it warms up. A richer mixture is also easier to ignite.
To provide the extra fuel, a choke is typically used; this is a device that restricts the flow of air at the entrance to the carburetor, before the venturi. With this restriction in place, extra vacuum is developed in the carburetor barrel, which pulls extra fuel through the main metering system to supplement the fuel being pulled from the idle and off-idle circuits. This provides the rich mixture required to sustain operation at low engine temperatures.
To put it in simple terms, carburetors create a combustible fuel air mixture by letting fuel evaporate into a stream of air in more or less controlled conditions. To do this, they reduce the pressure of the air by forcing it through a Venturi tube; this facilitates fuel evaporation.
An undesirable side effect of the process to reduce the air stream pressure is a drop in temperature. A lower temperature makes it harder to vaporize the fuel, and if the intake air and fuel are already colder than usual, the resulting mixture might be too lean to burn.
This is countered via special cold start devices such as chokes, manual mixture control and heaters. Of course if the engine is already hot, having been shut down recently, it might be able to restart without such contrivances. Keep in mind, however, that the carburetors will usually cool much faster than the engine block, being smaller often exposed to more airflow, and all it takes is for them to cool down to impede a restart.
answered 10 hours ago
AEhereAEhere
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$begingroup$
Hot starts are sometimes difficult on fuel injected engines because the engine heat will boil the fuel in the fuel lines, creating a vapor lock. Fuel pumps are designed to pump liquid fuel, not fuel vapor.
Look at your POH hot start procedure. Usually this involves running the fuel pump to move liquid fuel into the lines, flushing out the fuel vapor, and in most cases flooding the engine as well. Then the flooded start procedure must be used.
$endgroup$
add a comment
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$begingroup$
Hot starts are sometimes difficult on fuel injected engines because the engine heat will boil the fuel in the fuel lines, creating a vapor lock. Fuel pumps are designed to pump liquid fuel, not fuel vapor.
Look at your POH hot start procedure. Usually this involves running the fuel pump to move liquid fuel into the lines, flushing out the fuel vapor, and in most cases flooding the engine as well. Then the flooded start procedure must be used.
$endgroup$
add a comment
|
$begingroup$
Hot starts are sometimes difficult on fuel injected engines because the engine heat will boil the fuel in the fuel lines, creating a vapor lock. Fuel pumps are designed to pump liquid fuel, not fuel vapor.
Look at your POH hot start procedure. Usually this involves running the fuel pump to move liquid fuel into the lines, flushing out the fuel vapor, and in most cases flooding the engine as well. Then the flooded start procedure must be used.
$endgroup$
Hot starts are sometimes difficult on fuel injected engines because the engine heat will boil the fuel in the fuel lines, creating a vapor lock. Fuel pumps are designed to pump liquid fuel, not fuel vapor.
Look at your POH hot start procedure. Usually this involves running the fuel pump to move liquid fuel into the lines, flushing out the fuel vapor, and in most cases flooding the engine as well. Then the flooded start procedure must be used.
answered 7 hours ago
Skip MillerSkip Miller
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