Why would a jet engine that runs at temps excess of 2000°C burn when it crashes?Why do gases in the combustion chamber only flow one direction to the gas turbine in a jet engine?How are temperature differences handled in a jet engine?Why are propeller engines uncommon on airliners?What is high altitude testing?Why does a jet engine acquire a metallic whine when in full power?What would have happened if the jet engine on my aircraft had ingested caulk from the pavement?Is water a possible fuel for jet engines?Is it possible to build a jet engine that utilises all excess heat?Why is a (jet) engine in flight shutdown so critical?Why don't 747s use unreliable, but cheap, jet engines instead?Is it possible to calculate possible fuel savings of known turbofan engines if operational heat could be increasedHow to increase your chances of survival in a plane crash?

Multi tool use
Offered promotion but I'm leaving. Should I tell?
How does airport security verify that you can carry a battery bank over 100 Wh?
Replacing Windows 7 security updates with anti-virus?
Time travel short story where dinosaur doesn't taste like chicken
Can someone explain what is being said here in color publishing in the American Mathematical Monthly?
How do I deal with a powergamer in a game full of beginners in a school club?
Does splitting a potentially monolithic application into several smaller ones help prevent bugs?
Fourth person (in Slavey language)
What Happens when Passenger Refuses to Fly Boeing 737 Max?
Aliens englobed the Solar System: will we notice?
How do I express some one as a black person?
MTG: Can I kill an opponent in response to lethal activated abilities, and not take the damage?
Am I not good enough for you?
Do f-stop and exposure time perfectly cancel?
Placing subfig vertically
How much attack damage does the AC boost from a shield prevent on average?
Are the terms "stab" and "staccato" synonyms?
"One can do his homework in the library"
Algorithm to convert a fixed-length string to the smallest possible collision-free representation?
Latest web browser compatible with Windows 98
Good allowance savings plan?
How strictly should I take "Candidates must be local"?
How are such low op-amp input currents possible?
Good for you! in Russian
Why would a jet engine that runs at temps excess of 2000°C burn when it crashes?
Why do gases in the combustion chamber only flow one direction to the gas turbine in a jet engine?How are temperature differences handled in a jet engine?Why are propeller engines uncommon on airliners?What is high altitude testing?Why does a jet engine acquire a metallic whine when in full power?What would have happened if the jet engine on my aircraft had ingested caulk from the pavement?Is water a possible fuel for jet engines?Is it possible to build a jet engine that utilises all excess heat?Why is a (jet) engine in flight shutdown so critical?Why don't 747s use unreliable, but cheap, jet engines instead?Is it possible to calculate possible fuel savings of known turbofan engines if operational heat could be increasedHow to increase your chances of survival in a plane crash?
$begingroup$
Airline engines are designed to work at very high temperatures. Yet, when a plane crashes they're burnt (see below). Is it something in their design?
(bostonherald.com)
jet-engine accidents aerospace-materials
$endgroup$
add a comment |
$begingroup$
Airline engines are designed to work at very high temperatures. Yet, when a plane crashes they're burnt (see below). Is it something in their design?
(bostonherald.com)
jet-engine accidents aerospace-materials
$endgroup$
3
$begingroup$
The engine in the photograph is not melted.
$endgroup$
– Michael Hall
5 hours ago
$begingroup$
@MichaelHall: That's on me, I've fixed it. OP originally wrote burnt. Although judging by the LP section, it did melt.
$endgroup$
– ymb1
5 hours ago
$begingroup$
I have to challenge the premise. From the picture, it looks like the external housing of the engine burned and/or melted. The internal parts look like they've just suffered impact damage. The external housing does not experience high temperatures. Same reason the combustion temperature of your car's engine may reach 2000 C or so, yet the plastic components sitting nearby don't melt.
$endgroup$
– jamesqf
43 mins ago
add a comment |
$begingroup$
Airline engines are designed to work at very high temperatures. Yet, when a plane crashes they're burnt (see below). Is it something in their design?
(bostonherald.com)
jet-engine accidents aerospace-materials
$endgroup$
Airline engines are designed to work at very high temperatures. Yet, when a plane crashes they're burnt (see below). Is it something in their design?
(bostonherald.com)
jet-engine accidents aerospace-materials
jet-engine accidents aerospace-materials
edited 5 hours ago


ymb1
67k7212355
67k7212355
asked 6 hours ago


RegmiRegmi
1686
1686
3
$begingroup$
The engine in the photograph is not melted.
$endgroup$
– Michael Hall
5 hours ago
$begingroup$
@MichaelHall: That's on me, I've fixed it. OP originally wrote burnt. Although judging by the LP section, it did melt.
$endgroup$
– ymb1
5 hours ago
$begingroup$
I have to challenge the premise. From the picture, it looks like the external housing of the engine burned and/or melted. The internal parts look like they've just suffered impact damage. The external housing does not experience high temperatures. Same reason the combustion temperature of your car's engine may reach 2000 C or so, yet the plastic components sitting nearby don't melt.
$endgroup$
– jamesqf
43 mins ago
add a comment |
3
$begingroup$
The engine in the photograph is not melted.
$endgroup$
– Michael Hall
5 hours ago
$begingroup$
@MichaelHall: That's on me, I've fixed it. OP originally wrote burnt. Although judging by the LP section, it did melt.
$endgroup$
– ymb1
5 hours ago
$begingroup$
I have to challenge the premise. From the picture, it looks like the external housing of the engine burned and/or melted. The internal parts look like they've just suffered impact damage. The external housing does not experience high temperatures. Same reason the combustion temperature of your car's engine may reach 2000 C or so, yet the plastic components sitting nearby don't melt.
$endgroup$
– jamesqf
43 mins ago
3
3
$begingroup$
The engine in the photograph is not melted.
$endgroup$
– Michael Hall
5 hours ago
$begingroup$
The engine in the photograph is not melted.
$endgroup$
– Michael Hall
5 hours ago
$begingroup$
@MichaelHall: That's on me, I've fixed it. OP originally wrote burnt. Although judging by the LP section, it did melt.
$endgroup$
– ymb1
5 hours ago
$begingroup$
@MichaelHall: That's on me, I've fixed it. OP originally wrote burnt. Although judging by the LP section, it did melt.
$endgroup$
– ymb1
5 hours ago
$begingroup$
I have to challenge the premise. From the picture, it looks like the external housing of the engine burned and/or melted. The internal parts look like they've just suffered impact damage. The external housing does not experience high temperatures. Same reason the combustion temperature of your car's engine may reach 2000 C or so, yet the plastic components sitting nearby don't melt.
$endgroup$
– jamesqf
43 mins ago
$begingroup$
I have to challenge the premise. From the picture, it looks like the external housing of the engine burned and/or melted. The internal parts look like they've just suffered impact damage. The external housing does not experience high temperatures. Same reason the combustion temperature of your car's engine may reach 2000 C or so, yet the plastic components sitting nearby don't melt.
$endgroup$
– jamesqf
43 mins ago
add a comment |
2 Answers
2
active
oldest
votes
$begingroup$
How The Jet Engine Works:
Inside the typical commercial jet engine, the fuel burns in the combustion chamber at up to 2000 degrees Celsius. The temperature at which metals in this part of the engine start to melt is 1300 degrees Celsius, so advanced cooling techniques must be used.
You can read more about some of those cooling mechanisms in How are temperature differences handled in a jet engine?
See also, How do you stop a jet engine melting?:
Neil - The normal melting point of the nickel blade alloys that we use in the turbine is typically about 12-1400 degrees. But what you do, and this is the clever bit, is you actually cool these blades. You have internal cooling passages, which effectively has air that flows through and it's about 7-800 degrees. And this cooling air then exits from small little minute holes that have been drilled on the surface of the blade and this air then forms a kind of a film on the surface of the blade, and this technology is typically called a 'film cooling.'
What you also do - you coat these blades and typically use something called a thermal barrier coating. The thermal barrier coating, effectively, is ceramic, typically about quarter of a millimeter in thickness, but they have got very, very low thermal conductivity. So, effectively, even though the gas stream is at a much higher air temperature, the effective metal that exists beneath the thermal barrier coating is much colder, and you get thermal grade of the order of about 100 degrees C between the hot and the cold surface. So all of this put together - this whole cooling technology effectively helps to keep the blade below its melting temperature.
The engine is designed to manage the intense heat in a controlled way, by restricting it to certain components, injecting cool air around the hot parts, and choosing different materials for different parts of the engine. If the engine is severely damaged, doused in jet fuel, and set on fire, none of those mechanisms function; the entire engine (or whatever is left of it), as opposed to just the portions intended to manage heat, will be hot, and none of the cooling mechanisms will be working.
$endgroup$
$begingroup$
Those blades are little marvels of engineering. Something you can hold in one hand but costs some ~5000 dollars (and there's a whole lot of them in one turbine)
$endgroup$
– mbrig
2 hours ago
add a comment |
$begingroup$
Peters answer to this question has a nice chart that shows internal jet engine temps:
You can see that the temps are highest by a fairly large factor in the combustion chamber. This means that only the combustion chamber needs to be able to withstand those temperatures. To save weight and often use less expensive and less exotic materials the rest of the engine may be made out of materials that don't need to withstand such high temps. As such in an accident where jet fuel may be dispersed in an uncontrolled way and burn with as much oxygen as it can get its easy to scorch engine parts and anything else around.
It also is in part a question of time. The ability to withstand heat varies with time. In a crash of a fairly fueled aircraft that may burn uncontrolled for a long time you are likely to find scorched parts like this. Where as a plane that runs its tanks try and crashes in a field may not see the same fire marks. However if the plane hits the ground with enough force the heat generated from the impact can also lead to markings like this.
$endgroup$
4
$begingroup$
I'd like to add that there is no point of having a crashed engine survive the crash, +1.
$endgroup$
– ymb1
6 hours ago
add a comment |
Your Answer
StackExchange.ifUsing("editor", function ()
return StackExchange.using("mathjaxEditing", function ()
StackExchange.MarkdownEditor.creationCallbacks.add(function (editor, postfix)
StackExchange.mathjaxEditing.prepareWmdForMathJax(editor, postfix, [["$", "$"], ["\\(","\\)"]]);
);
);
, "mathjax-editing");
StackExchange.ready(function()
var channelOptions =
tags: "".split(" "),
id: "528"
;
initTagRenderer("".split(" "), "".split(" "), channelOptions);
StackExchange.using("externalEditor", function()
// Have to fire editor after snippets, if snippets enabled
if (StackExchange.settings.snippets.snippetsEnabled)
StackExchange.using("snippets", function()
createEditor();
);
else
createEditor();
);
function createEditor()
StackExchange.prepareEditor(
heartbeatType: 'answer',
autoActivateHeartbeat: false,
convertImagesToLinks: false,
noModals: true,
showLowRepImageUploadWarning: true,
reputationToPostImages: null,
bindNavPrevention: true,
postfix: "",
imageUploader:
brandingHtml: "Powered by u003ca class="icon-imgur-white" href="https://imgur.com/"u003eu003c/au003e",
contentPolicyHtml: "User contributions licensed under u003ca href="https://creativecommons.org/licenses/by-sa/3.0/"u003ecc by-sa 3.0 with attribution requiredu003c/au003e u003ca href="https://stackoverflow.com/legal/content-policy"u003e(content policy)u003c/au003e",
allowUrls: true
,
noCode: true, onDemand: true,
discardSelector: ".discard-answer"
,immediatelyShowMarkdownHelp:true
);
);
Sign up or log in
StackExchange.ready(function ()
StackExchange.helpers.onClickDraftSave('#login-link');
);
Sign up using Google
Sign up using Facebook
Sign up using Email and Password
Post as a guest
Required, but never shown
StackExchange.ready(
function ()
StackExchange.openid.initPostLogin('.new-post-login', 'https%3a%2f%2faviation.stackexchange.com%2fquestions%2f61046%2fwhy-would-a-jet-engine-that-runs-at-temps-excess-of-2000c-burn-when-it-crashes%23new-answer', 'question_page');
);
Post as a guest
Required, but never shown
2 Answers
2
active
oldest
votes
2 Answers
2
active
oldest
votes
active
oldest
votes
active
oldest
votes
$begingroup$
How The Jet Engine Works:
Inside the typical commercial jet engine, the fuel burns in the combustion chamber at up to 2000 degrees Celsius. The temperature at which metals in this part of the engine start to melt is 1300 degrees Celsius, so advanced cooling techniques must be used.
You can read more about some of those cooling mechanisms in How are temperature differences handled in a jet engine?
See also, How do you stop a jet engine melting?:
Neil - The normal melting point of the nickel blade alloys that we use in the turbine is typically about 12-1400 degrees. But what you do, and this is the clever bit, is you actually cool these blades. You have internal cooling passages, which effectively has air that flows through and it's about 7-800 degrees. And this cooling air then exits from small little minute holes that have been drilled on the surface of the blade and this air then forms a kind of a film on the surface of the blade, and this technology is typically called a 'film cooling.'
What you also do - you coat these blades and typically use something called a thermal barrier coating. The thermal barrier coating, effectively, is ceramic, typically about quarter of a millimeter in thickness, but they have got very, very low thermal conductivity. So, effectively, even though the gas stream is at a much higher air temperature, the effective metal that exists beneath the thermal barrier coating is much colder, and you get thermal grade of the order of about 100 degrees C between the hot and the cold surface. So all of this put together - this whole cooling technology effectively helps to keep the blade below its melting temperature.
The engine is designed to manage the intense heat in a controlled way, by restricting it to certain components, injecting cool air around the hot parts, and choosing different materials for different parts of the engine. If the engine is severely damaged, doused in jet fuel, and set on fire, none of those mechanisms function; the entire engine (or whatever is left of it), as opposed to just the portions intended to manage heat, will be hot, and none of the cooling mechanisms will be working.
$endgroup$
$begingroup$
Those blades are little marvels of engineering. Something you can hold in one hand but costs some ~5000 dollars (and there's a whole lot of them in one turbine)
$endgroup$
– mbrig
2 hours ago
add a comment |
$begingroup$
How The Jet Engine Works:
Inside the typical commercial jet engine, the fuel burns in the combustion chamber at up to 2000 degrees Celsius. The temperature at which metals in this part of the engine start to melt is 1300 degrees Celsius, so advanced cooling techniques must be used.
You can read more about some of those cooling mechanisms in How are temperature differences handled in a jet engine?
See also, How do you stop a jet engine melting?:
Neil - The normal melting point of the nickel blade alloys that we use in the turbine is typically about 12-1400 degrees. But what you do, and this is the clever bit, is you actually cool these blades. You have internal cooling passages, which effectively has air that flows through and it's about 7-800 degrees. And this cooling air then exits from small little minute holes that have been drilled on the surface of the blade and this air then forms a kind of a film on the surface of the blade, and this technology is typically called a 'film cooling.'
What you also do - you coat these blades and typically use something called a thermal barrier coating. The thermal barrier coating, effectively, is ceramic, typically about quarter of a millimeter in thickness, but they have got very, very low thermal conductivity. So, effectively, even though the gas stream is at a much higher air temperature, the effective metal that exists beneath the thermal barrier coating is much colder, and you get thermal grade of the order of about 100 degrees C between the hot and the cold surface. So all of this put together - this whole cooling technology effectively helps to keep the blade below its melting temperature.
The engine is designed to manage the intense heat in a controlled way, by restricting it to certain components, injecting cool air around the hot parts, and choosing different materials for different parts of the engine. If the engine is severely damaged, doused in jet fuel, and set on fire, none of those mechanisms function; the entire engine (or whatever is left of it), as opposed to just the portions intended to manage heat, will be hot, and none of the cooling mechanisms will be working.
$endgroup$
$begingroup$
Those blades are little marvels of engineering. Something you can hold in one hand but costs some ~5000 dollars (and there's a whole lot of them in one turbine)
$endgroup$
– mbrig
2 hours ago
add a comment |
$begingroup$
How The Jet Engine Works:
Inside the typical commercial jet engine, the fuel burns in the combustion chamber at up to 2000 degrees Celsius. The temperature at which metals in this part of the engine start to melt is 1300 degrees Celsius, so advanced cooling techniques must be used.
You can read more about some of those cooling mechanisms in How are temperature differences handled in a jet engine?
See also, How do you stop a jet engine melting?:
Neil - The normal melting point of the nickel blade alloys that we use in the turbine is typically about 12-1400 degrees. But what you do, and this is the clever bit, is you actually cool these blades. You have internal cooling passages, which effectively has air that flows through and it's about 7-800 degrees. And this cooling air then exits from small little minute holes that have been drilled on the surface of the blade and this air then forms a kind of a film on the surface of the blade, and this technology is typically called a 'film cooling.'
What you also do - you coat these blades and typically use something called a thermal barrier coating. The thermal barrier coating, effectively, is ceramic, typically about quarter of a millimeter in thickness, but they have got very, very low thermal conductivity. So, effectively, even though the gas stream is at a much higher air temperature, the effective metal that exists beneath the thermal barrier coating is much colder, and you get thermal grade of the order of about 100 degrees C between the hot and the cold surface. So all of this put together - this whole cooling technology effectively helps to keep the blade below its melting temperature.
The engine is designed to manage the intense heat in a controlled way, by restricting it to certain components, injecting cool air around the hot parts, and choosing different materials for different parts of the engine. If the engine is severely damaged, doused in jet fuel, and set on fire, none of those mechanisms function; the entire engine (or whatever is left of it), as opposed to just the portions intended to manage heat, will be hot, and none of the cooling mechanisms will be working.
$endgroup$
How The Jet Engine Works:
Inside the typical commercial jet engine, the fuel burns in the combustion chamber at up to 2000 degrees Celsius. The temperature at which metals in this part of the engine start to melt is 1300 degrees Celsius, so advanced cooling techniques must be used.
You can read more about some of those cooling mechanisms in How are temperature differences handled in a jet engine?
See also, How do you stop a jet engine melting?:
Neil - The normal melting point of the nickel blade alloys that we use in the turbine is typically about 12-1400 degrees. But what you do, and this is the clever bit, is you actually cool these blades. You have internal cooling passages, which effectively has air that flows through and it's about 7-800 degrees. And this cooling air then exits from small little minute holes that have been drilled on the surface of the blade and this air then forms a kind of a film on the surface of the blade, and this technology is typically called a 'film cooling.'
What you also do - you coat these blades and typically use something called a thermal barrier coating. The thermal barrier coating, effectively, is ceramic, typically about quarter of a millimeter in thickness, but they have got very, very low thermal conductivity. So, effectively, even though the gas stream is at a much higher air temperature, the effective metal that exists beneath the thermal barrier coating is much colder, and you get thermal grade of the order of about 100 degrees C between the hot and the cold surface. So all of this put together - this whole cooling technology effectively helps to keep the blade below its melting temperature.
The engine is designed to manage the intense heat in a controlled way, by restricting it to certain components, injecting cool air around the hot parts, and choosing different materials for different parts of the engine. If the engine is severely damaged, doused in jet fuel, and set on fire, none of those mechanisms function; the entire engine (or whatever is left of it), as opposed to just the portions intended to manage heat, will be hot, and none of the cooling mechanisms will be working.
edited 6 hours ago
answered 6 hours ago
Zach LiptonZach Lipton
6,18912442
6,18912442
$begingroup$
Those blades are little marvels of engineering. Something you can hold in one hand but costs some ~5000 dollars (and there's a whole lot of them in one turbine)
$endgroup$
– mbrig
2 hours ago
add a comment |
$begingroup$
Those blades are little marvels of engineering. Something you can hold in one hand but costs some ~5000 dollars (and there's a whole lot of them in one turbine)
$endgroup$
– mbrig
2 hours ago
$begingroup$
Those blades are little marvels of engineering. Something you can hold in one hand but costs some ~5000 dollars (and there's a whole lot of them in one turbine)
$endgroup$
– mbrig
2 hours ago
$begingroup$
Those blades are little marvels of engineering. Something you can hold in one hand but costs some ~5000 dollars (and there's a whole lot of them in one turbine)
$endgroup$
– mbrig
2 hours ago
add a comment |
$begingroup$
Peters answer to this question has a nice chart that shows internal jet engine temps:
You can see that the temps are highest by a fairly large factor in the combustion chamber. This means that only the combustion chamber needs to be able to withstand those temperatures. To save weight and often use less expensive and less exotic materials the rest of the engine may be made out of materials that don't need to withstand such high temps. As such in an accident where jet fuel may be dispersed in an uncontrolled way and burn with as much oxygen as it can get its easy to scorch engine parts and anything else around.
It also is in part a question of time. The ability to withstand heat varies with time. In a crash of a fairly fueled aircraft that may burn uncontrolled for a long time you are likely to find scorched parts like this. Where as a plane that runs its tanks try and crashes in a field may not see the same fire marks. However if the plane hits the ground with enough force the heat generated from the impact can also lead to markings like this.
$endgroup$
4
$begingroup$
I'd like to add that there is no point of having a crashed engine survive the crash, +1.
$endgroup$
– ymb1
6 hours ago
add a comment |
$begingroup$
Peters answer to this question has a nice chart that shows internal jet engine temps:
You can see that the temps are highest by a fairly large factor in the combustion chamber. This means that only the combustion chamber needs to be able to withstand those temperatures. To save weight and often use less expensive and less exotic materials the rest of the engine may be made out of materials that don't need to withstand such high temps. As such in an accident where jet fuel may be dispersed in an uncontrolled way and burn with as much oxygen as it can get its easy to scorch engine parts and anything else around.
It also is in part a question of time. The ability to withstand heat varies with time. In a crash of a fairly fueled aircraft that may burn uncontrolled for a long time you are likely to find scorched parts like this. Where as a plane that runs its tanks try and crashes in a field may not see the same fire marks. However if the plane hits the ground with enough force the heat generated from the impact can also lead to markings like this.
$endgroup$
4
$begingroup$
I'd like to add that there is no point of having a crashed engine survive the crash, +1.
$endgroup$
– ymb1
6 hours ago
add a comment |
$begingroup$
Peters answer to this question has a nice chart that shows internal jet engine temps:
You can see that the temps are highest by a fairly large factor in the combustion chamber. This means that only the combustion chamber needs to be able to withstand those temperatures. To save weight and often use less expensive and less exotic materials the rest of the engine may be made out of materials that don't need to withstand such high temps. As such in an accident where jet fuel may be dispersed in an uncontrolled way and burn with as much oxygen as it can get its easy to scorch engine parts and anything else around.
It also is in part a question of time. The ability to withstand heat varies with time. In a crash of a fairly fueled aircraft that may burn uncontrolled for a long time you are likely to find scorched parts like this. Where as a plane that runs its tanks try and crashes in a field may not see the same fire marks. However if the plane hits the ground with enough force the heat generated from the impact can also lead to markings like this.
$endgroup$
Peters answer to this question has a nice chart that shows internal jet engine temps:
You can see that the temps are highest by a fairly large factor in the combustion chamber. This means that only the combustion chamber needs to be able to withstand those temperatures. To save weight and often use less expensive and less exotic materials the rest of the engine may be made out of materials that don't need to withstand such high temps. As such in an accident where jet fuel may be dispersed in an uncontrolled way and burn with as much oxygen as it can get its easy to scorch engine parts and anything else around.
It also is in part a question of time. The ability to withstand heat varies with time. In a crash of a fairly fueled aircraft that may burn uncontrolled for a long time you are likely to find scorched parts like this. Where as a plane that runs its tanks try and crashes in a field may not see the same fire marks. However if the plane hits the ground with enough force the heat generated from the impact can also lead to markings like this.
edited 6 hours ago
answered 6 hours ago
DaveDave
66.8k4125241
66.8k4125241
4
$begingroup$
I'd like to add that there is no point of having a crashed engine survive the crash, +1.
$endgroup$
– ymb1
6 hours ago
add a comment |
4
$begingroup$
I'd like to add that there is no point of having a crashed engine survive the crash, +1.
$endgroup$
– ymb1
6 hours ago
4
4
$begingroup$
I'd like to add that there is no point of having a crashed engine survive the crash, +1.
$endgroup$
– ymb1
6 hours ago
$begingroup$
I'd like to add that there is no point of having a crashed engine survive the crash, +1.
$endgroup$
– ymb1
6 hours ago
add a comment |
Thanks for contributing an answer to Aviation Stack Exchange!
- Please be sure to answer the question. Provide details and share your research!
But avoid …
- Asking for help, clarification, or responding to other answers.
- Making statements based on opinion; back them up with references or personal experience.
Use MathJax to format equations. MathJax reference.
To learn more, see our tips on writing great answers.
Sign up or log in
StackExchange.ready(function ()
StackExchange.helpers.onClickDraftSave('#login-link');
);
Sign up using Google
Sign up using Facebook
Sign up using Email and Password
Post as a guest
Required, but never shown
StackExchange.ready(
function ()
StackExchange.openid.initPostLogin('.new-post-login', 'https%3a%2f%2faviation.stackexchange.com%2fquestions%2f61046%2fwhy-would-a-jet-engine-that-runs-at-temps-excess-of-2000c-burn-when-it-crashes%23new-answer', 'question_page');
);
Post as a guest
Required, but never shown
Sign up or log in
StackExchange.ready(function ()
StackExchange.helpers.onClickDraftSave('#login-link');
);
Sign up using Google
Sign up using Facebook
Sign up using Email and Password
Post as a guest
Required, but never shown
Sign up or log in
StackExchange.ready(function ()
StackExchange.helpers.onClickDraftSave('#login-link');
);
Sign up using Google
Sign up using Facebook
Sign up using Email and Password
Post as a guest
Required, but never shown
Sign up or log in
StackExchange.ready(function ()
StackExchange.helpers.onClickDraftSave('#login-link');
);
Sign up using Google
Sign up using Facebook
Sign up using Email and Password
Sign up using Google
Sign up using Facebook
Sign up using Email and Password
Post as a guest
Required, but never shown
Required, but never shown
Required, but never shown
Required, but never shown
Required, but never shown
Required, but never shown
Required, but never shown
Required, but never shown
Required, but never shown
aNPAaH BqEPpZlqdgb,HK3MPwLAIQnlEbWbpiJ,NFZexCgE aiN X6e,IoHV3 3fsdpdLuNbGMLggeUes0Wh3
3
$begingroup$
The engine in the photograph is not melted.
$endgroup$
– Michael Hall
5 hours ago
$begingroup$
@MichaelHall: That's on me, I've fixed it. OP originally wrote burnt. Although judging by the LP section, it did melt.
$endgroup$
– ymb1
5 hours ago
$begingroup$
I have to challenge the premise. From the picture, it looks like the external housing of the engine burned and/or melted. The internal parts look like they've just suffered impact damage. The external housing does not experience high temperatures. Same reason the combustion temperature of your car's engine may reach 2000 C or so, yet the plastic components sitting nearby don't melt.
$endgroup$
– jamesqf
43 mins ago