Why are fuel tanks located in wings?











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Passenger aircraft have fuel tanks in the wings. Why?
What are the advantages and disadvantages of this location ?



examples of disadvantages I would suspect:




  • added weight increases the structural load applied to the wings

  • different gravitational forces and wing-bending between full and empty tanks result in repeating stresses shortening the aircraft life-span

  • higher risk of catastrophic damage to wings in case of in-flight fuel ignition

  • higher risk of fire when lightning strikes a wing


img










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  • 13




    Keeping fuel in the wings actually helps to maintain their structural integrity, see aviation.stackexchange.com/questions/42613/…
    – DeepSpace
    20 hours ago








  • 2




    On the ground, the aircraft rests on the wheels. In flight, it rests on the wings - so weight in the wings reduces structural loading, not increases it.
    – Therac
    13 hours ago










  • @Therac: Following your explanation, I would see that it does not add structural load? But how would weight "reduce" structural load?
    – summerrain
    13 hours ago










  • @summerrain By balancing out the fuselage, which is a big central load. See A340 vs A330. Of course, this implies total weight is equal or within some limit.
    – Therac
    12 hours ago















up vote
10
down vote

favorite
1












Passenger aircraft have fuel tanks in the wings. Why?
What are the advantages and disadvantages of this location ?



examples of disadvantages I would suspect:




  • added weight increases the structural load applied to the wings

  • different gravitational forces and wing-bending between full and empty tanks result in repeating stresses shortening the aircraft life-span

  • higher risk of catastrophic damage to wings in case of in-flight fuel ignition

  • higher risk of fire when lightning strikes a wing


img










share|improve this question




















  • 13




    Keeping fuel in the wings actually helps to maintain their structural integrity, see aviation.stackexchange.com/questions/42613/…
    – DeepSpace
    20 hours ago








  • 2




    On the ground, the aircraft rests on the wheels. In flight, it rests on the wings - so weight in the wings reduces structural loading, not increases it.
    – Therac
    13 hours ago










  • @Therac: Following your explanation, I would see that it does not add structural load? But how would weight "reduce" structural load?
    – summerrain
    13 hours ago










  • @summerrain By balancing out the fuselage, which is a big central load. See A340 vs A330. Of course, this implies total weight is equal or within some limit.
    – Therac
    12 hours ago













up vote
10
down vote

favorite
1









up vote
10
down vote

favorite
1






1





Passenger aircraft have fuel tanks in the wings. Why?
What are the advantages and disadvantages of this location ?



examples of disadvantages I would suspect:




  • added weight increases the structural load applied to the wings

  • different gravitational forces and wing-bending between full and empty tanks result in repeating stresses shortening the aircraft life-span

  • higher risk of catastrophic damage to wings in case of in-flight fuel ignition

  • higher risk of fire when lightning strikes a wing


img










share|improve this question















Passenger aircraft have fuel tanks in the wings. Why?
What are the advantages and disadvantages of this location ?



examples of disadvantages I would suspect:




  • added weight increases the structural load applied to the wings

  • different gravitational forces and wing-bending between full and empty tanks result in repeating stresses shortening the aircraft life-span

  • higher risk of catastrophic damage to wings in case of in-flight fuel ignition

  • higher risk of fire when lightning strikes a wing


img







aircraft-design wing fuel-tanks aircraft-structures fuel-systems






share|improve this question















share|improve this question













share|improve this question




share|improve this question








edited 13 hours ago

























asked 22 hours ago









summerrain

613415




613415








  • 13




    Keeping fuel in the wings actually helps to maintain their structural integrity, see aviation.stackexchange.com/questions/42613/…
    – DeepSpace
    20 hours ago








  • 2




    On the ground, the aircraft rests on the wheels. In flight, it rests on the wings - so weight in the wings reduces structural loading, not increases it.
    – Therac
    13 hours ago










  • @Therac: Following your explanation, I would see that it does not add structural load? But how would weight "reduce" structural load?
    – summerrain
    13 hours ago










  • @summerrain By balancing out the fuselage, which is a big central load. See A340 vs A330. Of course, this implies total weight is equal or within some limit.
    – Therac
    12 hours ago














  • 13




    Keeping fuel in the wings actually helps to maintain their structural integrity, see aviation.stackexchange.com/questions/42613/…
    – DeepSpace
    20 hours ago








  • 2




    On the ground, the aircraft rests on the wheels. In flight, it rests on the wings - so weight in the wings reduces structural loading, not increases it.
    – Therac
    13 hours ago










  • @Therac: Following your explanation, I would see that it does not add structural load? But how would weight "reduce" structural load?
    – summerrain
    13 hours ago










  • @summerrain By balancing out the fuselage, which is a big central load. See A340 vs A330. Of course, this implies total weight is equal or within some limit.
    – Therac
    12 hours ago








13




13




Keeping fuel in the wings actually helps to maintain their structural integrity, see aviation.stackexchange.com/questions/42613/…
– DeepSpace
20 hours ago






Keeping fuel in the wings actually helps to maintain their structural integrity, see aviation.stackexchange.com/questions/42613/…
– DeepSpace
20 hours ago






2




2




On the ground, the aircraft rests on the wheels. In flight, it rests on the wings - so weight in the wings reduces structural loading, not increases it.
– Therac
13 hours ago




On the ground, the aircraft rests on the wheels. In flight, it rests on the wings - so weight in the wings reduces structural loading, not increases it.
– Therac
13 hours ago












@Therac: Following your explanation, I would see that it does not add structural load? But how would weight "reduce" structural load?
– summerrain
13 hours ago




@Therac: Following your explanation, I would see that it does not add structural load? But how would weight "reduce" structural load?
– summerrain
13 hours ago












@summerrain By balancing out the fuselage, which is a big central load. See A340 vs A330. Of course, this implies total weight is equal or within some limit.
– Therac
12 hours ago




@summerrain By balancing out the fuselage, which is a big central load. See A340 vs A330. Of course, this implies total weight is equal or within some limit.
– Therac
12 hours ago










6 Answers
6






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up vote
38
down vote













Several advantages:



Wing structures are hollow and voluminous in order to provide structural rigidity against flutter and carry flight loads. This provides the space needed to store fuel.



On a conventional aircraft, placing fuel tanks in the wings places the fuel mass very close to, or on, the center of lift. This dramatically reduces Cg shift during flight and reduces the size and weight of the tailplane to maintain stable flight.



In the event of a crash landing, having the fuel in the wings keeps it away from the cabin and the occupants, reducing risks of cabin fires.



The weight of the fuel reduces the loading moment on the wing roots, reducing the weight of the structure needed to support the aircraft during flight.






share|improve this answer




























    up vote
    13
    down vote














    added weight increases the structural load applied to the wings
    different gravitational forces and wing-bending between full and empty tanks result in repeating stresses shortening the aircraft life-span




    As a result of the effects of lift (and the deceasing need for it as the plane lightens) the reverse is actually true see here




    higher risk of catastrophic damage to wings in case of in-flight fuel ignition




    As opposed to higher risk of catastrophic damage to the cabin in the case of in-flight fuel ignition?



    Assuming a non-explosive ignition having the fuel in the wings means you can take action to dump the fuel. If you have a fire begin in the main fuselage however you've got a higher chance of the fire incapacitating the crew before they can take steps. Or damage occuring to the avionics, the pressure cabin etc.




    maybe higher risk of fire when lightning strikes a wing ?




    Wing tips are one of the locations on a plane that is more prone to lightning strikes - and the potential for fuel fires is there but steps are taken to counter this and in the vast majority of cases lightning does very little damage






    share|improve this answer




























      up vote
      9
      down vote













      Quite simply: there's a lot of empty space in those wings, and there's a lot of empty space needed for fuel.



      Creating space elsewhere for fuel would make the entire aircraft larger and heavier, so makes little sense.



      And it's not just the wings, many aircraft carry fuel in the vertical stabiliser as well.






      share|improve this answer

















      • 35




        In other words: Why are fuel tanks located in the wings? Because the passengers wouldn't fit in there. :)
        – Tanner Swett
        18 hours ago






      • 20




        @TannerSwett Don't give them any ideas...
        – pipe
        16 hours ago






      • 3




        @pipe en.wikipedia.org/wiki/Junkers_G.38 ?
        – DeepSpace
        14 hours ago










      • @TannerSwett hmm, Ryanair wants to talk with you about that idea.
        – jwenting
        2 hours ago


















      up vote
      9
      down vote













      I see what you're saying, but there's something you're overlooking in your logic. You're looking at an airplane sitting on the ground, where the wheels are under the fuselage and the wings are deadweight that creates strain on the structure.



      Think about one in flight. Now all the lift is coming from the wings, imagine the airplane suspended by a couple dozen (billion) cables spread around the wing surfaces. Now the fuselage is deadweight and the strain in the structure is from carrying the fuselage.



      So when you add weight to the wings evenly, it adds practically zero structural load for the wings. What's being lifted is inside the source of the lift. So from a structural load perspective, it's a wash: it doesn't matter.



      Whereas if you add more tanks in the fuselage, that's fine on the ground, but it adds huge stresses to the wings inflight, effectively reducing practical cargo capacity.



      The strain on wings from sitting on the ground is much less worrisome to designers than the strains inflight.



      See also "Zero Fuel Weight".






      share|improve this answer























      • Exactly what I was thinking, but you said it much better!
        – Michael Hall
        9 hours ago


















      up vote
      3
      down vote















      • added weight increases the structural load applied to the wings




      Only when the plane's on the ground. When it's in the air, it decreases the load on the wings because their lift balances the weight.





      • different gravitational forces and wing-bending between full and empty tanks result in repeating stresses shortening the aircraft life-span




      At the rate of one cycle per flight. And the wings already go through a stress cycle once per flight (flexed down when the plane's on the ground and up when it's in the air).





      • higher risk of catastrophic damage to wings in case of in-flight fuel ignition




      The fuel tanks catching fire in flight is catastrophic wherever you put them.





      • higher risk of fire when lightning strikes a wing




      When did that last happen? Wikipedia's list of plane crashes suggests LANSA flight 508 in 1971. Such incidents are so rare because fuel tanks have been fitted with inerting systems as recommended after the crash of Pan Am flight 214 in 1963.






      share|improve this answer




























        up vote
        3
        down vote













        Along with the other answers, I'll point out the cases where an aircraft fuel tank exploded, the center tank, which is in the fuselage, was implicated. There are two reasons:



        First, a fuselage tank is located lower than the engines and requires pumps to raise the fuel. Electrical pump failures have caused explosions. This also means that a pump failure results in unusable fuel, whereas wing tanks can naturally feed the engines via gravity.



        Second, fuselage tanks are closer to sources of heat. This was a cause of the TWA flight 800 accident, where heat from nearby air conditioning equipment lead to a flammable vapor in the fuel tanks. In contrast, wing tanks are naturally cooled by airflow and are less susceptible to forming such explosive vapors.






        share|improve this answer





















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          6 Answers
          6






          active

          oldest

          votes








          6 Answers
          6






          active

          oldest

          votes









          active

          oldest

          votes






          active

          oldest

          votes








          up vote
          38
          down vote













          Several advantages:



          Wing structures are hollow and voluminous in order to provide structural rigidity against flutter and carry flight loads. This provides the space needed to store fuel.



          On a conventional aircraft, placing fuel tanks in the wings places the fuel mass very close to, or on, the center of lift. This dramatically reduces Cg shift during flight and reduces the size and weight of the tailplane to maintain stable flight.



          In the event of a crash landing, having the fuel in the wings keeps it away from the cabin and the occupants, reducing risks of cabin fires.



          The weight of the fuel reduces the loading moment on the wing roots, reducing the weight of the structure needed to support the aircraft during flight.






          share|improve this answer

























            up vote
            38
            down vote













            Several advantages:



            Wing structures are hollow and voluminous in order to provide structural rigidity against flutter and carry flight loads. This provides the space needed to store fuel.



            On a conventional aircraft, placing fuel tanks in the wings places the fuel mass very close to, or on, the center of lift. This dramatically reduces Cg shift during flight and reduces the size and weight of the tailplane to maintain stable flight.



            In the event of a crash landing, having the fuel in the wings keeps it away from the cabin and the occupants, reducing risks of cabin fires.



            The weight of the fuel reduces the loading moment on the wing roots, reducing the weight of the structure needed to support the aircraft during flight.






            share|improve this answer























              up vote
              38
              down vote










              up vote
              38
              down vote









              Several advantages:



              Wing structures are hollow and voluminous in order to provide structural rigidity against flutter and carry flight loads. This provides the space needed to store fuel.



              On a conventional aircraft, placing fuel tanks in the wings places the fuel mass very close to, or on, the center of lift. This dramatically reduces Cg shift during flight and reduces the size and weight of the tailplane to maintain stable flight.



              In the event of a crash landing, having the fuel in the wings keeps it away from the cabin and the occupants, reducing risks of cabin fires.



              The weight of the fuel reduces the loading moment on the wing roots, reducing the weight of the structure needed to support the aircraft during flight.






              share|improve this answer












              Several advantages:



              Wing structures are hollow and voluminous in order to provide structural rigidity against flutter and carry flight loads. This provides the space needed to store fuel.



              On a conventional aircraft, placing fuel tanks in the wings places the fuel mass very close to, or on, the center of lift. This dramatically reduces Cg shift during flight and reduces the size and weight of the tailplane to maintain stable flight.



              In the event of a crash landing, having the fuel in the wings keeps it away from the cabin and the occupants, reducing risks of cabin fires.



              The weight of the fuel reduces the loading moment on the wing roots, reducing the weight of the structure needed to support the aircraft during flight.







              share|improve this answer












              share|improve this answer



              share|improve this answer










              answered 17 hours ago









              Carlo Felicione

              39.6k272147




              39.6k272147






















                  up vote
                  13
                  down vote














                  added weight increases the structural load applied to the wings
                  different gravitational forces and wing-bending between full and empty tanks result in repeating stresses shortening the aircraft life-span




                  As a result of the effects of lift (and the deceasing need for it as the plane lightens) the reverse is actually true see here




                  higher risk of catastrophic damage to wings in case of in-flight fuel ignition




                  As opposed to higher risk of catastrophic damage to the cabin in the case of in-flight fuel ignition?



                  Assuming a non-explosive ignition having the fuel in the wings means you can take action to dump the fuel. If you have a fire begin in the main fuselage however you've got a higher chance of the fire incapacitating the crew before they can take steps. Or damage occuring to the avionics, the pressure cabin etc.




                  maybe higher risk of fire when lightning strikes a wing ?




                  Wing tips are one of the locations on a plane that is more prone to lightning strikes - and the potential for fuel fires is there but steps are taken to counter this and in the vast majority of cases lightning does very little damage






                  share|improve this answer

























                    up vote
                    13
                    down vote














                    added weight increases the structural load applied to the wings
                    different gravitational forces and wing-bending between full and empty tanks result in repeating stresses shortening the aircraft life-span




                    As a result of the effects of lift (and the deceasing need for it as the plane lightens) the reverse is actually true see here




                    higher risk of catastrophic damage to wings in case of in-flight fuel ignition




                    As opposed to higher risk of catastrophic damage to the cabin in the case of in-flight fuel ignition?



                    Assuming a non-explosive ignition having the fuel in the wings means you can take action to dump the fuel. If you have a fire begin in the main fuselage however you've got a higher chance of the fire incapacitating the crew before they can take steps. Or damage occuring to the avionics, the pressure cabin etc.




                    maybe higher risk of fire when lightning strikes a wing ?




                    Wing tips are one of the locations on a plane that is more prone to lightning strikes - and the potential for fuel fires is there but steps are taken to counter this and in the vast majority of cases lightning does very little damage






                    share|improve this answer























                      up vote
                      13
                      down vote










                      up vote
                      13
                      down vote










                      added weight increases the structural load applied to the wings
                      different gravitational forces and wing-bending between full and empty tanks result in repeating stresses shortening the aircraft life-span




                      As a result of the effects of lift (and the deceasing need for it as the plane lightens) the reverse is actually true see here




                      higher risk of catastrophic damage to wings in case of in-flight fuel ignition




                      As opposed to higher risk of catastrophic damage to the cabin in the case of in-flight fuel ignition?



                      Assuming a non-explosive ignition having the fuel in the wings means you can take action to dump the fuel. If you have a fire begin in the main fuselage however you've got a higher chance of the fire incapacitating the crew before they can take steps. Or damage occuring to the avionics, the pressure cabin etc.




                      maybe higher risk of fire when lightning strikes a wing ?




                      Wing tips are one of the locations on a plane that is more prone to lightning strikes - and the potential for fuel fires is there but steps are taken to counter this and in the vast majority of cases lightning does very little damage






                      share|improve this answer













                      added weight increases the structural load applied to the wings
                      different gravitational forces and wing-bending between full and empty tanks result in repeating stresses shortening the aircraft life-span




                      As a result of the effects of lift (and the deceasing need for it as the plane lightens) the reverse is actually true see here




                      higher risk of catastrophic damage to wings in case of in-flight fuel ignition




                      As opposed to higher risk of catastrophic damage to the cabin in the case of in-flight fuel ignition?



                      Assuming a non-explosive ignition having the fuel in the wings means you can take action to dump the fuel. If you have a fire begin in the main fuselage however you've got a higher chance of the fire incapacitating the crew before they can take steps. Or damage occuring to the avionics, the pressure cabin etc.




                      maybe higher risk of fire when lightning strikes a wing ?




                      Wing tips are one of the locations on a plane that is more prone to lightning strikes - and the potential for fuel fires is there but steps are taken to counter this and in the vast majority of cases lightning does very little damage







                      share|improve this answer












                      share|improve this answer



                      share|improve this answer










                      answered 19 hours ago









                      motosubatsu

                      3337




                      3337






















                          up vote
                          9
                          down vote













                          Quite simply: there's a lot of empty space in those wings, and there's a lot of empty space needed for fuel.



                          Creating space elsewhere for fuel would make the entire aircraft larger and heavier, so makes little sense.



                          And it's not just the wings, many aircraft carry fuel in the vertical stabiliser as well.






                          share|improve this answer

















                          • 35




                            In other words: Why are fuel tanks located in the wings? Because the passengers wouldn't fit in there. :)
                            – Tanner Swett
                            18 hours ago






                          • 20




                            @TannerSwett Don't give them any ideas...
                            – pipe
                            16 hours ago






                          • 3




                            @pipe en.wikipedia.org/wiki/Junkers_G.38 ?
                            – DeepSpace
                            14 hours ago










                          • @TannerSwett hmm, Ryanair wants to talk with you about that idea.
                            – jwenting
                            2 hours ago















                          up vote
                          9
                          down vote













                          Quite simply: there's a lot of empty space in those wings, and there's a lot of empty space needed for fuel.



                          Creating space elsewhere for fuel would make the entire aircraft larger and heavier, so makes little sense.



                          And it's not just the wings, many aircraft carry fuel in the vertical stabiliser as well.






                          share|improve this answer

















                          • 35




                            In other words: Why are fuel tanks located in the wings? Because the passengers wouldn't fit in there. :)
                            – Tanner Swett
                            18 hours ago






                          • 20




                            @TannerSwett Don't give them any ideas...
                            – pipe
                            16 hours ago






                          • 3




                            @pipe en.wikipedia.org/wiki/Junkers_G.38 ?
                            – DeepSpace
                            14 hours ago










                          • @TannerSwett hmm, Ryanair wants to talk with you about that idea.
                            – jwenting
                            2 hours ago













                          up vote
                          9
                          down vote










                          up vote
                          9
                          down vote









                          Quite simply: there's a lot of empty space in those wings, and there's a lot of empty space needed for fuel.



                          Creating space elsewhere for fuel would make the entire aircraft larger and heavier, so makes little sense.



                          And it's not just the wings, many aircraft carry fuel in the vertical stabiliser as well.






                          share|improve this answer












                          Quite simply: there's a lot of empty space in those wings, and there's a lot of empty space needed for fuel.



                          Creating space elsewhere for fuel would make the entire aircraft larger and heavier, so makes little sense.



                          And it's not just the wings, many aircraft carry fuel in the vertical stabiliser as well.







                          share|improve this answer












                          share|improve this answer



                          share|improve this answer










                          answered 21 hours ago









                          jwenting

                          10.9k12743




                          10.9k12743








                          • 35




                            In other words: Why are fuel tanks located in the wings? Because the passengers wouldn't fit in there. :)
                            – Tanner Swett
                            18 hours ago






                          • 20




                            @TannerSwett Don't give them any ideas...
                            – pipe
                            16 hours ago






                          • 3




                            @pipe en.wikipedia.org/wiki/Junkers_G.38 ?
                            – DeepSpace
                            14 hours ago










                          • @TannerSwett hmm, Ryanair wants to talk with you about that idea.
                            – jwenting
                            2 hours ago














                          • 35




                            In other words: Why are fuel tanks located in the wings? Because the passengers wouldn't fit in there. :)
                            – Tanner Swett
                            18 hours ago






                          • 20




                            @TannerSwett Don't give them any ideas...
                            – pipe
                            16 hours ago






                          • 3




                            @pipe en.wikipedia.org/wiki/Junkers_G.38 ?
                            – DeepSpace
                            14 hours ago










                          • @TannerSwett hmm, Ryanair wants to talk with you about that idea.
                            – jwenting
                            2 hours ago








                          35




                          35




                          In other words: Why are fuel tanks located in the wings? Because the passengers wouldn't fit in there. :)
                          – Tanner Swett
                          18 hours ago




                          In other words: Why are fuel tanks located in the wings? Because the passengers wouldn't fit in there. :)
                          – Tanner Swett
                          18 hours ago




                          20




                          20




                          @TannerSwett Don't give them any ideas...
                          – pipe
                          16 hours ago




                          @TannerSwett Don't give them any ideas...
                          – pipe
                          16 hours ago




                          3




                          3




                          @pipe en.wikipedia.org/wiki/Junkers_G.38 ?
                          – DeepSpace
                          14 hours ago




                          @pipe en.wikipedia.org/wiki/Junkers_G.38 ?
                          – DeepSpace
                          14 hours ago












                          @TannerSwett hmm, Ryanair wants to talk with you about that idea.
                          – jwenting
                          2 hours ago




                          @TannerSwett hmm, Ryanair wants to talk with you about that idea.
                          – jwenting
                          2 hours ago










                          up vote
                          9
                          down vote













                          I see what you're saying, but there's something you're overlooking in your logic. You're looking at an airplane sitting on the ground, where the wheels are under the fuselage and the wings are deadweight that creates strain on the structure.



                          Think about one in flight. Now all the lift is coming from the wings, imagine the airplane suspended by a couple dozen (billion) cables spread around the wing surfaces. Now the fuselage is deadweight and the strain in the structure is from carrying the fuselage.



                          So when you add weight to the wings evenly, it adds practically zero structural load for the wings. What's being lifted is inside the source of the lift. So from a structural load perspective, it's a wash: it doesn't matter.



                          Whereas if you add more tanks in the fuselage, that's fine on the ground, but it adds huge stresses to the wings inflight, effectively reducing practical cargo capacity.



                          The strain on wings from sitting on the ground is much less worrisome to designers than the strains inflight.



                          See also "Zero Fuel Weight".






                          share|improve this answer























                          • Exactly what I was thinking, but you said it much better!
                            – Michael Hall
                            9 hours ago















                          up vote
                          9
                          down vote













                          I see what you're saying, but there's something you're overlooking in your logic. You're looking at an airplane sitting on the ground, where the wheels are under the fuselage and the wings are deadweight that creates strain on the structure.



                          Think about one in flight. Now all the lift is coming from the wings, imagine the airplane suspended by a couple dozen (billion) cables spread around the wing surfaces. Now the fuselage is deadweight and the strain in the structure is from carrying the fuselage.



                          So when you add weight to the wings evenly, it adds practically zero structural load for the wings. What's being lifted is inside the source of the lift. So from a structural load perspective, it's a wash: it doesn't matter.



                          Whereas if you add more tanks in the fuselage, that's fine on the ground, but it adds huge stresses to the wings inflight, effectively reducing practical cargo capacity.



                          The strain on wings from sitting on the ground is much less worrisome to designers than the strains inflight.



                          See also "Zero Fuel Weight".






                          share|improve this answer























                          • Exactly what I was thinking, but you said it much better!
                            – Michael Hall
                            9 hours ago













                          up vote
                          9
                          down vote










                          up vote
                          9
                          down vote









                          I see what you're saying, but there's something you're overlooking in your logic. You're looking at an airplane sitting on the ground, where the wheels are under the fuselage and the wings are deadweight that creates strain on the structure.



                          Think about one in flight. Now all the lift is coming from the wings, imagine the airplane suspended by a couple dozen (billion) cables spread around the wing surfaces. Now the fuselage is deadweight and the strain in the structure is from carrying the fuselage.



                          So when you add weight to the wings evenly, it adds practically zero structural load for the wings. What's being lifted is inside the source of the lift. So from a structural load perspective, it's a wash: it doesn't matter.



                          Whereas if you add more tanks in the fuselage, that's fine on the ground, but it adds huge stresses to the wings inflight, effectively reducing practical cargo capacity.



                          The strain on wings from sitting on the ground is much less worrisome to designers than the strains inflight.



                          See also "Zero Fuel Weight".






                          share|improve this answer














                          I see what you're saying, but there's something you're overlooking in your logic. You're looking at an airplane sitting on the ground, where the wheels are under the fuselage and the wings are deadweight that creates strain on the structure.



                          Think about one in flight. Now all the lift is coming from the wings, imagine the airplane suspended by a couple dozen (billion) cables spread around the wing surfaces. Now the fuselage is deadweight and the strain in the structure is from carrying the fuselage.



                          So when you add weight to the wings evenly, it adds practically zero structural load for the wings. What's being lifted is inside the source of the lift. So from a structural load perspective, it's a wash: it doesn't matter.



                          Whereas if you add more tanks in the fuselage, that's fine on the ground, but it adds huge stresses to the wings inflight, effectively reducing practical cargo capacity.



                          The strain on wings from sitting on the ground is much less worrisome to designers than the strains inflight.



                          See also "Zero Fuel Weight".







                          share|improve this answer














                          share|improve this answer



                          share|improve this answer








                          edited 12 hours ago

























                          answered 13 hours ago









                          Harper

                          2,105515




                          2,105515












                          • Exactly what I was thinking, but you said it much better!
                            – Michael Hall
                            9 hours ago


















                          • Exactly what I was thinking, but you said it much better!
                            – Michael Hall
                            9 hours ago
















                          Exactly what I was thinking, but you said it much better!
                          – Michael Hall
                          9 hours ago




                          Exactly what I was thinking, but you said it much better!
                          – Michael Hall
                          9 hours ago










                          up vote
                          3
                          down vote















                          • added weight increases the structural load applied to the wings




                          Only when the plane's on the ground. When it's in the air, it decreases the load on the wings because their lift balances the weight.





                          • different gravitational forces and wing-bending between full and empty tanks result in repeating stresses shortening the aircraft life-span




                          At the rate of one cycle per flight. And the wings already go through a stress cycle once per flight (flexed down when the plane's on the ground and up when it's in the air).





                          • higher risk of catastrophic damage to wings in case of in-flight fuel ignition




                          The fuel tanks catching fire in flight is catastrophic wherever you put them.





                          • higher risk of fire when lightning strikes a wing




                          When did that last happen? Wikipedia's list of plane crashes suggests LANSA flight 508 in 1971. Such incidents are so rare because fuel tanks have been fitted with inerting systems as recommended after the crash of Pan Am flight 214 in 1963.






                          share|improve this answer

























                            up vote
                            3
                            down vote















                            • added weight increases the structural load applied to the wings




                            Only when the plane's on the ground. When it's in the air, it decreases the load on the wings because their lift balances the weight.





                            • different gravitational forces and wing-bending between full and empty tanks result in repeating stresses shortening the aircraft life-span




                            At the rate of one cycle per flight. And the wings already go through a stress cycle once per flight (flexed down when the plane's on the ground and up when it's in the air).





                            • higher risk of catastrophic damage to wings in case of in-flight fuel ignition




                            The fuel tanks catching fire in flight is catastrophic wherever you put them.





                            • higher risk of fire when lightning strikes a wing




                            When did that last happen? Wikipedia's list of plane crashes suggests LANSA flight 508 in 1971. Such incidents are so rare because fuel tanks have been fitted with inerting systems as recommended after the crash of Pan Am flight 214 in 1963.






                            share|improve this answer























                              up vote
                              3
                              down vote










                              up vote
                              3
                              down vote











                              • added weight increases the structural load applied to the wings




                              Only when the plane's on the ground. When it's in the air, it decreases the load on the wings because their lift balances the weight.





                              • different gravitational forces and wing-bending between full and empty tanks result in repeating stresses shortening the aircraft life-span




                              At the rate of one cycle per flight. And the wings already go through a stress cycle once per flight (flexed down when the plane's on the ground and up when it's in the air).





                              • higher risk of catastrophic damage to wings in case of in-flight fuel ignition




                              The fuel tanks catching fire in flight is catastrophic wherever you put them.





                              • higher risk of fire when lightning strikes a wing




                              When did that last happen? Wikipedia's list of plane crashes suggests LANSA flight 508 in 1971. Such incidents are so rare because fuel tanks have been fitted with inerting systems as recommended after the crash of Pan Am flight 214 in 1963.






                              share|improve this answer














                              • added weight increases the structural load applied to the wings




                              Only when the plane's on the ground. When it's in the air, it decreases the load on the wings because their lift balances the weight.





                              • different gravitational forces and wing-bending between full and empty tanks result in repeating stresses shortening the aircraft life-span




                              At the rate of one cycle per flight. And the wings already go through a stress cycle once per flight (flexed down when the plane's on the ground and up when it's in the air).





                              • higher risk of catastrophic damage to wings in case of in-flight fuel ignition




                              The fuel tanks catching fire in flight is catastrophic wherever you put them.





                              • higher risk of fire when lightning strikes a wing




                              When did that last happen? Wikipedia's list of plane crashes suggests LANSA flight 508 in 1971. Such incidents are so rare because fuel tanks have been fitted with inerting systems as recommended after the crash of Pan Am flight 214 in 1963.







                              share|improve this answer












                              share|improve this answer



                              share|improve this answer










                              answered 11 hours ago









                              David Richerby

                              9,53833477




                              9,53833477






















                                  up vote
                                  3
                                  down vote













                                  Along with the other answers, I'll point out the cases where an aircraft fuel tank exploded, the center tank, which is in the fuselage, was implicated. There are two reasons:



                                  First, a fuselage tank is located lower than the engines and requires pumps to raise the fuel. Electrical pump failures have caused explosions. This also means that a pump failure results in unusable fuel, whereas wing tanks can naturally feed the engines via gravity.



                                  Second, fuselage tanks are closer to sources of heat. This was a cause of the TWA flight 800 accident, where heat from nearby air conditioning equipment lead to a flammable vapor in the fuel tanks. In contrast, wing tanks are naturally cooled by airflow and are less susceptible to forming such explosive vapors.






                                  share|improve this answer

























                                    up vote
                                    3
                                    down vote













                                    Along with the other answers, I'll point out the cases where an aircraft fuel tank exploded, the center tank, which is in the fuselage, was implicated. There are two reasons:



                                    First, a fuselage tank is located lower than the engines and requires pumps to raise the fuel. Electrical pump failures have caused explosions. This also means that a pump failure results in unusable fuel, whereas wing tanks can naturally feed the engines via gravity.



                                    Second, fuselage tanks are closer to sources of heat. This was a cause of the TWA flight 800 accident, where heat from nearby air conditioning equipment lead to a flammable vapor in the fuel tanks. In contrast, wing tanks are naturally cooled by airflow and are less susceptible to forming such explosive vapors.






                                    share|improve this answer























                                      up vote
                                      3
                                      down vote










                                      up vote
                                      3
                                      down vote









                                      Along with the other answers, I'll point out the cases where an aircraft fuel tank exploded, the center tank, which is in the fuselage, was implicated. There are two reasons:



                                      First, a fuselage tank is located lower than the engines and requires pumps to raise the fuel. Electrical pump failures have caused explosions. This also means that a pump failure results in unusable fuel, whereas wing tanks can naturally feed the engines via gravity.



                                      Second, fuselage tanks are closer to sources of heat. This was a cause of the TWA flight 800 accident, where heat from nearby air conditioning equipment lead to a flammable vapor in the fuel tanks. In contrast, wing tanks are naturally cooled by airflow and are less susceptible to forming such explosive vapors.






                                      share|improve this answer












                                      Along with the other answers, I'll point out the cases where an aircraft fuel tank exploded, the center tank, which is in the fuselage, was implicated. There are two reasons:



                                      First, a fuselage tank is located lower than the engines and requires pumps to raise the fuel. Electrical pump failures have caused explosions. This also means that a pump failure results in unusable fuel, whereas wing tanks can naturally feed the engines via gravity.



                                      Second, fuselage tanks are closer to sources of heat. This was a cause of the TWA flight 800 accident, where heat from nearby air conditioning equipment lead to a flammable vapor in the fuel tanks. In contrast, wing tanks are naturally cooled by airflow and are less susceptible to forming such explosive vapors.







                                      share|improve this answer












                                      share|improve this answer



                                      share|improve this answer










                                      answered 8 hours ago









                                      user71659

                                      2,244617




                                      2,244617






























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