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Longeron

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(Redirected fromStringer (aircraft))
Load-bearing component of a framework
Interior of a Boeing/Stearman PT-17 showing small channel section stringers

Inengineering, alongeron orstringer is a load-bearing component of a framework.

The term is commonly used in connection withaircraft fuselages andautomobilechassis. Longerons are used in conjunction with stringers to form structural frameworks.[1]

Aircraft

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Longerons, struts and stringers in atruss type fuselage structure[2]: 3–4 

In an aircraft fuselage, stringers are attached toformers (also called frames)[3] and run in the longitudinal direction of the aircraft. They are primarily responsible for transferring the aerodynamic loads acting on the skin onto the frames and formers. In the wings or horizontal stabilizer, longerons run spanwise (from wing root to wing tip) and attach between theribs. The primary function here also is to transfer the bending loads acting on the wings onto the ribs and spar.

The terms "longeron" and "stringer" are sometimes used interchangeably. Historically, though, there is a subtle difference between the two terms. If the longitudinal members in a fuselage are few in number (usually 4 to 8) and run all along the fuselage length, then they are called "longerons". The longeron system also requires that the fuselage frames be closely spaced (about every 4 to 6 in or 10 to 15 cm). If the longitudinal members are numerous (usually 50 to 100) and are placed just between two formers/frames, then they are called "stringers". In the stringer system the longitudinal members are smaller and the frames are spaced further apart (about 15 to 20 in or 38 to 51 cm). Generally, longerons are of larger cross-section when compared to stringers. On large modern aircraft the stringer system is more common because it is more weight-efficient, despite being more complex to construct and analyze. Some aircraft use a combination of both stringers and longerons.[4]

Longerons often carry larger loads than stringers and also help to transfer skin loads to internal structure. Longerons nearly always attach to frames orribs. Stringers are usually not attached to anything but theskin, where they carry a portion of the fuselage bending moment through axial loading.[5] It is not uncommon to have a mixture of longerons and stringers in the same major structural component.

Space launch vehicles

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Stringers are also used in the construction of somelaunch vehiclepropellant tanks. For example, theFalcon 9 launch vehicle uses stringers in thekerosene (RP-1) tanks, but not in theliquid oxygen tanks, on both the first and second stages.[6]

See also

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References

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  1. ^"Longeron".The Free Dictionary. Retrieved2018-05-15.
  2. ^"Pilot's Handbook of Aeronautical Knowledge".Federal Aviation Administration. August 24, 2016. Retrieved16 January 2023.
  3. ^V, Vignesh."Reconnaisance [sic] aircraft design project".{{cite journal}}:Cite journal requires|journal= (help)
  4. ^Bruhn, E. F (1973).Analysis and Design of Flight Vehicle Structures(PDF). Tri-State Offset Company. p. C11.29.
  5. ^Michael C. Y. Niu (1988).Airframe Structural Design(PDF). Conmilit Press LTD. p. 376.
  6. ^"Falcon 9 Launch Vehicle Payload User's Guide, Rev 2"(PDF). 21 October 2015. p. 11. Archived fromthe original(PDF) on 14 March 2017. Retrieved29 January 2016.
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