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  2. Longeron - Wikipedia

    en.wikipedia.org/wiki/Longeron

    Interior of a Boeing/Stearman PT-17 showing small channel section stringers. In engineering, a longeron or stringer is a load-bearing component of a framework. The term is commonly used in connection with aircraft fuselages and automobile chassis. Longerons are used in conjunction with stringers to form structural frameworks. [1]

  3. Spar (aeronautics) - Wikipedia

    en.wikipedia.org/wiki/Spar_(aeronautics)

    The spar carries flight loads and the weight of the wings while on the ground. Other structural and forming members such as ribs may be attached to the spar or spars, with stressed skin construction also sharing the loads where it is used. There may be more than one spar in a wing or none at all.

  4. Rib (aeronautics) - Wikipedia

    en.wikipedia.org/wiki/Rib_(aeronautics)

    Wing ribs of a de Havilland DH.60 Moth. In an aircraft, ribs are forming elements of the airframe structure of a wing, especially in traditional construction.. By analogy with the anatomical definition of "rib", the ribs attach to the main spar, and by being repeated at frequent intervals, form a skeletal shape for the wing.

  5. Airframe - Wikipedia

    en.wikipedia.org/wiki/Airframe

    The internal structure comprises stringers, spars, bulkheads, chord members, and various attaching fittings made of aluminum extrusions, formed sheet, forgings, and castings. The alloys most used for extruded members are 2024-T4 for sections less than 0.125 in. thick and for general application, and 2014-T6 for thicker, more highly stressed ...

  6. Wingbox - Wikipedia

    en.wikipedia.org/wiki/Wingbox

    While internal wing structure commonly provides much of the strength via a combination of spars, ribs and stringers, the external skin typically carries a proportion of the loads too. On many aircraft, the inner volume of the wingbox has also been used to store fuel, which is commonly referred to as being a wet wing design. [1]

  7. Boeing C-17 Globemaster III - Wikipedia

    en.wikipedia.org/wiki/Boeing_C-17_Globemaster_III

    A static test of the C-17 wing in October 1992 resulted in its failure at 128% of design limit load, below the 150% requirement. Both wings buckled rear to the front and failures occurred in stringers, spars, and ribs. [17] Some $100 million was spent to redesign the wing structure; the wing failed at 145% during a second test in September 1993 ...

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    www.aol.com/games/play/masque-publishing/hearts

    Enjoy a classic game of Hearts and watch out for the Queen of Spades!

  9. Airspeed Oxford - Wikipedia

    en.wikipedia.org/wiki/Airspeed_Oxford

    Both the elevator and fin of the tail unit used a wooden spar and rib structure covered by fabric. [5] The fuselage can be partially dismantled, the wing dividing into three separate sections, so that it can be road-transported. The wing uses a stressed-skin ply-covered structure using spruce flanges and ply webs. [5]