Applications
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Marine Aircraft By the late 1920s many manufacturers started using aluminum to replace the internal framing, and in some cases, the external skin. The structure of the plane consisted of a latticework of U-shaped aluminum beams, with a thin skin of aluminum riveted to it. When these designs started appearing it was realized that the skin itself had significant structural properties of its own. Combining structural skin with a greatly reduced internal framing to provide strength against buckling in compression led to what is known as "semi-monocoque". The result was a structure that was just as strong as ones made with older methods, but weighed considerably less. As well, the monocoque structure has high torsion stiffness, important in reducing aero elastic effects as aircraft speeds increased. At the beginning of World War II the technique was just starting to appear, and many aircraft still used mixed construction. By the end, all planes were monocoque. Automobiles In the post-war period the technique became more widely used. The Alec Issigonis designed Morris Minor of 1948 featured a monocoque body. The Ford Consul introduced an evolution called unit body or unibody. In this system, separate body panels are still used but are bolted to a monocoque body-shell. Spot welded unibody construction is now the dominant technique in automobiles, though some vehicles (particularly trucks) still use the older body-on-frame technique. In automobiles, it is common to see true monocoque frames, where the structural members around the window and door frames are built by folding the skin material several times. Compared to older techniques, in which a body is bolted to a frame, monocoque cars are less expensive and stronger. Bicycles |
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