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The word monocoque is a French term for "single shell". [1] First used for boats, [2] a true monocoque carries both tensile and compressive forces within the skin and can be recognised by the absence of a load-carrying internal frame. Few metal aircraft other than those with milled skins can strictly be regarded as pure monocoques, as they use ...
Fuselage of a Boeing 737 shown in brown. The fuselage (/ ˈ f juː z əl ɑː ʒ /; from the French fuselé "spindle-shaped") is an aircraft's main body section. It holds crew, passengers, or cargo.
Van's RV-14 cutaway showing its airframe. The mechanical structure of an aircraft is known as the airframe. [1] This structure is typically considered to include the fuselage, undercarriage, empennage and wings, and excludes the propulsion system.
The monocoque sections were very early examples of double-skinned construction, with a smooth outer skin riveted to a longitudinally-corrugated inner skin. The detailed design was by W.T.Read. The complete fuselage was of round-cornered rectangular cross-section and quite slender, mounted between the wings.
The Zeppelin-Lindau D.I had stressed skin fuselage and wings.. In mechanical engineering, stressed skin is a rigid construction in which the skin or covering takes a portion of the structural load, intermediate between monocoque, in which the skin assumes all or most of the load, and a rigid frame, which has a non-loaded covering.
The Deperdussin Monocoque was a mid-wing monoplane with parallel-chord wings with the spars made of hickory and ash, and ribs made of pine.The fuselage was made in two halves, each made by glueing and pinned a layer of tulip wood to a framework of hickory supported by a former, and then applying two further layers of tulipwood, the thickness of the shell being around 4 mm (5 ⁄ 32 in). [5]
Diagram of the I-250's engine installation The I-250 was a low-wing, all-metal aircraft with a monocoque fuselage. Other than the VRDK the aircraft was largely conventional in layout, although the cockpit was set very far back in the fuselage, almost to the base of the vertical tail.
The oval-section fuselage was a frameless monocoque shell built in two vertically separate halves formed over a mahogany or concrete mould. [ nb 11 ] Pressure was applied with band clamps . Some of the 1/2—3/4" shell sandwich skins comprised 3/32" birch three-ply outers, with 7/16" cores of Ecuadorean balsa .