By Brett Smith
British Airways Airbus A321-231 taking off from Boryspil airport, Ukraine
Image credit: turbo83 / Shutterstock.com
The fuselage is the principal structure of an aircraft and the part to which all other units attach. It supplies room for the crew, passengers, freight, accessories and other important equipment.
Aerodynamics mostly dictate the size and layout of the various compartments in fuselages of conventional aircraft. Only highly-specialized, modern planes, like the SR-71 Blackbird, vary distinctly from conventional planes with respect to their design and materials used to build them.
During the early days of aviation, primitive fuselages were built with wood. In the late 1920s and early 1930s, airplane manufacturers started producing more fuselages from aluminum and steel. These metals offered more stability and greater protection from the elements. Many military and reconnaissance planes today are made from titanium or carbon composite materials because of the unique advantages these materials offer.
Some airplane fuselages are constructed in what is called a monocoque design, a design that relies largely on the strength of the plane’s shell to carry different loads. A semimonocoque fuselage has the shell reinforced by a complete framework of structural members.
Bending stresses on a semimonocoque fuselage are absorbed by reinforcement beams called “longerons,” which usually extend across the width of the plane. These supports are supplemented by other members, called “stringers,” which stretch the length of the craft. Stringers are lighter, but used more extensively than longerons.
Vertical reinforcements on a fuselage are referred to as bulkheads, frames, and formers. These reinforcements are spaced
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