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In aeronautics, bracing comprises additional structural members which stiffen the functional airframe to give it rigidity and strength under load. Bracing may be applied both internally and externally, and may take the form of struts, which act in compression or tension as the need arises, and/or wires, which act only in tension.
This change prevented the landing brace wires from whipping and chafing during flight. Otherwise, it had an orthodox structure, comprising wooden members attached to metal joint fixtures. [13] The fuselage consisted of four square-section longerons, with wooden struts and cross-members while braced with heavy-gauge piano wire. Wire cable was ...
One of many many common design features between the new SPAD V and the S.A.2 was the use of a single-bay biplane wing with additional struts mounted mid-bay at the point of junction of the flying and landing wires. This design simplified rigging and reduced drag.
Wire braced A braced multiplane may have one or more "bays", which are the compartments created by adding interplane struts; the number of bays refers to one side of the aircraft's wing panels only. For example, the de Havilland Tiger Moth is a single-bay biplane where the Bristol F.2 Fighter is a two-bay biplane.
Blériot produced a report for the French government which came to the conclusion that the problem was not the strength of the wing spars but a failure to take into account the amount of downward force to which aircraft wings could be subjected, and that the problem could be solved by increasing the strength of the upper bracing wires.
The Fokker Spin was the first airplane built by Dutch aviation pioneer Anthony Fokker. The many bracing wires used to strengthen the aircraft made it resemble a giant spider, hence its name Spin, Dutch for "spider". [1]
Bracing struts and wires of many kinds were extensively used in early aircraft to stiffen and strengthen, and sometimes even to form, the main functional airframe. Throughout the 1920s and 1930s they fell out of use in favour of the low drag cantilever construction. Most aircraft bracing struts are principally loaded in compression, with wires ...
The wings had a single bay, but to prevent the long flying and landing wires from vibrating in flight, light vertical struts were added mid-bay to brace the wires, giving the aircraft the appearance of a two-bay biplane, much as was done for the later, more conventional SPAD S.VII and SPAD S.XIII single-seat fighters. SPAD S.A-2 at Somme-Vesle ...
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