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The Warren truss is a prominent structural feature in hundreds of hastily constructed aircraft hangars in WW2. In the early parts of the war, the British and Canadian government formed an agreement known as the British Commonwealth Air Training Plan which used newly constructed airbases in Canada to train aircrew needed to sustain emerging air forces.
A Handley Page H.P.42 showing the Warren Truss diagonal interplane struts. The Warren truss design was used in early aviation when biplanes were dominant, the alternating diagonal truss being used for the interplane struts in aircraft such as the Handley Page H.P.42 airliner and the Fiat CR.42 fighter. The Warren truss is one of the most widely ...
While remaining broadly similar in configuration, the new design replaced the CANT 7's conventional struts with Warren truss bracing for the wings. Most of the aircraft produced were used by S.I.S.A.
The most obvious was the construction of the wings, which had a single spar forming the leading edges of the wings which was an exposed warren truss of a type designed and patented by Fabre. The ribs were cantilevered from this spar, each rib being enclosed in a pocket in the covering, which was laced to the leading edge and attached to the ...
Some biplane wings are braced with struts leaned sideways with the bays forming a zigzag Warren truss. Examples include the Ansaldo SVA series of single-engined high-speed reconnaissance biplanes of World War I, and the early World War II-era Fiat CR.42 Falco. Other variations have also been used.
Production of the aircraft continued well after the war, the final examples were delivered during 1918. The SVA was a conventionally laid-out unequal-span biplane with unusual Warren Truss-style struts joining its wings having no transverse (spanwise) bracing wires.
B.R.1 - improved version with new radiator and landing gear, and Warren truss struts (150 built) B.R.2 - strengthened structure, new landing gear, and Fiat A.25 engine R.22 - reconnaissance aircraft of which two prototypes and 23 production versions were built. Although resembling the BR.2 it was of smaller dimensions and the wing and fuselage ...
The aircraft had conventional construction for the period with a welded steel-tube fuselage having Warren truss structure for its sides; and composite metal, wood and fabric design features, with Frise ailerons, a flat-bottom airfoiled, variable incidence (trimmable) lifting two-piece tailplane; and similarly "lifting airfoil" on the fixed ...
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