The Caudron Type C was a single seat
French biplane
A biplane is a fixed-wing aircraft with two main wings stacked one above the other. The first powered, controlled aeroplane to fly, the Wright Flyer, used a biplane wing arrangement, as did many aircraft in the early years of aviation. While ...
, intended for military evaluation. Two were built in 1911.
Design and development
From the
Type B of 1911 to the
World War I
World War I or the First World War (28 July 1914 – 11 November 1918), also known as the Great War, was a World war, global conflict between two coalitions: the Allies of World War I, Allies (or Entente) and the Central Powers. Fighting to ...
Caudron G.3 Caudron biplanes had a common layout with
tractor
A tractor is an engineering vehicle specifically designed to deliver a high tractive effort (or torque) at slow speeds, for the purposes of hauling a Trailer (vehicle), trailer or machinery such as that used in agriculture, mining or constructio ...
engines, occupants in a
nacelle
A nacelle ( ) is a streamlined container for aircraft parts such as Aircraft engine, engines, fuel or equipment. When attached entirely outside the airframe, it is sometimes called a pod, in which case it is attached with a Hardpoint#Pylon, pylo ...
mounted between the wings and
empennage
The empennage ( or ), also known as the tail or tail assembly, is a structure at the rear of an aircraft that provides stability during flight, in a way similar to the feathers on an arrow.Crane, Dale: ''Dictionary of Aeronautical Terms, third ed ...
on twin booms. The earlier Types B-D in this sequence began as equal span biplanes, then were modified into
sesquiplane
A biplane is a fixed-wing aircraft with two main wings stacked one above the other. The first powered, controlled aeroplane to fly, the Wright Flyer, used a biplane wing arrangement, as did many aircraft in the early years of aviation. While a ...
s.
[
In its original form, the Type C was an equal-span, wire-braced two-bay biplane, though the inner bay was only about half the width of the outer. The two- spar fabric-covered wings had the same rectangular plan apart from angled tips. Wing area was . There was no stagger, so the two sets of parallel ]interplane strut
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 ...
s were parallel and vertical. The rear spar was ahead of mid- chord, leaving the rib
In vertebrate anatomy, ribs () are the long curved bones which form the rib cage, part of the axial skeleton. In most tetrapods, ribs surround the thoracic cavity, enabling the lungs to expand and thus facilitate breathing by expanding the ...
s in the rear part of the wing flexible and allowing roll control
Roll may refer to:
Physics and engineering
* Rolling, a motion of two objects with respect to each-other such that the two stay in contact without sliding
* Roll angle (or roll rotation), one of the 3 angular degrees of freedom of any stiff bo ...
by wing warping
Wing warping was an early system for lateral (roll) control of a fixed-wing aircraft or kite. The technique, used and patented by the Wright brothers, consisted of a system of pulleys and cables to twist the trailing edges of the wings in opposit ...
.[
The nacelle was a simple, flat sided structure. As on the Type B, it was supported above the lower wing on two more pairs of interplane struts but on the Type C the left and right pairs passed within the nacelle, rather than down its sides. A ]Gnome Omega
The Gnome 7 Omega (commonly called the Gnome 50 hp) is a French seven-cylinder, air-cooled aero engine produced by Gnome et Rhône. It was shown at the Paris Aero Salon held in December 1908 and was first flown in 1909. It was the world's ...
rotary engine
The rotary engine is an early type of internal combustion engine, usually designed with an odd number of cylinders per row in a radial configuration. The engine's crankshaft remained stationary in operation, while the entire crankcase and its ...
was mounted in the front under a rudimentary shield to protect the pilot from oil spray, though a Anzani 3-cylinder radial engine
The radial engine is a reciprocating engine, reciprocating type internal combustion engine, internal combustion engine configuration in which the cylinder (engine), cylinders "radiate" outward from a central crankcase like the spokes of a wheel. ...
could also fitted. The nacelle extended aft at the wing trailing edge
The trailing edge of an aerodynamic surface such as a wing is its rear edge, where the airflow separated by the leading edge meets.Crane, Dale: ''Dictionary of Aeronautical Terms, third edition'', page 521. Aviation Supplies & Academics, 1997. ...
, with the pilot just aft of mid-chord.[
The ]empennage
The empennage ( or ), also known as the tail or tail assembly, is a structure at the rear of an aircraft that provides stability during flight, in a way similar to the feathers on an arrow.Crane, Dale: ''Dictionary of Aeronautical Terms, third ed ...
of the Type C was supported on a pair of girders arranged parallel to one another in plan. The upper girder members were attached to the upper wing spars at the tops of the innermost interplane struts and the lower ones ran under the lower wing, mounted on downward extensions of the inner interplane struts. The mounting was strengthened with two diagonal struts on each side, one from the base of the forward interplane strut to the upcurved tip of the lower member and the other from the rear interplane strut to the junction of the lower member and its first vertical cross member. Each of these lower members, which supported the aircraft on the ground as skids, carried twin, rubber sprung landing wheels. Behind the wing the upper and lower members converged to the rear; the drag on the lower members reduced the landing run to There were three vertical cross braces on each girder but the only lateral inter-girder cross-members were near the tail, though there was wire bracing. The broad chord, roughly rectangular, warping tailplane
A tailplane, also known as a horizontal stabilizer, is a small lift (force), lifting surface located on the tail (empennage) behind the main lifting surfaces of a fixed-wing aircraft as well as other non-fixed-wing aircraft such as helicopters ...
was mounted a little below the upper girder member. Above it, a pair of rectangular rudder
A rudder is a primary control surface used to steer a ship, boat, submarine, hovercraft, airship, or other vehicle that moves through a fluid medium (usually air or water). On an airplane, the rudder is used primarily to counter adverse yaw ...
s were separated by about one third of the tailplane span.[
Two Type Cs were built and delivered to the military in November 1911. In July 1912 they were modified into sesquiplanes to ease their accommodation in field tents. The Type C appeared in the Caudron catalogue of 1912 in that form, with the upper wing overhang supported by parallel, outward leaning ]strut
A strut is a structural component commonly found in engineering, aeronautics, architecture and anatomy. Struts generally work by resisting longitudinal compression, but they may also serve in tension.
A stay is sometimes used as a synonym for ...
s from the bases of the outer interplane struts.[
]
Specifications (1912 catalogue sesquiplane, Gnome engine)
References
Further reading
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{{Caudron aircraft
1910s French military aircraft
TC
Twin-boom aircraft
Sesquiplanes
Rotary-engined aircraft
Aircraft first flown in 1911