Kellner-Béchereau 28VD
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The Kellner-Béchereau 28VD was a French racing aircraft built to compete in the 1933
Coupe Deutsch de la Meurthe The Coupe Deutsch de la Meurthe was an international aeronautical speed competition instituted on 25 August 1909 by the French oil magnate Henry Deutsch de la Meurthe. The race was reinstated three times through the years at the initiative of the ...
. Engine failure and damage sustained in the consequent emergency landing prevented the 28VD from participation in the race.


Design and development

The Kellner-Béchereau 28VD was designed to compete in the 1933 Coupe Deutsch, a race around a circuit from Etampes in two flights separated by a refuelling stop. Engines of less than were stipulated; the Delage 12C.E.D.irs engine of the 28VD just met this limit. The 28VD was a
low wing A monoplane is a fixed-wing aircraft configuration with a single mainplane, in contrast to a biplane or other types of multiplanes, which have multiple planes. A monoplane has inherently the highest efficiency and lowest drag of any wing confi ...
,
cantilever A cantilever is a rigid structural element that extends horizontally and is supported at only one end. Typically it extends from a flat vertical surface such as a wall, to which it must be firmly attached. Like other structural elements, a canti ...
monoplane A monoplane is a fixed-wing aircraft configuration with a single mainplane, in contrast to a biplane or other types of multiplanes, which have multiple planes. A monoplane has inherently the highest efficiency and lowest drag of any wing confi ...
. Its
wing span The wingspan (or just span) of a bird or an airplane is the distance from one wingtip to the other wingtip. For example, the Boeing 777–200 has a wingspan of , and a wandering albatross (''Diomedea exulans'') caught in 1965 had a wingspan of ...
was small (; a wing area large enough to keep the
wing loading In aerodynamics, wing loading is the total mass of an aircraft or flying animal divided by the area of its wing. The stalling speed of an aircraft in straight, level flight is partly determined by its wing loading. An aircraft or animal with a ...
to values comparable to those of
World War II World War II or the Second World War, often abbreviated as WWII or WW2, was a world war that lasted from 1939 to 1945. It involved the vast majority of the world's countries—including all of the great powers—forming two opposin ...
fighter aircraft Fighter aircraft are fixed-wing military aircraft designed primarily for air-to-air combat. In military conflict, the role of fighter aircraft is to establish air superiority of the battlespace. Domination of the airspace above a battlefield ...
designed a few years later produced an aspect ratio of only 4.2. In plan the wing was carefully faired into the
fuselage The fuselage (; from the French ''fuselé'' "spindle-shaped") is an aircraft's main body section. It holds crew, passengers, or cargo. In single-engine aircraft, it will usually contain an engine as well, although in some amphibious aircraft t ...
and had a swept, straight
leading edge The leading edge of an airfoil surface such as a wing is its foremost edge and is therefore the part which first meets the oncoming air.Crane, Dale: ''Dictionary of Aeronautical Terms, third edition'', page 305. Aviation Supplies & Academics, ...
, rounded tips and a curved
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. ...
entirely occupied by
ailerons An aileron (French for "little wing" or "fin") is a hinged flight control surface usually forming part of the trailing edge of each wing of a fixed-wing aircraft. Ailerons are used in pairs to control the aircraft in Flight dynamics, roll (or ...
. There were two
spar SPAR, originally DESPAR, styled as DE SPAR, is a Dutch multinational that provides branding, supplies and support services for independently owned and operated food retail stores. It was founded in the Netherlands in 1932, by Adriaan van Well, ...
s, one perpendicular to the fuselage at mid- chord and one at an angle bearing the ailerons. Its fuselage was slender, with a rounded cross-section. The water-cooled, double-
supercharged In an internal combustion engine, a supercharger compresses the intake gas, forcing more air into the engine in order to produce more power for a given displacement. The current categorisation is that a supercharger is a form of forced induct ...
, inverted V-12 Delage engine drove a large diameter, two blade propeller. Its
radiator Radiators are heat exchangers used to transfer thermal energy from one medium to another for the purpose of cooling and heating. The majority of radiators are constructed to function in cars, buildings, and electronics. A radiator is always a ...
s were in the wing. There were two on each side, one inboard and one outboard, both occupying the full chord and forming the wing skin. An open
cockpit A cockpit or flight deck is the area, usually near the front of an aircraft or spacecraft, from which a Pilot in command, pilot controls the aircraft. The cockpit of an aircraft contains flight instruments on an instrument panel, and the ...
was placed a little in front of the trailing edge of the wing, within a narrow dorsal fairing which stretched over half the fuselage, starting close to the nose. The fuselage tapered rearwards to a conventional tail, with a round-tipped triangular
tailplane A tailplane, also known as a horizontal stabiliser, is a small 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 and gyroplane ...
, mounted at mid-fuselage, which had an adjustable angle of incidence. Its
vertical tail A vertical stabilizer or tail fin is the static part of the vertical tail of an aircraft. The term is commonly applied to the assembly of both this fixed surface and one or more movable rudders hinged to it. Their role is to provide control, sta ...
was tall and slightly rounded and the unbalanced rudder extended down to the keel. The
landing gear Landing gear is the undercarriage of an aircraft or spacecraft that is used for takeoff or landing. For aircraft it is generally needed for both. It was also formerly called ''alighting gear'' by some manufacturers, such as the Glenn L. Martin ...
of the 28VD had retractable mainwheels, mounted on shock absorbing forward-raked, parallel legs from the wing. These were hinged to the lower fuselage on opened U-shaped frames. Retraction was vacuum-powered; to raise the wheels the tops of the legs were translated outward, swinging frames and wheels upwards. The tailskid was fixed to a small ventral extension of the fuselage under the fin. The 1933 Coupe Deutsch de la Meurthe was scheduled to start on 28 May and each aircraft had to make a flight at more than over a course in the period 8–14 May to participate. The 28VD arrived at Etampes on 3 May to be flown by Vernhol; it is not known how much flying it had done before that, though it was only completed a fortnight before the competition. The early days of the test period were occupied with the refinement of the 28VD but on the 12–13 May it was reported to have engine problems. During the early tests it was decided to set a finer propeller pitch as the initial setting was producing to much drag on the engine. When the aircraft attempted its qualifying flight on the last allowed day, this change of setting allowed the engine to overspeed. As a result, a rubber joint in the cooling system failed, releasing a cloud of vapour which temporarily blinded the pilot and forced an emergency landing in which the undercarriage collapsed and the aircraft overturned. Vernhol was thrown clear and was not seriously hurt but the 28VD was too damaged to take part in the contest for which it was built.


Specifications


References

{{DEFAULTSORT:Kellner-Bechereau 28VD Kellner-Béchereau aircraft 1930s French sport aircraft Low-wing aircraft Single-engined tractor aircraft Aircraft first flown in 1933