The Breguet Type II was the second fixed-wing aircraft design produced by

Louis Breguet Louis Charles Breguet (2 January 1880 in Paris – 4 May 1955 in Saint-Germain-en-Laye, Île-de-France) was a French aircraft designer and builder, one of the early aviation pioneers. Biography Louis Charles Breguet was the grandson of L ...

. Built during late 1909, it was soon discarded in favour of his next design, the Breguet Type III

Design

Like Breguet's previous design, the

Breguet Type I Breguet or Bréguet may refer to: * Breguet (watch), watch manufacturer **Abraham-Louis Breguet (1747–1823), Swiss watchmaker **Louis-François-Clement Breguet (1804–1883), French physicist, watchmaker, electrical and telegraph work * Bréguet ...

, the structure was principally of metal, although less highly stressed parts such as the tail surfaces used wood. It had a triangular section

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 ...

of wire-braced steel tube with the air-cooled Renault engine at the front: this drove a three-bladed propeller which was connected to the engine's

camshaft A camshaft is a shaft that contains a row of pointed cams, in order to convert rotational motion to reciprocating motion. Camshafts are used in piston engines (to operate the intake and exhaust valves), mechanically controlled ignition systems ...

and so revolved at half the speed of the engine. The wings had pressed aluminium

rib In vertebrate anatomy, ribs ( la, costae) are the long curved bones which form the rib cage, part of the axial skeleton. In most tetrapods, ribs surround the chest, enabling the lungs to expand and thus facilitate breathing by expanding the ches ...

s threaded onto a mainspar of diameter steel tube. These were connected by a single interplane strut on either side. Tail surfaces consisted of a pair of horizontal surfaces, the lower carried on the rear of the fuselage and the upper by a pair of booms running back from the centre section of the upper wing. The upper surface was movable to achieve pitch control. A rectangular balanced rudder was mounted between the two horizontal surfaces. In addition a pair of small horizontal stabilising surfaces were mounted at the front of the aircraft either side of the engine. The pilot's seat was positioned halfway between the wings and the tail surfaces: a passenger seat was fitted behind the engine. The main undercarriage employed oleo-pneumatic suspension, and there was a single steerable tailwheel. It was intended that lateral stability would be achieved by automatic differential movement of the two halves of the upper wing, this feature being the subject of a patent filed by Bréguet. In a turn, the greater speed of the outer wing would cause the

angle of attack In fluid dynamics, angle of attack (AOA, α, or \alpha) is the angle between a reference line on a body (often the chord line of an airfoil) and the vector representing the relative motion between the body and the fluid through which it is m ...

to be reduced, so eliminating the increase in lift that the greater speed would otherwise have produced. Lateral control was effected by a pair of mid-gap ailerons mounted on the interplane struts: these were evidently not effective and Bréguet intended to use another method for lateral control in his next design.

Operational history

Its first recorded flight was made on 5 January 1910, when Louis Breguest made three circuits of the flying field at La Brayelle near Douai. and on 16 January 1910 it made a flight of However, by April 1910 Bréguet was flying his next design, the Type III.

Specifications

References

{{Breguet aircraft II 1910s French experimental aircraft Biplanes Aircraft first flown in 1910 Single-engined tractor aircraft