Английская Википедия:Caudron Types M and N

Содержание

Текст

Текст

Текст

Текст

Текст

Текст

Текст

Текст

Текст

The Caudron Types M and N were small, fast French sports monoplanes, flown 1911–13 under a wide range of engine powers. There was also a military version.

Design and development

Although almost all the aircraft designed by the Caudron brothers in the twenty years from their first attempts in 1908 were biplanes, they did in 1911-2 produce three monoplane types. These were the single seat racing Types M and N and the related but somewhat larger Type M2 military version. The Types M and N were very similar and, though the designations were reported together with some details in contemporary accounts, for example in l'Aérophile in 1912, it has proved difficult for modern historians to distinguish them. They shared the same fuselage and both used a variety of engines but a comparison of data from different contemporary sources suggests that the Type M had a larger wing than the Type N. Though there is some scatter, the span of the Type M was close to Шаблон:Convert and of the Type N to Шаблон:Convert. In contrast, wing area varied within types.

Around this time, various French manufacturers like Voisin and Farman were hoping to improve the stability of aircraft against gusts by using wings that were partly flexible like those of birds and the Caudron Types M and N also included this feature. Each wing had two steel tube, wood filled spars, one at the leading edge and the other Шаблон:Convert aft, a little behind one third chord, with ash ribs and wire bracing. The number of ribs varied between 10, 11 and 12 and they were conventionally rigid between the spars. Behind the rear spar the upper part of each rib was also rigid, ending at about 70% chord; the lower part was completed by a thin, flexible extension strip for about 60% of the chord. The wing was then fabric covered, though the flexible portion was only covered on the upper side. The wings were supported from above by landing wires from a four-legged pylon above the fuselage and by lifting wires from another below, shorter on the Type N than on the Type M. On the latter the tip of the lower pylon was braced by a horizontal, longitudinal strut to the centre of the undercarriage frame. Lateral control was by wing warping.

The structural fuselage of the Types M and N was a rectangular section, ash framed lattice girder with wire cross bracing. Poplar formers and stringers produced a more rounded, fabric covered section. The pilot sat well down in an open cockpit over the wing and behind the upper pylon. A wide range of engines were fitted, including the Шаблон:Convert Anzani three cylinder inverted Y radial engine, the Шаблон:Convert Anzani 6-cylinder two row radial and the Шаблон:Convert Gnome. The last, a rotary engine, was usually covered over the upper part to screen the pilot from oil spray; the Anzanis were mounted uncowled. They all drove large, rather broad chord propellers. The very broad chord, low aspect ratio tailplane was constructed like the wing with a flexible rear surface acting both to improve stability and, by warping, act like conventional elevators, its trailing edge extending well beyond the end of the fuselage. A small, near rectangular, one piece, rigid fin was pivoted near its leading edge from the extreme tail.

The Types M and N had a tailskid undercarriage. A transverse steel bar was fixed at each end to an ash V-strut from the lower fuselage and further braced with a steel V-strut from its centre. A pair of axles, hinged at the centre of the bar, passed through the vertices of the ash struts via rubber shock absorbers with the mainwheels, slightly toed out and Шаблон:Convert apart, beyond them. Early versions of the undercarriage used a single axle rather than a split one. There was an unusually long, curved, tall tailskid at the rear to keep the long tailplane clear of the ground.

Apart from basic specification (dimensions, weights and speed) in Laérophile and Jane's All the World's Aircraft 1913, no records of the Type M2 are currently known.

Operational history

The first flight dates are not currently known, nor which type flew first, but there are reports of a Type N, piloted by Renée Caudron, flying on 23 December 1911. Fitted with the Шаблон:Convert Anzani engine, it flew an out and return flight from Caudron's Le Crotoy base to Pointe-Saint-Quentin at Шаблон:Convert. Two days later it was on display at the 1911 Paris Salon. It was re-engined with a Шаблон:Convert Anzani for an English owner, E.W. Ewen, who flew it home across the English Channel on 2 May 1912. Flown by Maurice Guillaux it took part in a circuit of London race in June 1912, starting from Hendon, but retired from lack of fuel just before the end when it looked a likely winner. After many modifications it was on display at the Olympia show in February 1913. In September 1913 F. Goodden demonstrated it the Aerial Derby at Hendon, powered by a Шаблон:Convert Anzani; it had been entered for the race with the Шаблон:Convert engine but did not compete. The Шаблон:Convert wing area of this aircraft, possibly the only Type N, was much smaller than that usually quoted (Шаблон:Convert). Though its span was Шаблон:Convert less than the Шаблон:Convert said to indicate a Type N and shown on the three-view in L'Aérophile, the main cause was a narrow chord (Шаблон:Convert) compared with the Шаблон:Convert found in the French references.

Emile Obre flew many demonstration flights in early 1912 with a Type M, powered by a Шаблон:Convert Gnome engine. He flew across mainland France and in Corsica, Sardinia and French colonies in North Africa, visiting Tunis and Carthage, where the aircraft was damaged in an accident. At least three Type Ms were built.

Variants

Type M

Span Шаблон:Convert and long lower pylon braced to the undercarriage cross-member.

Type M2

Military machine, span Шаблон:Convert, wing area Шаблон:Convert, length Шаблон:Convert, weight Шаблон:Convert, maximum speed about Шаблон:Convert.

Type N

Span Шаблон:Convert and short lower pylon.