Hydro-triplane | |
---|---|
Role | Amphibious triplane flying boat |
National origin | Germany |
Manufacturer | Euler-Werke |
Designer | August Euler |
Number built | 1 |
The Euler Hydro-triplane was an unusual pusher configuration amphibious triplane flying boat, built in Germany in 1913.
The April 1913 issue of the French magazine L'Aérophile contains a brief, unillustrated reference [1] to an Euler triplane seaplane, powered by a 70 hp (52 kW) Gnome engine, a possible relative of the Hydro-triplane reported in detail by Flight early in the following year. Flight described it as "to the best of our knowledge, the first successful hydro-triplane constructed." [2]
The Euler Hydro-triplane was a large aircraft, powered by a 100 hp (75 kW), nine cylinder Gnome Delta rotary engine, with an upper wingspan of 14 m (45 ft 11 in). All its wings were of essentially rectangular plan though with trailing edge cut-outs. The lower two wings were successively 2 m (6 ft 7 in) shorter. The upper pair formed a three bay structure with pairs of parallel interplane struts and upper wing overhangs supported by outward leaning parallel pairs. The central and lower wings formed a similar but two bay structure. There was strong stagger, with the interplane struts at about 30° to the wing normal. The Gnome engine was mounted, uncowled and in pusher configuration, just above the central wing. Because of the stagger the engine was shielded from spray by the lower wing. There were ailerons on both upper and lower wings. [2]
The lower wings were mounted on the top of a flat bottomed, single-stepped hull with flat sides which tapered in profile toward the rear. The wings were further braced to the hull by a pair of struts reaching back from the nose to the centre wing leading edge. The nose also had raised decking protecting of the pilot, who sat in the front of the open cockpit with a passenger seat behind him. [2]
The empennage of the Hydro-triplane was supported on a pair of lattice girders, parallel in plan and each constructed from a horizontal member fixed to the upper wing at the top of the innermost interplane struts and a member below it which sloped upward from the lower wing to meet the upper one at the tail. Three sloping cross braces completed each girder. The rectangular tailplane, fitted with elevators, was placed over the ends of the girders, its leading edge braced by a central, vertical strut to the hull which also supported the rudder post out beyond the hull on upper and lower sloping struts. The trapezoidal rudder extended a little above the horizontal tail, which had a deep V-shaped cut-out to accommodate its movement. [2]
The Euler Hydro-triplane was a true amphibian with twin mainwheels on upper and lower pairs of struts attached to the hull, the former rubber sprung. Ground clearance was minimal. The wheels could be raised by the pilot in flight on a land to water flight and lowered at the end of the reverse journey. [2]
Flight's description of the Euler Hydro-triplane as "successful" [2] implies that it had flown by January 1914. It was not mentioned again in that magazine until October 1914, after the outbreak of World War I, when it was amongst those 'Aircraft "made in Germany" which may be used against the Allies'; [3] there is no suggestion that it was ever armed.
Data from Flight 24 January 1914 p.95 [2]
General characteristics
The Voisin Canard was an aircraft developed by Voisin brothers during 1910 and first flown early in 1911. It was named the Canard because of the resemblance of its forward fuselage to that of a duck's long neck while in flight. It was originally flown as a landplane: with the addition of floats it became one of the first seaplanes used by the French Navy.
The Blackburn Triplane was a single-engine pusher single-seater, designed specifically to attack Zeppelins. It flew in 1917, but was not successful.
The Dunne D.8 of 1912 was a tailless swept wing biplane, designed by J. W. Dunne to have inherent stability. One example was supplied to RAE Farnborough. License-built Burgess-Dunne models were used by the US Signal Corps and United States Navy and the short-lived Canadian Aviation Corps. It was the latter's first and only warplane.
The Graham-White Type VII "Popular" was an early British aircraft designed by J. D. North and built by the Grahame-White Aviation company, with the intention of producing a low-cost aircraft to popularize aviation. It was initially produced with a 35 hp Anzani 3-cylinder Y configuration engine and offered for sale at a price of less than £400. Despite its low price the aircraft included structural refinements such as hollow-section interplane struts. It was first flown in 1913.
The Caproni-Pensuti 2 was a small single-engine sports triplane aircraft designed and built in Italy just before the end of World War I. It had a wingspan of only 4.0 m or a little over 13 ft.
The Paalson Type 1, (Pålson), was a Swedish single-seat sport aircraft built around 1920. It was of conventional single-seat biplane layout but had some unusual features such as girder type interplane struts, a novel main undercarriage axle mounting and a mechanism allowing adjustment of the angle of incidence of the upper wing.
The Voisin Type de Course was an early French aircraft built by Voisin Frères. It was first flown early in 1910.
The Paulhan biplane was a French experimental aircraft designed in 1910 by the successful aviator Louis Paulhan in collaboration with Henri Fabre. The prototype became the second aircraft bought by the British War Office: two further examples, differing in constructional detail, were built.
The Bréguet Type II was the second fixed-wing aircraft design produced by Louis Bréguet. Built during late 1909, it was soon discarded in favour of his next design, the Bréguet Type III
The Potez XVIII was a French airliner from the early 1920s, a three-engine biplane carrying up to twelve passengers.
The Caudron Type O was a French single seat air racing biplane first flown in 1914.
The Hydroaéroplane Caudron-Fabre, (Caudron-Fabre), was a French amphibious seaplane which competed in the 1912 Monaco event. It was one of the first true amphibians, able to take-off from water and touch down on land.
The Caudron Type H was a collective name for three different Caudron designs of 1912-3. One of these was an amphibious three seat biplane built for the French military. Two were completed, one appearing at the Paris Aero Salon in November 1912.
The Caudron Type L was a two-seat French pusher configuration amphibious biplane, flown around 1913 and intended for naval use.
The Caudron Type B was a 1911 development of the earliest Caudron type, the Caudron Type A, with a nacelle style fuselage and more powerful engine. Initially an equal span biplane, it was modified into a sesquiplane.
The Caudron Type K was a French floatplane with a very powerful, twenty cylinder radial engine in pusher configuration. It took part in a French seaplane competition in 1913, but was lost in a take-off accident during the competition.
The Caudron Type C was a single seat French biplane, intended for military evaluation. Two were built in 1911.
The Caudron Type F was a French single seat biplane produced just before World War I. A dozen were bought by China and at least two other examples, with different engines, competed in 1913, coming first and second in the biplane category of the cross-country race at Reims. Flown by Pierre Chanteloup, one was the first biplane to loop-the-loop.
The Caudron Type D was a French pre-World War I single seat, twin-boom tractor biplane, a close but slightly smaller relative of the two seat Caudron Type C. More than a dozen were completed, one exported to the United Kingdom, where they may also have been licence built, and three to China.
The Caudron Type E two seat trainer was a larger and more powerful development of the Type C. Two or three were bought by the French military and one by the Royal Navy just before World War I but its sales were overtaken by the superior Type G.