Potez 28 | |
---|---|
Renault powered Potez 28 | |
Role | Long range record aircraft |
National origin | France |
Manufacturer | Henri Potez |
First flight | 1926 |
Number built | 2 |
The Potez 28 was a French aircraft designed in the 1920s to set distance records, built in both sesquiplane and monoplane versions. Only two were completed but both set several long distance records.
The Potez 28, known also as the Potez 28/2 [1] or the Potez 28 G.R. (Grands Raids or long distance flights, a standard French description of such types) was a close relative of both the Potez 25 and the Potez 25 G.R., all single engine sesquiplanes. In its original biplane form it was particularly like the latter, though strengthened and somewhat enlarged with an upper wingspan increased by 19% to allow for the weight of extra fuel. Unusually for such a large machine, it was a single bay biplane, with two spar wings. The lower wing was both shorter and narrower (55%) in chord than the upper, resulting in it having only 36% of the area. Pairs of interplane struts leaned outwards and diverged toward the more widely separated upper wing spars. The upper wing was supported over the fuselage by further pairs of outward leaning struts from the upper fuselage, converging to its spars. [2]
The fuselage of the Potez 28 was flat sided, with rounded decking and two open cockpits placed well behind the upper wing. There was a cut-out in the trailing edge of the upper wing to improve the pilot's field of view. Large external supplementary fuel tanks could be carried below the fuselage to extend the range. The sesquiplane was powered by a 410 kW (550 hp) Renault 12Kg engine, driving a two blade propeller. At the rear the fin was small and roughly quadrantal, topped by the horn of the balanced rudder. It had a fixed tail wheel undercarriage with single main wheels mounted on vertical, streamlined, shock absorbing legs attached to the lower fuselage. These were hinged on trailing struts to the outer lower fuselage and on inner struts to its central lower underside. [2]
The first Potez 28 was first flown in the first half of 1926. [3]
A second Potez 28 was built, powered by a 500 hp (370 kW) W-12 configuration Farman 12We engine. The three cylinder banks each had their own cowlings. During 1927 it was converted into a monoplane, with a parasol wing with an area of 63 m2 (678 sq ft), almost the same as the biplane. Its wing had a straight leading edge but there was straight taper on the trailing edges of the outer panels. The crew of two were now enclosed under a long, continuous canopy. [4] [5] It was test flown in May 1927. [6]
The Potez 28 and 28M were built to compete with the Breguet 19 GR over long distances. The Renault engined machine set a new world distance record with a flight from Paris to Basra, piloted by the brothers Ludovic and Paul Arrachart. [3] Leaving Paris on 26 June they landed at RAF Shaibah, a few kilometers from Basra, with a broken fuel pipe, having covered a distance of 4,313 km (2,680 mi) in 26 hours 30 min. [3] [6]
The Potez 28M set six speed, distance and duration records whilst carrying loads of 500 kg (1,102 lb) and 1,000 kg (2,205 lb) over distances between 500–2,000 km (311–1,243 mi). It was lost during the take-off for a record attempt, a flight from Etampes to Siberia, when the weight caused a tyre to burst; the pilots escaped unhurt. [5] [6]
Data from Flight, 2 December 1926 [2]
General characteristics
Performance
The Polikarpov DI-1, also known as 2I-N1, Russian: Поликарпов ДИ-1 (2И-Н1), was a prototype Soviet two-seat fighter designed during the 1920s. The sole prototype built crashed on its ninth flight, due to manufacturing defects, and the program was cancelled.
The Fairey G.4/31 was a British single-engined, two-seat biplane contender for an Air Ministry specification for a multi-role or general purpose aircraft. Unsuccessful, only one was built.
The Farman F.160 A.2 was a 1920s French sesquiplane designed as a military reconnaissance and observation aircraft. Only one was built.
The Junkers T 23 was a two-seat, single-engined experimental training aircraft, built in Germany in the early 1920s. It could be configured either as a parasol winged monoplane or as a biplane to compare handling characteristics. 4 were constructed.
The Farman F.280 was a three engine, cantilever wing monoplane designed in France as a mail carrier in the early 1930s. Underpowered and slow, only two were built and briefly used.
The Farman F.90 was a single engine biplane transport, carrying 6 passengers. It was built and developed in France in the early 1920s. Though it had some competition successes, it was not put into production
The Meyers Midget was a one-off small, low-powered, sporting single-seat sesquiplane, designed and built in the United States in 1926, incorporating several innovative structural features.
The Lightwing Type 4 Rooster is an experimental biplane glider, capable of powered or unpowered flight, built in the UK in the 1980s to explore the properties of this unusual glider configuration.
The Pander E was the first indigenous Dutch training aircraft, used by clubs and also privately owned. A two-seat, single-engine biplane, 17 were built in the Netherlands from 1926 with engines of increasing power.
The Wibault 2, Wib 2 or Wib 2 BN.2 was a single engine biplane aircraft designed and built in France in the early 1920s. It was intended as a heavy night bomber, though a thirteen-seat passenger version was proposed. Only one was built.
The Potez VIII was a French training aircraft which first flew in 1920. Originally it had a very unusual vertical inline engine and a four-wheeled undercarriage, though the production version was more conventional.
The Potez 26 was a single seat fighter aircraft designed and flown in France in the mid-1920s. It did not reach production.
The Potez 35 was a twin engine bomber aircraft, designed and built in France in the late 1920s. Only one was completed.
The Potez 31 was a prototype French two-seat night fighter, flown in about 1928, intended to fill the Cn.2 specification for the Armee de l'Air. Only one was built.
The Caudron C.140 was a French tandem cockpit sesquiplane designed in 1928 as a combination of liaison aircraft and observer and gunnery trainer.
The Caudron C.91 was a French single engine biplane with an enclosed passenger cabin seating four. It first flew in 1923.
The Potez 50 or Potez 50 A2 was a French two seat military multi-role aircraft, first flown in 1931. It did not go into service but seven variants using five different engines were produced, one of them setting several speed with useful load records and another, the Potez 506, setting three altitude world records.
The CAMS 110 was a French twin engine biplane flying boat built to fill a range of maritime military roles including long range reconnaissance, bombing and general exploration. It was not selected for production and only one was built.
The Caudron C.860 was a single engine, single seat monoplane ordered by the French government as a long distance communications aircraft. First flown in 1938, it was also expected to set speed and altitude records but the outbreak of World War II ended developments.
The Potez 24 A.2 was a mid-1920s French biplane intended to replace the Potez 15 as an army observation aircraft. The further improved and larger Potez 25 was preferred for production.