Descamps 17

Descamps 17 A2
Prototype with V-12, 400 hp engine in 1924
Role Two seat fighter-reconnaissance aircraft
National origin France
Manufacturer Elisée Alfred Descamps
Designer André Brunet
First flight Spring 1924
Primary user Armée de l'Air
Number built 7


The Descamps 17 A2 was a two seat reconnaissance fighter built under a French government programme of 1923. Two versions, with different engines, were tested and six examples were built under licence by Caudron as the Caudron C.17 A2.

Design and development

The Descamps A2 was designed to a government programme for a two seat reconnaissance aircraft, a category denoted by the military code A2. When the first prototype appeared in March 1924 the manufacturer's name was hyphenated with that of the designer, André Brunet, though the order varied. The first accounts[1][2] of it did not include a Descamps type number, though according to a more recent source it was the Descamps-Brunet DB-16.[3] Initially, it was powered by a 400 hp (300 kW) Lorraine-Dietrich 12D V-12 engine[4] but by 1926 it had received a 450 hp (340 kW) Lorraine-Dietrich 12E W-12 engine. This version, identical to the DB-16 apart from the new and somewhat heavier engine, was designated the Descamps 17.[5][6] The new engine improved performance, increasing the top speed at sea level from 203 to 230 km/h (126 to 143 mph).[5][7]

The structure of the Descamps A2 was all metal. Such designs were quite new at this time and were criticised as being more difficult to repair compared with wooden-framed machines but Brunet's design enabled any part to be exchanged rapidly. It had no wire bracing and required no rigging.[4] The A2 was a sesquiplane, with an upper wing with twice the span and 3.4 times the area of the lower one, which was not only short but narrow. The two wings had similar plans, rectangular apart from straight angled tips. Only the upper wing carried ailerons.[1] Both wings were built around two I-section spars and were braced together on each side by two sets of airfoil section, N-form interplane struts, one from the upper fuselage to mid-way along the lower wing and the other from there outwards to the upper wing. There was significant stagger, with the leading edge of the lower wing ahead of that of the upper, so the N-struts leaned backwards. There was no dihedral on the lower wing but the upper one was set at 1.5° and slightly swept (2°). The lower wing was mounted on the lower fuselage frame and the upper on a very short upper fuselage pillar. The wings, like the rest of the aircraft, were fabric covered.[4]

The deep but narrow rectangular section fuselage, constructed from duralumin tubes, tapered to a knife edge at the rear and had rounded decking.[4] The nose differed according to engine; the early V-12 had two distinct bulges over the cylinders and a separate rectangular radiator, attached to the fuselage underside, which could be partially retracted by the pilot,[4][1] whereas the three cylinder banks of the W-12 required an additional central bulge[7] and the radiator was integrated into the nose in front of the engine.[6] There were two open cockpits. The pilot sat in front under the trailing edge of the wing, which had a V-shaped cut-out to improve his field of view. He controlled two fixed, forward firing machine guns and behind him the observer's position was equipped with two more on a gun mount. This post was far enough aft to provide a good all-round view. The tail was conventional, with the tailplane, which had swept leading edges, placed near the top of the fuselage and braced by a single strut on each side from below.[4] The angle of incidence of the tailplane was in-flight adjustable for trim[1] and its elevators were balanced. The vertical tail was rounded and reached down to the keel, operating in a small elevator cut-out. The Descamp's landing gear had mainwheels mounted under the wings at the meeting point of the inner and outer interplane struts, providing a wide track. There was no cross-axle; instead the wheels were mounted on rubber shock absorbers within trouser fairings. This arrangement allowed bombs to be released from under the fuselage;[4] up to 3×120 kg (260 lb) bombs could be carried.[2] The tailskid was free to pivot to assist ground steering.[4]

Operational history

Caudron purchased a licence to build the Descamps 17 A2 from 1927 as the Caudron C.17 A2. After the aircraft had satisfied the reconnaissance programme requirements, six were constructed for the Armée de l'Air.[8]

A notable tour of six European countries was made between 18 October and 19 November 1927 by Massot and an engineer in a civil registered C.17. They covered 8,200 km (5,100 mi).[8]

Variants

Descamps 16 or DB-16
400 hp (300 kW) Lorraine-Dietrich 12D V-12 engine
Descamps 17 or DB-17
450 hp (340 kW) Lorraine-Dietrich 12E W-12 engine
Caudron C.17 A2
Caudron-built Descamps 17.

Operators

 France
L'Armée de l'Air

Specifications (Descamps 17)

Data from [5] Performance[7]

General characteristics

Performance

Armament

References

  1. 1 2 3 4 "L'avion Brunet-Descamps A2". L'Aérophile. Vol. 32 no. 5-6. 1–15 March 1924. pp. 157–9.
  2. 1 2 "L'Avion Descamps-Brunet". Les Ailes (152). 15 March 1924.
  3. ↑ Bruno Parmentier. "Descamps-Brunet DB-16". Retrieved 25 July 2015.
  4. 1 2 3 4 5 6 7 8 "The Descamps-Brunet A2 Sesquiplane". Flight. Vol. XVI no. 31. 31 July 1924. pp. 473–4.
  5. 1 2 3 "The Paris Aero Show 1926 - Descamps". Flight. Vol. XVIII no. 48. 2 December 1926. p. 778.
  6. 1 2 "La Xe Exposition Internationale de l'Aéronautique". le Sport Universel illustré (1241): 829. 10 December 1926.
  7. 1 2 3 "The Paris Aero Show 1926 (cont.) - Descamps". Flight. Vol. XVIII no. 50. 16 December 1926. pp. 830–1.
  8. 1 2 3 4 Hauet, André (2001). Les Avions Caudrons 1. Outreau: Lela Presse. p. 199. ISBN 2 914017-08-1.
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