Engineering:Udet U 1
| U 1 | |
|---|---|
| |
| The Siemens-Halske Sh 4 powered U 10 | |
| Role | Low power sport aircraft |
| National origin | Germany |
| Manufacturer | Udet Flugzeugbau |
| Designer | Hans Henry Herrmann |
| First flight | May 1922 |
| Number built | 22 including later variants |
The Udet U 1 was the first of a line of small, low-powered, low wing, cantilever monoplanes built in Germany in the early 1920s.
Design and development
In the summer of 1921, a new aviation company was formed using the WWI German flying ace Ernst Udet's name. William Pohl from Milwaukee, Hans Henry Herrmann and Erich Scheuermann joined the company to fund the aircraft before postwar treaty restrictions were lifted on aircraft production, with the intent of building an inexpensive aircraft for the American market.[1][2][3] The builders produced and flew the U 1 five months before the formation of the Udet Flugzeubau GmbH company.[4]
The design was a low wing, cantilever monoplane in an era dominated by biplanes. The U 1 was a single-seater, as the air-cooled, 22 kW (30 hp) Haacke HFM-2 flat-twin did not have enough power for more than one person.[5] An enlarged-bore version of the engine, the 26 kW (35 hp) HFM-2a was used in the two seat U-2.
The U-2, like its predecessor, had a one-piece wing with a high aspect ratio of 9. In plan it was trapezoidal out to angled tips and had light dihedral. It was built around twin wooden spars; ahead of the leading spar the wing was plywood-covered, forming a torsion-resistant D-box. Ailerons, which filled about 40% of the trailing edge, reached out to the tips.[6]
Behind the engine in its aluminium cowling the fuselage was structurally rectangular in section apart from raised upper decking and was ply-covered. Pilot and passenger sat in tandem in a single, open cockpit, with the pilot in front and over the centre of the wing. It had a conventional, rather angular tail, with a fin of greater area than the rudder, though this reached down to the keel; the tailplane, mounted on top of the fuselage, was also large compared with the elevators.[6]
The U 2 had a conventional undercarriage, with pairs of outward-reaching V-struts from the lower fuselage joined at their vertices by a transverse member, to which the single axle was held by shock absorbing rubber rings.[6]
With a passenger the U-2 was slower than the U 1 and clearly under-powered, so the last three variants, the U 4, U 6 and U 10, were fitted with more powerful Siemens-Halske radial engines.
Operational history
The Siemens-Halske-powered U 6 and U 10 variants sold best, with about 16 built. Flown by Udet, the longer span U 10 was the fastest aircraft in the Coupe d'Italie des Avions de Tourisme held in November 1924, though criticized for its high landing speed.[7] In 1925 a U 10 came first in the under-80 hp (60 kW) class of the Deutschen Rundflug.[8]
Variants
Data from German Aviation 1919-1945[9]
- Udet U 1
- Single seat prototype with 22 kW (30 hp) Haacke HFM-2 flat-twin. One only.
- Udet U 2
- Two seat production variant with 26 kW (35 hp) Haacke HFM-2a flat-twin. Four built.
- Udet U 4
- 41 kW (55 hp) Siemens-Halske Sh 4 five cylinder radial powered. One built.
- Udet U 6
- 62 kW (83 hp) Siemens-Halske Sh 5 radial powered with revised, more rounded wing plan and tail surfaces. "Bathtub" cockpit replaced with separate single cockpits. Five built.
- Udet U 10
- 41 kW (55 hp) Siemens-Halske Sh 4 five cylinder radial powered. 10.60 m (34 ft 9 in) wingspan. Eleven built.
- Udet U 10a
- Floatplane variant with 75 kW (101 hp) Siemens-Halske Sh 11. One only, possibly a conversion.
Aircraft on display
.JPG)
- German Museum of Technology, Berlin: Udet U 10, D-452
Specifications (U 2)
Data from Les Ailes 1923,[6]
General characteristics
- Crew: one pilot
- Capacity: one passenger
- Length: 5.53 m (18 ft 2 in)
- Wingspan: 8.90 m (29 ft 2 in)
- Height: 2.10 m (6 ft 11 in)
- Wing area: 8.8 m2 (95 sq ft)
- Empty weight: 230 kg (507 lb)
- Gross weight: 400 kg (882 lb)
- Powerplant: 1 × Haake HFM 2a air-cooled flat twin, 26 kW (35 hp)
- Propellers: 2-bladed, 2.15 m (7 ft 1 in) diameter
Performance
- Maximum speed: 150 km/h (93 mph, 81 kn)
- Range: 500 km (310 mi, 270 nmi)
- Rate of climb: 2.1 m/s (410 ft/min)
References
- ↑ Armand van Ishoven. The fall of an eagle: the life of fighter ace Ernst Udet. p. 90.
- ↑ Nina Berman. Impossible Missions German Economic, Military, and Humanitarian Efforts. p. 109.
- ↑ Joanne Gernstein London. Fly Now!: A Colorful Story of Flight from Hot Air Balloon to the 777. p. 61.
- ↑ William Green. Augsburg Eagle: the story of the Messerschmitt 109. p. 9.
- ↑ Jean-Denis G.G. Lepage. Aircraft of the Luftwaffe, 1935-1945: An Illustrated Guide. p. 28.
- ↑ 6.0 6.1 6.2 6.3 Serryer, J. (19 April 1923). "Le monoplan Udet". Les Ailes (96): 9. http://gallica.bnf.fr/ark:/12148/bpt6k65560420/f2.
- ↑ "Coupe d'Italie des Avions de Tourisme". L'Aérophile 1924 (21-22): 356-7. 1–15 November 1924. https://gallica.bnf.fr/ark:/12148/bpt6k6554816n/f355.
- ↑ "Quelles enseignements techniques de "Circuits des Airs"". Les Ailes (212): 3. 9 July 1925. https://gallica.bnf.fr/ark:/12148/bpt6k9607209v/f3.
- ↑ "German Aviation 1919-1945". https://www.histaviation.com/udet.html. Retrieved 3 April 2021.
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