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Share of the Siemens & Halske AG, issued May 1920 [1] Siemens & Halske AG (or Siemens-Halske) was a German electrical engineering company that later became part of Siemens. It was founded on 12 October 1847 as Telegraphen-Bauanstalt von Siemens & Halske by Werner von Siemens and Johann Georg Halske.
Later in its development programme the Dr.I crashed and was seriously damaged. Siemens-Schuckert rebuilt it, though adding 2.90 m 2 (31.2 sq ft) to the wing area. [1] Construction of a version powered by a more powerful 110 hp (82 kW) Siemens-Halske Sh.III eleven cylinder rotary engine, the Dr.II, was well advanced when it was abandoned. [1]
Data from German Aircraft of the First World War General characteristics Crew: One Length: 5.8 m (19 ft 0 in) Wingspan: 10.9 m (35 ft 9 in) Wing area: 30 m 2 (320 sq ft) Empty weight: 680 kg (1,499 lb) Gross weight: 910 kg (2,006 lb) Powerplant: 2 × Siemens-Halske Sh.1 9-cylinder rotary, 82 kW (110 hp) each Propellers: 2/4-bladed ; the tractor propeller had two blades and the pusher four ...
Siemens & Halske (S & H) was incorporated in 1897 and then merged parts of its activities with Schuckert & Co., Nuremberg, in 1903 to become Siemens-Schuckert. In 1907, Siemens (Siemens & Halske and Siemens-Schuckert) had 34,324 employees and was the seventh-largest company in the German empire by number of employees.
Siemens-Schuckert's first production fighter aircraft was the Siemens-Schuckert D.I, which was based closely on the French Nieuport 17.Apart from the use of the Siemens-Halske Sh.I, a geared rotary engine in which the crankshaft and the propeller rotated in opposite directions, the D.I was in fact a fairly close copy of the Nieuport.
The Siemens-Halske Sh 12 was a nine-cylinder, air-cooled, radial engine for aircraft built in Germany in the 1920s. First run in 1925, it was rated at 80 kW (110 hp). The Sh 12 was also produced in the United States by Ryan Aeronautical Corp. as the Ryan-Siemens 9.
The fuselage of the D.VI was circular in cross-section, with its 11-cylinder, 160 hp (119 kW) Siemens-Halske Sh.IIIa rotary engine completely cowled in the nose driving a four blade propeller. The fuselage diameter decreased markedly to the tail but an unusual jettisonable fuel tank bulged out below for about 35% of the overall length.
The most important difference from the Nieuport 17 was the powerplant - instead of the Le Rhone 9J of the Nieuport (licensed, as with the Oberursel Ur.II; and un-licensed versions of which were actually available in Germany at the time), Siemens-Schukert chose to use their own 110 hp (82 kW) Siemens-Halske Sh.I rotary engine - in which the ...
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