Dornier Do K

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Dornier Do K
ETH-BIB-Flug- Dornier DO K3, Zurich, Bern, Ing.Gsell-Inlandflug-LBS MH05-93-12 (cropped) .tif
Type: Passenger plane
Design country:

German EmpireGerman Empire German Empire

Manufacturer:

Dornier works

First flight:

May 7, 1929

Number of pieces:

3 prototypes

The Dornier Do K was a German passenger aircraft, of which only three aircraft in different versions were built at the Dornier works in Friedrichshafen .

history

Claude Dornier developed a new airliner at the end of the 1920s, which was unsuccessful during the global economic crisis and due to the concept's inefficiency. In a comparison flight in Switzerland, the K3 of the first Ju 52 / 3m of Deutsche Luft Hansa was defeated . The project was discontinued due to disappointing flight performance.

construction

Motor pod of the Do K3 with Walter Castor star motors in tandem arrangement and two-winged push and four-winged pull propellers, Berlin-Tempelhof 1932

The three built prototypes K1, K2 and K3 differed significantly from each other.

Thu K1

The first Do K had a conventionally braced wing in a high- wing arrangement . A single Bristol Jupiter VI star engine powered the aircraft. The rectangular fuselage offered space for eight passengers and had an enclosed cockpit.

Thu K2

The second prototype essentially had a modified drive with two engine nacelles next to the fuselage, in each of which two Gnome Rhône radial engines worked in tandem.

Thu K3

The third prototype was a completely new design with an oval and elongated fuselage for now ten passengers and a new wing without struts. The wing shape was also found on Do 10 and Do Y again. A tail wheel replaced the tail spur. The engine pods were attached lower down the hull; Four Czechoslovak Walter Castor star engines were used as drive . The front engines had four-blade propellers; the rear pusher propeller only had two blades.

Technical specifications

Three-sided view Do K3
Parameter Data of the K1 Data of the K2 Data of the K3
crew 2 2
Passengers 8th 10
length 15.25 m 15.00 m 16.5 m
span 20.60 m 25 m
height 4.50 m 4.10 m 4.2 m
Wing area 76.0 m² 88 m²
Wing extension 5.6 7.1
Empty mass 2700 kg 3400 kg 3600 kg
payload 1400 kg 1600 kg k. A.
Max. Takeoff mass 4100 kg 5000 kg 6000 kg
Top speed 190 km / h near the ground 195 km / h near the ground 220 km / h
Cruising speed k. A. k. A. 200 km / h
Rise time 17.5 min at 2000 m 18 min at 2000 m k. A.
Service ceiling 3100 m 2800 m 6300 m
Range 700 km k. A. k. A.
Engine (s) a Siemens Jupiter-VI-U star engine
with 450 HP (approx. 330 kW)
four Gnome-Rhône-Titan radial engines
with 240 HP each (approx. 180 kW)
four Walter Castor star engines
, each with 240 hp (approx. 180 kW)

gallery

See also

literature

  • Dornier Foundation for Aviation and Space Travel (Ed.): Dornier. Plant history and aircraft types . Delius Klasing, Bielefeld 2009, ISBN 978-3-7688-2610-5 .
  • Günter Frost, Karl Kössler , Volker Koos: Dornier . From the beginning until 1945. Heel, Königswinter 2010, ISBN 978-3-86852-049-1 , p. 104/105 and 123-125 .

Web links

Commons : Dornier Do K  - collection of images, videos and audio files

Individual evidence

  1. ^ The Zurich Meeting. (PDF; 320 kB) Circuit of the Alps (Commercial Aircraft). In: FLIGHT, AUGUST 5, 1932. Flightglobal.com, August 5, 1932, p. 726 , accessed on October 18, 2019 (English): “Five machines had been entered for this contest, and three finished. They were a Junkers three-engined "Ju.52" (Hornet), a Dornier four-engined "Do.K" (Walter), and a Fokker three-engined "F.VII" (Wright). The "Ju.52" secured first place, the "Do.K" second, and the * 'F.VII "third."
  2. ^ A b Edwin PA Heinze: The New Dornier Landplane. (PDF; 260 kB) In: FLIGHT, OCTOBER 30, 1931. Flightglobal.com , October 30, 1931, pp. 1165–1167 , accessed on October 18, 2019 (English): “Owing to the kindness of the makers, which we duly acknowledge, the writer has received further interesting details of the machine, which give a good idea of ​​the constructional features of the plane. "
  3. ^ A b Günter Frost, Karl Kössler, Volker Koos: Dornier . From the beginning until 1945. Heel, Königswinter 2010, ISBN 978-3-86852-049-1 , p. 105 .
  4. ^ A New Dornier Machine. (PDF; 280 kB) The Do-K Twin-Tandem Engined Monoplane. In: FLIGHT, OCTOBER 9, 1931. Flightglobal.com, October 9, 1931, p. 1014 , accessed on October 18, 2019 : “In his latest type Dr. Claudius Dornier has departed considerably from what has come to be regarded as standard Dornier practice. "