Daimler-Benz DB 600
Daimler-Benz DB 600 | |
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A DB 600 in the Mercedes-Benz Museum |
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Type: | Twelve-cylinder - V engine |
Design country: | |
Manufacturer: | |
First flight: |
1935 |
Production time: |
1936-1938 |
Number of pieces: |
2281 |
The Daimler-Benz DB 600 was a liquid-cooled, twelve-cylinder engine - aircraft engine with a displacement of 33.9 liters and a take-off power of up to 1050 hp. Series production at Daimler-Benz began in 1936. The DB 600, which was still provided with carburettors for mixture formation , was installed in many Luftwaffe aircraft in the 1930s , such as the first He 111 series .
As early as 1934, the further development of the same-displacement DB 601 with gasoline direct injection began , which completed its first test runs in 1935 and went into series production in November 1937. After the DB 600 built in 2281, production ended in 1938.
Prehistory and Development
The two Daimler-Benz predecessor companies DMG and Benz manufactured the six-cylinder Mercedes D III and Benz Bz III aircraft engines in large numbers during the First World War . During the Weimar Republic , aircraft engine production in the company that merged to form Daimler-Benz AG in 1926 was completely discontinued. Only after the seizure of power of the Nazis in 1933 could Stuttgart company through the upgrade of the Armed Forces expect new demand again.
As early as the early 1930s, the German engine manufacturers were asked by the Reich Ministry of Transport to develop an 800 HP aircraft engine, which was to be designed as a V-engine with "hanging" cylinders ( crankshaft above) and which was suitable for military and civil purposes. Based on this requirement, Daimler-Benz designed the Daimler-Benz F4A with a displacement of 30 liters. Two prototypes of the twelve-cylinder V-engine with 60 ° bank angle and two mechanical radial loaders were completed in 1932.
The F4A was further developed into the DB 600, the first test runs of which took place in late summer 1935. The Daimler-Benz plant in Berlin-Marienfelde began series production of the DB 600 in 1936.
description
The V-engine was installed rotated by 180 degrees so that the crankshaft was on top (hence also called " A-engine "). This type of engine installation also made it easier to access cylinder heads ( valve control ) and spark plugs for maintenance.
This left enough space above the engine for the installation of ( synchronized ) on-board weapons firing through the propeller circle , while the hollow propeller shaft located between the cylinder banks could accommodate the barrel of a machine gun or cannon . Since this weapon, which was mounted behind the engine block, quickly overheated, loading jams or compression ignition caused by overheating were frequent and installation in the Bf 109 , for example , was quickly abandoned.
The engine block was made of cast aluminum and contained steel cylinder liners . It had an overhead camshaft ( OHC valve control ) driven by a vertical shaft for each cylinder bank , which actuated four valves per cylinder via roller rocker arms ( four-valve technology ). Each cam operated an exhaust valve and an intake valve in turn. The exhaust valves were sodium cooled . The engine had a contact-controlled dual ignition ( Bosch - twin magneto ignition ) with two spark plugs per cylinder. The firing order was 1–8–5–10–3–7–6–11–2–9–4–12–1.
variants
- DB 600A 1
- Up to 1000 PS (810 kW) at 2350 min −1 at sea level
- DB 600B 2
- Up to 1000 PS (810 kW) at 2350 min −1 at sea level
- DB600C 1
- Up to 850 hp (634 kW) at 2350 min -1 to 4000 m. 910 hp takeoff power.
- DB600D 2
- Up to 850 hp (634 kW) at 2350 min -1 to 4000 m. 910 hp takeoff power.
- DB600G 1
- Up to 950 hp (708 kW) at 2350 min -1 to 4000 m. 1050 hp takeoff power.
DB600Ga was a version with a height loader for 4000 m full pressure height .
- DB600H 2
- Up to 950 hp (708 kW) at 2350 min -1 to 4000 m. 1050 hp takeoff power.
DB600Ha was a version with a height loader for 4000 m full pressure height.
- 1 1.55: 1
- 2 1.88: 1
Technical specifications
(DB 600C)
- Twelve-cylinder V-engine with 60 ° bank angle
- Valve control : each cylinder bank via a vertical shaft driven overhead camshaft ( OHC ), each cylinder two intake and two exhaust valves actuated (four valves per cylinder).
- Bore : 150 mm
- Stroke : 160 mm
- Displacement : 33.9 liters
- Compression ratio : 6.9: 1
- Cooling: liquid cooling
- Lubrication: dry sump lubrication with one pressure and two suction pumps (one per cylinder head )
- Dry matter: 560 kg
- Start Power: 900 hp (662 kW) at 2400 min -1
- Continuous power: 770 hp (566 kW) at 2200 min -1
- Output per liter : 26.5 HP / l (19.5 kW / l)
- Weight-related power : 1.61 PS / kg (1.18 kW / kg)
- Fuel: gasoline , type B4 with an octane rating of 87 RON
Similar engines
Applications
- Arado Ar 197 V1: 1937 - Prototype, marine variant of the Arado Ar 68 H
- Dornier Do 17 S-0 : three pre-production aircraft
- Focke-Wulf Fw 187 V6
- Heinkel He 60 C: a tested aircraft
- Heinkel He 111 V5: DB 600A, B-1, B-2: DB 600C, G-4: DB 600G, G-5: DB 600C, J-1: DB 600C
- Heinkel He 112 V7, V8
- Heinkel He 114 : three He 114 B-2, exported to Romania
- Junkers Ju 90 V1
- Henschel Hs 128 V1: twin-engine, pressurized cabin, high-altitude research aircraft
- Messerschmitt Bf 109 V10 to V14: prototypes
- Messerschmitt Bf 110 V1, V2, V3: prototypes
- Messerschmitt Bf 162 V1, V2
swell
- Helmut Schubert: German engines - aircraft engines and jet engines from the beginning to 1999. Aviatic Verlag GmbH, Oberhaching 1984, ISBN 3-925505-49-0 .
- Heinz J. Nowarra: The German Air Armament 1933-1945. Bernard & Graefe Verlag, ISBN 3-8289-5315-8 .
English:
- Roy Cross, Gerald Scarborough: Messerschmitt Bf 109: Versions B – E - Classic Aircraft No.2. Patrick Stephens Ltd, Cambridge 1972, ISBN 0-85059-106-6 .
- William Green: The Augsburg Eagle: A Documentary History - Messerschmitt Bf 109. Macdonald and Jane's Publishing Group Ltd, London 1980, ISBN 0-7106-0005-4 .
- JR Smith, Anthony L. Kay: German Aircraft of the Second World War. Putman & Company Ltd., London 1972, ISBN 0-370-00024-2 .
See also
Web links
Individual evidence
- ↑ German Aircraft Industry and Production, 1933-1945, ISBN 1-85310-864-2 , p. 310; google.books: limited preview
- ↑ MTU Museum of Engine History - yesterday, today and tomorrow at www.mtu.de (PDF, 4.4 MB)