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Initially, Junkers proposed modifications of the Jumo 004, specifically the 109-004G and 109-004H. However, these variants were rejected as they were not powerful enough, and Junkers began to design the 109-012. [1] The engine was to feature an 11-stage axial compressor enclosed in a sheet-steel casing and a 2-stage, air-cooled turbine.
Download QR code; Print/export ... Pages in category "Junkers aircraft engines" ... 0–9. Junkers Jumo 012; J. Junkers Jumo 004; Junkers Jumo 204; Junkers Jumo 205;
Junkers EF 082, combat battle aircraft project. Junkers EF 094, design designation for Ju 322. Junkers EF 100, six-engine, wide-body transatlantic airliner, 1940; Junkers EF 101, Mistel aircraft design; Junkers EF 112, twin-boom ground attack aircraft project, 1942. Junkers EF 115, bomber project with four Jumo 211 engines or 2 jet engines
The Jumo 211 became the major bomber engine of the war, in no small part due to Junkers also building a majority of the bombers then in use. Of course, since it was the Luftwaffe that selected the final engine to be used after competitive testing on prototypes (such as the Dornier Do 217 ), there is certainly more to it.
Download as PDF; Printable version; In other projects Wikidata item; Appearance. ... Junkers Jumo 004; Junkers Jumo 012; K. Klimov RD-500; Klimov VK-1; L. Lockheed ...
The Junkers Jumo 213 was a World War II-era V-12 liquid-cooled aircraft engine, a development of Junkers Motoren's earlier design, the Jumo 211.The design added two features, a pressurized cooling system that required considerably less cooling fluid which allowed the engine to be built smaller and lighter, and a number of improvements that allowed it to run at higher RPM.
The basic conception was a further development of the design already applied with high perfection on Junkers Jumo 004 and Junkers Jumo 012, as well as the BMW 003 and BMW 018 engines. In this design, the compressor, combustion chamber and turbine are traversed in axial direction by the air taken directly from the inlet.
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