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・ Junkers Ju 49
・ Junkers Ju 52
・ Junkers Ju 60
・ Junkers Ju 86
・ Junkers Ju 87
・ Junkers Ju 88
・ Junkers Ju 89
・ Junkers Ju 90
・ Junkers Jumo 004
・ Junkers Jumo 204
・ Junkers Jumo 205
・ Junkers Jumo 210
・ Junkers Jumo 211
・ Junkers Jumo 213
・ Junkers Jumo 222
Junkers Jumo 223
・ Junkers K 16
・ Junkers K 37
・ Junkers K 47
・ Junkers L1
・ Junkers L2
・ Junkers L5
・ Junkers L55
・ Junkers L88
・ Junkers Profly
・ Junkers Profly Junkers Trike
・ Junkers Profly Ultima
・ Junkers T 19
・ Junkers T 23
・ Junkers T.21


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Junkers Jumo 223 : ウィキペディア英語版
Junkers Jumo 223

The Junkers Jumo 223 was an experimental 24-cylinder aircraft engine based on the Junkers Jumo 205. Like the Jumo 205, it was an opposed piston two-stroke diesel engine. It had four banks of six cylinders in a rhomboid configuration, with four crankshafts one at each vertex of the rhombus, and 48 pistons. It was designed for a power of 2,500 horsepower at 4,400 rpm, and weighed around 2,370 kg.
Only one example is known to have been built. It is rumoured to have been taken to Moscow after the war, where development may have continued.
== Jumo 224 ==
In 1942 the 223 was abandoned in favour of an even larger engine, the Jumo 224 with an intended output power of 4,500 horsepower.〔
The Jumo 223 series was influential to the successful three-crankshaft Napier Deltic engine.

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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