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・ Junkers J.I
・ Junkers Ju 160
・ Junkers Ju 187
・ Junkers Ju 188
・ Junkers Ju 252
・ Junkers Ju 268
・ Junkers Ju 287
・ Junkers Ju 288
・ Junkers Ju 290
・ Junkers Ju 322
・ Junkers Ju 352
・ Junkers Ju 388
・ Junkers Ju 390
・ Junkers Ju 46
・ Junkers Ju 488
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


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Junkers Ju 49 : ウィキペディア英語版
Junkers Ju 49

The Junkers Ju 49 was a German aircraft designed to investigate high-altitude flight and the techniques of cabin pressurization. It was the world's second working pressurized aircraft, following the Engineering Division USD-9A which first flew in the United States in 1921.〔Cornelisse, Diana G. Splended Vision, Unswerving Purpose; Developing Air Power for the United States Air Force During the First Century of Powered Flight. Wright-Patterson Air Force Base, Ohio: U.S. Air Force Publications, 2002. ISBN 0-16-067599-5. pp. 128-129.
〕 By 1935, it was flying regularly to around 12,500 m (41,000 ft).
==Development==
The Junkers Ju 49 was developed entirely to investigate techniques for flight at high altitude. To this end, it had a specially developed engine and the first pressurized cabin in a German aircraft. The engine was the Junkers L88a, which combined two six-cylinder inline L8 motors into an upright V-12 and had a two-stage supercharger plus intercooler to sustain power at high altitudes. It produced 522 kW (700 hp) at about 5,800 m (19,000 ft). This engine drove a large four-blade propeller. The pressure cabin held the two crew. The original intention was for operation at about 6,000 m (20,000 ft).〔
The Ju 49 was built in typical Junkers fashion as a cantilever-wing monoplane of all-metal construction with stressed duralumin skin throughout, corrugated on the flying surfaces. The wing trailing edge featured the standard Junkers "double wing", combining adjustable flap and aileron surfaces outboard, together with plain flaps inboard. The aircraft had a fixed, split-axle main undercarriage which was noticeably tall, to accommodate the large-diameter propeller, plus a tailskid.
A retractable rectangular radiator descended between and just in front of the undercarriage legs. The pressurized cabin had five small portholes for the pilot, two forward, two sideways and one overhead, and there were two more, one on each side for the second crew member. The forward view was so poor that a periscope was fitted with a downward view for landing.〔

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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