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・ Kawane-Koyama Station
・ Kawane-Ryōgoku Station
・ Kawanehon
・ Kawaneonsen-Sasamado Station
・ Kawang Gewog
・ Kawang, Chin State
・ Kawang, Kachin State
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・ Kawanishi Baika
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・ Kawanishi E11K
Kawanishi E15K
・ Kawanishi E5K
・ Kawanishi E7K
・ Kawanishi H3K
・ Kawanishi H6K
・ Kawanishi H8K
・ Kawanishi K-11
・ Kawanishi K-12 Sakura
・ Kawanishi K-200
・ Kawanishi K-7 Transport Seaplane
・ Kawanishi K-8 Transport Seaplane
・ Kawanishi N1K
・ Kawanishi Station
・ Kawanishi Station (Osaka)
・ Kawanishi Station (Yamaguchi)


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Kawanishi E15K : ウィキペディア英語版
Kawanishi E15K

The Kawanishi E15K ''Shiun'' (紫雲, "Violet Cloud") was a single-engined Japanese reconnaissance floatplane of World War II. The Allied reporting name for the type was "Norm" after Squadron Leader Norman O. Clappison of the RAAF, a member of the Allied Technical Air Intelligence Unit (ATAIU).
==Design and development==
In 1939 the Imperial Japanese Navy instructed the Kawanishi Aircraft Company to develop a two-seat high-speed reconnaissance floatplane, which was required to have sufficient performance to escape interception by land based fighters. It was planned to equip a new class of cruisers, intended to act as a flagship for groups of submarines, operating six of the new floatplanes to find targets. The first of the new cruisers, ''Ōyodo'' was also ordered in 1939.
Kawanishi designed a single-engined low-wing monoplane, powered by a 1,460 hp (1,090 kW) Mitsubishi MK4D Kasei 14 14-cylinder radial driving two Contra-rotating two-bladed propellers, the first installation of contra-rotating propellers produced in Japan, while a laminar flow airfoil section was chosen to reduce drag. It had a single main float under the fuselage and two stabilising floats under the wing. The stabilising floats were designed to retract into the wing, while the central float was designed to be jettisoned in case of emergency, giving a sufficient increase in speed (estimated as approximately 50 knots (90 km/h)〔) to escape enemy fighters.
The first prototype of Kawanishi's design, designated E15K1 in the Navy's short designation system made its maiden flight on 5 December 1941.〔 Five more prototypes followed during 1941-42. Problems were encountered with the retractable stabilising floats, resulting in several accidents when the floats could not be lowered for landing, and the system was eventually abandoned, with the stabilising floats being fixed, and a more powerful Mitsubishi MK4S Kasei 24 engine fitted to compensate for the increased drag.

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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