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・ PZL M-20 Mewa
・ PZL M-24 Dromader Super
・ PZL M-4 Tarpan
・ PZL M26 Iskierka
・ PZL M28 Skytruck
・ PZL MD-12
・ PZL Mielec
・ PZL P.1
・ PZL P.11
・ PZL P.24
・ PZL P.6
・ PZL P.7
・ PZL S-1
・ PZL S-4 Kania
・ PZL SM-2
PZL SM-4 Łątka
・ PZL SW-4
・ PZL TS-11 Iskra
・ PZL TS-16 Grot
・ PZL TS-8 Bies
・ PZL W-3 Sokół
・ PZL WS Foka
・ PZL Ł.2
・ PZL-101 Gawron
・ PZL-102 Kos
・ PZL-104 Wilga
・ PZL-105 Flaming
・ PZL-106 Kruk
・ PZL-112 Junior
・ PZL-126 Mrówka


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PZL SM-4 Łątka : ウィキペディア英語版
PZL SM-4 Łątka

The PZL SM-4 Łątka (Polish: Dragonfly) was a prototype three-seat helicopter of the 1960s, developed by WSK PZL-Świdnik in Poland. Of largely conventional design and construction, a single prototype was built, but was not flown as a result of engine problems.
==Design and development==
In 1960, a design team led by Jerzy Kotliński at the Polish WSK PZL-Świdnik factory began work on a new short-range light helicopter, which was given the designation SM-4 Łątka.〔Taylor 1966, p. 116.〕〔("Projekty Śmigłowców WSK-Świdnik" ). ''Polska Technika Lotnicza: Materiały Historyczne''. 16 October 2005.〕 WSK PZL-Świdnik had previously license-built Soviet Mil Mi-1 helicopters, designated SM-1, starting in 1955. They had also designed and built the PZL SM-2 derivative of the Mi-1; the SM-4 was the first completely original aircraft design to be developed by them.〔〔
The Łątka was designed as a three-seat, single-engined helicopter of conventional layout. It was equipped with a single three-bladed glass-fibre main rotor and a two-bladed tail rotor, with power provided by a Narkiewicz WN-6S air-cooled flat-six horizontally-opposed piston engine, which was mounted behind the cabin. The pilot and two passengers were accommodated in an enclosed cabin with extensive glazing. The tail rotor was carried on the end of an open tail boom constructed of welded steel tube, giving a layout similar to that of a Bell 47. The undercarriage consisted of two skids.〔
A single prototype of the SM-4 was completed; the helicopter was used to carry out ground tests, but it never flew as the WN-06S engine failed to receive clearance for flight operations, and the program was abandoned.〔〔("PZL-Swidnik History - Helicopter Design" ). ''Globalsecurity.org''. Retrieved 6 June 2012.〕

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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