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・ CN Tower (Edmonton)
・ CN U-1-a and U-1-b
・ CN U-1-f
・ CN York Subdivision
・ CN&L Subdivision
・ CN-105-57
・ CN-E 85mm T1.3 L F
・ CN-group
・ CN-MoM
・ CN2
・ CN2 algorithm
・ Cn3D
・ CNA
・ CNA (nonprofit)
・ CNA C-7
CNA C.II
・ CNA C.VI
・ CNA Center
・ CNA D
・ CNA Eta
・ CNA Financial
・ CNA PM.1
・ CNA2
・ CNAC
・ Cnaemidophorus
・ Cnaemidophorus horribilis
・ Cnaemidophorus rhododactyla
・ Cnaemidophorus smithi
・ Cnaemidophorus urbicella
・ Cnaeus Pompeius Longinus


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CNA C.II : ウィキペディア英語版
CNA C.II

The CNA C.II was a small, air-cooled, two cylinder horizontally opposed aircraft engine designed and built in Italy in the late 1930s.
==Design==
The low power, unsupercharged C.II had offset cylinders with special steel barrels and light alloy cylinder heads. The pistons were light alloy castings; the connecting rods were heat treated chrome-nickel steel, with split big ends. The CN.II had a one piece chrome-nickel steel crankshaft ruuning in two roller bearings, with a ball thrust bearing. The crankcase was a one piece light alloy casting.〔



抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
ウィキペディアで「CNA C.II」の詳細全文を読む



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