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JPX PUL 425
The JPX PUL 425, also called simply the JPX 425, is a French twin-cylinder, horizontally opposed, two-stroke aircraft engine.〔Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' 8th Edition, page G-4 Cybair Limited Publishing, 2001. ISBN 0-9680628-1-4〕 The engine was produced only until the company went out of business in the early 1990s. The company was re-formed but the engine remains out of production and unsupported for parts.〔 ==Design and development== The engine has two cylinders in a horizontally opposed configuration, with cooling fins on the cylinders. The single ignition system uses a coil and points. Fuel is metered by a single Tillotson butterfly-type carburetor. Starting is by a recoil starter system with electric start as an option.〔 The 425 has a redline rpm of 4600 and does not use a reduction drive. Its weight of just gives the engine a high power-to-weight ratio.〔
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「JPX PUL 425」の詳細全文を読む
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