1,721,206 research outputs found

    A SI Engine for Ultra Light Aircraft Propulsion

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    Peculiarity of this new engine : 4-stroke, 4 cylinder horizontally opposed, spark ignition, air-cooled unit with reduction gera; power output greater than 60kW, weight less than 65 kg (ready to fly), high reliability and small overall dimension, due to reduction of components. Experimental tests demonstrate a remarkable weight to power ratio (1,02 kg/kW) comparable with the reference engine Rotax 912 UL-S (0,98 kg/kW)

    Iniezione con attuatori piezoelettrici nei piccoli motori alternativi ad A. C.

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    San Martino di Castrozza (TN) – Italy. Edited by SGE-Padova. (in Italian)

    Un simulatore di trasmissione ferroviaria in similitudine dinamica

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    Riv. Ingegneria Ferroviaria – Marzo 200
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