发明名称 Temperature conpensated fuel jet
摘要 A fuel supply system (1) for an internal combustion engine, arranged in a suction channel (2) leading to the very engine body, said system comprising one or several nozzles (3, 3'), at least one nozzle (3) being configured in such a manner that its fuel through-flow resistance changes upon temperature changes because a movable part (5) in the nozzle being connected to a temperature-responsive member (6), such as a bimetal member (6), whereby the movable part (5), upon lower temperature levels, is moved by the member (6) for reduction of the fuel through-flow resistance, usually by an increase of the fuel through-flow opening, and thus the fuel through-flow is increased and a richer fuel mixture is obtained, i.e. a temperature compensation of the fuel supply with the aid of a temperature-compensated nozzle (3).
申请公布号 AU3820895(A) 申请公布日期 1996.05.15
申请号 AU19950038208 申请日期 1995.10.20
申请人 AKTIEBOLAGET ELECTROLUX 发明人 BO ANDREASSON;MATS BOBERG
分类号 F02M1/02;F02M1/10;F02M7/20;F02M17/04 主分类号 F02M1/02
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