Abstract:
A radiant heat discharge arrangement (30) for a large internal combustion engine (10) may comprise a cover (32). The cover (32) may be configured to cover an outlet manifold (18) of the internal combustion engine (10) with a clearance between cover (32) and outlet manifold (18). The cover (32) may have at least one outlet opening (36). The radiant heat discharge arrangement (30) may further comprise an air duct (38) and a fan (46). The air duct (38) may be fluidly connected to the at least one outlet opening (36) of the cover (32), and the fan (46) may be fluidly connected to air duct (42).
Abstract:
An engine support system (10) comprising a support structure (12), which have a top section (18) with outer mounting sections (20), and a counterweight section (19). Each outer mounting section (20) have an upper face (24) and a lower face (26). The counterweight have a mass of at least 80 % of a mass of the internal combustion engine unit (40). The engine support (10) further comprise a plurality of upper resilient mountings (14) and a plurality of lower resilient mountings (16). Upper resilient mountings are arranged at the upper faces (24) of outer mounting sections (20), and support the internal combustion engine unit (40). Lower resilient mountings (16) are arranged at the lower faces (26) of outer mounting sections (20), and support the support structure (12).
Abstract:
An engine support system (10) comprising a support structure (12), which have a top section (18) with outer mounting sections (20), and a counterweight section (19). Each outer mounting section (20) have an upper face (24) and a lower face (26). The counterweight have a mass of at least 80 % of a mass of the internal combustion engine unit (40). The engine support (10) further comprise a plurality of upper resilient mountings (14) and a plurality of lower resilient mountings (16). Upper resilient mountings are arranged at the upper faces (24) of outer mounting sections (20), and support the internal combustion engine unit (40). Lower resilient mountings (16) are arranged at the lower faces (26) of outer mounting sections (20), and support the support structure (12).
Abstract:
Bei einer aufgeladenen Brennkraftmaschine wird das im Ladeluftkühler anfallende Kondenswasser mittels Rohrleitungen in die Abgasleitung hinter der Abgasturbine eingeleitet und zur Verdampfung gebracht.
Abstract:
A fuel change-over module (10) for a combustion engine (12) may be installed in a fuel supply system of the combustion engine (12). The fuel change-over module (10) may be configured to alternatively supply heavy fuel from a heavy fuel tank (102) or light fuel from a light fuel tank (104) to the combustion engine (10) via a fuel circuit (72) formed between the fuel supply module (10) and the combustion engine (12). The heavy fuel and the light fuel may have different temperatures. The fuel change-over module may comprise a fuel mixing tank (40). The volume of the fuel mixing tank (40) may be such that the total volume of fuel circulating in the fuel circuit (72) results in a desired temperature change rate and a desired change-over time when changing the type of fuel supplied to the combustion engine (12) by the fuel change-over module (10).