An engine assembly with an air intake system and a turbocharger device in fluid communication with the air intake system includes an electronic control unit in communication with the air intake system and turbocharger device. A CAC system is in downstream fluid communication with the turbocharger device and in upstream fluid communication with the air intake system and includes at least one flow adjustment mechanism in communication with the electronic control unit and selectively positionable between a first position and one or more second positions to adjust velocity of air from the turbocharger device flowing through the CAC system and to manage condensation buildup in the CAC system and/or to open a bypass duct in order for some or all of the turbo airflow to bypass the CAC system to reduce or eliminate condensation buildup in the CAC system at warm ambient conditions and ice buildup at cold ambient conditions.

A combustion engine for combustion of an air-fuel mixture containing air and fuel, comprising at least one temperature adjusting means for cooling or heating the air, fuel, and/or air-fuel mixture and a control unit configured to determine the methane number and/or hydrogen content of the fuel and/or air-fuel mixture, wherein the control unit is configured to control a temperature of the air, fuel and/or air-fuel mixture based on the determined methane number and/or hydrogen content by controlling the at least one temperature adjusting means.

Control of an internal combustion engine system in response to a condensation condition associated with a charge air cooler is disclosed. One or more operating parameters of the internal combustion engine are monitored to the control charge air cooler coolant inlet temperature to keep the charge temperature above the estimated dew point to reduce or prevent condensation upstream of the intake manifold.

The present invention relates to a device (1) for the thermal management of the intake air of an internal combustion engine (3) equipped with a turbocharger (5), said device comprising: a first heat exchanger (7) placed in the air intake circuit (9), a second heat exchanger (10) placed on the main exhaust line (12) and connected to the first heat exchanger (7) to form a heating loop (A), said thermal management device (1) furthermore comprising a so-called low-pressure exhaust gas recuperation system (14), comprising a first take-off (141) placed downstream of the turbine (5b), an outlet (142) placed upstream of the compressor (5a), and a control valve (140), the second heat exchanger (10) being placed between the turbine (5b) and the first take-off (141), the main exhaust line (12) comprising a take-off branch (26) between a second take-off (201) placed on the main exhaust line (12) upstream of the second heat exchanger (10), a take-off device (200) able to manage the circulation of the exhaust gases, and an outlet (202).

A method to ignite a gaseous fuel in an engine of an engine system is disclosed. The method includes introducing a compound having a peroxide group into a main combustion chamber of the engine for igniting the gaseous fuel. Further, the method includes controlling, by a controller, one or more parameters of the engine system to attain a temperature in the main combustion chamber within a temperature range. The compound decomposes into a radical, thus facilitating ignition of the gaseous fuel.

A charge air cooler may include inlet and outlet chambers adjacent one another and separated by a baffle defining a bypass passage for airflow therethrough. The charge air cooler may also include heat exchange conduits connected between the inlet and outlet chambers. A valve may be disposed in the bypass passage and configured to selectively redirect at least a portion of the airflow through the bypass passage responsive to a charge air cooler outlet temperature being below a condensation temperature of the airflow.

Methods and systems are provided for increasing airflow through a charge air cooler (CAC) in order to purge condensate from the CAC. In one example, a method includes increasing airflow through the CAC while maintaining torque by selectively deactivating one or more engine cylinders and increasing boost. The number of deactivated cylinders may be based on an amount of condensate within the CAC.

A charge air cooler (CAC) includes a first header including a first interior portion, a second header spaced from the first header. The second header includes a second interior portion. At least one conduit extends between the first header and the second header. The at least one conduit includes a first end fluidically connected to the first interior portion, a second end fluidically connected to the second interior portion, and an intermediate portion extending therebetween. A heating system is arranged in a heat exchange relationship with the at least one conduit. The heating system is selectively operable to increase a temperature of fluids passing through the at least one conduit into one of the first and second headers.

An internal combustion engine (1) is provided with a supercharger (12) and a cylinder direct injection fuel injector (10). When the engine shifts in a low-speed supercharging region at a state where the wall temperature of a cylinder bore (3) is low, liquid fuel adheres to a wall surface of the cylinder bore (3) so that lubricating oil is diluted with the liquid fuel and released into a combustion chamber (4). As a result, there occurs abnormal combustion. In the present invention, the fuel injection amount is increased at the time when the engine shifts in a predetermined low-speed supercharging region. The lower the wall temperature of the cylinder bore, the larger the rate of increase of the fuel injection amount. This makes it possible to suppress the temperature of air-fuel mixture in the vicinity of compression top dead center and prevent the occurrence of abnormal combustion.

The present invention relates to a device (1) for the thermal management of the intake air of an internal combustion engine (3) equipped with a turbocharger (5), said device comprising: a first heat exchanger (7) placed in the air intake circuit (9), a second heat exchanger (10) placed on the main exhaust line (12) and connected to the first heat exchanger (7) to form a heating loop (A), said thermal management device (1) furthermore comprising a so-called low-pressure exhaust gas recuperation system (14), comprising a first take-off (141) placed downstream of the turbine (5b), an outlet (142) placed upstream of the compressor (5a), and a control valve (140), the second heat exchanger (10) being placed between the turbine (5b) and the first take-off (141), the main exhaust line (12) comprising a take-off branch (26) between a second take-off (201) placed on the main exhaust line (12) upstream of the second heat exchanger (10), a take-off device (200) able to manage the circulation of the exhaust gases, and an outlet (202).