A cooling water passage structure (10) for an internal combustion engine (1) provided with a supercharger (8), comprises a passage forming member (14) attached to a main body (2) of the internal combustion engine, and internally defining a branch passage (13) communicating with an outlet (12B) of a main body water jacket (12) formed in the main body of the internal combustion engine, and a water temperature sensor (80) provided in the passage forming member to detect a temperature of the cooling water flowing through the branch passage. The water temperature sensor is positioned in a part of a main supply passage (31) defined in the passage forming member closer to an inlet end of the main supply passage than a junction between the main supply passage and a supercharger return passage (34) is.

A head-side jacket through which coolant flows is formed in a cylinder head. A main circulation path and a sub circulation path through which coolant fed from a coolant pump respectively circulates are formed. The head-side jacket is separated into an exhaust-port side jacket formed around an exhaust port, and a combustion-chamber-side jacket closer to a combustion chamber than the exhaust-port-side jacket. A heat exchanger is not formed in the main circulation path including the combustion-chamber-side jacket, but is formed in the sub circulation path excluding the combustion-chamber-side jacket and including the exhaust-port-side jacket.

A cooling device for an internal combustion engine includes a pump portion, a circulation water passage, a thermostat configured to switch between a state where the coolant is circulated to a heat exchange water passage on which a radiator is disposed and a state where the coolant is not circulated to the heat exchange water passage, and a control unit configured to control the pump portion. The control unit is configured to control a three-way valve such that a first pump and a second pump are connected in parallel when the thermostat switches to the state where the coolant is circulated to the heat exchange water passage and controls the three-way valve such that the first pump and the second pump are connected in series when the thermostat switches to the state where the coolant is not circulated to the heat exchange water passage.

A thermal management system for a vehicle includes an engine cooling circuit that causes a heat medium to circulate through an engine, and an engine radiator that exchanges heat between the heat medium in the engine cooling circuit and outside air. The thermal management system for a vehicle further includes a switching device that switches between an independent mode in which the heat medium circulates respectively independently through a cooler cooling circuit and the engine cooling circuit, and a communication mode in which the cooler cooling circuit and the engine cooling circuit communicate with each other to cause the heat medium to flow between a chiller and the engine radiator; and a controller that controls an operation of the switching device to switch to the communication mode when a temperature of the heat medium in the engine cooling circuit is lower than a first heat-medium temperature.

A controller includes a forced-induction-device controlling section, an obtaining section that is configured to repeatedly obtain a temperature of the coolant in the intake-air cooling system, a determining section that is configured to determine whether the temperature obtained by the obtaining section is higher than or equal to a forced-induction limiting control starting temperature. On condition that the temperature of the coolant has risen to a value at which the determining section determines that the temperature obtained by the obtaining section is higher than or equal to the forced-induction limiting control starting temperature, the forced-induction-device controlling section starts a forced-induction limiting control to lower a forced-induction pressure In the forced-induction limiting control, the forced-induction-device controlling section increases an extent of limiting of the forced induction as the temperature obtained by the obtaining section becomes closer to the boiling point.

A cooling water passage structure (10) for an internal combustion engine (1) provided with a supercharger (8), comprises a passage forming member (14) attached to a main body (2) of the internal combustion engine, and internally defining a branch passage (13) communicating with an outlet (12B) of a main body water jacket (12) formed in the main body of the internal combustion engine, and a water temperature sensor (80) provided in the passage forming member to detect a temperature of the cooling water flowing through the branch passage. The water temperature sensor is positioned in a part of a main supply passage (31) defined in the passage forming member closer to an inlet end of the main supply passage than a junction between the main supply passage and a supercharger return passage (34) is.

In an internal combustion engine, a thermostat valve for changing over between coolant circulation through a radiator-routing passage to coolant circulation through a bypass passage, is provided with a first valve for opening and closing the radiator-routing passage, and a second valve for opening and closing the bypass passage. The first and second valves and are operable concurrently. A cylinder coolant jacket around cylinder bores of a cylinder portion is partitioned into two in a cylinder axis direction to thereby form a main cylinder coolant jacket on a side of a cylinder head portion and a sub-cylinder coolant jacket on a side of a crankcase portion. The bypass passage is formed partly by the sub-cylinder coolant jacket. The above arrangement expedites warming-up during the engine start and achieves favorable appearance by a simplified structure.

An assembly for an aircraft propulsion system includes an engine, an aircraft aerostructure, and a heat exchanger. The engine includes a coolant system. The aircraft aerostructure forms a fuel tank for the engine. The aircraft aerostructure includes an aerostructure skin including an interior skin side and an exterior skin side. The interior skin side forms a bottom side of the fuel tank. The exterior skin side forms an aerodynamic surface of the aircraft aerostructure. The heat exchanger is disposed at the aerostructure skin. The heat exchanger includes a heat exchanger body forming a coolant passage. The coolant passage extends through the heat exchanger body between and to an inlet and an outlet. The inlet and the outlet are connected in fluid communication with the coolant system.