A plate (3) having a pair of first communication holes (34) and a pair of second communication holes (35) and a plate (4) having a pair of first communication holes (44) and a pair of second communication holes (45) are alternately laminated to alternately form, between the plates (3) and (4) adjacent to each other, a first coolant flow path (81) and a second coolant flow path (82); a first spacer (5) is interposed around each of the first communication holes (34) and (44) within the first coolant flow path (81); and a second spacer (6) is interposed within the second coolant flow path (82) and at a position corresponding to a periphery of each of the first communication holes (34) and (44).

A plate (3) having a pair of first communication holes (34) and a pair of second communication holes (35) and a plate (4) having a pair of first communication holes (44) and a pair of second communication holes (45) are alternately laminated to alternately form, between the plates (3) and (4) adjacent to each other, a first coolant flow path (81) and a second coolant flow path (82); a first spacer (5) is interposed around each of the first communication holes (34) and (44) within the first coolant flow path (81); and a second spacer (6) is interposed within the second coolant flow path (82) and at a position corresponding to a periphery of each of the first communication holes (34) and (44).

An aircraft heat exchanger arranged longitudinally and including a casing with an inner chamber configured so that coolant flows longitudinally from an inlet to an outlet, a plurality of laterally spaced longitudinally extending inner chamber plates, and a plurality of channels defined between contiguous plates. Each plate includes a leading edge oriented towards the inlet and configured to divert coolant towards the channels. A plurality of the plates include an inner hollow area configured to conduct a flow of hot bleed air therethrough. Leading edges of a first group of plates are arranged in a stepped pattern. A gap defined between the first group of plates and a first casing lateral wall establishes a fluid coolant communication through the first group of plates between the casing inlet and outlet. The lateral distance between each leading edge of the first group of plates and the first lateral wall decreases longitudinally.

An aircraft heat exchanger arranged longitudinally and including a casing with an inner chamber configured so that coolant flows longitudinally from an inlet to an outlet, a plurality of laterally spaced longitudinally extending inner chamber plates, and a plurality of channels defined between contiguous plates. Each plate includes a leading edge oriented towards the inlet and configured to divert coolant towards the channels. A plurality of the plates include an inner hollow area configured to conduct a flow of hot bleed air therethrough. Leading edges of a first group of plates are arranged in a stepped pattern. A gap defined between the first group of plates and a first casing lateral wall establishes a fluid coolant communication through the first group of plates between the casing inlet and outlet. The lateral distance between each leading edge of the first group of plates and the first lateral wall decreases longitudinally.

A condenser includes first and second header tanks provided on one side of the condenser, and a third header tank provided on another side of the condenser. A plurality of second heat exchange tubes extend in an extending direction between the second header tank and the third header tank to connect the second header tank and the third header tank. A plurality of first heat exchange tubes are provided to extend in the extending direction between the first header tank and the third header tank to connect the first header tank and the third header tank. The plurality of first heat exchange tubes are directly connected to the first header tank. The plurality of first heat exchange tubes are longer than the plurality of second heat exchange tubes and are positioned downstream of the plurality of second heat exchange tubes with respect to a flow of refrigerant.

A heat exchanger is provided. The heat exchanger (40) provides a first plurality of tubes (50) and a second plurality of flow passages (52) which furcate near one of the first (42) and second (44) manifolds into two or more furcated flow passages and subsequently converge to exit the heat exchanger. The plurality of furcated flow passages are intertwined, reducing the distance between flow passages (50,52) containing each fluid therebetween to improve thermal transfer. Further, the furcations create changes of direction of the fluid to re-establish new thermal boundary layers within the flow passages to further reduce resistance to thermal transfer.

In cooling/heating cycles of a heat exchanger, to prevent cracks that tend to occur in a brazed portion between an end portion of a horizontal cross-section of a tube and a header plate. An end portion cover body is provided for an end portion of a tank main body or a header to cover hereby an end portion in a longer side direction of an opening end portion of a flat tube.

A stub connection for a heat exchanger that is arranged in a housing and has a stack including plates and fins. The housing consists of housing parts which can be joined together, and at least one first stub for a first heat-exchanging medium being integrated directly into the housing. The stub connection also includes at least one second stub for a second heat-exchanging medium that extends to outside the housing. The at least one second stub is configured for the connection of a line and is integrated directly or indirectly into the housing.

Leakage of a heating medium from a condenser or an evaporator can be quickly detected by a simple structure. A refrigeration apparatus 1 according to the present invention is formed by connecting a compressor 11, a condenser 12, an expansion valve 13 and an evaporator 14 by a pipe 15 such that a heating medium circulates therethrough in this order. The refrigeration apparatus 1 further includes a pressure detection unit 31, 32 that detects a pressure of the heating medium flowing through the pipe 15, and a control unit 41 that determines that leakage of the heating medium from the condenser 12 or the evaporator 14 has occurred, when a pressure detected by the pressure detection unit 31, 32 becomes not more than a predetermined value.

Leakage of a heating medium from a condenser or an evaporator can be quickly detected by a simple structure. A refrigeration apparatus 1 according to the present invention is formed by connecting a compressor 11, a condenser 12, an expansion valve 13 and an evaporator 14 by a pipe 15 such that a heating medium circulates therethrough in this order. The refrigeration apparatus 1 further includes a pressure detection unit 31, 32 that detects a pressure of the heating medium flowing through the pipe 15, and a control unit 41 that determines that leakage of the heating medium from the condenser 12 or the evaporator 14 has occurred, when a pressure detected by the pressure detection unit 31, 32 becomes not more than a predetermined value.