A rocker chiller includes a chilling tank and a baffle assembly. The baffle assembly includes a drive shaft, a baffle blade extending along a bottom of the tank and a plurality of spaced-apart and elongate baffle members extending in a radial direction from the drive shaft towards the bottom of the tank. The elongate baffle members contact the drive shaft at spaced-apart locations along the drive shaft and define a plurality of openings therebetween. The elongate baffle members are sized and shaped to push at least a majority of the carcasses laterally through the heat exchanging liquid in a direction generally orthogonal to a lengthwise forward movement of the carcasses from the first end of the tank to the second end of the tank.

A pin fin cooling system may include at least one first surface defining at least a base portion of the cooling system, and at least one pin fin array of a plurality of pin fins and at least one coolant fluid flow detector extending from the first surface. The coolant fluid flow deflector may be configured to split a coolant fluid flow from a primary flow into at least two secondary flows that follow a predetermined path over local heat sources, and may have a maximum wall thickness that is equal to a diameter of a cross-section of one of the pin fins. The cooling system may further include at least one boundary fin extending from the first surface that is in the shape of a spline, at least a portion of which may correspond and match at least a portion of a pattern of the pin fin array.

A pin fin cooling system may include at least one first surface defining at least a base portion of the cooling system, and at least one pin fin array of a plurality of pin fins and at least one coolant fluid flow detector extending from the first surface. The coolant fluid flow deflector may be configured to split a coolant fluid flow from a primary flow into at least two secondary flows that follow a predetermined path over local heat sources, and may have a maximum wall thickness that is equal to a diameter of a cross-section of one of the pin fins. The cooling system may further include at least one boundary fin extending from the first surface that is in the shape of a spline, at least a portion of which may correspond and match at least a portion of a pattern of the pin fin array.

An air handling system that includes at least one earth-coupled heat exchanger assembly that further includes a first pipe section having an inner diameter and an outer diameter; a second pipe section concentrically surrounding a portion of the first pipe section, wherein the second pipe section includes an inner diameter and an outer diameter, wherein the outer diameter of the first pipe section and the inner diameter of the second pipe section define a space therebetween, and wherein the space between the first pipe section and the second pipe section is evacuated to form an insulating vacuum therein; and a third pipe section concentrically surrounding a portion of the second pipe section, wherein the third pipe section includes an inner diameter and an outer diameter, and wherein the outer diameter of the second pipe and the inner diameter of the third pipe section define a passageway therebetween.

An air handling system that includes at least one earth-coupled heat exchanger assembly that further includes a first pipe section having an inner diameter and an outer diameter; a second pipe section concentrically surrounding a portion of the first pipe section, wherein the second pipe section includes an inner diameter and an outer diameter, wherein the outer diameter of the first pipe section and the inner diameter of the second pipe section define a space therebetween, and wherein the space between the first pipe section and the second pipe section is evacuated to form an insulating vacuum therein; and a third pipe section concentrically surrounding a portion of the second pipe section, wherein the third pipe section includes an inner diameter and an outer diameter, and wherein the outer diameter of the second pipe and the inner diameter of the third pipe section define a passageway therebetween.

Disclosed are various turbulent, corrosion-resistant heat exchangers used in desiccant air conditioning systems.

Disclosed are various turbulent, corrosion-resistant heat exchangers used in desiccant air conditioning systems.

A device is provided that includes a heat conductive structure; a heat transfer structure for extracting heat from the heat conductive structure by means of a boundary layer; a motor for rotating the heat transfer structure relative to the heat conductive structure; and a vertical fixing mechanism for allowing the heat transfer structure to rotate above the heat transfer structure without making contact with the heat transfer structure so as to define a boundary layer between the heat conductive structure and heat transfer structure, wherein the heat transfer structure extracts heat from the heat conductive structure by means of the boundary layer, and wherein the heat conductive structure includes small geometric turbulators.

A device is provided that includes a heat conductive structure; a heat transfer structure for extracting heat from the heat conductive structure by means of a boundary layer; a motor for rotating the heat transfer structure relative to the heat conductive structure; and a vertical fixing mechanism for allowing the heat transfer structure to rotate above the heat transfer structure without making contact with the heat transfer structure so as to define a boundary layer between the heat conductive structure and heat transfer structure, wherein the heat transfer structure extracts heat from the heat conductive structure by means of the boundary layer, and wherein the heat conductive structure includes small geometric turbulators.

A cooling system for an information handling system comprises a fan with a sunflower type heat exchanger having two heat exchanger bodies separated by a gap and rotationally offset an angle sized such that a fin of the first heat exchanger body is aligned relative to a channel between two adjacent fins of the second heat exchanger body. As airflow flows through channels between adjacent fins of the first heat exchanger body, the air temperature increases. Air exiting the first heat exchanger body mixes with a second airflow entering the gap between the two heat exchanger bodies and the combined airflow is cooler and turbulent for additional heat absorbing capability for improved cooling.