Abstract: Predictive monitoring of a rotational machine of a cooling apparatus is provided by integrating a predictive vibration analyzer into an electronics rack being cooled by the cooling apparatus. The integrating includes associating at least one sensor of the predictive vibration analyzer with the rotational machine of the cooling apparatus. The analyzer includes a predetermined harmonics table of one or more base operational frequencies and associated rotational speed harmonics for the rotational machine indicative of one or more rotational faults, and the predictive vibration analyzer automatically evaluates vibration of the rotational machine during operation of the machine by analyzing vibration data therefor, and automatically ascertains, based on the vibration data, and the predetermined harmonics table, whether the rotational machine is predicted to possess a rotational fault of the one or more rotational faults.

Abstract: An anti-counterfeiting technique presents, to a test thermoreflective mark at a first temperature, a first electromagnetic wave. A first test reflective profile for the test thermoreflective mark associated with the first temperature is recorded. A second electromagnetic wave is presented to the test thermoreflective mark at a second temperature. A second test reflective profile for the test thermoreflective mark associated with the second temperature is recorded. The first test reflective profile is compared with a first control reflective profile that is associated with a genuine thermoreflective mark. The second test reflective profile is compared with a second control reflective profile that is associated with the genuine thermoreflective mark.

Abstract: Some embodiments of the inventive subject matter include a computer program product for validating a test thermoreflective mark. The computer program product can include computer usable program code configured to control a temperature regulation unit configured to govern a temperature of a thermoreflective mark. The computer usable program code can be further configured to control an electromagnetic waver emitter to present at a first temperature, a first electromagnetic wave. The computer usable program code can be further configured to record a first reflective profile. The computer usable program code can be further configured to control the electromagnetic wave emitter to present at a second temperature, a second electromagnetic wave. The computer usable program code can be further configured to record a second reflective profile. The computer usable code can be further configured to validate the thermoreflective mark based on the first reflective profile and the second reflective profile.

Abstract: A method for hybrid computational fluid dynamics (CFD) approach for modeling a bounded domain, such as a data center, is disclosed. The CFD modeling approach divides the bounded domain into one or more viscous regions and one or more inviscid regions, and then performs a viscous domain solve for the viscous region(s) using a computational fluid dynamics model with turbulence equations (i.e., a turbulence model), and performs inviscid domain solve for the inviscid region(s) using a set of inviscid equations (or potential flow equations). After solving for the different regions, results of the viscous domain solve and the inviscid domain solve are provided as a model of the bounded domain.

Abstract: A hybrid computational fluid dynamics (CFD) approach for modeling a bounded domain, such as a data center, is disclosed. The CFD modeling approach divides the bounded domain into one or more viscous regions and one or more inviscid regions, and then performs a viscous domain solve for the viscous region(s) using a computational fluid dynamics model with turbulence equations (i.e., a turbulence model), and performs inviscid domain solve for the inviscid region(s) using a set of inviscid equations (or potential flow equations). After solving for the different regions, results of the viscous domain solve and the inviscid domain solve are provided as a model of the bounded domain.

Abstract: An apparatus to cool a computing device is provided and includes a structure. The structure includes a coolant moving device and a heat generating component. The structure is formed such that the coolant moving device is configured to generate a first flow of coolant into a plenum in a first direction and a second flow of coolant from the plenum in a second direction, which is transverse to the first direction, such that the coolant thermally interacts with the heat generating component. The structure further includes a plate interposed between the plenum and the heat generating component. The plate includes aerodynamic elements disposed to extend into the plenum.

Abstract: An inlet recirculation apparatus for an air moving device includes a housing defined by a wall extending from a base. The base includes an aperture therethrough receptive to alignment with an inlet of the air moving device. A plurality of flaps each pivotally extends radially outwardly from a center pivot to another corresponding pivot disposed around a perimeter of the wall. The center pivot is coaxial with a center of the aperture. Each flap moves to an open position due to air pressure from the air moving device causing air to flow into the inlet wherein each flap pivotally rotates about the center pivot and corresponding pivot at the wall, and moves to a closed position when air pressure from the air moving device ceases wherein a space between contiguous flaps is eliminated when each flap pivotally rotates to the closed position about the center pivot and corresponding pivot at the wall to prevent reverse airflow through the air moving device.

Abstract: A hybrid computational fluid dynamics (CFD) approach for modeling a bounded domain, such as a data center, is disclosed. The CFD modeling approach divides the bounded domain into one or more viscous regions and one or more inviscid regions, and then performs a viscous domain solve for the viscous region(s) using a computational fluid dynamics model with turbulence equations (i.e., a turbulence model), and performs inviscid domain solve for the inviscid region(s) using a set of inviscid equations (or potential flow equations). After solving for the different regions, results of the viscous domain solve and the inviscid domain solve are provided as a model of the bounded domain.

Abstract: A method for hybrid computational fluid dynamics (CFD) approach for modeling a bounded domain, such as a data center, is disclosed. The CFD modeling approach divides the bounded domain into one or more viscous regions and one or more inviscid regions, and then performs a viscous domain solve for the viscous region(s) using a computational fluid dynamics model with turbulence equations (i.e., a turbulence model), and performs inviscid domain solve for the inviscid region(s) using a set of inviscid equations (or potential flow equations). After solving for the different regions, results of the viscous domain solve and the inviscid domain solve are provided as a model of the bounded domain.

Abstract: An electronics component cabinet cover test device includes a housing that defines a test apparatus provided with first and second openings. A cover member is mounted to one of the openings, and an air moving device is arranged in the test apparatus. The air moving device includes an air inlet and an air outlet and generates airflow within the test apparatus. A sensor capable of measuring a characteristic of the airflow is mounted within the test apparatus. An airflow impedance device mounted to the inlet or the outlet of the air moving device. The airflow impedance device is configured to simulate an airflow obstruction. A controller establishes a flow rate of air from the air moving device and receives airflow data corresponding to the characteristic of the airflow from the sensor to determine one of an acoustical performance characteristic and a thermal performance characteristic of the cover member.

Abstract: A centrifugal magnetic clutch device includes, an input shaft and, a plurality of input magnets that are rotatable about an axis of the input shaft, and are radially movable relative to the input shaft axis, and are rotationally fixed to the input shaft. The device further includes, a plurality of output magnets rotatable about the input shaft axis and in axial alignment with the plurality of input magnets, and an output shaft rotationally fixed to the plurality of output magnets. The device further includes, a housing for fluidically sealing the plurality of output magnets and the output shaft relative to the plurality of input magnets and the input shaft.

Abstract: An inlet recirculation apparatus for an air moving device includes a housing defined by a wall extending from a base. The base includes an aperture therethrough receptive to alignment with an inlet of the air moving device. A plurality of flaps each pivotally extends radially outwardly from a center pivot to another corresponding pivot disposed around a perimeter of the wall. The center pivot is coaxial with a center of the aperture. Each flap moves to an open position due to air pressure from the air moving device causing air to flow into the inlet wherein each flap pivotally rotates about the center pivot and corresponding pivot at the wall, and moves to a closed position when air pressure from the air moving device ceases wherein a space between contiguous flaps is eliminated when each flap pivotally rotates to the closed position about the center pivot and corresponding pivot at the wall to prevent reverse airflow through the air moving device.

Abstract: Disclosed herein is a device that relates to a centrifugal magnetic clutch device. The device comprising an input shaft and, a plurality of input magnets that are rotatable about an axis of the input shaft, and are radially movable relative to the input shaft axis, and are rotationally fixed to the input shaft. The device further comprising, a plurality of output magnets rotatable about the input shaft axis and in axial alignment with the plurality of input magnets, and an output shaft rotationally fixed to the plurality of output magnets. The device further comprising, a housing for fluidically sealing the plurality of output magnets and the output shaft relative to the plurality of input magnets and the input shaft.

Abstract: A system for airflow management in an electronic enclosure includes a backplane assembly having at least one backplane connector, at least one daughter card, and components disposed on the daughter card oriented to facilitate front-to-back airflow, wherein inlet cooling air impinges on the backplane assembly and splits into at least two flow portions flowing in different directions along a surface defining the backplane assembly

Abstract: A dual-blower assembly includes a single blower housing, the single blower housing defined by a base and opposite top, a pair of opposing side walls and a pair of opposing end walls intermediate the base and the top; a pair of inlet openings in the top; a front blower and a rear blower serially packaged in the single blower housing in a same plane, each blower aligned with a respective inlet opening of the pair of inlet openings; a rear blower exhaust opening for the rear blower disposed in one of the pair of end walls proximate the rear blower; and a front blower side exhaust opening for the front blower disposed in one of the pair of opposing side walls, the front blower side exhaust opening aligned with the front blower. Both the front and rear blowers are configured to force air in a direction from the front blower to the rear blower.