Abstract: A cooling system for a data center in which equipment racks are disposed has a cooling unit and a controller coupled to the cooling unit. The cooling system includes temperature sensors at or near the cooling unit's air return inlet, at or near the cooling unit's air supply outlet, and at or near the equipment racks air inlet(s). The controller measures these temperatures. A relative humidity sensor is located at or near the air return inlet of the cooling unit. The relative humidity where the relative humidity sensor is located is measured by the controller using the relative humidity sensor. The controller calculates the dew point temperature from the temperature sensor and relative humidity. Using this dew point, which is essentially constant throughout the space being conditioned, and the temperatures from the other locations, the controller then calculates the relative humidity at each location.

Abstract: A cooling system for a data center in which equipment racks are disposed has a cooling unit and a controller coupled to the cooling unit. The cooling system includes temperature sensors at or near the cooling unit's air return inlet, at or near the cooling unit's air supply outlet, and at or near the equipment racks air inlet(s). The controller measures these temperatures. A relative humidity sensor is located at or near the air return inlet of the cooling unit. The relative humidity where the relative humidity sensor is located is measured by the controller using the relative humidity sensor. The controller calculates the dew point temperature from the temperature sensor and relative humidity. Using this dew point, which is essentially constant throughout the space being conditioned, and the temperatures from the other locations, the controller then calculates the relative humidity at each location.

Abstract: The inlet of a turbofan jet propulsion engine is coupled to the engine fan casing via a unique uniflange coupling assembly. One of the inlet and casing components carries a radial flange while the other of the components carries a pair of radial flanges each spaced on opposite sides of the flange carried by the first component. A pair of toroidally shaped members are positioned respectively between the two pairs of spaced opposing abutment surfaces thus formed by the three flanges. Preferably the members are hollow, have flexible but substantially inelastic walls, and are filled with a fluid. These members allow the two components to angulate relative to each other while allowing loads to be transferred from the first component to the second component only in an axial direction. Other loads are transferred to the engine mounting structure through other linkage.