Airfoil frame for computer room air conditioning unit
A computer room air conditioner (CRAC) unit includes a housing having an inlet configured to receive IT air and an outlet configured to exhaust treated air. The CRAC unit further includes a heat exchanger supported by the housing and disposed between the inlet and the outlet of the housing and at least one fan module supported by the housing. The at least one fan module is configured to draw IT air into the housing through the inlet, direct IT air through the heat exchanger, and exhaust treated air through the outlet. The CRAC unit further includes an airfoil frame secured to the housing at the inlet of the housing.
1. A method of reducing pressure drops within a computer room air conditioner unit comprising a housing including a front, a back, two sides, a bottom and an open top, the open top of the housing being configured to receive and direct air toward an interior region of the housing, a heat exchanger supported by the housing within the interior region of the housing, at least one fan module supported by the housing, the at least one fan module being configured to draw air into the housing through the inlet, direct air through the heat exchanger, and exhaust treated air through the outlet, and an airfoil frame secured to the upper portions of the front and the sides of the housing at the open top of the housing, the arrangement being such that the heat exchanger is disposed below the airfoil frame, the airfoil frame defining an inlet of the housing and being configured to direct air to the heat exchanger and to create a boundary layer that substantially eliminates pressure drops at the inlet of the housing, the method comprising:
directing air over the airfoil frame of the housing of the computer room air conditioner unit.
2. The method of claim 1 , wherein the airfoil frame includes at least one airfoil frame member secured to the housing at the inlet of the housing, the at least one airfoil frame member including a leading edge extending from the front of the housing and a trailing edge extending in a direction that is parallel to the front of the housing.
3. The method of claim 2 , wherein the at least one airfoil frame member is hollow in construction and further includes an outer surface extending from the leading edge to the trailing edge.
4. The method of claim 3 , wherein the at least one airfoil frame member further includes a plurality of slots formed in the outer surface.