Patent ID: 8015824

Claim:
A system for regulating a cooling fluid within a turbomachine, the turbomachine comprising a compressor section and at least one wheelspace area, the system comprising: a cooling circuit comprising: a heat exchanging system comprising: an upstream port that is connected to an extraction port on compressor section, wherein a cooling fluid comprising air exits the compressor section via the extraction port and enters the heat exchanger; and a downstream port; wherein the heat exchanger receives the cooling fluid at a first temperature and discharges the cooling fluid at a second temperature; an external flow conditioning system comprising: an inlet portion connected to the downstream port of the heat exchanger; wherein an upstream end of the inlet portion receives the cooling fluid from the heat exchanger via the downstream port; a branch connection comprising: a first section comprising an upstream end connected to a downstream end of the inlet portion; a second section comprising an upstream end connected to a first downstream end of the first section, and a control valve that modulates the cooling fluid flowing through the branch connection; and a third section comprising an upstream end connected to a second downstream end of the first section, and a bypass orifice that adjusts flow properties of the cooling fluid; and a stop valve comprising an upstream end connected to downstream ends of the second section and the third section: and an outlet portion comprising upstream end that connected to a discharge end of the stop valve, and a downstream end connected to a connection port located on a compressor discharge casing of the turbomachine; a plurality of flow chambers integrated with the compressor discharge casing, wherein an upstream end of each of the plurality of flow chambers is connected to the connection port in an arrangement that non-cooling fluid flows downstream through the compressor as the cooling fluid, received from the connection port, flows through the plurality of flow chambers; wherein each of the plurality of flow chambers is fastened to the compressor discharge casing in a manner that creates a cavity between an aft end of each of the plurality of flow chambers and a downstream area of the compressor discharge casing; an angular section located on an aft end of the plurality of flow chambers and positioned adjacent to the cavity; wherein the angular section comprises an angle measured relative to the axis of rotation of a plurality of rotating components within the turbine section; and the angular section comprises surfaces that pre-swirls the cooling fluid that exits the plurality of flow chambers and enters the wheelspace areas, wherein an angle of the angular section comprises a range of from about 30 degrees to about 70 degrees.