Turbine blade tip cooling system

1. A turbine blade, comprising:

a generally elongated blade having a leading edge, a trailing edge, a tip section at a first end, a root coupled to the blade at an end generally opposite the first end for supporting the blade and for coupling the blade to a disc, and at least one cavity forming a cooling system in the blade;

a plurality of elongated tip cooling chambers forming a portion of the cooling system and positioned in the tip section proximate to an outer end of the tip section, wherein each of the elongated tip cooling chambers includes openings in a pressure sidewall for exhausting cooling fluids from the cooling system in the blade;

wherein the elongated tip cooling chambers each comprise a plurality of parallel, linear ribs extending from the pressure sidewall toward a suction sidewall forming parallel flow cooling channels for directing cooling fluids and enhancing the cooling capabilities of the turbine blade by acting as a heat transfer rib; and

a cooling fluid orifice extending between the at least one cavity and each of the elongated tip cooling chambers, wherein each of the elongated tip cooling chambers includes the cooling fluid orifice that spans each of the parallel, linear ribs in the elongated tip cooling chamber and is in fluid communication with each of the parallel flow cooling channels in the elongated tip cooling chamber for providing a uniform cooling fluid flow through the elongated tip cooling chamber from proximate a suction sidewall to the pressure sidewall.

2. The turbine blade of claim 1 , wherein each of the elongated tip cooling chambers has a low profile with a longitudinal axis of the elongated tip cooling chamber that is generally orthogonal to a longitudinal axis of the generally elongated blade.

3. The turbine blade of claim 1 , wherein the elongated tip cooling chambers extend from a parting line of the elongated blade to the pressure sidewall.

4. The turbine blade of claim 1 , wherein the at least one cooling fluid orifice comprises a plurality of metering slots extending between the at least one cavity and each of the elongated tip cooling chambers.

5. The turbine blade of claim 4 , wherein the metering slots are independently sized relative to each other to enable the cooling flow from the turbine blade to be tailored relative to cooling fluid supply pressures.

6. A turbine blade, comprising:

a generally elongated blade having a leading edge, a trailing edge, a tip section at a first end, a root coupled to the blade at an end generally opposite the first end for supporting the blade and for coupling the blade to a disc, and at least one cavity forming a cooling system in the blade, wherein the at least one cavity comprises a cooling fluid supply cavity positioned in the generally elongated blade for supplying cooling fluid to the turbine blade;

a plurality of elongated tip cooling chambers forming a portion of the cooling system and positioned in the tip section proximate to an outer end of the tip section, wherein each of the elongated tip cooling chambers includes openings in a pressure sidewall for exhausting cooling fluids from the cooling system in the blade;

wherein the elongated tip cooling chambers each comprise a plurality of parallel, linear ribs extending from the pressure sidewall toward a suction sidewall forming parallel flow cooling channels;

a cooling fluid orifice extending between the at least one cavity and each of the elongated tip cooling chambers, wherein each of the elongated tip cooling chambers includes a cooling fluid orifice that spans each of the parallel, linear ribs in the elongated tip cooling chamber and is in fluid communication with each of the parallel flow cooling channels in the elongated tip cooling chamber for providing a uniform cooling fluid flow through the elongated tip cooling chamber from proximate a suction sidewall to the pressure sidewall; and

wherein the at least one cooling fluid orifice comprises a plurality of metering slots extending between the cooling fluid supply cavity and the elongated tip cooling chambers.

7. The turbine blade of claim 6 , wherein the elongated tip cooling chambers have a low profile with longitudinal axes that are generally orthogonal to a longitudinal axis of the generally elongated blade.

8. The turbine blade of claim 6 , wherein the elongated tip cooling chambers extend from a parting line of the elongated blade to the pressure sidewall.

9. The turbine blade of claim 6 , wherein the metering slots are independently sized relative to each other to enable the cooling flow from the turbine blade to be tailored relative to cooling fluid supply pressures.

10. A method of cooling a tip of a turbine blade of a turbine engine, comprising:

passing cooling fluids from a root of a turbine blade through an internal cooling system, wherein the turbine blade comprises a generally elongated blade having a leading edge, a trailing edge, a tip section at a first end, a root coupled to the blade at an end generally opposite the first end for supporting the blade and for coupling the blade to a disc, at least one cavity forming the cooling system in the blade, wherein the at least one cavity comprises a cooling fluid supply cavity positioned in the generally elongated blade for supplying cooling fluid to the turbine blade elongated tip cooling chambers forming a portion of the cooling system and positioned in the tip section proximate to an outer end of the tip section, wherein each of the elongated tip cooling chambers include openings in a pressure sidewall for exhausting cooling fluids from the cooling system in the blade, wherein the elongated tip cooling chambers each comprise a plurality of parallel, linear ribs extending from the pressure sidewall toward a suction sidewall forming parallel flow cooling channels, a cooling fluid orifice extending between the cooling fluid supply cavity and each of the elongated tip cooling chambers, and wherein each of the elongated tip cooling chambers includes the cooling fluid orifice that spans each of the parallel, linear ribs in the elongated tip cooling chamber and is in fluid communication with each of the parallel flow cooling channels in the elongated tip cooling chamber for providing a uniform cooling fluid flow through the elongated tip cooling chamber from proximate a suction sidewall to the pressure sidewall;

wherein passing cooling fluids through the internal cooling system comprises passing cooling fluids through the at least one opening between the cavity and the elongated tip cooling chambers, passing cooling fluids through the elongated tip cooling chambers between the ribs forming parallel flow cooling channels, and exhausting cooling fluids from the turbine blade through openings in the pressure sidewall.