Cooling system for turbines

Claim 2

A cooling structure for supplying cooling air to a chamber at a face of a turbine disk the structure being a single unitary case article including: spaced annular walls defining an air flow chamber and terminating at one end in an axially positioned discharge nozzle having vanes therein extending between the walls and integral therewith; an annular connecting element integral with and connecting said walls at the ends remote from the nozzle, said element extending from said walls and having mounting means on the end remote from the wall; radially extending partitions integral with extending between and connecting the spaced walls and defining circumferentially spaced flow passages for air from said connecting element to the nozzle, the element having air inlet holes therein; an interrupted substantially cylindrical partition integral with and between said walls at a point spaced from said connecting element, said cylindrical partition being interrupted to form openings therein at points in alignment with the holes in the connecting element for a flow of air from said holes to said openings between selected partitions and one of said annular walls having first access openings therein out of alignment with the holes in the connecting walls and the openings in the cylindrical partition, the other of said annular walls having attachment means therein for access through the openings in said one of said annular walls.

Claim 3

A cooling structure as in claim 1 in which the openings in said one of said walls are located between partitions other than the selected positions between which the cooling flow is directed.

Claim 4

A cooling structure as in claim 1 in which certain adjacent radially extending partitions on the one side of the cylindrical element converge toward one another and merge to form a single partition extending to and integral with certain of the vanes.

Claim 5

A cooling structure as in claim 1 in which said other wall has second access openings therein substantially in radial alignment with the openings in said one of said walls, said second access openings being located on the opposite side of the cylindrical partitions from said first access openings.

Claim 6

A cooling structure for supplying cooling air to a chamber at a face of a turbine disk, the structure being a single unitary cast article including: spaced annular walls extending in a generally radial direction from their outer ends and changing direction to an axial direction at their inner ends, said walls having integral vanes adjacent their inner ends to form nozzles for directing cooling air against the disk; an annular connecting element integral with the spaced outer ends of the annular walls and extending outwardly therefrom, said element having an attachment flange at its outer end; an annular cylindrical partition extending between the spaced walls and integral therewith and spaced radially inwardly from said connecting element; substantially radial partitions between and integral with the spaced walls and between said connecting element and said cylindrical partition and integral therewith, said connecting element and cylindrical partition having openings therein in radial alignment and located between selected pairs of radial partitions for a flow of air therethrough and to the nozzles; inward extensions of certain selected adjacent partitions of said radial partitions between which the cooling air flows diverging to merge with adjacent partitions to define triangular spaces therebetween; and one of said spaced annular walls having openings therein communicating with the said triangular spaces, the other wall having mounting means at these triangular spaces for access through said openings in said one of said walls.

Claim 7

A cooling structure for supplying cooling air to a chamber at a face of a turbine disk, the structure being a single unitary cast article including: spaced annular walls extending in a generally radial direction from their outer ends and changing direction to an axial direction at their inner ends, said walls having integral vanes adjacent their inner ends to form nozzles for directing cooling air against the disk; an annular connecting element integral with the spaced outer ends of the annular walls and extending outwardly therefrom, said element having an attachment flange at its outer end; an annular cylindrical partition extending between the spaced walls and integral therewith and spaced radially inwardly from said connecting element; substantially radial partitions between and integral with the spaced walls and between said connecting element and said cylindrical partition and integral therewith, said connecting element and cylindrical partition having openings therein in radial alignment and located between selected pairs of radial partitions for a flow of air therethrough and to the nozzles; inward extensions of certain selected adjacent partitions of said radial partitions between which the cooling air flows diverging to merge with adjacent partitions to define triangular spaces therebetween; and one of said spaced annular walls having openings therein communicating with the said triangular spaces, the other wall having mounting means at these triangular spaces for access through said openings in said one of said walls.

Claim 8

A cooling structure as in claim 5 in which one of said walls has mounting means located between the radial partitions in the area where there is no air flow and the other wall has openings therein for access to said mounting means.