Device for cooling excitation-current supply lines in liquid-cooled turbogenerator rotors

Claim 2

Device for cooling excitation-current supply lines in a shaft connected at one end thereof to a liquid-cooled turbogeneration rotor having coil windings mounted thereon, the excitation-current supply lines being disposed in bifilar fashion within a bore formed along the axis of the shaft, comprising coolant supply and discharge channels for the coil windings extending in the shaft coaxially to the excitation supply lines and terminating in coolant collecting chambers at the rotor end of the shaft, coolant supply and discharge channels subdivided into a multiplicity of individual subchannels extending in the shaft at minimal spacing from the axial bore for the excitation-current supply lines, said subchannels terminating through radial bores with said coolant collecting chambers at the rotor end of the shaft.

Claim 3

Device according to claim 1 wherein said individual subchannels surround the axial bore so that, alternatingly, a subchannel for coolant supply and a sub-channel for coolant discharge are disposed about the periphery of the axial bore.

Claim 4

Device according to claim 1 wherein a multiplicity of individual sub-channels serving, respectively, as supply and discharge channels are disposed adjacent one another at the periphery of the axial bore.

Claim 5

Device for cooling excitation-current supply lines in liquid cooled turbogenerator rotors which have the excitation-current supply lines disposed in a bifilar fashion in a bore of the shaft comprising coolant supply and discharge channels for the rotor windings running coaxially to the excitation-current supply lines with said channels terminating in coolant collecting chamber subdivided in four ring-segment shaped subchambers for coolant supply and discharge, said axial bore containing said excitation supply lines being surrounded by a multiplicity of coolant supply and discharge channels spaced a minimal distance from each other, said coolant supply channels surrounding said axial bore connected to radial bores leading to an annular channel disposed radially inwardly of said coolant collecting chamber and connected to said ring-segment shaped subchambers for coolant supply, and said coolant discharge channels surrounding said axial bore connected to other radial bores leading to another annular channel also disposed radially inwardly of said coolant collecting chamber and connected to said ring-segment shaped subchambers for coolant discharge.

Claim 6

Device for cooling excitation-current supply lines in liquid cooled turbogenerator rotors which have the excitation-current supply lines disposed in a bifilar fashion in a bore of the shaft comprising coolant supply and discharge channels for the rotor windings running coaxially to the excitation-current supply lines with said channels terminating in coolant collecting chamber subdivided in four ring-segment shaped subchambers for coolant supply and discharge, said axial bore containing said excitation supply lines being surrounded by a multiplicity of coolant supply and discharge channels spaced a minimal distance from each other, said coolant supply channels surrounding said axial bore connected to radial bores leading to an annular channel disposed radially inwardly of said coolant collecting chamber and connected to said ring-segment shaped subchambers for coolant supply, and said coolant discharge channels surrounding said axial bore connected to other radial bores leading to another annular channel also disposed radially inwardly of said coolant collecting chamber and connected to said ring-segment shaped subchambers for coolant discharge.

Claim 7

Device according to claim 4 wherein said radial bores and said ring channels respectively connected thereto are disposed in axially offset planes, the radial bores in one of said planes being connected to sub-channels serving to supply coolant, and the radial bores in the other of said planes being connected to sub-channels serving discharge coolant.

Claim 8

Device according to claim 4 including radial current contact bolts threadedly secured in the excitation-current supply lines at the ends thereof located at the rotor end of the shaft, and high-pressure insulated hoses connecting said individual subchambers of said coolant collecting chamber with said current contact bolts for supplying coolant thereto.

Claim 9

Device according to claim 6 wherein said current contact bolts extend radially inwardly to a location at which a contact connection is formed with the excitation-current supply lines, said current contact bolts being formed with axial coolant supply and discharge bores extending radially to said inner contact connection location.