Rotor for electrical device

Claim 2

A rotor for a bi-polar turbo-generator, comprising: a core of magnetic material having a rotational axis; at least one winding on said core, said winding having a plurality of turns of hollow conductor, said turns having axial portions oriented substantially parallel to said axis and a pair of end portions oriented substantially transverse to said axis; a pair of shaft ends disposed axially outside said end portions and flanged to opposite ends of said core, each of said shaft ends having an integral shaft end flange; a pair of spacing pieces of non-magnetic material, each of said spacing pieces being disposed between the core and one of said shaft end flanges; means for securing each of said spacing pieces to an adjacent end flange; means located at one of said spacing pieces and cooperating with one of said shaft ends for conveying coolant into said turns of hollow conductor at one of said end portions; means located at one of said spacing pieces and cooperating with the other of said shaft ends for conveying coolant from said turns of hollow conductor at the opposite one of said end portions; a cylindrical casing surrounding said core to exert a pressure against the air gap surface thereof; and means for securing said cylindrical casing in pressure tight relationship to said spacing pieces.

Claim 3

A rotor according to claim 1, wherein said means for securing comprise an annular slot in each of said spacing pieces, each slot facing said core, said cylindrical casing being received at each end in one of said annular slots.

Claim 4

A rotor according to claim 2, wherein each of said slots is provided with at least one sealing ring of resilient material recessed in a slot wall.

Claim 5

A rotor according to claim 1, wherein each of said shaft ends includes a bearing, and said means for conveying coolant into said turns comprises: first oil channel means leading from said one bearing through its associated shaft and; an oil distributing space defined between said shaft and said core and connected to said oil channel means, said space communicating with said turns through a plurality of axially directed holes bored in said turns at said one end portion.

Claim 6

A rotor according to claim 4, wherein said means for conveying coolant from said turns comprises: an oil receiving space defined between the other shaft end and said core, said receiving space communicating with said turns through a further plurality of axially directed holes bored in said turns at said other end portion; second oil channel means leading from said oil receiving space to the other bearing on said other shaft end.

Claim 7

A rotor according to claim 1, wherein said core is provided with a plurality of axially directed cooling channels connected in parallel with said means for conveying coolant into and from said turns.

Claim 8

A rotor according to claim 4, wherein said core is provided with a plurality of axially directed cooling channels connected in parallel with said means for conveying coolant into and from said turns.

Claim 9

A rotor according to claim 6, wherein said axially directed cooling channels are limited in radial direction by the inner surface of said cylindrical casing.

Claim 10

A rotor according to claim 1 further comprising at least one non-magnetic filling body located between said axial portions of said turns and said cylindrical casing, said filling body having a plurality of axially directed cooling channels connected in parallel with said means for conveying coolant into and from said turns, said cooling channels being limited in radial direction by the inner surface of said cylindrical casing.

Claim 11

A rotor according to claim 1, wherein said cylindrical casing is prestressed to exert said pressure during operation, said pressure being evenly distributed along said core in the axial direction.

Claim 12

A rotor according to claim 10, wherein said cylindrical casing is spaced from said core by a body of pressurized, thermosetting resin, arranged between said core and said casing.

Claim 13

A rotor according to claim 10, wherein said cylindrical casing is spaced from said core by a plurality of axially directed metal tubes filled with a pressurized, themosetting plastic.

Claim 14

A rotor for a bi-polar turbo-generator, comprising: a core of magnetic material having a rotational axis; at least one winding on said core, said winding having a plurality of turns of hollow conductor, said turns having axial portions oriented substantially parallel to said axis and a pair of end portions oriented substantially transverse to said axis; a pair of shaft ends disposed axially outside said end portions and flanged to opposite ends of said core, each of said shaft ends having an integral shaft end flange; a pair of spacing pieces of non-magnetic material, each of said spacing pieces being disposed between the core and one of said shaft end flanges; means located at one of said spacing pieces and cooperating with one of said shaft ends for conveying coolant into said turns of hollow conductor at one of said end portions; means located at one of said spacing pieces and cooperating with the other of said shaft ends for conveying coolant from said turns of hollow conductor at the opposite one of said end portions; a cylindrical casing surrounding said core to exert a pressure against the air gap surface thereof; and a tightening surface formed in each of said shaft end flanges facing the inside of said cylindrical casing for securing said cylindrical casing in pressure tight relationship to said shaft end flanges.

Claim 15

A rotor for a bi-polar turbo-generator, comprising: a core of magnetic material having a rotational axis; at least one winding on said core, said winding having a plurality of turns of hollow conductor, said turns having axial portions oriented substantially parallel to said axis and a pair of end portions oriented substantially transverse to said axis; a pair of shaft ends disposed axially outside said end portions and flanged to opposite ends of said core, each of said shaft ends having an integral shaft end flange; a pair of spacing pieces of non-magnetic material, each of said spacing pieces being disposed between the core and one of said shaft end flanges; means located at one of said spacing pieces and cooperating with one of said shaft ends for conveying coolant into said turns of hollow conductor at one of said end portions; means located at one of said spacing pieces and cooperating with the other of said shaft ends for conveying coolant from said turns of hollow conductor at the opposite one of said end portions; a cylindrical casing surrounding said core to exert a pressure against the air gap surface thereof; and a tightening surface formed in each of said shaft end flanges facing the inside of said cylindrical casing for securing said cylindrical casing in pressure tight relationship to said shaft end flanges.

Claim 16

A rotor according to claim 13, wherein at least one of said shaft end flanges is provided with a sealing ring of resilient material recessed in said tightening surface.

Claim 17

A rotor according to claim 13, wherein said means for securing comprises an annular slot in each of said spacing pieces, each slot facing said core, said cylindrical casing being received at each end in one of said annular slots.

Claim 18

A rotor according to claim 15, wherein each of said slots is provided with at least one sealing ring of resilient material recessed in a slot wall.

Claim 19

A rotor according to claim 13, wherein each of said shaft ends includes a bearing, and said means for conveying coolant into said turns comprises: first oil channel means leading from said one bearing through its associated shaft and; an oil distributing space defined between said shaft and said core and connected to said oil channel means, said space communicating with said turns through a plurality of axially directed holes bored in said turns at said one end portion.

Claim 20

A rotor according to claim 17, wherein said means for conveying coolant from said turns comprises: an oil receiving space defined between the other shaft end and said core, said receiving space communicating with said turns through a further plurality of axially directed holes bored in said turns at said other end portion; second oil channel means leading from said oil receiving space to the other bearing on said other shaft end.

Claim 21

A rotor according to claim 13, wherein said core is provided with a plurality of axially directed cooling channels connected in parallel with said means for conveying coolant into and from said turns.

Claim 22

A rotor according to claim 17, wherein said core is provided with a plurality of axially directed cooling channels connected in parallel with said means for conveying coolant into and from said turns.

Claim 23

A rotor according to claim 19, wherein said axially directed cooling channels are limited in radial direction by the inner surface of said cylindrical casing.

Claim 24

A rotor according to claim 13 further comprising at least one non-magnetic filling body located between said axial portions of said turns and said cylindrical casing, said filling body having a plurality of axially directed cooling channels connected in parallel with said means for conveying coolant into and from said turns, said cooling channels being limited in radial direction by the inner surface of said cylindrical casing.

Claim 25

A rotor according to claim 13, wherein said cylindrical casing is prestressed to exert said pressure during operation, said pressure being evenly distributed along said core in the axial direction.

Claim 26

A rotor according to claim 23, wherein said cylindrical casing is spaced from said core by a body of pressurized, thermosetting resin, arranged between said core and said casing.

Claim 27

A rotor according to claim 23, wherein said cylindrical casing is spaced from said core by a plurality of axially directed metal tubes filled with a pressurized, thermosetting plastic.