Foil bearing turbomachine

Claim 2

A turbine wheel rotatably supported by bearings within a turbine housing, said wheel comprising: a hub; a back plate disposed at one end of said hub; and a plurality of blades generally extending between said hub and said back plate; said back plate, in areas of negative pressure on the blade side thereof, including a plurality of peripheral slots extending through said back plate to relieve pressure from the non-blade side thereof, an individual slot extending from the suction side of each blade along the periphery of said back plate.

Claim 3

The turbine wheel of claim 1 wherein each peripheral slot is generally shallow and extends from the suction side of each blade generally to the mid-point between adjacent blades.

Claim 4

The turbine wheel of claim 2 wherein each shallow slot is approximately 0.050 inches in depth.

Claim 5

The turbine wheel of claim 1 wherein each peripheral slot is generally deep.

Claim 6

The turbine wheel of claim 4 wherein each deep slot is approximately 0.190 inches in depth.

Claim 7

A turbomachine comprising: a turbine housing; a rotatable turbine wheel disposed within said turbine housing; and bearing means to rotatably support said turbine wheel within said turbine housing, said bearing means including a foil thrust bearing to axially restrain said rotatable turbine wheel; said turbine wheel comprising a hub, a back plate disposed at one end of said hub, and a plurality of blades extending between said hub and said back plate, said back plate, in areas of negative pressure on the blade side thereof when a pressurized fluid is directed against the blades of said turbine wheel, including a plurality of peripheral slots extending through said back plate to relieve fluid pressure from the non-blade side thereof.

Claim 8

A turbomachine comprising: a turbine housing; a rotatable turbine wheel disposed within said turbine housing; and bearing means to rotatably support said turbine wheel within said turbine housing, said bearing means including a foil thrust bearing to axially restrain said rotatable turbine wheel; said turbine wheel comprising a hub, a back plate disposed at one end of said hub, and a plurality of blades extending between said hub and said back plate, said back plate, in areas of negative pressure on the blade side thereof when a pressurized fluid is directed against the blades of said turbine wheel, including a plurality of peripheral slots extending through said back plate to relieve fluid pressure from the non-blade side thereof.

Claim 9

The turbomachine of claim 6 wherein said foil thrust bearing comprises a rotatable thrust runner connected to said turbine wheel, a first thrust plate disposed on one side of said thrust runner, a second thrust plate disposed on the other side of said thrust runner, a first plurality of compliant foils disposed between said first thrust plate and said thrust runner, and a second plurality of compliant foils disposed between said second thrust plate and said thrust runner.

Claim 10

The turbine wheel of claim 7 wherein one peripheral slot is included between each two adjacent blades.

Claim 11

The turbine wheel of claim 8 wherein each peripheral slot is generally shallow and extends from the suction side of each blade generally halfway toward the pressure side of each adjacent blade.

Claim 12

The turbine wheel of claim 9 wherein each shallow slot is approximately 0.050 inches in depth.

Claim 13

The turbine wheel of claim 8 wherein each peripheral slot is generally deep and situated at the suction side of each blade.

Claim 14

The turbine wheel of claim 11 wherein each deep slot is approximately 0.190 inches in depth.

Claim 15

A turbomachine comprising: a turbine housing; a rotatable turbine wheel disposed within said turbine housing, said wheel including a hub, a back plate disposed at one end of said hub, and a plurality of blades extending between said hub and said back plate; and bearing means, including a foil thrust bearing to axially restrain said rotatable turbine wheel, to rotatably support said turbine wheel within said turbine housing, the foil thrust bearing comprising a rotatable thrust runner connected to said turbine wheel, a first thrust plate disposed on one side of said thrust runner, a second thrust plate disposed on the other side of said thrust runner, a first plurality of compliant foils disposed between said first thrust plate and said thrust runner, and a second plurality of compliant foils disposed between said second thrust plate and said thrust runner; said turbine housing including a nozzle ring disposed around said turbine wheel and including a plurality of nozzles to direct the flow of a pressurized fluid against the turbine wheel, said nozzle ring having an annular projection extending towards the turbine wheel back plate to reduce the clearance and thereby restrict the flow of pressurized fluid therebetween; said turbine wheel back plate, in areas of negative pressure on the blade side thereof when a pressurized fluid is directed from the turbine ring nozzles against said turbine wheel, including a plurality of peripheral slots extending through said back plate to relieve fluid pressure from the nonblade side thereof.

Claim 16

A turbomachine comprising: a turbine housing; a rotatable turbine wheel disposed within said turbine housing, said wheel including a hub, a back plate disposed at one end of said hub, and a plurality of blades extending between said hub and said back plate; and bearing means, including a foil thrust bearing to axially restrain said rotatable turbine wheel, to rotatably support said turbine wheel within said turbine housing, the foil thrust bearing comprising a rotatable thrust runner connected to said turbine wheel, a first thrust plate disposed on one side of said thrust runner, a second thrust plate disposed on the other side of said thrust runner, a first plurality of compliant foils disposed between said first thrust plate and said thrust runner, and a second plurality of compliant foils disposed between said second thrust plate and said thrust runner; said turbine housing including a nozzle ring disposed around said turbine wheel and including a plurality of nozzles to direct the flow of a pressurized fluid against the turbine wheel, said nozzle ring having an annular projection extending towards the turbine wheel back plate to reduce the clearance and thereby restrict the flow of pressurized fluid therebetween; said turbine wheel back plate, in areas of negative pressure on the blade side thereof when a pressurized fluid is directed from the turbine ring nozzles against said turbine wheel, including a plurality of peripheral slots extending through said back plate to relieve fluid pressure from the nonblade side thereof.

Claim 17

The turbine wheel of claim 13 wherein one peripheral slot is included between each two adjacent blades.

Claim 18

The turbine wheel of claim 14 wherein each slot is generally shallow and extends along the periphery thereof of said back plate from the suction side of each blade generally to the mid-point between adjacent blades.

Claim 19

The turbine wheel of claim 15 wherein each shallow slot is approximately 0.050 inches in depth.

Claim 20

The turbine wheel of claim 14 wherein each peripheral slot is generally deep and situated at the suction side of each blade.

Claim 21

The turbine wheel of claim 17 wherein each deep slot is approximately 0.190 inches in depth.