High efficiency turboexpander

Claim 3

The method of claim 1 wherein the fluid is a gas.

Claim 4

The method of claim 2 wherein the gas is nitrogen.

Claim 5

The method of claim 1 wherein the rotatable assembly is within a stationary housing and each fluid flow path is also defined by the housing surface.

Claim 6

The method of claim 1 wherein a shroud covers the blades and each fluid flow path is also defined by the shroud surface.

Claim 7

The method of claim 1 further comprising passing the fluid out from the fluid flow path having substantially zero tangential velocity.

Claim 8

A turboexpander having a rotatable assembly comprising a shaft, an impeller hub mounted on the shaft, and a plurality of blades on the impeller hub to form a plurality of fluid flow channels, each fluid flow channel defined by the impeller hub surface and two adjacent blades, characterized by: (A) means to provide fluid into a fluid flow channel at the design point of the turboexpander at an angle directed toward the leading edge of the trailing blade of the two adjacent blades forming the fluid flow channel wherein the angle is within the range of from about -10 to -40 degrees wherein the negative sign of the angle denotes the direction from orthogonal opposite to that in which the rotatable assembly rotates; and (B) the impeller hub and the two adjacent blade surfaces forming the fluid flow channel being contoured so that as a fluid element moves through the fluid flow channel along the mean streamline, the sum of the forces on the element normal to the streamline in the meridional plane is about zero.

Claim 9

A turboexpander having a rotatable assembly comprising a shaft, an impeller hub mounted on the shaft, and a plurality of blades on the impeller hub to form a plurality of fluid flow channels, each fluid flow channel defined by the impeller hub surface and two adjacent blades, characterized by: (A) means to provide fluid into a fluid flow channel at the design point of the turboexpander at an angle directed toward the leading edge of the trailing blade of the two adjacent blades forming the fluid flow channel wherein the angle is within the range of from about -10 to -40 degrees wherein the negative sign of the angle denotes the direction from orthogonal opposite to that in which the rotatable assembly rotates; and (B) the impeller hub and the two adjacent blade surfaces forming the fluid flow channel being contoured so that as a fluid element moves through the fluid flow channel along the mean streamline, the sum of the forces on the element normal to the streamline in the meridional plane is about zero.

Claim 10

The turboexpander of claim 7 wherein the rotatable assembly is within a stationary housing, each fluid flow channel is also defined by the housing surface, and the housing surface is also contoured to achieve the defined force sum.

Claim 11

The turboexpander of claim 7 further comprising a shroud covering the blades wherein each fluid flow channel is also defined by the shroud surface, and the shroud surface is also contoured the achieve the defined force sum.