Pump with axially-elongated annular seal element between inducer and impeller

Patent metadata

Field	Value
Publication number	US-11560899-B2
Application number	US-201817282395-A
Country	US
Kind code	B2
Filing date	Oct 19, 2018
Priority date	Oct 19, 2018
Publication date	Jan 24, 2023
Grant date	Jan 24, 2023

Abstract

A pump includes a shaft that is rotatable about a central axis. An inducer is mounted on the shaft and has an inducer blade and inducer shroud attached at an outer end of the inducer blade. An impeller is mounted on the shaft downstream of the inducer and has an impeller blade and an impeller shroud attached at an outer end of the impeller blade. There is an axially-elongated annular seal element disposed at an axial end of the inducer shroud that provides sealing between the inducer shroud and the impeller shroud.

First claim

What is claimed is:

1. A pump comprising:
a shaft rotatable about a central axis;
an inducer mounted on the shaft, the inducer having an inducer blade and an inducer shroud attached at an outer end of the inducer blade;
an impeller mounted on the shaft downstream of the inducer, the impeller having an impeller blade and an impeller shroud attached at an outer end of the impeller blade;
an axially-elongated annular seal element disposed at an axial end of the inducer shroud providing sealing between the inducer shroud and the impeller shroud, the axially-elongated annular seal element is in a flexed state such that a resiliency of the axially-elongated annular seal element provides a radial clamping force on the impeller shroud, the axially-elongated annular seal element defines an axial length and a radial thickness, and an aspect ratio of the axial length to the radial thickness is from 3 to 10.

2. The pump as recited in claim 1 , wherein the inducer shroud has an inside diameter surface that defines a passage through the inducer shroud, and the axially-elongated annular seal element is radially offset from the inside diameter surface.

3. The pump as recited in claim 1 , wherein the axially-elongated annular seal element projects axially from an enlarged base section on the inducer shroud to a free tip.

4. The pump as recited in claim 3 , wherein a distal portion of the axially-elongated annular seal element, including the free tip, is radially overlapping with the impeller shroud and a proximal portion of the axially-elongated annular seal element is non-overlapping with the impeller shroud.

5. The pump as recited in claim 4 , wherein an axial length of the distal portion that is overlapping with the impeller shroud is 25% or less of a total axial length of the axially-elongated annular seal element from the enlarged base to the free tip.

6. The pump as recited in claim 1 , wherein the axially-elongated annular seal element is formed of steel, titanium-based alloy, nickel-based alloy, aluminum, or composite.

7. The pump as recited in claim 1 , wherein the axially-elongated annular seal element is integral with the inducer shroud.

8. The pump as recited in claim 1 , wherein the inducer shroud includes a lip radially inwards of the axially-elongated annular seal element, the axially-elongated annular seal element and the lip defining an axially-extending slot in a radial space there between.

9. The pump as recited in claim 8 , wherein the lip is spaced from an axial edge of the impeller shroud.

Assignees

• Aerojet Rocketdyne Inc
• Aerojet Ricketdyne Inc

Inventors

• Miller Jeff
• Grota Steven

Classifications

• F04D29/22 Primary

  specially for centrifugal pumps · CPC title

• F04D29/2277 Primary

  for increasing NPSH or dealing with liquids near boiling-point · CPC title