IP Library › Granted Patent US 11,236,764
Granted Patent B2
US 11,236,764 · App. 16/767,820 · Granted Feb 1, 2022

Pump with housing having internal grooves

Inventors: Khin Phui (Cucamonga, CA); Sen Meng (Reseda, CA)
Assignee: Aerojet Rocketdyne, Inc.
F04D29/52F04D29/4293F04D29/688F05D2250/50
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Quick Facts
Patent No.
US 11,236,764
App. No.
16/767,820
Granted
Feb 1, 2022
Kind
B2
Abstract

A pump includes an axial inducer. The axial inducer includes a housing that has an internal surface that defines an axial fluid passage. A rotor is disposed about a central axis in the fluid passage. The rotor includes at least one blade that defines at least one blade tip. The internal surface of the housing defines a plurality of grooves adjacent the at least one blade tip. The grooves are elongated in a circumferential direction.

Claims (25)

1. A pump comprising:

an axial inducer including

a housing having an internal surface defining an axial fluid passage, and

a rotor disposed about a central axis in the fluid passage of the housing and having at least one blade defining at least one blade tip,

the internal surface of the housing defining a plurality of grooves adjacent the at least one blade tip, the plurality of grooves being elongated in a circumferential direction, the plurality of grooves including an endless groove and an ended groove aft of the endless groove.

2. The pump as recited in claim 1 , wherein the endless groove is one of a plurality of endless grooves and the ended groove is one of a plurality of ended grooves that are aft of the plurality of endless grooves.

3. The pump as recited in claim 2 , wherein the plurality of endless grooves are uniformly axially-spaced apart.

4. The pump as recited in claim 1 , wherein the plurality of grooves are of common aspect ratio with respect to groove depth and groove width.

5. The pump as recited in claim 1 , wherein the plurality of grooves have a constant cross-section.

6. The pump as recited in claim 1 , wherein the at least one blade begins at a first axial location, the at least one blade terminates at a second axial position, the plurality of grooves begin at a third axial location, the plurality of grooves terminate at a fourth axial position, and the fourth axial location is forward of the second axial location.

7. The pump as recited in claim 1 , wherein the internal surface of the housing includes a band aft of the plurality of grooves that excludes any of the plurality of grooves.

8. The pump as recited in claim 1 , wherein the plurality of grooves define, with respect to a reference plane perpendicular to the central axis, a forward pitch angle, and the at least one blade defines, with respect to the reference plane, an aft pitch angle.

9. A pump comprising:

an axial inducer including

a housing having an internal surface defining an axial fluid passage, and

a rotor disposed about a central axis in the fluid passage of the housing and having at least one blade defining at least one blade tip,

the internal surface of the housing defining a plurality of grooves adjacent the at least one blade tip, the plurality of grooves defining, with respect to a reference plane perpendicular to the central axis, a forward pitch angle and the at least one blade defining, with respect to the reference plane, an aft pitch angle, the plurality of grooves including an endless groove and an ended groove aft of the endless groove.

10. The pump as recited in claim 9 , wherein the forward pitch angle and the aft pitch angle are congruent angles.

11. The pump as recited in claim 10 , wherein the congruent angles are in a range from 5° to 40°.

12. A pump comprising:

an axial inducer including

a housing having an internal surface defining an axial fluid passage, and

a rotor disposed about a central axis in the fluid passage of the housing and having at least one blade defining at least one blade tip,

the internal surface of the housing defining a plurality of grooves adjacent the at least one blade tip, each of the grooves defining, with respect to a reference plane perpendicular to the central axis, a pitch angle that varies along the groove, the plurality of grooves including an endless groove and an ended groove aft of the endless groove.

13. The pump as recited in claim 12 , wherein the pitch angle is a forward pitch angle.

Assignments (3)
TERMINATION AND RELEASE OF SECURITY INTEREST IN PATENTS Recorded Jul 28, 2023
From: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 064423/0966 →
NOTICE OF GRANT OF SECURITY INTEREST IN PATENTS Recorded Sep 28, 2022
From: AEROJET ROCKETDYNE, INC.
To: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
Reel/Frame 061561/0451 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 1, 2020
From: PHUI, KHIN; MENG, SEN
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 052800/0657 →
Continuity (2)
Provisional Application 62592662 · Nov 30, 2017
Related Publication 20210003138A1 · Jan 7, 2021