Helical seal for multi-stage compressor

Patent metadata

Field	Value
Publication number	US-2025283476-A1
Application number	US-202418670028-A
Country	US
Kind code	A1
Filing date	May 21, 2024
Priority date	Mar 11, 2024
Publication date	Sep 11, 2025
Grant date	—

Abstract

A compressor comprising: an drive shaft; a first compressor wheel; a second compressor wheel connected to the first compressor wheel via the drive shaft; and two or more helical seals disposed on the drive shaft, each helical seal of the two or more helical seals extending away from an outer surface of the drive shaft and around a circumference of the drive shaft, wherein the two or more helical seals are configured to inhibit flow of fluid between the first compressor wheel and the second compressor wheel.

First claim

1 . A compressor comprising:
a first compressor wheel; a second compressor wheel; a drive shaft connecting the first compressor wheel to the second compressor wheel, the drive shaft comprising:
an outer shaft extending from the first compressor wheel to the second compressor wheel; and
an inner shaft disposed radially inwards of the outer shaft and extending through the first compressor wheel and the second compressor wheel; and
two or more helical seals disposed on the outer shaft of the drive shaft, each helical seal of the two or more helical seals extending away from an outer surface of the outer shaft and around a circumference of the outer shaft, wherein an outer diameter of each helical seal of the two or more helical seals is greater than an outer diameter of the outer shaft, and wherein the two or more helical seals are configured to inhibit flow of fluid between the first compressor wheel and the second compressor wheel.

2 . The compressor of claim 1 , wherein the two or more helical seals comprise a first helical seal adjacent to the first compressor wheel and a second helical seal adjacent to the second compressor wheel.

3 . The compressor of claim 2 , wherein the compressor is configured to direct the fluid from the first compressor wheel to the second compressor wheel, wherein the first helical seal is wound in a same direction as a direction of rotation of the drive shaft, and wherein the second helical seal is wound in an opposite direction relative to the direction of rotation of the drive shaft.

4 . The compressor of claim 3 , wherein the first helical seal is configured to direct the fluid around the drive shaft towards the first compressor wheel, and wherein the second helical seal is configured to direct the fluid around the drive shaft towards the second compressor wheel.

5 . The compressor of claim 1 , wherein the two or more helical seals are integrated into the drive shaft.

6 . The compressor of claim 1 , wherein the first compressor wheel extends along a longitudinal axis from a first end to a second end, wherein the second compressor wheel extends along the longitudinal axis from a third end to a fourth end, and wherein the two or more helical seals are longitudinally disposed between the second end of the first compressor wheel and the third end of the second compressor wheel.

7 . (canceled)

8 . The compressor of claim 1 , wherein each helical seal of the two or more helical seals defines at least two complete revolutions around the circumference of the drive shaft.

9 . The compressor of claim 1 , wherein each helical seal of the two or more helical seals extends from the outer surface of the drive shaft to an outermost edge.

10 . The compressor of claim 1 , further comprising a housing configured to retain the first compressor wheel, the second compressor wheel, and the drive shaft, wherein the housing defines a channel sized to retain the drive shaft, and wherein a distance between the outermost edge of each helical seal and an inner surface of the channel is up to 0.05 millimeters (mm).

11 . The compressor of claim 1 , wherein for each helical seal of the two or more helical seals, a first set of one or more parameters defining the helical seal are substantially similar to a second set of one or more parameters defining another helical seal of the two or more helical seals, and wherein each of the first set of one or more parameters and the second set of one or more parameters comprises one or more of:
a pitch of the helical seal; a helical angle of the helical seal; a number of revolutions around the circumference of the drive shaft; a longitudinal length of the helical seal; or an outer diameter of the helical seal.

12 . The compressor of claim 11 , wherein each helical seal of the two or more helical seals defines a same number of revolutions around the circumference of the drive shaft.

13 . A compressor system comprising:
a compressor comprising:
a first compressor wheel;
a second compressor wheel;
a drive shaft extending along a longitudinal axis from a proximal end to a distal end, the drive shaft comprising:
an outer shaft extending from the first compressor wheel to the second compressor wheel; and
an inner shaft disposed radially inwards of the outer shaft and extending through the first compressor wheel and the second compressor wheel,
wherein the drive shaft connects the first compressor wheel to the second compressor wheel, and wherein the distal end of the drive shaft is distal to the first compressor wheel; and

two or more helical seals disposed on the outer shaft of the drive shaft, each helical seal of the two or more helical seals extending away from an outer surface of the outer shaft and around a circumference of the outer shaft, wherein an outer diameter of each helical seal of the two or more helical seals is greater than an outer diameter of the outer shaft;
a housing configured to retain the compressor, the housing comprising:
a channel extending along the longitudinal axis and configured to retain the drive shaft, wherein the two or more helical seals are configured to inhibit flow of fluid between the first compressor wheel and the second compressor wheel through the channel; and
a motor coupled to the proximal end of the drive shaft and configured to apply a rotary force on the drive shaft.

14 . The compressor system of claim 13 , wherein the two or more seals comprise a first helical seal adjacent to the first compressor wheel and a second helical seal adjacent to the second compressor wheel.

15 . The compressor system of claim 14 , wherein the housing comprises one or more channels fluidically connecting the first compressor wheel to the second compressor wheel, wherein rotation of the drive shaft in a first direction causes the first compressor wheel to direct the fluid along the one or more channels and into the second compressor wheel.

16 . The compressor system of claim 15 , wherein the first helical seal is wound in the first direction, and wherein the second helical seal is wound in a second direction opposite the first direction.

17 . The compressor system of claim 14 , wherein the first helical seal is configured to direct fluid entering a distal end of the channel towards the first compressor wheel, and wherein the second helical seal is configured to direct fluid entering a proximal end of the channel towards the second compressor wheel.

18 . The compressor system of claim 13 , wherein the two or more helical seals are integrated into the drive shaft.

19 . A method comprising:
position a first compressor wheel of a compressor within a housing; connecting a second compressor wheel of the compressor to the first compressor wheel by at least partially inserting an outer shaft of a drive shaft of the compressor into the first compressor wheel, wherein the outer shaft is connected to the second compressor wheel, and wherein the outer shaft of the drive shaft comprises:
two or more helical seals disposed on the outer shaft, each helical seal of the two or more helical seals extending away from an outer surface of the outer shaft and around a circumference of the outer shaft;
inserting an inner shaft of the drive shaft through an inner lumen of the outer shaft along a longitudinal axis of the compressor; and affixing the inner shaft to the first compressor wheel and the second compressor wheel.

20 . The method of claim 19 , wherein the housing defines an inner channel extending along the longitudinal

Assignees

• Honeywell Int Inc

Inventors

• Gattu Raghavendra
• G Bharath Chandra
• Jayamurugan Chandiran
• Mccabe Niall

Classifications

• F04D25/028

  the driving means being a planetary gear · CPC title

• F04D29/102

  especially adapted for elastic fluid pumps · CPC title

• F04D17/122

  the individual rotor discs being, one for each stage, on a common shaft and axially spaced, e.g. conventional centrifugal multi- stage compressors · CPC title

• F04D29/124 Primary

  with special means for adducting cooling or sealing fluid · CPC title