Sealing system for a turboexpander compressor

• US 4,477,223 A
• Filed: 06/11/1982
• Issued: 10/16/1984
• Est. Priority Date: 06/11/1982
• Status: Expired due to Term

• Current Assignee: Turbine Incorporated (Warner Bros. Discovery, Inc.)
• Original Assignee: Turbine Incorporated (Warner Bros. Discovery, Inc.)
• Inventors: Giroux, Claude
• Primary Examiner(s): Yuen, Henry C.
• Assistant Examiner(s): Kwon, John
• Application Number:
  US06/387,504
• Time in Patent Office: 858 Days
• Field of Search: 415/110, 415/111, 415/112, 415/113, 415/180, 415/170 R, 415/168, 415/169 R, 277/92, 277/93 SD, 277/94, 277/95, 277/84, 277/83, 277/177, 384/152
• US Class Current: 415/168.2
• CPC Class Codes: F01D 11/02 by non-contact sealings, e.g. of labyrinth type for sealing space between rotor blade tips and stator F01D11/08
• CPC Class Codes: F01D 25/12 Cooling
• CPC Class Codes: F01D 25/183 Sealing means
• CPC Class Codes: F05D 2210/42 Axial inlet and radial outlet
• CPC Class Codes: F05D 2210/43 Radial inlet and axial outlet
• CPC Class Codes: F05D 2220/40 in turbochargers
• CPC Class Codes: F16J 15/004 forming of recuperation chamber for the leaking fluid
• CPC Class Codes: F16J 15/344 the pressing force being applied by means of an elastic ring supporting the slip-ring
• CPC Class Codes: F16J 15/443 provided with discharge channels
• CPC Class Codes: Y10S 277/91 O-ring seal
• CPC Class Codes: Y10S 277/93 Seal including heating or cooling feature

Abstract

A turboexpander compressor for use in a gas processing system has a seal system that avoids communication of gas with the oil being pumped through the bearings. The device has a shaft carried in a housing on bearings with a compressor wheel on one side and an expander wheel on the other side. Labyrinth seals seal the wheels from the interior of the housing and the bearings. Mechanical seals are located between the bearings and the labyrinth seals for preventing leakage of oil. The mechanical seals are located in a drainage chamber that allows any oil or gas leaked past the seals to be drained from the system, rather than dilute the oil. Gas is injected from the compressor discharge into a groove on the expander side of the shaft to provide a thermal barrier. The mechanical seals each have a rotating ring carried by the shaft and a nonrotating ring carried by the housing. The nonrotating ring is biased into the rotating ring by means of an O-ring. The O-ring is located in a groove in the bore and a recess formed in the nonrotating ring. The recess is offset to deform the ring and cause it to exert a force on the nonrotating ring against the rotating ring.

Claims

1. In a gas processing apparatus having a housing containing a shaft with a compressor turbine in a compressor chamber on one end and an expander turbine in an expander chamber on the other end, bearing means for rotatably supporting the shaft, and pump means for circulating lubricant through the bearing means, an improved seal system comprising in combination:

chamber seal means at each end of the housing for reducing leakage of fluid between the housing and each chamber; and

a mechanical seal located between the bearing means and each chamber seal means, having a nonrotating ring carried by the housing and a rotating ring carried by the shaft, the rings having opposed faces that are biased toward and engage each other;

the opposed faces of the mechanical seals being in communication with a drainage chamber in the housing, the drainage chamber having drainage means for removing any lubricant leaked past the mechanical seals and any gas leaked past the seal means.

2. In a gas processing apparatus having a housing containing a shaft with a compressor turbine in a compressor chamber on one end and an expander turbine in an expander chamber on the other end, bearing means for rotatably supporting the shaft, and pump means for circulating lubricant through the bearing means, an improved seal system comprising in combination:

labyrinth seals located at each end of the housing for reducing leakage of fluid between the housing and each chamber;

a mechanical seal located between the bearing means and each labyrinth seal, having a nonrotating ring carried by the housing and a rotating ring carried by the shaft, the rings having opposed faces that are biased toward each other and separated when rotating by a fluid film, the opposed faces of the mechanical seal being located within a drainage chamber of the housing;

injection means for injecting gas around the shaft between one of the mechanical seals and the expander chamber for creating a thermal barrier; and

drainage means leading from the drainage chamber for removing any lubricant leaked past the mechanical seals and any gas leaked past the labyrinth seals.

3. The apparatus according to claim 2 wherein the drainage means comprises:

a passage leading from the drainage chamber to a collection chamber means for receiving gas and lubricant from the drainage chamber, the collection chamber being at a pressure greater than ambient, the collection chamber having an outlet for discharging gas and valve means for discharging lubricant when the level reaches a selected maximum.

4. The apparatus according to claim 2 wherein the injection means comprises:

a pair of annular, spaced-apart grooves located in the housing and at the labyrinth seal that is next to the expander chamber, the groove closest to the mechanical seal being connected to a discharge of the compressor, the groove closest to the expander chamber being vented to a low pressure gas line.