US3180135A - Seal evaluation machine - Google Patents

Seal evaluation machine Download PDF

Info

Publication number
US3180135A
US3180135A US123811A US12381161A US3180135A US 3180135 A US3180135 A US 3180135A US 123811 A US123811 A US 123811A US 12381161 A US12381161 A US 12381161A US 3180135 A US3180135 A US 3180135A
Authority
US
United States
Prior art keywords
seal
chambers
tested
pressure
chamber
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US123811A
Inventor
Jr Earl S Cain
Gene L Green
Jr Paul D Smith
Amos S Baccus
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Garrett Corp
Original Assignee
Garrett Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Garrett Corp filed Critical Garrett Corp
Priority to US123811A priority Critical patent/US3180135A/en
Application granted granted Critical
Publication of US3180135A publication Critical patent/US3180135A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M3/00Investigating fluid-tightness of structures
    • G01M3/02Investigating fluid-tightness of structures by using fluid or vacuum
    • G01M3/26Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors
    • G01M3/32Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors for containers, e.g. radiators
    • G01M3/3218Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors for containers, e.g. radiators for flexible or elastic containers

Definitions

  • This invention relates to an apparatus for testing seals for rotatable shafts and aims to provide a novel machine for making various qualitative and quantitative determinations of the operating characteristics of seals which are designed for use with high-speed rotatable shafts.
  • Another object of the invention is to provide a sealtesting apparatus including a plurality of pressure chambers so that various portions of a seal may be subjected to dirferent simulated operating pressures.
  • Another object is to provide a seal-testing apparatus as specified in the last paragraph and including means for indicating and measuring any fluid leakage between chambers.
  • Still another object of the invention is to provide a eal-testing apparatus which permits shaft speeds up to 120,000 r.p.m., and operating pressures on all exposed areas of the seal up to 200 p.s.i.
  • a further object of the invention is to provide a sealtesting machine which includes instruments for controlling and monitoring gas pressures in a plurality of pressure chambers, test spindle speeds, test seal temperatures, gas flow rates between pressure chambers, and oil pressure.
  • Still another object of the invention is to provide a seal evaluation apparatus which includes a spindle adapted to operate over a wide range of speeds and a removable adapter in which the seal to be tested may be mounted.
  • Another object of the invention is to provide a seal evaluation apparatus as specified in the last preceding paragraph and in which the adapter includes a first passage for supplying oil to oil-test the seal and a second passage and an associated chamber for applying pressure to the peripheral edge of the seal being tested.
  • PEG. 1 is a side elevational view, partly in section and partly schematic, showing a seal evaluation apparatusembodying the principles of this invention.
  • FIG. 2 is a somewhat enlarged fragmentary elevational view with portions broken away and in section, showing the details of the removable adapter and associated parts for s .pporting the seal to be tested.
  • an improved seal-testing and evaluating machine it constructed in accordance with this invention, comprises a seal supporting device 11 having a large tank-like housing 12 on one side thereof and a smaller removable housing or enclosure means 13 on the other side thereof.
  • the tank or housing 12 is rigidly supported on a suitable base 14 and provides a first pressure chamber 15 in which a motor 16 and transmission 17 are mounted. Speeds from zero to above 120,000 r.p.m. may be transmitted to a spindle or stub shaft 13 by the motor and transmission which are mounted to keep shaft vibrations at a minimum.
  • coupling spindle 2 having an enlarged hub 21 and oil deflecting grooves 22 is mounted on the end or" stub shaft 13 and positioned and centered in a flanged supporting member 23 which is fitted into an axially aligned opening 24 in the tank 12.
  • the coupling spindle 20 is separately supported on resiliently mounted antifriction bearings (not shown) to reduce resonant vibrations of the associated parts; and the enlarged hub 21 is designed to act as a clearance-typeoil seal to prevent uncontrolled oil l akage from chamber 15.
  • Opening 24 is formed with outwardly extending supporting flanges 25, to which the housing 13 is firmly attached in any convenient manner.
  • the housing 13 has a supporting member so formed or mounted on the inner wall thereof and provided with a cylindrical opening 27 for purposes which will hereinafter'appear.
  • Coupling spindle 24 has an axial bore for the reception of the inner reduced end 28 of a test spindle 3% which is provided with an enlarged flange 31 so that it may be securely fastened to the face of the hub 21.
  • a cylindrical bushing 32 is fitted on spindle it for the reception of a cylindrical seal 33 which is suitably centered in an opening provided in a special adapter plate 34, and separated therefrom by a flanged retainer 35 forming part of the seal.
  • Seal 33 is the seal to be tested, and, along with the adapter plate 34, acts to close the cylindrical opening 27 so as to provide an oil and pressure chamber 36.
  • This chamber 36 is in fluid communication with the large housing chamber 15, both through the clearance or space around the hub 21 and through a special passage 37.
  • the spindle 39 and associated bushing 32 are held for rotation with the coupling member by a washer and lock nut 33 threaded on a reduced outer end 39 of said spindle 3d.
  • Pressure is applied to chamber 36 through a passage which is connected to a conduit having a pressure regulator and gauge All and fiowmeter 42 therein and, in turn, is connected to a suitable source of fluid pressure 43.
  • a conduit having a pressure regulator and gauge All and fiowmeter 42 therein is connected to a suitable source of fluid pressure 43.
  • fluid pressure in chamber 36 will be applied to the exposed inner face of the eal 33.
  • fluid pressure of predetermined amount may be applied to the other or outer exposed face of the seal 33 by a conduit 44 which is connected at one end to the source 43 and at the other end to a closed chamber 45 formed by the housing 13.
  • a fiowmeter 46 andpressure regulator and gauge 47 may be provided in conduit 44 if desired.
  • fluid pressure may also be applied to the peripheral edge of the seal 33 through a passage 48 which is connected at one end to an annular groove 50 surrounding'the seal and at the other end to a conduit 51.
  • This conduit runs through the wall of housing F13, has a pressure regulator and gauge 52, and flowmeter 53 therein, and is connected to the fluid pressure supply 32.
  • a gasket or O-ring 54 between the inner face of the adapter 34 and the support 26 provides a pressure seal for chamber 36; and gasket 55 on both sides of the groove or chamber 50 efiectively seal the adapter 34 against the flanged retainer 55 of the seal 33.
  • chamber 36 is connected by a passage 56 with an oil supply line 57. It will be apparent that oil entering the chamber 36 through passage 56 will flow through passage 37 into the chamber 15 and will settle in the bottom thereof. A predetermined quantity of oil is placed in the chamber 15 and circulated by a pump 58 and conduit 59 to all parts of the machine for lubrication. With this pressure supply and a control valve 6%, oil fiow'may be controlled to conduit 57, passage 56 and chamber 35. This arrangement of parts thus constitutes a means for supplying and circulating oil in the sealtesting system.
  • suitable pyrometers may be provided at strategic locations in the apparatus.
  • One such pyrometer s1 is shown mounted adjacent the outer face of the seal 33 and connected by a wire or lead 62 to a temperature gauge 63. This gauge will give a ready indication of the temperature of the seal and may also be connected to controls to de-energize motor 16 if seal or bearing temperatures get too high.
  • a heater 64 may be located in the chamber 45 inside housing 13 and/ or at other suitable places in the apparatus.
  • Such cooling means may include a cooling coil 65 connected to conduit 59 outside the housing 12, a fan 66 for forcing air over the coil 65, a second coil 67 in the chamber 15 and suitable thermostats or temperature i controls 68.
  • Special adapter plates 34 are provided for seals of widely different types and sizes; and these may be installed in the apparatus through the housing 13.
  • said housing has a removable outside cover 70 which may be attached to the housing with a suitable sealing mechanism 7t; and said cover may be provided with an observation window 72 and handle '73 if desired.
  • seals and adapter plates may be provided to allow for changing seals without removing the entire adapter plate; andin such case, it is merely necessary to remove the nut and washer 38.
  • Certain operational safety features may be incorporated in the apparatus if desired.
  • a control may be included which will prevent activation of the motor 16 until the electrical systemand bearings are properly heated, and further until there is a predetermined acceptable oil flow to eifect necessary lubrication.
  • safety valves 74 may be provided in any of the pressure lines to prevent over-pressurization of any of the three pressure chambers.
  • the meters, indicators and controls may be arranged in a single accessible control panel, and that environmental conditions, such as speed, pressure magnitude and ratio, temperature, oil flow rate, and the like, may be varied as desired during operation. Direct reading fluid leakage between chambers may then be correlated with dynamic conditions of operation.
  • the arrangement and mounting of the spindles render them substantially free of vibration, but shimming adjustments may be made to simulate environmental conditions of both misalignment and radial runout.
  • the spindle design and changeable adapter plates permit testing seals of various sizes, for example, from a -inch bore up to a 3-inch bore.
  • the design and arrangement of the apparatus permit easy changes of seals and allow the parts to be observed during operation.
  • Apparatus for testing annular seals for the shafts of rotating machinery comprising: a support; a rotatable spindle extending through said support and adapted to receive the seal to be tested; an adapter plate removably connected to said support for holding said seal; passage means in said adapter plate .in fluid communication with said outer peripheral edge; and means for independently applying fluid underpressure to both inner and outer faces of said seal and to said passage means.
  • Apparatus for testing annular seals for the shafts of rotating machinery comprising: a support; a rotatable spindle extending through said support and adapted to receive the seal to be tested; an adapter plate removably connected to said support for holding said seal; passage means in said adapter plate in fluid communication with said outer peripheral edge; means for independently applying fluid under pressure to both inner and outer faces of said seal and to said passage means; and means for measuring any fluid flow between said peripheral edge and said inner and outer faces so as to provide a measure of fluid leakage through said seal.
  • Apparatus for testing annular seals for rotating shafts comprising: means providing a pair of chambers separated by a Wall; means on said Wall for holding a seal to be tested with opposite ends of said seal exposed to the respective chambers; shaft means extending through the seal to be tested; means in one of said chambers and connected with said shaft means to impart rotary motion thereto; and means for introducing fluid under different controlled pressures to said chambers.
  • Apparatus for testing annular seals for rotating shafts comprising: means providing a pair of chambers separated by a wall; means on said Wall for holding a seal to be tested with opposite ends of said seal exposed to the respective chambers; shaft means extending through the seal to be tested, said seal forming the only potential path for communication between said chambers; means in one of said chambers and connected with said shaft means for imparting rotary motion thereto; means communicating with at least one of said chambers for creating a controlled pressure differential between said chambers; and means for detecting any changes in said pressure differential.
  • Apparatus for testing annular seals for rotating shafts comprising: means providing a pair of chambers separated by a wall; means on said wall for holding a seal to be tested with opposite ends of said seal exposed to the respective chambers; shaft means extending through the seal to be tested, said seal forming the only potential path for communication between said chambers; means in one of said chambers and connected with said shaft means for imparting rotary motion thereto; means communicating with said chambers for supplying fluid at diiferent controlling pressures thereto; and means for detecting change and rate of change in pressures in said chambers.
  • Apparatus for testing annular seals for rotating shafts comprising: means providing a pair of chambers separated by a wall; means on said Wall for holding a seal to be tested with opposite ends of said seal exposed to the respective chambers, said wall providing a third chamber around the periphery of said seal intermediate the ends thereof; gasket means between said seal and said wall at points between said third chamber and the chambers of said pair of chambers; shaft means extending through the seal to be tested, said seal forming the only potential path for communication between said chambers; means in one of said chambers and connected with said shaft means for imparting rotary motion thereto; means communicating with said chambers for selectively supply. ing controlled pressures thereto; and means for detecting pressure changes in any one of said chambers.
  • Apparatus for testing annular seals for rotating shafts comprising: means providing a pair of chambers separated by a wall; means on said wall for holding a seal to be tested with opposite ends of said seal exposed to the respective chambers; shaft means extending through the seal to be tested, said seal forming the only potential path for communication between said chambers; means in one of said chambers and connected with said shaft means for imparting rotary motion thereto; means communicating with said chambers for supplying fluid at diflerent controlled pressures thereto; means for varying the temperature of the fluid supplied to said chambers; and means for detecting changes in pressure in said chambers due to leakage through the seal being tested.
  • Apparatus for testing annular seals for rotating shafts comprising: means providing a pair of chambers separated by a wall; means on said Wall for holding a seal to be tested with opposite ends of said seal exposed to the respective chambers; shaft means extending through the seal to be tested, said seal forming the only potential path for communication between said chambers; means in one of said chambers and connected with said shaft means for imparting rotary motion thereto; means communicating with said chambers for supplying fluid at different controlled pressures thereto; means for varying the temperature of the fluid supplied to said chambers; means for indicating the temperature of the seal being tested; and means for detecting changes in pressure in said chambers due to leakage through said seal.

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Examining Or Testing Airtightness (AREA)

Description

April 27, 1965 E. s. CAIN, JR., ETAL 3,180,135
SEAL EVALUATION MACHINE Filed July 15. 1961 2 SheetS -S heet 1 PM l H l l O I Aw UZM/ A TTORNE Y April 27, 1965 E. s. CAIN, JR., ETAL 3,180, 35
SEAL EVALUATION MACHINE Filed July 13. 1961 2 Sheets-Sheet 2 INVENTORS EARL 5'. CAI/V JR. GENE L. GREEN BY PAUL 0. SMITH JR.
7 AMOS .5. B46 US PM WMQ 3,139,135 Patented Apr. 27, 1965 3,189,135 EAL EVALUATEUN MACHKNE Earl S. Cain, 5n, Phoenix, Gene L. Green, Glendale, and
Paul D. Smith, 3:2, and Amos S. Eaccus, Scottsdale, Ariz., assignors to The Garrett Corporation, 1.05 Angeles, Lalih, a corporation of (Ialifornia ilerl July 13, 1951, Ser. No. 123,811
3 Claims. (Cl. 73-46) This invention relates to an apparatus for testing seals for rotatable shafts and aims to provide a novel machine for making various qualitative and quantitative determinations of the operating characteristics of seals which are designed for use with high-speed rotatable shafts.
Many types of high-speed rotary machines, such as turbomachinery, require fluid-tight seals which will withstand the high pressures and temperatures encountered in such machines. In the past there have been no satisfactory testing machines which would make it possible to check shaft seals under conditions which might be encountered in actual use. The result of this deficiency has been that pretesting of shaft seals has been superficial, and in many cases unreliable, so that actual operating failures have been more numerous than is desirable.
it is an object of this invention to provide a sealtesting apparatus which is eficient in use and gives data showing the performance of shaft seals under simulated operating conditions.
Another obiect of the invention is to provide a sealtesting apparatus including a plurality of pressure chambers so that various portions of a seal may be subjected to dirferent simulated operating pressures.
Another object is to provide a seal-testing apparatus as specified in the last paragraph and including means for indicating and measuring any fluid leakage between chambers.
Still another object of the invention is to provide a eal-testing apparatus which permits shaft speeds up to 120,000 r.p.m., and operating pressures on all exposed areas of the seal up to 200 p.s.i.
A further object of the invention is to provide a sealtesting machine which includes instruments for controlling and monitoring gas pressures in a plurality of pressure chambers, test spindle speeds, test seal temperatures, gas flow rates between pressure chambers, and oil pressure.
Still another object of the invention is to provide a seal evaluation apparatus which includes a spindle adapted to operate over a wide range of speeds and a removable adapter in which the seal to be tested may be mounted.
Another object of the invention is to provide a seal evaluation apparatus as specified in the last preceding paragraph and in which the adapter includes a first passage for supplying oil to oil-test the seal and a second passage and an associated chamber for applying pressure to the peripheral edge of the seal being tested.
The above and other features and advantages of the invention will be apparent from the following more detailed description and the accompanying drawing, in which:
PEG. 1 is a side elevational view, partly in section and partly schematic, showing a seal evaluation apparatusembodying the principles of this invention; and
2 is a somewhat enlarged fragmentary elevational view with portions broken away and in section, showing the details of the removable adapter and associated parts for s .pporting the seal to be tested.
Referring now to FIG. 1, it will be noted that an improved seal-testing and evaluating machine it constructed in accordance with this invention, comprises a seal supporting device 11 having a large tank-like housing 12 on one side thereof and a smaller removable housing or enclosure means 13 on the other side thereof. The tank or housing 12 is rigidly supported on a suitable base 14 and provides a first pressure chamber 15 in which a motor 16 and transmission 17 are mounted. Speeds from zero to above 120,000 r.p.m. may be transmitted to a spindle or stub shaft 13 by the motor and transmission which are mounted to keep shaft vibrations at a minimum. A.
coupling spindle 2:? having an enlarged hub 21 and oil deflecting grooves 22 is mounted on the end or" stub shaft 13 and positioned and centered in a flanged supporting member 23 which is fitted into an axially aligned opening 24 in the tank 12. The coupling spindle 20 is separately supported on resiliently mounted antifriction bearings (not shown) to reduce resonant vibrations of the associated parts; and the enlarged hub 21 is designed to act as a clearance-typeoil seal to prevent uncontrolled oil l akage from chamber 15. Opening 24 is formed with outwardly extending supporting flanges 25, to which the housing 13 is firmly attached in any convenient manner.
As best shown in FIG. 2, the housing 13; has a supporting member so formed or mounted on the inner wall thereof and provided with a cylindrical opening 27 for purposes which will hereinafter'appear. Coupling spindle 24 has an axial bore for the reception of the inner reduced end 28 of a test spindle 3% which is provided with an enlarged flange 31 so that it may be securely fastened to the face of the hub 21. A cylindrical bushing 32 is fitted on spindle it for the reception of a cylindrical seal 33 which is suitably centered in an opening provided in a special adapter plate 34, and separated therefrom by a flanged retainer 35 forming part of the seal. Seal 33 is the seal to be tested, and, along with the adapter plate 34, acts to close the cylindrical opening 27 so as to provide an oil and pressure chamber 36. This chamber 36 is in fluid communication with the large housing chamber 15, both through the clearance or space around the hub 21 and through a special passage 37. The spindle 39 and associated bushing 32 are held for rotation with the coupling member by a washer and lock nut 33 threaded on a reduced outer end 39 of said spindle 3d. By having the motor and transmission enclosed in the chamber 15, which is in fluid communication with the chamber 36 and one side of the seal 33, it is unnecessary to have another seal for the transmission shaft.
Pressure is applied to chamber 36 through a passage which is connected to a conduit having a pressure regulator and gauge All and fiowmeter 42 therein and, in turn, is connected to a suitable source of fluid pressure 43. It will be understood that the fluid pressure in chamber 36 will be applied to the exposed inner face of the eal 33. Similarly, fluid pressure of predetermined amount may be applied to the other or outer exposed face of the seal 33 by a conduit 44 which is connected at one end to the source 43 and at the other end to a closed chamber 45 formed by the housing 13. A fiowmeter 46 andpressure regulator and gauge 47 may be provided in conduit 44 if desired. Finally, fluid pressure may also be applied to the peripheral edge of the seal 33 through a passage 48 which is connected at one end to an annular groove 50 surrounding'the seal and at the other end to a conduit 51. This conduit runs through the wall of housing F13, has a pressure regulator and gauge 52, and flowmeter 53 therein, and is connected to the fluid pressure supply 32. A gasket or O-ring 54 between the inner face of the adapter 34 and the support 26 provides a pressure seal for chamber 36; and gasket 55 on both sides of the groove or chamber 50 efiectively seal the adapter 34 against the flanged retainer 55 of the seal 33.
It will be understood that by subjecting the three pressure chambers 15, 45 and 59 to different pressure conditions, so that there may be a predetermined pressure differential between chambers, and then by observing the various flowmeters and gauges described above, it is possible to indicate and measure fluid leakage between chambers; and said gauges and flowmeters constitute means for indicating and/ or measuring such fluid leakage.
To make it possible to test the seal 33 under different oil conditions, chamber 36 is connected by a passage 56 with an oil supply line 57. It will be apparent that oil entering the chamber 36 through passage 56 will flow through passage 37 into the chamber 15 and will settle in the bottom thereof. A predetermined quantity of oil is placed in the chamber 15 and circulated by a pump 58 and conduit 59 to all parts of the machine for lubrication. With this pressure supply and a control valve 6%, oil fiow'may be controlled to conduit 57, passage 56 and chamber 35. This arrangement of parts thus constitutes a means for supplying and circulating oil in the sealtesting system.
Temperature conditions of the seal 33 under test and other parts of the apparatus, such as the main bearings (not shown) for the coupling spindle 2d, are also important. To observe and measure temperatures, suitable pyrometers may be provided at strategic locations in the apparatus. One such pyrometer s1 is shown mounted adjacent the outer face of the seal 33 and connected by a wire or lead 62 to a temperature gauge 63. This gauge will give a ready indication of the temperature of the seal and may also be connected to controls to de-energize motor 16 if seal or bearing temperatures get too high. Should it be desired to increase the seal temperature or change the temperature of the pressurized fluid, a heater 64 may be located in the chamber 45 inside housing 13 and/ or at other suitable places in the apparatus.
Provision may also be made for cooling the oil to a predetermined temperature level so as to cool the chamber 15 and other parts over which the oil circulates. Such cooling means may include a cooling coil 65 connected to conduit 59 outside the housing 12, a fan 66 for forcing air over the coil 65, a second coil 67 in the chamber 15 and suitable thermostats or temperature i controls 68.
Operation of the entire seal-testing apparatus will be apparent from the foregoing description. Special adapter plates 34 are provided for seals of widely different types and sizes; and these may be installed in the apparatus through the housing 13. For this purpose, said housing has a removable outside cover 70 which may be attached to the housing with a suitable sealing mechanism 7t; and said cover may be provided with an observation window 72 and handle '73 if desired. With the adapter plate 34 and seal shown in FIG. 2, it is necessary to remove the plate in order to install a dilferent seal, since the flange of the retainer 35 is on the inside of said plate. Obviously, seals and adapter plates may be provided to allow for changing seals without removing the entire adapter plate; andin such case, it is merely necessary to remove the nut and washer 38.
Certain operational safety features may be incorporated in the apparatus if desired. For example, a control may be included which will prevent activation of the motor 16 until the electrical systemand bearings are properly heated, and further until there is a predetermined acceptable oil flow to eifect necessary lubrication. Also, safety valves 74 may be provided in any of the pressure lines to prevent over-pressurization of any of the three pressure chambers.
It will be understood that all of, the meters, indicators and controls may be arranged in a single accessible control panel, and that environmental conditions, such as speed, pressure magnitude and ratio, temperature, oil flow rate, and the like, may be varied as desired during operation. Direct reading fluid leakage between chambers may then be correlated with dynamic conditions of operation. The arrangement and mounting of the spindles render them substantially free of vibration, but shimming adjustments may be made to simulate environmental conditions of both misalignment and radial runout. Furthermore, the spindle design and changeable adapter plates permit testing seals of various sizes, for example, from a -inch bore up to a 3-inch bore. Also, the design and arrangement of the apparatus permit easy changes of seals and allow the parts to be observed during operation.
Various changes may be made in the apparatus herein described and certain features may be employed without others without departing from the invention or sacrificing any of its advantages.
We claim:
1. Apparatus for testing annular seals for the shafts of rotating machinery, such annular seals having inner and outer faces and an outer peripheral edge, said apparatus comprising: a support; a rotatable spindle extending through said support and adapted to receive the seal to be tested; an adapter plate removably connected to said support for holding said seal; passage means in said adapter plate .in fluid communication with said outer peripheral edge; and means for independently applying fluid underpressure to both inner and outer faces of said seal and to said passage means.
2. Apparatus for testing annular seals for the shafts of rotating machinery, such annular seals having inner and outer faces and an outer peripheral edge, said apparatus comprising: a support; a rotatable spindle extending through said support and adapted to receive the seal to be tested; an adapter plate removably connected to said support for holding said seal; passage means in said adapter plate in fluid communication with said outer peripheral edge; means for independently applying fluid under pressure to both inner and outer faces of said seal and to said passage means; and means for measuring any fluid flow between said peripheral edge and said inner and outer faces so as to provide a measure of fluid leakage through said seal.
3. Apparatus for testing annular seals for rotating shafts comprising: means providing a pair of chambers separated by a Wall; means on said Wall for holding a seal to be tested with opposite ends of said seal exposed to the respective chambers; shaft means extending through the seal to be tested; means in one of said chambers and connected with said shaft means to impart rotary motion thereto; and means for introducing fluid under different controlled pressures to said chambers.
4. Apparatus for testing annular seals for rotating shafts comprising: means providing a pair of chambers separated by a wall; means on said Wall for holding a seal to be tested with opposite ends of said seal exposed to the respective chambers; shaft means extending through the seal to be tested, said seal forming the only potential path for communication between said chambers; means in one of said chambers and connected with said shaft means for imparting rotary motion thereto; means communicating with at least one of said chambers for creating a controlled pressure differential between said chambers; and means for detecting any changes in said pressure differential.
5. Apparatus for testing annular seals for rotating shafts comprising: means providing a pair of chambers separated by a wall; means on said wall for holding a seal to be tested with opposite ends of said seal exposed to the respective chambers; shaft means extending through the seal to be tested, said seal forming the only potential path for communication between said chambers; means in one of said chambers and connected with said shaft means for imparting rotary motion thereto; means communicating with said chambers for supplying fluid at diiferent controlling pressures thereto; and means for detecting change and rate of change in pressures in said chambers.
6. Apparatus for testing annular seals for rotating shafts comprising: means providing a pair of chambers separated by a wall; means on said Wall for holding a seal to be tested with opposite ends of said seal exposed to the respective chambers, said wall providing a third chamber around the periphery of said seal intermediate the ends thereof; gasket means between said seal and said wall at points between said third chamber and the chambers of said pair of chambers; shaft means extending through the seal to be tested, said seal forming the only potential path for communication between said chambers; means in one of said chambers and connected with said shaft means for imparting rotary motion thereto; means communicating with said chambers for selectively supply. ing controlled pressures thereto; and means for detecting pressure changes in any one of said chambers.
7. Apparatus for testing annular seals for rotating shafts comprising: means providing a pair of chambers separated by a wall; means on said wall for holding a seal to be tested with opposite ends of said seal exposed to the respective chambers; shaft means extending through the seal to be tested, said seal forming the only potential path for communication between said chambers; means in one of said chambers and connected with said shaft means for imparting rotary motion thereto; means communicating with said chambers for supplying fluid at diflerent controlled pressures thereto; means for varying the temperature of the fluid supplied to said chambers; and means for detecting changes in pressure in said chambers due to leakage through the seal being tested.
8. Apparatus for testing annular seals for rotating shafts comprising: means providing a pair of chambers separated by a wall; means on said Wall for holding a seal to be tested with opposite ends of said seal exposed to the respective chambers; shaft means extending through the seal to be tested, said seal forming the only potential path for communication between said chambers; means in one of said chambers and connected with said shaft means for imparting rotary motion thereto; means communicating with said chambers for supplying fluid at different controlled pressures thereto; means for varying the temperature of the fluid supplied to said chambers; means for indicating the temperature of the seal being tested; and means for detecting changes in pressure in said chambers due to leakage through said seal.
References Cited by the Examiner UNITED STATES PATENTS 2,467,960 4/49 Brady 73-40 X FOREIGN PATENTS 500,128 6/30 Germany.
OTHER REFERENCES Kahn & Co., Inc., Bulletin on KC-300, Series, Hydraulic Test Stands, received in US. Patent Ofiice July 21, 1958 (single sheet, 2 sides).
ISAAC LISANN, Primary Examiner.

Claims (1)

  1. 4. APPARATUS FOR TESTING ANNULAR SEALS FOR ROTATING SHAFTS COMPRISING: MEANS PROVIDING A PAIR OF CHAMBERS SEPARATED BY A WALL; MEANS ON SAID WALL FOR HOLDING A SEAL TO BE TESTED WITH OPPOSITE ENDS OF SAID SEAL EXPOSED TO THE RESPECTIVE CHAMBERS; SHAFT MEANS EXTENDING THROUGH THE SEAL TO BE TESTED, SAID SEAL FORMING THE ONLY POTENTIAL PATH FOR COMMUNICATION BETWEEN SAID CHAMBERS; MEANS IN ONE OF SAID CHAMBERS AND CONNECTED WITH SAID SHAFT MEANS FOR IMPARTING ROTARY MOTION THERETO; MEANS
US123811A 1961-07-13 1961-07-13 Seal evaluation machine Expired - Lifetime US3180135A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US123811A US3180135A (en) 1961-07-13 1961-07-13 Seal evaluation machine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US123811A US3180135A (en) 1961-07-13 1961-07-13 Seal evaluation machine

Publications (1)

Publication Number Publication Date
US3180135A true US3180135A (en) 1965-04-27

Family

ID=22411036

Family Applications (1)

Application Number Title Priority Date Filing Date
US123811A Expired - Lifetime US3180135A (en) 1961-07-13 1961-07-13 Seal evaluation machine

Country Status (1)

Country Link
US (1) US3180135A (en)

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3228242A (en) * 1963-06-19 1966-01-11 Worthington Corp Apparatus for testing pumps
US3313141A (en) * 1963-05-15 1967-04-11 Angus George Co Ltd Shaft seal testing apparatus
US3375015A (en) * 1966-09-30 1968-03-26 Judson S. Swearingen Shaft seal employing seal gas with means for indicating proper flow thereof
US3987663A (en) * 1974-10-29 1976-10-26 Federal-Mogul Corporation Method and apparatus for quickly testing the sealing effectiveness of a radial-lip shaft seal
US4051717A (en) * 1976-04-21 1977-10-04 Phillips Petroleum Company Testing shaft seals without pressuring system to operating pressure
US4765631A (en) * 1985-03-22 1988-08-23 Krupp-Koppers Gmbh Stuffing box sealing arrangement
US5383351A (en) * 1993-11-12 1995-01-24 Atlantic Richfield Company Pump seal test apparatus and method
US6269705B1 (en) * 1999-09-09 2001-08-07 Saargummi Americas, Inc. Glass run seal testing machine
US6276194B1 (en) * 1999-06-01 2001-08-21 Federal-Mogul World Wide, Inc. Apparatus and method for testing the effectiveness of dynamic seals in a dust-laden operating environment
US6802203B1 (en) 2002-07-18 2004-10-12 Warn Industries Rotary seal testing machine
US20090272177A1 (en) * 2008-05-05 2009-11-05 Baker Hughes Incorporated Seal Section Assembly Mechanical Face Seal Integrity Verification Tool
US20120143519A1 (en) * 2010-12-02 2012-06-07 Parker-Hannifin Corporation System and method for monitoring health of a fluid seal member
DE102019002235A1 (en) 2018-04-23 2019-10-24 Sew-Eurodrive Gmbh & Co. Kg Device, in particular test device, and test stand
US20230366807A1 (en) * 2022-05-12 2023-11-16 Gm Cruise Holdings Llc Rotary seal testing apparatus

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE500128C (en) * 1929-02-03 1930-06-18 Fried Krupp Grusonwerk Akt Ges Device for detecting leaks in the piston seals of hydraulic presses
US2467960A (en) * 1944-07-13 1949-04-19 Jr Francis E Brady Sealing unit

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE500128C (en) * 1929-02-03 1930-06-18 Fried Krupp Grusonwerk Akt Ges Device for detecting leaks in the piston seals of hydraulic presses
US2467960A (en) * 1944-07-13 1949-04-19 Jr Francis E Brady Sealing unit

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3313141A (en) * 1963-05-15 1967-04-11 Angus George Co Ltd Shaft seal testing apparatus
US3228242A (en) * 1963-06-19 1966-01-11 Worthington Corp Apparatus for testing pumps
US3375015A (en) * 1966-09-30 1968-03-26 Judson S. Swearingen Shaft seal employing seal gas with means for indicating proper flow thereof
US3987663A (en) * 1974-10-29 1976-10-26 Federal-Mogul Corporation Method and apparatus for quickly testing the sealing effectiveness of a radial-lip shaft seal
US4051717A (en) * 1976-04-21 1977-10-04 Phillips Petroleum Company Testing shaft seals without pressuring system to operating pressure
US4765631A (en) * 1985-03-22 1988-08-23 Krupp-Koppers Gmbh Stuffing box sealing arrangement
US5383351A (en) * 1993-11-12 1995-01-24 Atlantic Richfield Company Pump seal test apparatus and method
US6276194B1 (en) * 1999-06-01 2001-08-21 Federal-Mogul World Wide, Inc. Apparatus and method for testing the effectiveness of dynamic seals in a dust-laden operating environment
US6269705B1 (en) * 1999-09-09 2001-08-07 Saargummi Americas, Inc. Glass run seal testing machine
US6802203B1 (en) 2002-07-18 2004-10-12 Warn Industries Rotary seal testing machine
US20090272177A1 (en) * 2008-05-05 2009-11-05 Baker Hughes Incorporated Seal Section Assembly Mechanical Face Seal Integrity Verification Tool
US8096169B2 (en) * 2008-05-05 2012-01-17 Baker Hughes Incorporated Seal section assembly mechanical face seal integrity verification tool
US20120143519A1 (en) * 2010-12-02 2012-06-07 Parker-Hannifin Corporation System and method for monitoring health of a fluid seal member
US8949041B2 (en) * 2010-12-02 2015-02-03 Parker-Hannifin Corporation System and method for monitoring health of a fluid seal member
DE102019002235A1 (en) 2018-04-23 2019-10-24 Sew-Eurodrive Gmbh & Co. Kg Device, in particular test device, and test stand
US20230366807A1 (en) * 2022-05-12 2023-11-16 Gm Cruise Holdings Llc Rotary seal testing apparatus
US12130225B2 (en) * 2022-05-12 2024-10-29 Gm Cruise Holdings Llc Rotary seal testing apparatus

Similar Documents

Publication Publication Date Title
US3180135A (en) Seal evaluation machine
Iversen et al. Volute pressure distribution, radial force on the impeller, and volute mixing losses of a radial flow centrifugal pump
CN103630301B (en) The method of testing of a kind of hydrodynamic lubrication mechanical seal sealing property and device thereof
CN105699074B (en) A kind of blade rotor system fluid structurecoupling dynamic property tester
US5383351A (en) Pump seal test apparatus and method
CN109540519A (en) Bearing test device
CN111323223B (en) Oil seal acceleration life testing device and method for new energy automobile
US2449556A (en) Differential leakage indicator
CN107063668A (en) A kind of dry gas seals experimental system suitable for multi-state
CN114878163A (en) High-precision dynamic pressure thrust foil bearing dynamic and static synchronous loading testing device
US3176497A (en) Method and apparatus for determining seal temperatures and shaft torque
US3302447A (en) Pressurized 4-ball wear tester
US2603968A (en) Performance indicating means for use with dynamometers
US2344331A (en) Frictional resistance test apparatus
STAN ON THE DURABILITY OF CENTRIFUGAL PUMPS.
US6260426B1 (en) Test stand for fuel components using low viscosity/high flashpoint fuel look-alike
CN213274739U (en) Static pressure dry gas seal test device for kettle
US2847850A (en) Fluid density measurement device
US6260413B1 (en) Rotating device for measuring aerodynamic characteristics of a wall and its method
CN108120739A (en) A kind of thermal deformation measurement device for high-precision machine tool hydrostatic bearing
CN115077810A (en) Multi-parameter controllable oil-gas seal leakage test system
CN104792446B (en) A kind of magnetic flow liquid power measurement arrangement
CN218066921U (en) Double-end-face mechanical seal static pressure operation test bed
CN115342956A (en) A ball-disc type aerospace bearing lubricant friction tester
US2706405A (en) Air absorption dynamometer