US3438351A - Means for simultaneously indicating the spacing between two opposed attritioning elements and their condition of wear - Google Patents

Means for simultaneously indicating the spacing between two opposed attritioning elements and their condition of wear Download PDF

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US3438351A
US3438351A US576967A US3438351DA US3438351A US 3438351 A US3438351 A US 3438351A US 576967 A US576967 A US 576967A US 3438351D A US3438351D A US 3438351DA US 3438351 A US3438351 A US 3438351A
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attritioning
rod
elements
opposed
bracket
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US576967A
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Robert B Kirkwood
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Voith Morden Inc
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Morden Machine Co
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01BMEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B5/00Measuring arrangements characterised by the use of mechanical techniques
    • G01B5/14Measuring arrangements characterised by the use of mechanical techniques for measuring distance or clearance between spaced objects or spaced apertures
    • DTEXTILES; PAPER
    • D21PAPER-MAKING; PRODUCTION OF CELLULOSE
    • D21DTREATMENT OF THE MATERIALS BEFORE PASSING TO THE PAPER-MAKING MACHINE
    • D21D1/00Methods of beating or refining; Beaters of the Hollander type
    • D21D1/20Methods of refining
    • D21D1/30Disc mills

Definitions

  • This invention relates to grinding or attritioning devices in which the attritioning action is performed by a pair of elements presenting opposed attritioning surfaces, and in which one of the elements is rotated at a different speed with respect to the other, particularly where one element alone is rotated while the other remains stationary, and also in which the spacing or gap between the two attri;ioning elements is adjustable.
  • the invention relates especially to such attritioning devices as pulp treating machines having a pair of opposed axially aligned attritioning elements, one of which, commonly referred to as a rotor, is rotated, and the other of which, commonly referred to as the stator, is not rotated, and with one of these two elements being adjustable in an axial direction for adjusting the spacing between them while the other remains in fixed axial position.
  • the object of the present invention is to provide an improved indicating assembly for such attritioning devices which will show not only the spacing between the opposed attritioning elements or surfaces, but also the extent of wear which has taken place on them.
  • a related object of the invention is to provide improved means for indicating the gap or spacing between opposed attritioning surfaces in which compensation for wear on the attritioning surfaces will automatically be made each time the means indicating the gap between them is reset, with the result that the gap or spacing indicated will be the actual and true spacing.
  • a further object is to provide practical and eflicient means for indicating both the correct or actual spacing between two such elements and the amount of wear on their opposed surfaces, which means will be simple and relatively inexpensive and will present no maintenance problem.
  • FIG. 1 is a front elevation of the indicating assembl by itself;
  • FIG. 2 is a section on line 22 of FIG. 1;
  • FIG. 3 is a fragmentary sectional elevation drawn to 2 smaller scale, of a well-known type of pulp-refining ma chine on which the indicating assembly may be used.
  • the reference character 10 indicates a stationar member or bracket which is firmly secured, for example by bolts 11 or any. other suitable means, to the casing for the attritioning device or pulp refining machine, 2 portion of which is indicated at 20 in broken line.
  • the stationary member or bracket 10 has an extending por tion 10 on which a horizontal scale 12 is mounted.
  • An indicator rod 13 has one end (thus the right hand end as viewed in the drawing) connected with the axiallymovable element of the attritioning device.
  • the rod 13 is fastened to the axially-adjust able stator" 21 of the pulp-refining machine of FIG. 3
  • the attritioning element 22, which con stitutes the rotor, is not axially adjustable.
  • the stator 21 is not rotatable but is axially adjustable through the medium of a plurality of hydraulic cylinders indicatec at 23.
  • the rotor of the pulp refiner should be the axially adjustable element due to the fact that the rotor shaft is mounted in a bearing housing which in turn is movable so as to enable the rotor shaft and rotor to be moved in an axial direction, then the rod 13 would be attached to such bearing housing.
  • the rod 13 is slidable in an aperture provided in the stationary member or bracket 10 (FIGS. 1 and 2).
  • a separate indicator bracket 14 is mounted on the rod 13 by means of a sliding friction bushing 15 (FIG. 2).
  • This bracket 14 has a pointer 16 which moves over the scale 12 on the extending portion 10' of the stationary member 10.
  • the pointer 16 is so arranged that when the indicator bracket 14 is in engagement with the stationary member 10, as shown in the drawing, the pointer 16 will indicate the zero mark on the scale 12, and the bracket 14 is so set on the rod 13 at the time of installation that when the two opposed attritioning elements are in actual contact (for example, when the axially-movable stator" 21 (FIG.
  • the rod 13 With the development of wear on the opposed surfaces of the two attritioning elements, the rod 13 will be moved slightly further (to the right as viewed in FIG. 1) each time the device is reset by the bringing of the axiallyadjustable element into contact with the opposing element.
  • the fact that the indicator bracket 14 is mounted on the rod 13 by the frictionally slidable bushing 15, enables the rod to be pulled further (to the right) while the bracket 14 is held against the stationary member 10 when the wear on the attritioning surfaces makes this possible.
  • the pointer 16 will always indicate on the scale 12 the exact (I spacing between the attritioning elements regardless of the wear which may have taken place on the opposed surfaces.
  • the slidable cooperating indicator bracket 14 has an extending portion 14 on which is mounted a wear-indicating scale 17.
  • a second pointer 18 is rigidly mounted on the rod 13 to move over the scale 17 whenever the rod 13 is moved relatively with respect to the indicator bracket 14.
  • an indicator rod connected with and moving in unison in the same axial direction with the axially-movable element, a stationary member, a bearing for said rod in said stationary member, said rod slidable in said bearing, an indicator bracket mounted on said rod beyond said bearing, a friction bushing slidably holding said bracket on said rod, said bracket so positioned on said rod that said bracket will be brought into engagement with said stationary member whenever said axially-movable attritioning element is moved into actual contact with the other opposed attritioning element, cooperating indicating means on said stationary member and on said rod for indicating the gap between said opposed elements, and separate cooperating indicating means on said rod and on said bracket for automatically indicating the extent to which said rod is moved relatively with respect to said bracket, and thereby the extent of wear on said opposed
  • a pulp refining machine having a pair of axiallyaligned attritioning elements comprising a stator and a rotor and means for moving the stator in an axial direction for adjusting the spacing between stator and rotor, an indicator rod attached to and in axial alignment with the stator, a stationary member, a bearing for said rod in said stationary member, said rod slidable in said bearing, an indicator bracket mounted on said rod beyond said bearing, a friction bushing slidably holding said bracket on said rod, said bracket so positioned on said rod that said bracket will be brought into engagement with said stationary member whenever said stator is moved into actual contact with the rotor, cooperating indicating means on said stationary member and on said rod for indicating the spacing between said stator and said rotor, and separate cooperating indicating means on said rod and on said bracket for automatically indicating the extent to which said rod is moved with respect to said bracket, and thereby the extent of wear on the opposed faces of said stator and rotor, when the moving of said stator into contact with

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Description

April 15, 1969 MEANS FOR SIMUILTANEOUSLY INDICA'IING THE SPAGING BETWEEN TWO OPPOSED ATTRI-TIONING ELEMENTS AND THEIR CONDITION OF WEAR Filed Sept. 2. 1966 Fla 1' INVENTOR. ROBERT 5. HI RKWOOD ATTORNEY B.KIRKWOOD 3,438,351-
April 15, 1969 R. B. KIRKWOOD 3,438,351
MEANS FOR SIMULTANEOUSLY INDICA'IING THE SPACING BETWEEN TWO OPPOSED ATTRI'IIONING ELEMENTS AND THEIR CONDITION OF WEAR Filed Sept. 2. 1966 Sheet 2 of 2 IINVENTOR.
ROBERT B. KIRKWOOD ATTORNEY United States Patent MEANS FOR SIMULTANEOUSLY INDICATING THE SPACING BETWEEN TWO OPPOSED ATTRITIONING ELEMENTS AND THEIR CONDITION OF WEAR Robert B. Kirkwood, Portland, Oreg., assignor to Morden Machines Company, Portland, Oreg., a corporation of Oregon Filed Sept. 2, 1966, Ser. No. 576,967 Int. Cl. G09f 9/00 U.S. Cl. 116-124 3 Claims ABSTRACT OF THE DISCLOSURE A rod attached to the axially-adjustable element in a pair of axially-aligned attritioning elements and sliding through a stationary member; a slidable bracket on the rod engaging the member when the axially-adjustable element is brought into actual contact with the opposing element at each-setting; a pointer on the bracket moving over a stationary scale to indicate the actual spacing between the elements when separated; a second scale carried by the slidable bracket; and a pointer fixed on the rod indicating on the second scale the amount of wear of the elements at each setting.
This invention relates to grinding or attritioning devices in which the attritioning action is performed by a pair of elements presenting opposed attritioning surfaces, and in which one of the elements is rotated at a different speed with respect to the other, particularly where one element alone is rotated while the other remains stationary, and also in which the spacing or gap between the two attri;ioning elements is adjustable.
The invention relates especially to such attritioning devices as pulp treating machines having a pair of opposed axially aligned attritioning elements, one of which, commonly referred to as a rotor, is rotated, and the other of which, commonly referred to as the stator, is not rotated, and with one of these two elements being adjustable in an axial direction for adjusting the spacing between them while the other remains in fixed axial position.
In such pulp treating machines, as is well known, very careful adjustment and control of the spacing between the opposed attritioning surfaces of the two elements is most essential for eflicient performance. However, since wear of the attritioning surfaces gradually occurs with use, such wear should also be taken into consideration with the adjustment of the spacing or gap. Furthermore, it is desirable to know at any time the amount of wear which has taken place on the attritioning surfaces.
The object of the present invention is to provide an improved indicating assembly for such attritioning devices which will show not only the spacing between the opposed attritioning elements or surfaces, but also the extent of wear which has taken place on them.
A related object of the invention is to provide improved means for indicating the gap or spacing between opposed attritioning surfaces in which compensation for wear on the attritioning surfaces will automatically be made each time the means indicating the gap between them is reset, with the result that the gap or spacing indicated will be the actual and true spacing.
A further object is to provide practical and eflicient means for indicating both the correct or actual spacing between two such elements and the amount of wear on their opposed surfaces, which means will be simple and relatively inexpensive and will present no maintenance problem.
3,433,351 Patented Apr. 15, 196
The manner in which the improved double purpose in dicator assembly of the present invention is constructer and the manner in which it functions will be readily ap parent from the following brief description with referencr to the accompanying drawing.
In the drawing:
FIG. 1 is a front elevation of the indicating assembl by itself; FIG. 2 is a section on line 22 of FIG. 1; ant FIG. 3 is a fragmentary sectional elevation drawn to 2 smaller scale, of a well-known type of pulp-refining ma chine on which the indicating assembly may be used. It FIG. 1 the reference character 10 indicates a stationar member or bracket which is firmly secured, for example by bolts 11 or any. other suitable means, to the casing for the attritioning device or pulp refining machine, 2 portion of which is indicated at 20 in broken line. The stationary member or bracket 10 has an extending por tion 10 on which a horizontal scale 12 is mounted.
An indicator rod 13 has one end (thus the right hand end as viewed in the drawing) connected with the axiallymovable element of the attritioning device. For example and for the purpose of this description, it may be assumed that the rod 13 is fastened to the axially-adjust able stator" 21 of the pulp-refining machine of FIG. 3
' In this machine the attritioning element 22, which con stitutes the rotor, is not axially adjustable. The stator 21 is not rotatable but is axially adjustable through the medium of a plurality of hydraulic cylinders indicatec at 23. However, in the event the rotor of the pulp refiner should be the axially adjustable element due to the fact that the rotor shaft is mounted in a bearing housing which in turn is movable so as to enable the rotor shaft and rotor to be moved in an axial direction, then the rod 13 would be attached to such bearing housing. The rod 13 is slidable in an aperture provided in the stationary member or bracket 10 (FIGS. 1 and 2).
A separate indicator bracket 14 is mounted on the rod 13 by means of a sliding friction bushing 15 (FIG. 2). This bracket 14 has a pointer 16 which moves over the scale 12 on the extending portion 10' of the stationary member 10. The pointer 16 is so arranged that when the indicator bracket 14 is in engagement with the stationary member 10, as shown in the drawing, the pointer 16 will indicate the zero mark on the scale 12, and the bracket 14 is so set on the rod 13 at the time of installation that when the two opposed attritioning elements are in actual contact (for example, when the axially-movable stator" 21 (FIG. 3) has been moved into contact with the rotor" 22) the bracket 14 will be moved by the rod 13 into contact with the stationary member 10 and the pointer 16 will be positioned at the zero mark on the scale 12 as shown in the drawing, thus indicating that there is no spacing between the opposed attritioning elements. Then subsequently, as the axially-movable element 21 is moved away from contact with the opposing element 22, the pointer 16 will indicate on the scale 12 the gap or spacing between the two elements.
With the development of wear on the opposed surfaces of the two attritioning elements, the rod 13 will be moved slightly further (to the right as viewed in FIG. 1) each time the device is reset by the bringing of the axiallyadjustable element into contact with the opposing element. However, the fact that the indicator bracket 14 is mounted on the rod 13 by the frictionally slidable bushing 15, enables the rod to be pulled further (to the right) while the bracket 14 is held against the stationary member 10 when the wear on the attritioning surfaces makes this possible. Consequently, when the axially-movable element is subsequently moved away from the opposed attritioning element after each re-setting of the device, the pointer 16 will always indicate on the scale 12 the exact (I spacing between the attritioning elements regardless of the wear which may have taken place on the opposed surfaces.
The slidable cooperating indicator bracket 14 has an extending portion 14 on which is mounted a wear-indicating scale 17. A second pointer 18 is rigidly mounted on the rod 13 to move over the scale 17 whenever the rod 13 is moved relatively with respect to the indicator bracket 14. Thus, as wear on the opposed attritioning surfaces causes the rod 13 to be moved further (to the right) with respect to the stationary member 10, and also with respect to the indicator bracket 14, each time the device is reset by the bringing of the two opposed elements into contact with each other, the pointer 18 would indicate on the scale 17 the extent of wear which has occurred. At the same time, when the axially-movable element is again moved away from the opposing element for the operation of the attritioning device or pulp refining machine, the position of the pointer 18 with respect to the scale 17 will not change although the pointer 16 moves with respect to the stationary scale 12 and indicates the actual spacing or gap between the opposed attritioning surfaces.
Consequently, with each resetting of the indicating assembly, by the bringing of the axially-movable attritioning element into contact with the opposing attritioning element in the attritioning device, the adjusting of the two indicators, the one for the wear on the surfaces and the one for the spacing between the surfaces, takes place automatically.
I claim:
1. In an attritioning device having a pair of opposed axially-aligned attritioning elements, one of which is rotated relatively with respect to the other and one of which is movable in an axial direction for adjusting the gap between the elements, an indicator rod connected with and moving in unison in the same axial direction with the axially-movable element, a stationary member, a bearing for said rod in said stationary member, said rod slidable in said bearing, an indicator bracket mounted on said rod beyond said bearing, a friction bushing slidably holding said bracket on said rod, said bracket so positioned on said rod that said bracket will be brought into engagement with said stationary member whenever said axially-movable attritioning element is moved into actual contact with the other opposed attritioning element, cooperating indicating means on said stationary member and on said rod for indicating the gap between said opposed elements, and separate cooperating indicating means on said rod and on said bracket for automatically indicating the extent to which said rod is moved relatively with respect to said bracket, and thereby the extent of wear on said opposed attritioning elements, when the bringing of said elements into face to face contact with each other causes said rod to move in said bracket while said bracket is held by said stationary member.
2. In a pulp refining machine having a pair of axiallyaligned attritioning elements comprising a stator and a rotor and means for moving the stator in an axial direction for adjusting the spacing between stator and rotor, an indicator rod attached to and in axial alignment with the stator, a stationary member, a bearing for said rod in said stationary member, said rod slidable in said bearing, an indicator bracket mounted on said rod beyond said bearing, a friction bushing slidably holding said bracket on said rod, said bracket so positioned on said rod that said bracket will be brought into engagement with said stationary member whenever said stator is moved into actual contact with the rotor, cooperating indicating means on said stationary member and on said rod for indicating the spacing between said stator and said rotor, and separate cooperating indicating means on said rod and on said bracket for automatically indicating the extent to which said rod is moved with respect to said bracket, and thereby the extent of wear on the opposed faces of said stator and rotor, when the moving of said stator into contact with said rotor causes said rod to move in said bracket while said bracket is held by said stationary member.
3. The combination set forth in claim 2 with said first mentioned cooperating indicating means comprising an indicator scale on said stationary member and a pointer on said bracket moving over said scale, and with said second mentioned cooperating means comprising an indicator scale on said bracket and a pointer element on said rod arranged to move over said latter mentioned indicating scale.
References Cited UNITED STATES PATENTS 2,032,584 3/1936 Lengel et al. 33-182 2,068,071 1/1937 Quehl 241256 XR 2,743,874 5/1956 Asplund 241-256 XR 2,854,894 10/1958 Kline et al 241256 XR 3,212,721 10/1965 Asplund et a1. 241256 XR 2,931,586 4/1960 Messing 241256 3,212,721 10/ 1965 Asplund et a1. 241-256 XR 3,327,952 6/1967 Rosenfeld 241-28 XR LOUIS J. CAPOZI, Primary Examiner.
US. Cl. X.R
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Cited By (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4396097A (en) * 1980-02-01 1983-08-02 Lucas Industries Limited Friction pod material adjuster and continuous wear indicator
US4606374A (en) * 1983-04-05 1986-08-19 Nupro Company Valve
US4776438A (en) * 1987-09-11 1988-10-11 Schandelmeier John L Brake adjustment indicator
US4814664A (en) * 1988-02-16 1989-03-21 Champion Spark Plug Company Igniter with wear indicator
US4889184A (en) * 1987-05-27 1989-12-26 Shell Internationale Research Polished rod stuffing box with safety valve for a beam pumped production well
US4991310A (en) * 1989-09-19 1991-02-12 Melia Clifford T Brake chamber stroke indicator
US5699880A (en) * 1996-06-03 1997-12-23 Mr. Safety Check Systems Inc Brake adjustment indicator
US5913385A (en) * 1997-02-20 1999-06-22 Spectra Products Inc. Visual brake stroke indicator
US6135242A (en) * 1996-06-03 2000-10-24 Mr. Safety-Check Systems, Inc. Braking system for a vehicle having a stroke indicator
US6390244B1 (en) * 2001-01-17 2002-05-21 Dana Corporation Brake wear indicator
EP1213503A2 (en) * 2000-12-07 2002-06-12 Caterpillar Inc. Brake wear indicator
EP1323605A2 (en) * 2001-12-04 2003-07-02 Hydro-Aire, Inc. System and method for aircraft braking system usage monitoring
US20040205977A1 (en) * 2003-04-18 2004-10-21 Halliar William R Apparatus for measuring piston travel
US20060033382A1 (en) * 2004-08-11 2006-02-16 Steph James C Gravity based brake stroke sensor methods and systems
US20070080028A1 (en) * 2005-10-11 2007-04-12 Pinel Lloyd J Device and method for measuring slack and tread depth
US20100037476A1 (en) * 2008-08-14 2010-02-18 Thomas Clark Grantham Brake chamber stroke gauge
US20130133565A1 (en) * 2011-11-28 2013-05-30 Chi-Wen Chen Pressure indication device of inflation machine
US20140318260A1 (en) * 2013-04-25 2014-10-30 Chi-Wen Chen Pressure indication device of inflation machine with safety pressure relief
RU167368U1 (en) * 2016-04-29 2017-01-10 Открытое акционерное общество "Ритм" Тверское производство тормозной аппаратуры (ОАО "Ритм" ТПТА) RAILWAY STOCK EXIT DEVICE FOR MOBILE RAILWAY CYLINDER
US20170008645A1 (en) * 2015-07-06 2017-01-12 The Boeing Company Body Fuel Tank Critical Gap Measurement and Validation Template
RU177342U1 (en) * 2017-07-05 2018-02-16 Открытое акционерное общество МТЗ ТРАНСМАШ Brake indicator for rolling stock
RU179901U1 (en) * 2017-06-02 2018-05-28 Вячеслав Николаевич Бочкарев DEVICE FOR PRESSURE CONTROL IN THE BRAKE CYLINDER

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Cited By (48)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4396097A (en) * 1980-02-01 1983-08-02 Lucas Industries Limited Friction pod material adjuster and continuous wear indicator
US4606374A (en) * 1983-04-05 1986-08-19 Nupro Company Valve
US4889184A (en) * 1987-05-27 1989-12-26 Shell Internationale Research Polished rod stuffing box with safety valve for a beam pumped production well
US4776438A (en) * 1987-09-11 1988-10-11 Schandelmeier John L Brake adjustment indicator
US4814664A (en) * 1988-02-16 1989-03-21 Champion Spark Plug Company Igniter with wear indicator
US4991310A (en) * 1989-09-19 1991-02-12 Melia Clifford T Brake chamber stroke indicator
US5699880A (en) * 1996-06-03 1997-12-23 Mr. Safety Check Systems Inc Brake adjustment indicator
US6135242A (en) * 1996-06-03 2000-10-24 Mr. Safety-Check Systems, Inc. Braking system for a vehicle having a stroke indicator
US5913385A (en) * 1997-02-20 1999-06-22 Spectra Products Inc. Visual brake stroke indicator
EP1213503A2 (en) * 2000-12-07 2002-06-12 Caterpillar Inc. Brake wear indicator
EP1213503A3 (en) * 2000-12-07 2002-10-02 Caterpillar Inc. Brake wear indicator
US6390244B1 (en) * 2001-01-17 2002-05-21 Dana Corporation Brake wear indicator
US7416059B2 (en) 2001-12-04 2008-08-26 Hydro-Aire, Inc. System and method for aircraft braking system usage monitoring
US20090120735A1 (en) * 2001-12-04 2009-05-14 Hydro-Aire, Inc. System and method for aircraft braking system usage monitoring
EP1323605A3 (en) * 2001-12-04 2004-10-06 Hydro-Aire, Inc. System and method for aircraft braking system usage monitoring
US8201666B2 (en) 2001-12-04 2012-06-19 Hydro-Aire, Inc. System and method for aircraft braking system usage monitoring
US8041490B2 (en) 2001-12-04 2011-10-18 Hydro-Aire, Inc. System and method for aircraft braking system usage monitoring
US6929333B2 (en) 2001-12-04 2005-08-16 Hydro-Aire, Inc. System and method for aircraft braking system usage monitoring
US20050269873A1 (en) * 2001-12-04 2005-12-08 Devlieg Garrett H System and method for aircraft braking system usage monitoring
US7946394B2 (en) 2001-12-04 2011-05-24 Hydro-Aire, Inc. System and method for aircraft braking system usage monitoring
US20100250028A1 (en) * 2001-12-04 2010-09-30 Hydro-Aire, Inc. System and method for aircraft braking system usage monitoring
US20070200426A1 (en) * 2001-12-04 2007-08-30 Hydro-Aire, Inc. System and Method for Aircraft Braking System Usage Monitoring
US20070200427A1 (en) * 2001-12-04 2007-08-30 Hydro-Aire, Inc. System and Method for Aircraft Braking System Usage Monitoring
US20100170752A1 (en) * 2001-12-04 2010-07-08 Hydro-Aire, Inc. System and method for aircraft braking system usage monitoring
EP1323605A2 (en) * 2001-12-04 2003-07-02 Hydro-Aire, Inc. System and method for aircraft braking system usage monitoring
US7699408B2 (en) 2001-12-04 2010-04-20 Hydro-Aire, Inc. System and method for aircraft braking system using monitoring
US20080275599A1 (en) * 2001-12-04 2008-11-06 Hydro-Aire, Inc. System and Method for Aircraft Braking System Usage Monitoring
US7464796B2 (en) 2001-12-04 2008-12-16 Hydro-Aire, Inc. System and method for aircraft braking system usage monitoring
US7484599B2 (en) * 2001-12-04 2009-02-03 Hydro-Aire, Inc. System and method for aircraft braking system usage monitoring
US20040084252A1 (en) * 2001-12-04 2004-05-06 Devlieg Garrett H. System and method for aircraft braking system usage monitoring
US20090150031A1 (en) * 2001-12-04 2009-06-11 Hydro-Aire, Inc. System and method for aircraft braking system usage monitoring
US6904698B2 (en) 2003-04-18 2005-06-14 Ttx Company Apparatus for measuring piston travel
US20040205977A1 (en) * 2003-04-18 2004-10-21 Halliar William R Apparatus for measuring piston travel
US20080269983A1 (en) * 2004-08-11 2008-10-30 Stemco Lp Gravity based brake stroke sensor methods and systems
US7398141B2 (en) * 2004-08-11 2008-07-08 Stemco Lp Gravity based brake stroke sensor methods and systems
US20060033382A1 (en) * 2004-08-11 2006-02-16 Steph James C Gravity based brake stroke sensor methods and systems
US8078375B2 (en) 2004-08-11 2011-12-13 Stemco Lp Gravity based brake stroke sensor methods and systems
US20070080028A1 (en) * 2005-10-11 2007-04-12 Pinel Lloyd J Device and method for measuring slack and tread depth
US20100037476A1 (en) * 2008-08-14 2010-02-18 Thomas Clark Grantham Brake chamber stroke gauge
US20130133565A1 (en) * 2011-11-28 2013-05-30 Chi-Wen Chen Pressure indication device of inflation machine
US8733270B2 (en) * 2011-11-28 2014-05-27 Chi-Wen Chen Pressure indication device of inflation machine
US20140318260A1 (en) * 2013-04-25 2014-10-30 Chi-Wen Chen Pressure indication device of inflation machine with safety pressure relief
US9057656B2 (en) * 2013-04-25 2015-06-16 Chi-Wen Chen Pressure indication device of inflation machine with safety pressure relief
US20170008645A1 (en) * 2015-07-06 2017-01-12 The Boeing Company Body Fuel Tank Critical Gap Measurement and Validation Template
US9815542B2 (en) * 2015-07-06 2017-11-14 The Boeing Company Body fuel tank critical gap measurement and validation template
RU167368U1 (en) * 2016-04-29 2017-01-10 Открытое акционерное общество "Ритм" Тверское производство тормозной аппаратуры (ОАО "Ритм" ТПТА) RAILWAY STOCK EXIT DEVICE FOR MOBILE RAILWAY CYLINDER
RU179901U1 (en) * 2017-06-02 2018-05-28 Вячеслав Николаевич Бочкарев DEVICE FOR PRESSURE CONTROL IN THE BRAKE CYLINDER
RU177342U1 (en) * 2017-07-05 2018-02-16 Открытое акционерное общество МТЗ ТРАНСМАШ Brake indicator for rolling stock

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