US3308524A - Method of making a die bushing with a replaceable liner - Google Patents

Method of making a die bushing with a replaceable liner Download PDF

Info

Publication number
US3308524A
US3308524A US339526A US33952664A US3308524A US 3308524 A US3308524 A US 3308524A US 339526 A US339526 A US 339526A US 33952664 A US33952664 A US 33952664A US 3308524 A US3308524 A US 3308524A
Authority
US
United States
Prior art keywords
liner
bushing
post
die
bore
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
US339526A
Inventor
Moyer Robert Franklin
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.)
Enviri Corp
Original Assignee
Harsco 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 Harsco Corp filed Critical Harsco Corp
Priority to US339526A priority Critical patent/US3308524A/en
Application granted granted Critical
Publication of US3308524A publication Critical patent/US3308524A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21DWORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D37/00Tools as parts of machines covered by this subclass
    • B21D37/10Die sets; Pillar guides
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C29/00Bearings for parts moving only linearly
    • F16C29/02Sliding-contact bearings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/02Parts of sliding-contact bearings
    • F16C33/04Brasses; Bushes; Linings
    • F16C33/06Sliding surface mainly made of metal
    • F16C33/08Attachment of brasses, bushes or linings to the bearing housing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2220/00Shaping
    • F16C2220/80Shaping by separating parts, e.g. by severing, cracking
    • F16C2220/82Shaping by separating parts, e.g. by severing, cracking by cutting
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2223/00Surface treatments; Hardening; Coating
    • F16C2223/30Coating surfaces
    • F16C2223/70Coating surfaces by electroplating or electrolytic coating, e.g. anodising, galvanising
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2226/00Joining parts; Fastening; Assembling or mounting parts
    • F16C2226/30Material joints
    • F16C2226/32Material joints by soldering
    • F16C2226/34Material joints by soldering by brazing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2322/00Apparatus used in shaping articles
    • F16C2322/14Stamping, deep-drawing or punching, e.g. die sets
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/02Parts of sliding-contact bearings
    • F16C33/04Brasses; Bushes; Linings
    • F16C33/06Sliding surface mainly made of metal
    • F16C33/12Structural composition; Use of special materials or surface treatments, e.g. for rust-proofing
    • F16C33/121Use of special materials
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/02Parts of sliding-contact bearings
    • F16C33/04Brasses; Bushes; Linings
    • F16C33/06Sliding surface mainly made of metal
    • F16C33/14Special methods of manufacture; Running-in
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49636Process for making bearing or component thereof
    • Y10T29/49643Rotary bearing
    • Y10T29/49647Plain bearing
    • Y10T29/49668Sleeve or bushing making
    • Y10T29/49677Sleeve or bushing making having liner
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49764Method of mechanical manufacture with testing or indicating
    • Y10T29/49778Method of mechanical manufacture with testing or indicating with aligning, guiding, or instruction
    • Y10T29/4978Assisting assembly or disassembly
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining
    • Y10T29/49885Assembling or joining with coating before or during assembling
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining
    • Y10T29/49908Joining by deforming
    • Y10T29/49938Radially expanding part in cavity, aperture, or hollow body
    • Y10T29/4994Radially expanding internal tube
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining
    • Y10T29/49945Assembling or joining by driven force fit

Definitions

  • This invention relates to die bushing liners and more particularly to die bushing liners which may be removed and replaced in die bushings and a method for fabricating said die bushing liners.
  • One of the objects of the present invention is to provide a method of making a die bushing with a replaceable liner.
  • Another object is to provide a method for fabricating a die bushing liner.
  • the upper or punch carrying plate is provided with either two or four bushings located in the corner areas of the upper plate.
  • the lower or die carrying plate is provided with either two or four posts located in the corner areas of the lower plate.
  • the posts cooperatively mate with the bushings in the normal function of the die set as a punch press reciprocates the upper plate toward and away from the lower plate.
  • the sliding movement of the bushing upon the mating post wears the bushing.
  • the accuracy of the mating relationship is thereby destroyed.
  • the accuracy of the mating relationship between the post and mating bushing determines the accuracy between the punch and die and therefore of the article produced by the punch and die.
  • the dust and splinters find their way between the post and mating bushing.
  • the heat generated by friction, the pressure of the punch press, and the dust and splinters combine to reduce the space or tolerance between the outside diameter of the post and the inside diameter of the bushing.
  • Eventually the dust and splinter accumulation cause galling and/or welding of the post of the bushing.
  • the post becomes frozen or jammed into the bushing.
  • the punch press having a positive action, thereby causes an accident to the operative and destruction to the very valuable punch and die.
  • the present invention was created to alleviate all of these undesirable and costly conditions in a die set by providing a liner which may be removed from the bushing, regardless of the adverse conditions under which the die set functions.
  • FIGURE 1 is a side elevational view of the new and improved die bushing provided with a removable liner.
  • FIGURE 2 is a top plan view of FIGURE 1.
  • FIGURE 3 is a bottom plan view of FIGURE 1.
  • FIGURE 4 is a vertical cross sectional view taken on line 4-4 of FIGURE 2.
  • FIGURE 5 is a perspective view of a liner fabricated from a bimetallic material.
  • FIGURE 6 is a perspective view of a liner fabricated from a single metallic material.
  • FIGURE 7 is a side elevational view of a die set provided with the new and improved die bushing liners.
  • FIGURE 8 is a cross sectional view of a die bushing taken along line 88 of FIGURE 1, in the process of having a liner placed therein.
  • FIGURE 9 is a cross sectional view of a die bushing similar to FIGURE 8 indicating another method of placing a liner therein.
  • a die bushing fabricated of steel generally indicated by reference numeral 10, consists of a cylindrical body, externally provided with a reucked diameter 11 terminating in a flange 12. Internally, die bushing 10 is provided with an axial bore 13 and two grooves 14 and 15 adjacent opposite ends of said die bushing 10 (see FIGURE 4). Die bushing 10 may be provided with a tapped hole 9. Said cylindrical body constituting a supporting shell.
  • a liner, cylindrical in form, generally indicated by reference numeral 25, may be fabricated from a bimetallic element as shown in FIGURE 5 or a single metallic element as shown in FIGURE 6 by 25A.
  • a layer of bearing metal 27 is laminated to a sheet of steel 26.
  • the bimetallic laminated sheet is cut into strips which are formed into a round or cylindrical shape and brazed to provide a permanent cylinder.
  • the steel outside diameter 26 of liner 25 is ground to a precision size.
  • the internal diameter 28 of bearing metal is reamed to a precision size.
  • the outside diameter 26 of the liner 25 in FIGURE 5 and the outside diameter 26A of liner 25A in FIGURE 6 is then subjected to an electrolytic coating of a nonferrous metal such as copper or a steam pressure application of cadmium 29 in FIGURE 5 and 29A in FIGURE 6.
  • a nonferrous metal such as copper or a steam pressure application of cadmium 29 in FIGURE 5 and 29A in FIGURE 6.
  • the coating is kept to approximately five ten-thousandths of an inch in thickness thus limiting the increase in outside diameter of the liner to approximately one-thousandth of an inch.
  • the internal diameters 28 and 28A may be provided with an oil groove 31 and 31A respectively. Both liners 25 and 25A may be provided with slots 32 and 32A respectively for purposes which will presently appear.
  • the difference between the diameter of the axial bore 13 and the outside diameters 26 or 26A is preferably approximately one thousandth of an inch after the coating 29 or 29A is applied.
  • Both liners 25 and 25A are placed or forced into axial bore 13.
  • the copper or cadmium coatings 29 or 29A serve two functions. The first function is as an insulating medium between the steel of the die bushing 10 and the main material of the liners. Should the die bushing 10 steel and the liner material engage, they could rust into position and be jammed or frozen 3 permanently or they could gall together due to frictional heat.
  • the second and most important function served by the copper or cadmium coatings 29 or 29A isits cooperative function as a backing up fuller.
  • the coating 29 compensates for irregularities in either axial bore 13 or outside diameters 26 or 26A when they unite, thus preserving the vital size and concentric shape of the inside diameters 28 and 28A so vital to the proper function of the post 40 and the die set.
  • FIGURES '8 and 9 Two preferred ways of fitting liners to die bushings are illustrated in FIGURES '8 and 9. These liners are indicated by the numerals 125 and 225 in FIGURES 8 and 9 respectively.
  • liner 225 prior to being pressed into axial bore 13, is placed upon a gage or aligning post 50.
  • the gage or aligning post 50 is provided with an exacting outside diameter. The highest skill of the tool making art plus precision machinery is needed to provide the exacting outside diameter.
  • the gage or aligning post 50 is placed within internal diameter 228 with a slight slop in the fit. With the coating 229 the outside diameter 226 of the liner 225 is slightly larger than the interior diameter of bore 13 of the bushing 10. The aligning post 56 then forces liner 225 into die bushing 10 with the copper coating 29 engaging the steel surface of axial bore 13. Because of its slight oversize the liner 225 is squeezed down onto post 50 as it is pressed into the bushing 10. During this procedure the coating 229 acts as a lubricant.
  • the arrows 250 illustrate the inward pressing of the liner during this procedure.
  • the tolerance between a one inch diameter gage post an the inside diameter of a mating bushing liner is normally between three ten thousandths of an inch and four ten thousandths of an inch. In a two inch diameter gage post the tolerance between a mating bushing liner would normally be between five ten-thousandths and eight ten-thousandths of an inch.
  • the aligning post 50 in FIGURE 8, as it is forced into liner 125 While in position within die bushing 10, causes the liner 125, which is slightly smaller in its internal diameter 128 than the outside diameter of the post 50 to increase in size as shown by arrows 150 to fit properly within the bore 13.
  • the coating 129 which is softer than the steel of either bushing 10 or liner 125, accommodates itself to tolerance variation, so that, any tolerance variation between axial bore 13 and outside diameter 126 of liner 125 is not reflected in the dimension of the inside diameter 128 of liner 125. If the coating 129 is not applied a tolerance variation may be present in the inside diameter 128 due to misalignment, to the detriment of the proper funtcioning of the mating die set post (See FIGURE 7.)
  • a collar 16 (see FIGURE 4) provided with an axial passageway 17 and a shelf consisting of a cylindrical wall 18 and a wall 19 at right angles to said cylindrical wall 18 is removably secured to one end of die bushing 10 by means of screws 29. Said axial passageway 17 having a diameter larger than internal diameter 28.
  • a wiping ring 21 is fixed in position between the shelf and the end of die bushing 10. Wiping ring 21 is shaped to lie against cylindrical wall 18 and wall 19 with a flexible tongue 22 overlying axial passageway 17.
  • a die set generally indicated by reference numeral 41 (see FIGURE 7) consists of an upper or punch carrying plate 42 provided with a punch press attaching stem 43 and a die carrying plate 44 normally secured to the bed of a punch press.
  • the punch carrying plate 42 is provided (as illustrated) with two bushing receiving orifices into which the reduced diameters 11 of the die bushings 10 are forced with a drive fit.
  • the die carrying plate 44 is adapted to have die posts 40 secured therein.
  • die posts 40 slidingly engage the inside diameters 28 of liners 25 secured in die bushings 10, for example, by means of snap rings 45, 46 located in grooves 14, 15, respectively.
  • Lubricating oil may be passed through tapped hole 9, through slot 32 into oil groove 31.
  • the film of oil coating inside diameter 28 will be approximately one ten-throusandth of an inch thick.
  • a method of fabricating a substantially cylindrical die bushing containing a liner in an axial bore thereof comprising the steps of forming a cylindrical liner member of bimetallic laminate material having an outer steel shell and an inner layer of bearing metal which is softer than said steel, coating the outer surface of the outer steel shell with a layer of non-ferrous metal having a thickness in the order of five ten-thousandths of an inch, placing said liner member on a gage post having a standard outside diameter, the internal diameter of said liner member being larger than the outside diameter of said post to a limit of .04% of the outside diameter of said post, forcing said liner member into said bore of said bushing by means of said gage post whereby said layer of non-ferrous metal is caused to conform to any variations present in said bore, removing said gage post and inserting locking means at each end of said liner for retaining said liner in said bushing.
  • a method of fabricating a substantially cylindrical die bushing containing a liner in an axial bore thereof comprising the steps of forming a hollow cylindrical liner member containing an inner surface of bearing metal, coating the outer surface of said liner member with a layer of non-ferrous metal having a thickness in the order of five ten-thousandths of an inch, placing said liner member on a gage post having a standard outside diameter which is slightly smaller than the internal diameter of said liner, forcing said liner member, which has an outside diameter slightly larger than the internal diameter of said bore of said die bushing, into said bore by means of said gage post whereby said bore compresses said liner about said gage post to properly size said liner and said outer layer of non-ferrous metal on said liner acts as a lubricant and is caused to conform to any variations present in said bore, removing said gage post and locking said liner in place.
  • a method of fabricating a substantially cylindrical die bushing containing a liner in an axial bore thereof comprising the steps of forming a hollow cylindrical liner member having an interior bore containing an inner surface of bearing metal, coating the outer surface of said liner member with a layer of non-ferrous metal having a thickness in the order of five ten-thousandths of an inch, placing said liner member within said bore of said die bushing which bore has an internal diameter slightly larger than the external diameter of said liner, forcing a gage post having a standard outside diameter Which is slightly larger than the interior bore of said liner member whereby said gage post expands said liner into firm engagement with the bore of said die bushing with said outer layer of non-ferrous metal conforming to any variations present in said bore, and said liner is properly sized on said gage post, removing said gage post and locking said liner in place.
  • a method of fabricating a substantially cylindrical die bushing containing a liner in an axial bore thereof comprising the steps of forming a hollow cylindrical liner member having an interior bore containing an inner surface of bearing metal, coating the outer surface of said liner member with a layer of non-ferrous metal having a thickness in the order of five ten-thousandths of an inch, utilizing a gage post having a standard outside diameter to force said liner into a proper desired size within said die bushing with said outer layer of non-ferrous metal being squeezed between said liner and said die bushing and conforming to any irregularities in the bore of said die bushing, removing said gage post and locking said liner in place.

Description

March 9 7 R. F. MOYER 3,308,524
METHOD OF MAKING A DIE BUSHING WITH A REPLACEABLE LINER Filed Jan. 22, 1964 Hill I I Q I F I G. I
o o 0 /Q o o o o o 0 8 0 O o 0 O O o 0 26 o o O O o o o o o o o o 0 o o o o o 0 o o o o o o o o 9 o o 0 0 O o INVENTOR.
ROBERT FRANKLIN MOYER ATTORNEY United States Patent 3,308,524 METHOD OF MAKING A DIE BUSHING WITH A REPLACEABLE LINER Robert Franklin Meyer, Warwick, R.I., assignor to Harsco Corporation, Harrisburg, Pa., a corporation of Delaware Filed Jan. 22, 1964, Ser. No. 339,526 6 Claims. (Cl. 29149.5)
This invention relates to die bushing liners and more particularly to die bushing liners which may be removed and replaced in die bushings and a method for fabricating said die bushing liners.
This case is a continuation-in-part of U8. Patent No. 3,149,887, dated September 22, 1964.
One of the objects of the present invention is to provide a method of making a die bushing with a replaceable liner.
Another object is to provide a method for fabricating a die bushing liner.
In the conventional die set the upper or punch carrying plate is provided with either two or four bushings located in the corner areas of the upper plate. The lower or die carrying plate is provided with either two or four posts located in the corner areas of the lower plate.
The posts cooperatively mate with the bushings in the normal function of the die set as a punch press reciprocates the upper plate toward and away from the lower plate. The sliding movement of the bushing upon the mating post wears the bushing. The accuracy of the mating relationship is thereby destroyed. The accuracy of the mating relationship between the post and mating bushing determines the accuracy between the punch and die and therefore of the article produced by the punch and die.
As the bushings wear play develops between the post and mating bushing. Thus accurately and uniformly sized and shaped articles are no longer produced by the die set. In addition the play causes misalignment of the punch carrying plate with the die carrying plate, thereby, causing the punch to be misaligned with the die. As the punch press forces the punch against the die in misaligned relationship, the punch is broken or damaged and the die is damaged. The cost of producing punches and dies runs into many thousands of dollars.
It would appear to be a simple matter to provide a die bushing with a replaceable sleeve or liner when the bushing becomes worn and the accurate mating relationship between the post and bushing is destroyed. However, such is not the case because the reciprocating movement of the punch press causes heat to develop due to friction, in both the post and mating bushing. The heat generated in the bushing causes a liner to freeze or bind to the bushing, thereby destroying the purpose for which the liner was placed in the bushing, namely, to be removed and replaced when the inside diameter of the liner becomes worn.
As the punch and die mate during the work cycle, fine metallic dust and splinters are created. The dust and splinters are created from the action of the punch piercing the metal strip.
The dust and splinters find their way between the post and mating bushing. The heat generated by friction, the pressure of the punch press, and the dust and splinters combine to reduce the space or tolerance between the outside diameter of the post and the inside diameter of the bushing. Eventually the dust and splinter accumulation cause galling and/or welding of the post of the bushing. The post becomes frozen or jammed into the bushing. The punch press having a positive action, thereby causes an accident to the operative and destruction to the very valuable punch and die.
The present invention was created to alleviate all of these undesirable and costly conditions in a die set by providing a liner which may be removed from the bushing, regardless of the adverse conditions under which the die set functions.
Other objects of the present invention will become apparent in part and be pointed out in part in the following specification and claims.
Referring to the drawings in which similar characters of reference indicate corresponding part in all the figures:
FIGURE 1 is a side elevational view of the new and improved die bushing provided with a removable liner.
FIGURE 2 is a top plan view of FIGURE 1.
FIGURE 3 is a bottom plan view of FIGURE 1.
FIGURE 4 is a vertical cross sectional view taken on line 4-4 of FIGURE 2.
FIGURE 5 is a perspective view of a liner fabricated from a bimetallic material.
FIGURE 6 is a perspective view of a liner fabricated from a single metallic material.
FIGURE 7 is a side elevational view of a die set provided with the new and improved die bushing liners.
FIGURE 8 is a cross sectional view of a die bushing taken along line 88 of FIGURE 1, in the process of having a liner placed therein.
FIGURE 9 is a cross sectional view of a die bushing similar to FIGURE 8 indicating another method of placing a liner therein.
In proceeding with this invention reference is made to all figures in the drawing. A die bushing fabricated of steel, generally indicated by reference numeral 10, consists of a cylindrical body, externally provided with a re duced diameter 11 terminating in a flange 12. Internally, die bushing 10 is provided with an axial bore 13 and two grooves 14 and 15 adjacent opposite ends of said die bushing 10 (see FIGURE 4). Die bushing 10 may be provided with a tapped hole 9. Said cylindrical body constituting a supporting shell.
A liner, cylindrical in form, generally indicated by reference numeral 25, may be fabricated from a bimetallic element as shown in FIGURE 5 or a single metallic element as shown in FIGURE 6 by 25A. Referring to FIGURE 5, a layer of bearing metal 27 is laminated to a sheet of steel 26. The bimetallic laminated sheet is cut into strips which are formed into a round or cylindrical shape and brazed to provide a permanent cylinder. The steel outside diameter 26 of liner 25 is ground to a precision size. The internal diameter 28 of bearing metal is reamed to a precision size.
The outside diameter 26 of the liner 25 in FIGURE 5 and the outside diameter 26A of liner 25A in FIGURE 6 is then subjected to an electrolytic coating of a nonferrous metal such as copper or a steam pressure application of cadmium 29 in FIGURE 5 and 29A in FIGURE 6. Preferably the coating is kept to approximately five ten-thousandths of an inch in thickness thus limiting the increase in outside diameter of the liner to approximately one-thousandth of an inch.
The internal diameters 28 and 28A may be provided with an oil groove 31 and 31A respectively. Both liners 25 and 25A may be provided with slots 32 and 32A respectively for purposes which will presently appear.
The difference between the diameter of the axial bore 13 and the outside diameters 26 or 26A is preferably approximately one thousandth of an inch after the coating 29 or 29A is applied. Both liners 25 and 25A are placed or forced into axial bore 13. The copper or cadmium coatings 29 or 29A serve two functions. The first function is as an insulating medium between the steel of the die bushing 10 and the main material of the liners. Should the die bushing 10 steel and the liner material engage, they could rust into position and be jammed or frozen 3 permanently or they could gall together due to frictional heat.
The second and most important function served by the copper or cadmium coatings 29 or 29A isits cooperative function as a backing up fuller. The coating 29 compensates for irregularities in either axial bore 13 or outside diameters 26 or 26A when they unite, thus preserving the vital size and concentric shape of the inside diameters 28 and 28A so vital to the proper function of the post 40 and the die set.
Two preferred ways of fitting liners to die bushings are illustrated in FIGURES '8 and 9. These liners are indicated by the numerals 125 and 225 in FIGURES 8 and 9 respectively.
In FIGURE 9 liner 225 prior to being pressed into axial bore 13, is placed upon a gage or aligning post 50. The gage or aligning post 50 is provided with an exacting outside diameter. The highest skill of the tool making art plus precision machinery is needed to provide the exacting outside diameter.
The gage or aligning post 50 is placed within internal diameter 228 with a slight slop in the fit. With the coating 229 the outside diameter 226 of the liner 225 is slightly larger than the interior diameter of bore 13 of the bushing 10. The aligning post 56 then forces liner 225 into die bushing 10 with the copper coating 29 engaging the steel surface of axial bore 13. Because of its slight oversize the liner 225 is squeezed down onto post 50 as it is pressed into the bushing 10. During this procedure the coating 229 acts as a lubricant. The arrows 250 illustrate the inward pressing of the liner during this procedure.
It is well known in the art, that is is impossible for all practical and commercial and manufacturing purposes, to fabricate the inside diameter of one member and the outside diameter of a mating member to absolute zero variation. The variation is called tolerance. The tolerance between a one inch diameter gage post an the inside diameter of a mating bushing liner is normally between three ten thousandths of an inch and four ten thousandths of an inch. In a two inch diameter gage post the tolerance between a mating bushing liner would normally be between five ten-thousandths and eight ten-thousandths of an inch.
In another approach the aligning post 50, in FIGURE 8, as it is forced into liner 125 While in position within die bushing 10, causes the liner 125, which is slightly smaller in its internal diameter 128 than the outside diameter of the post 50 to increase in size as shown by arrows 150 to fit properly within the bore 13. The coating 129, which is softer than the steel of either bushing 10 or liner 125, accommodates itself to tolerance variation, so that, any tolerance variation between axial bore 13 and outside diameter 126 of liner 125 is not reflected in the dimension of the inside diameter 128 of liner 125. If the coating 129 is not applied a tolerance variation may be present in the inside diameter 128 due to misalignment, to the detriment of the proper funtcioning of the mating die set post (See FIGURE 7.)
A collar 16 (see FIGURE 4) provided with an axial passageway 17 and a shelf consisting of a cylindrical wall 18 and a wall 19 at right angles to said cylindrical wall 18 is removably secured to one end of die bushing 10 by means of screws 29. Said axial passageway 17 having a diameter larger than internal diameter 28. A wiping ring 21 is fixed in position between the shelf and the end of die bushing 10. Wiping ring 21 is shaped to lie against cylindrical wall 18 and wall 19 with a flexible tongue 22 overlying axial passageway 17.
A die set generally indicated by reference numeral 41, (see FIGURE 7) consists of an upper or punch carrying plate 42 provided with a punch press attaching stem 43 and a die carrying plate 44 normally secured to the bed of a punch press. The punch carrying plate 42 is provided (as illustrated) with two bushing receiving orifices into which the reduced diameters 11 of the die bushings 10 are forced with a drive fit. The die carrying plate 44 is adapted to have die posts 40 secured therein.
In nomal punch press operation die posts 40 slidingly engage the inside diameters 28 of liners 25 secured in die bushings 10, for example, by means of snap rings 45, 46 located in grooves 14, 15, respectively. Lubricating oil may be passed through tapped hole 9, through slot 32 into oil groove 31. The film of oil coating inside diameter 28 will be approximately one ten-throusandth of an inch thick. Thus, the precision and magnitude of the very slight tolerances or variations of the parts constituting the present invention can be understood and appreciated.
Having shown and described various embodiments of the present invention by way of example, it should be realized that structural changes could be made and other examples given without departing from either the spirit or scope of this invention.
What I claim is:
1. A method of fabricating a substantially cylindrical die bushing containing a liner in an axial bore thereof comprising the steps of forming a cylindrical liner member of bimetallic laminate material having an outer steel shell and an inner layer of bearing metal which is softer than said steel, coating the outer surface of the outer steel shell with a layer of non-ferrous metal having a thickness in the order of five ten-thousandths of an inch, placing said liner member on a gage post having a standard outside diameter, the internal diameter of said liner member being larger than the outside diameter of said post to a limit of .04% of the outside diameter of said post, forcing said liner member into said bore of said bushing by means of said gage post whereby said layer of non-ferrous metal is caused to conform to any variations present in said bore, removing said gage post and inserting locking means at each end of said liner for retaining said liner in said bushing.
2. A method of fabricating a substantially cylindrical die bushing containing a liner in an axial bore thereof comprising the steps of forming a hollow cylindrical liner member containing an inner surface of bearing metal, coating the outer surface of said liner member with a layer of non-ferrous metal having a thickness in the order of five ten-thousandths of an inch, placing said liner member on a gage post having a standard outside diameter which is slightly smaller than the internal diameter of said liner, forcing said liner member, which has an outside diameter slightly larger than the internal diameter of said bore of said die bushing, into said bore by means of said gage post whereby said bore compresses said liner about said gage post to properly size said liner and said outer layer of non-ferrous metal on said liner acts as a lubricant and is caused to conform to any variations present in said bore, removing said gage post and locking said liner in place.
3. A method according to claim 2 wherein the differences between the outside diameter of said gage post and the internal diameter of said liner, also between the outside diameter of said liner and the internal diameter of said bore of said die bushing is on the order of .04% of the outside diameter of said gage post.
4. A method of fabricating a substantially cylindrical die bushing containing a liner in an axial bore thereof comprising the steps of forming a hollow cylindrical liner member having an interior bore containing an inner surface of bearing metal, coating the outer surface of said liner member with a layer of non-ferrous metal having a thickness in the order of five ten-thousandths of an inch, placing said liner member within said bore of said die bushing which bore has an internal diameter slightly larger than the external diameter of said liner, forcing a gage post having a standard outside diameter Which is slightly larger than the interior bore of said liner member whereby said gage post expands said liner into firm engagement with the bore of said die bushing with said outer layer of non-ferrous metal conforming to any variations present in said bore, and said liner is properly sized on said gage post, removing said gage post and locking said liner in place.
5. A method according to claim 4 wherein the differences between the internal diameter of said bore of die bushing and the external diameter of said liner, also between the outside diameter of said gage post and the interior diameter of said interior bore of said liner member is on the order of .04% of the outside diameter of said gage post' 6. A method of fabricating a substantially cylindrical die bushing containing a liner in an axial bore thereof comprising the steps of forming a hollow cylindrical liner member having an interior bore containing an inner surface of bearing metal, coating the outer surface of said liner member with a layer of non-ferrous metal having a thickness in the order of five ten-thousandths of an inch, utilizing a gage post having a standard outside diameter to force said liner into a proper desired size within said die bushing with said outer layer of non-ferrous metal being squeezed between said liner and said die bushing and conforming to any irregularities in the bore of said die bushing, removing said gage post and locking said liner in place.
References Cited by the Examiner UNITED STATES PATENTS JOHN F. CAMPBELL, Primary Examiner.
THOMAS H. EAGER, Examiner.

Claims (1)

1. A METHOD OF FABRICATING A SUBSTANTIALLY CYLINDRICAL DIE BUSHING CONTAINING A LINER IN AN AXIAL BORE THEREOF COMPRISING THE STEPS OF FORMING A CYLINDRICAL LINER MEMBER OF BIMETALLIC LAMINATE MATERIAL HAVING AN OUTER STEEL SHELL AND AN INNER LAYER OF BEARING METAL WHICH IS SOFTER THAN SAID STEEL, COATING THE OUTER SURFACE OF THE OUTER STEEL SHELL WITH A LAYER OF NON-FERROUS METAL HAVING A THICKNESS IN THE ORDER OF FIVE TEN-THOUSANDTHS OF AN INCH, PLACING SAID LINER MEMBER ON A GAGE POST HAVING A STANDARD OUTSIDE DIAMETER, THE INTERNAL DIAMETER OF SAID LINER MEMBER BEING LARGER THAN THE OUTSIDE DIAMETER OF SAID POST TO A LIMIT OF .04% OF THE OUTSIDE DIAMETER OF SAID POST, FORCING SAID LINER MEMBER INTO SAID BORE OF SAID BUSHING BY MEANS OF SAID GAGE POST WHEREBY SAID LAYER OF NON-FERROUS METAL IS CAUSED TO CONFORM TO ANY VARIATIONS PRESENT IN SAID BORE, REMOVING SAID GAGE POST AND INSERTING LOCKING MEANS AT EACH END OF SAID LINER FOR RETAINING SAID LINER IN SAID BUSHING.
US339526A 1964-01-22 1964-01-22 Method of making a die bushing with a replaceable liner Expired - Lifetime US3308524A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US339526A US3308524A (en) 1964-01-22 1964-01-22 Method of making a die bushing with a replaceable liner

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US339526A US3308524A (en) 1964-01-22 1964-01-22 Method of making a die bushing with a replaceable liner

Publications (1)

Publication Number Publication Date
US3308524A true US3308524A (en) 1967-03-14

Family

ID=23329421

Family Applications (1)

Application Number Title Priority Date Filing Date
US339526A Expired - Lifetime US3308524A (en) 1964-01-22 1964-01-22 Method of making a die bushing with a replaceable liner

Country Status (1)

Country Link
US (1) US3308524A (en)

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3468024A (en) * 1965-10-20 1969-09-23 John L Yonkers Method and apparatus for orienting and assembling small parts
US4117583A (en) * 1975-12-24 1978-10-03 Werner & Pfleiderer Method of providing a wear-resistant lining in the work chamber of a screw extruder
US4179780A (en) * 1976-08-04 1979-12-25 Federal-Mogul Corporation Method of making a clutch throw-out bearing assembly
US4227756A (en) * 1978-12-29 1980-10-14 Mechanical Technology Incorporated High temperature low friction surface coating
US4253714A (en) * 1980-02-27 1981-03-03 Mechanical Technology Incorporated High temperature low friction surface coating and method of application
US4263814A (en) * 1977-04-19 1981-04-28 Kabushiki Kaisha Toyoda Jidoshokki Seisakusho Shoe for use in a swash-plate type compressor
US4302874A (en) * 1978-12-13 1981-12-01 Cegedur Societe De Transformation De L'aluminium Pechiney Method of forming pipe union
US4309064A (en) * 1979-09-28 1982-01-05 Taiho Kogyo Co., Ltd. Bearing of an internal combustion engine and process for producing the same
US4458405A (en) * 1982-03-01 1984-07-10 Clevepak Corporation Method of assembling a motor bearing and seal in a motor
US4640650A (en) * 1983-06-09 1987-02-03 Bochumer Eisenhutte Heintzmann Gmbh & Co. Kg Hydraulically operated unit for roof support
US6212753B1 (en) * 1997-11-25 2001-04-10 General Electric Company Complaint joint for interfacing dissimilar metals in X-ray tubes
CN105889319A (en) * 2016-06-03 2016-08-24 苏州同佳精密五金厂 Oil-free guiding sleeve
CN112549381A (en) * 2020-10-30 2021-03-26 哈尔滨飞机工业集团有限责任公司 Detachable lining assembly of composite material mold and mounting and replacing method

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2274961A (en) * 1938-10-14 1942-03-03 Timken Roller Bearing Co Process of producing wheel and axle assemblies
US2646824A (en) * 1951-07-18 1953-07-28 Livermore Corp H F Boss for dobby jacks
US2751260A (en) * 1950-09-12 1956-06-19 Janiszewski Kasimir Replaceable leader pin bushing
US2855666A (en) * 1954-02-16 1958-10-14 Curtiss Wright Corp Methods of producing textile mill spindles
US3039829A (en) * 1958-11-10 1962-06-19 Locke Steel Chain Co Press
US3149887A (en) * 1961-01-03 1964-09-22 Harsco Corp Die bushing with removable liner

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2274961A (en) * 1938-10-14 1942-03-03 Timken Roller Bearing Co Process of producing wheel and axle assemblies
US2751260A (en) * 1950-09-12 1956-06-19 Janiszewski Kasimir Replaceable leader pin bushing
US2646824A (en) * 1951-07-18 1953-07-28 Livermore Corp H F Boss for dobby jacks
US2855666A (en) * 1954-02-16 1958-10-14 Curtiss Wright Corp Methods of producing textile mill spindles
US3039829A (en) * 1958-11-10 1962-06-19 Locke Steel Chain Co Press
US3149887A (en) * 1961-01-03 1964-09-22 Harsco Corp Die bushing with removable liner

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3468024A (en) * 1965-10-20 1969-09-23 John L Yonkers Method and apparatus for orienting and assembling small parts
US4117583A (en) * 1975-12-24 1978-10-03 Werner & Pfleiderer Method of providing a wear-resistant lining in the work chamber of a screw extruder
US4179780A (en) * 1976-08-04 1979-12-25 Federal-Mogul Corporation Method of making a clutch throw-out bearing assembly
US4263814A (en) * 1977-04-19 1981-04-28 Kabushiki Kaisha Toyoda Jidoshokki Seisakusho Shoe for use in a swash-plate type compressor
US4302874A (en) * 1978-12-13 1981-12-01 Cegedur Societe De Transformation De L'aluminium Pechiney Method of forming pipe union
US4227756A (en) * 1978-12-29 1980-10-14 Mechanical Technology Incorporated High temperature low friction surface coating
US4309064A (en) * 1979-09-28 1982-01-05 Taiho Kogyo Co., Ltd. Bearing of an internal combustion engine and process for producing the same
US4470184A (en) * 1979-09-28 1984-09-11 Taiho Kogyo, Ltd. Bearing of an internal combustion engine and process for producing the same
US4253714A (en) * 1980-02-27 1981-03-03 Mechanical Technology Incorporated High temperature low friction surface coating and method of application
US4458405A (en) * 1982-03-01 1984-07-10 Clevepak Corporation Method of assembling a motor bearing and seal in a motor
US4640650A (en) * 1983-06-09 1987-02-03 Bochumer Eisenhutte Heintzmann Gmbh & Co. Kg Hydraulically operated unit for roof support
US6212753B1 (en) * 1997-11-25 2001-04-10 General Electric Company Complaint joint for interfacing dissimilar metals in X-ray tubes
CN105889319A (en) * 2016-06-03 2016-08-24 苏州同佳精密五金厂 Oil-free guiding sleeve
CN105889319B (en) * 2016-06-03 2018-06-19 苏州同佳精密五金厂 A kind of no oil feeding guide sleeve
CN112549381A (en) * 2020-10-30 2021-03-26 哈尔滨飞机工业集团有限责任公司 Detachable lining assembly of composite material mold and mounting and replacing method

Similar Documents

Publication Publication Date Title
US3308524A (en) Method of making a die bushing with a replaceable liner
US3713714A (en) Methods of manufacturing flanged bearings
US2441580A (en) Method of forming screw threads
US4377084A (en) Press apparatus having resilient stop blocks
JPH0118298B2 (en)
US2369896A (en) Punching metal bars, plates, and the like
US1959068A (en) Method of producing valve seat rings
US3149887A (en) Die bushing with removable liner
US2187661A (en) Valve tappet
US4095513A (en) Piston with gudgeon pin and method of making same
US1991723A (en) Bearing seal
US5442947A (en) Tooling apparatus and method for high speed production of drawn metal cup-like articles
US2368799A (en) Composite metal coupling member
US2870533A (en) Joining together of metal parts
US2674780A (en) Die mechanism
US2481025A (en) Method of making shafts having sheet metal journal surfaces
US2885532A (en) Method of making pump bushings and the like
US3182379A (en) Method of forming bearing mountings
US2384444A (en) Method of forming counterbored receptacles
US3452633A (en) Die set shank construction
US3588990A (en) Manufacturing technique of self-punch and self-clinch component assembly
US3461528A (en) Method of producing a rotary joint between at least two members having a rotationally symmetrical construction at the joint
US3269785A (en) Flanged bearing
US3504576A (en) Method for making precision die sets
US2330741A (en) Method of assembling retainers