US1483018A - Method of producing composite bearings - Google Patents

Method of producing composite bearings Download PDF

Info

Publication number
US1483018A
US1483018A US503475A US50347521A US1483018A US 1483018 A US1483018 A US 1483018A US 503475 A US503475 A US 503475A US 50347521 A US50347521 A US 50347521A US 1483018 A US1483018 A US 1483018A
Authority
US
United States
Prior art keywords
core
liner
casting
studs
openings
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
US503475A
Inventor
George A Shoemaker
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.)
Bound Brook Oil Less Bearing Co
Original Assignee
Bound Brook Oil Less Bearing Co
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 Bound Brook Oil Less Bearing Co filed Critical Bound Brook Oil Less Bearing Co
Priority to US503475A priority Critical patent/US1483018A/en
Application granted granted Critical
Publication of US1483018A publication Critical patent/US1483018A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C9/00Moulds or cores; Moulding processes
    • B22C9/10Cores; Manufacture or installation of cores

Definitions

  • a further object is to provide an arrange- -ment and method of production, by which the radial studs, fins or webs, may be held in true radial relation and at the same time have undercut formation; that is, the forlarger body of metal at the inner most surface than at the point of juncture with the mainbody of the casting.
  • Figure 1 illustrates in section, a mould for a split bearing.
  • Figure 7 illustrates the method of indentlngthe core radially through the orifices of the liner.
  • Figure 8 is a cross sectional View of the parts shown in Figure 7.
  • Figure 9 is a longitudinal section through the complete mould with the core in place.
  • Figure 10 is a cross sectional view of the mould in Figure 9.
  • Figure 11 is a longitudinal View of a casting formed in said mould.
  • Figure 12 is a cross sectional view through the bearing illustrating a filling about the studs, fins or webs.
  • present invention overcomes these diiiiculties and provides for the casting of cylindrical or semi-cylindrical shells with any desired or required disposition of metal for the bearing surface.
  • numeral 1 denotes half of the mould box with a pattern imprint 52, formed in the sand 3.
  • a core box 4 In or er to provide a proper core for easting protuberances such as studs, fins or webs, a core box 4, is employed and within the core box is located a liner 5, which has openings therethrough, corresponding to the design of stud or other protuberance responding which it is desired to form on the inner surface of the final casting.
  • this liner 5 is represented as having stud openings 6, which are arranged in staggered relation and extending in lon' itudinal lines, with reference to the axis the liner.
  • This liner 5, with its pattern of openings is placed in the core box 4, and the core is then rammed up in the usual manner. Of course, the material of the core is forced into the openings 6.
  • the core box is inverted.
  • the core box 4, is removed and a suitable implement such as illustrated at 6*, having projections 7, corin arrangement to the openings 6, of the liner 5, is forced through the openings of the liner and into the core. This produces a series of pockets or depressions in the core.
  • the same core boxes and liners with different patterns may be made so that they will provide a means for producin'g different types of patterns or studs or fins on finished castings utilizin cores made in the same core boxes but wit different forms of liners,
  • the implement as illustrated, is shown in the form of a comb and has shoulders 8, which engage the outer surface of the liner and limitthe depth, to which the studs 7, are forced into the core.
  • Anydesired type of implement for effecting this result may be employed, for instance, each openin'g of the liner might be individually punched out, in place of using a comb, simultaneously punching out an entire longitudinal line of openings.
  • the liner 5 is removed and the core is then treated in the usual manner and applied to the mould imprint.
  • the pattern openings of the liner and removing the implement and linerto provide a core having openings radially disposed to the axis of the core and casting the metal about the core to provide protuberances about the inner wall thereof.

Description

Feb. 5 9 1924, 1,483,118
G. A. SHOEMAKER v METHOD OF PRODUCING COMPOSITE BEARINGS Filed Sept. 27. 1921 Em Mk [IV VENTOR 1 e14, kj/eoem aker Patented Feb. 5, 192
GEORGE A. SHOEMAKER, OF PHILADELPHIA, PENNSYLVANIA, ASSIGNOR TO BOUND BROOK OIL-LESS BEARING COMPANY, A CORPORATION OF NEW JERSEY.
" METHOD OF PRODUCING COMPOSITE BEARINGS.
Application filed September 27, 1921. Serial No. 503,475.
To all whom it may concern:
Be it known that I, GEORGE A. SHOE- MAKER, a citizen of the United States, and a resident of Philadelphia, in the county of Philadelphia and State of Pennsylvania,
have invented certain new and useful improvements in Methods of Producin Oompos1te Bearings, of which the following is a full, clear and exact description, whereby to anyone skilled in the art may make and use the same.
While the invention is termed a method of producing composite bearings, it actually relates to the art of casting hollow cylindrical bodies wherein it is desired to secure radial protuberance on the inner wall of the cast shell. A bearing such as hereinafter described is used as a means of illustrating the process or method inasmuch as it forms a good example of the advantages attained.
' It has been a usual practice, in casting cylindrical or semicyhndrical bodies having rotuberances such as studs, fins or webs on t eir inner wall, to employ cores. These re cores, of necessity have been so formed that the could be withdrawn from the core box an as a result it has been quite impossible to secure radially dis osed studs, fins or webs.
It is the principa object of the present invention to provide cores which wlll produce, in the operation of casting, radially disposed studs, fins or webs which may be employed for any useful purpose and which are particularly well adapted for use in the casting of bearings.
A further object is to provide an arrange- -ment and method of production, by which the radial studs, fins or webs, may be held in true radial relation and at the same time have undercut formation; that is, the forlarger body of metal at the inner most surface than at the point of juncture with the mainbody of the casting.
Referring to the drawings Figure 1, illustrates in section, a mould for a split bearing.
core box with the liner in place.
mation of-the studs, fins or webs with a Figure 6, illustrates the core box inverted and partially removed.
Figure 7, illustrates the method of indentlngthe core radially through the orifices of the liner.
Figure 8, is a cross sectional View of the parts shown in Figure 7.
Figure 9, is a longitudinal section through the complete mould with the core in place.
Figure 10, is a cross sectional view of the mould in Figure 9.
Figure 11, is a longitudinal View of a casting formed in said mould.
Figure 12, is a cross sectional view through the bearing illustrating a filling about the studs, fins or webs.
It has been a common practice in casting bearings to provide cores with protuberances of various forms which, when employed in casting the bearing shell, produce sockets or pockets or grooves of various forms, which serve as retainers for a lubrieating metal or a lubricating compound.
Considerable difiiculty has attended the formation of these cores, with anything approaching true radial formation of the pockets. The reason for this, is obvious, as it is quite impossible to fashion a core box, which can give radial walls to the pockets. Relief has had to be provided for separating the core from its pockets, even where, multipart core boxeshave been em loyed.
As a result, accurate disposition of metal be withdrawn from the core and for a device such as a bearing could not be secured. As hereinafter explained, the
present invention overcomes these diiiiculties and provides for the casting of cylindrical or semi-cylindrical shells with any desired or required disposition of metal for the bearing surface.
It is to be understood, that the invention is not confined necessarily to bearings, as it may be employed in casting any structure where the radlal projections are. desirable.
In the accompanying drawings, numeral 1, denotes half of the mould box with a pattern imprint 52, formed in the sand 3.
In or er to provide a proper core for easting protuberances such as studs, fins or webs, a core box 4, is employed and within the core box is located a liner 5, which has openings therethrough, corresponding to the design of stud or other protuberance responding which it is desired to form on the inner surface of the final casting.
As illustrated in the drawings, this liner 5, is represented as having stud openings 6, which are arranged in staggered relation and extending in lon' itudinal lines, with reference to the axis the liner.
This liner 5, with its pattern of openings is placed in the core box 4, and the core is then rammed up in the usual manner. Of course, the material of the core is forced into the openings 6. When finally rammed, the core box is inverted. The core box 4, is removed and a suitable implement such as illustrated at 6*, having projections 7, corin arrangement to the openings 6, of the liner 5, is forced through the openings of the liner and into the core. This produces a series of pockets or depressions in the core.
By utilizing the liner 5, it is apparent that a very simple and effective arrangement is provided for giving any desired pattern and arrangement of studs or fins on the interior diameter of the casting.
The same core boxes and liners with different patterns may be made so that they will provide a means for producin'g different types of patterns or studs or fins on finished castings utilizin cores made in the same core boxes but wit different forms of liners,
The implement, as illustrated, is shown in the form of a comb and has shoulders 8, which engage the outer surface of the liner and limitthe depth, to which the studs 7, are forced into the core. Anydesired type of implement for effecting this result may be employed, for instance, each openin'g of the liner might be individually punched out, in place of using a comb, simultaneously punching out an entire longitudinal line of openings.
After the comb or other implement has been applied to form the pockets or indentations in the core, the liner 5, is removed and the core is then treated in the usual manner and applied to the mould imprint.
The casting operation is, of course, such as may be preferred under any given practice and when the metal has flown to the mould and core, the resultant product is such as illustrated in the drawings in Figures 11 and 12, wherein a half bearing is shown with radially disposed studs.
If it is desired to give an undercut formation to the studs, the comb 6 or other suitable implement may be'moved laterally after insertion through the openings of the liner 5, and this will press back the core material so that studs or protuberances will be formed, having a wider face at the in= nermost diameter than at the point of juncture with the main body of the casting.
In Figure 11, this arrangement of radial may be employed ramming said core mama studs is clearly indicated and the purpose of forming studs for bearings is illustrated in Figure 12. In said figure, the studs are shown as surrounded with a bearing "material 9, which may be of any desired composition suitable for producing lubrication or may be a bearing metal suitably cast into the shell.
What I claimas my invention and desire to secure by Letters Patent is:
1. A core for casting hollow cylindrical or 'semicylindrical bodies havingradial openings therein to provide radial studs or protuberances on the inner face of the casting, said radial openings of the core being formed by displacing the material of the core through openings in a liner arranged within the core box while filling and ramming the core.
2. The method of'casting radial protuberances on the inner walls of a cylindrical body which consists in inserting a perforated pattern liner in the core box, filling and ramming said core box with the core material, removin the core box and depressing the core throug the openings of the attern of the liner, removing said liner an utilizing the core in the pattern. print of the mould to cast a hollow-cylindrical body having protuberances on its inner wall. x
3. The method or process of producing protuberances on the inner walls of a cylin drical or semi-cylindrical body which con-v sists in placing a perforated pattern liner within a core box ramming said corebox with a core material, removlng the core box and inserting an implement through the pattern openings of the liner and moving said implement, after insertion, to provide openings in the core havin a greater area adjacent "to the axis of the core than at the surface thereof, removing the implement and liner and casting about the core to provide rotuberances on the inner wall of the cylin rical or semi-cylindrical body.
4. The method of producing protuberances upon the inner walls of cast bodies of cylindrical or semi-cylindrical form which consists in inserting a liner, having a definite perforated pattern, within the core box, box with its inserted liner, inverting the core box and removing the same to give access to the outer surface of the liner, inserting an implement through;
the pattern openings of the liner and removing the implement and linerto provide a core having openings radially disposed to the axis of the core and casting the metal about the core to provide protuberances about the inner wall thereof.
GEO. A. SHOEMAKER. Witnesses:
GEO. O. SMALLEY,
. 10m 0. Jomvsox.
US503475A 1921-09-27 1921-09-27 Method of producing composite bearings Expired - Lifetime US1483018A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US503475A US1483018A (en) 1921-09-27 1921-09-27 Method of producing composite bearings

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US503475A US1483018A (en) 1921-09-27 1921-09-27 Method of producing composite bearings

Publications (1)

Publication Number Publication Date
US1483018A true US1483018A (en) 1924-02-05

Family

ID=24002249

Family Applications (1)

Application Number Title Priority Date Filing Date
US503475A Expired - Lifetime US1483018A (en) 1921-09-27 1921-09-27 Method of producing composite bearings

Country Status (1)

Country Link
US (1) US1483018A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3954132A (en) * 1973-06-22 1976-05-04 Selly Oak Diecastings Limited Manufacture of cast ferrous metal dies

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3954132A (en) * 1973-06-22 1976-05-04 Selly Oak Diecastings Limited Manufacture of cast ferrous metal dies

Similar Documents

Publication Publication Date Title
US6634410B1 (en) Mold apparatus and method
DE112005002155T5 (en) Cylinder bore bushings for cast engine cylinder blocks
US1483018A (en) Method of producing composite bearings
US1874503A (en) Extrusion die
US2042015A (en) Apparatus for casting sleeve-like bodies
US1535330A (en) Method of centrifugal casting
US1815344A (en) Bushing bearing and method of making it
JPS619959A (en) Casting method of hollow shaft
US2033093A (en) Manufacture of piston rings
US2368718A (en) Method of making molds having accommodation cores
US1726902A (en) Apparatus for casting bearings
US1891867A (en) Method of producing castings with tapped holes therein
US2078562A (en) Casting
US2962777A (en) Method of and means for making castings
US1597428A (en) Bearing and method of making it
US1357503A (en) Process of making dies
US2838961A (en) Method of making dies
US1851934A (en) Bearing liner or sleeve
JPS5834229A (en) Manufacturing method of bearing
DE477287C (en) Process for the production of composite castings, in particular of rolls with a large surface hardness
US3263288A (en) Method of casting cored objects
DE112014006831T5 (en) Set of molds, method for manufacturing and housing of rotating electrical machines
US1892175A (en) Method of making bearing sleeves
US1059954A (en) Process of making self-lubricating journals.
US2755528A (en) Apparatus and method for the casting of shaped articles or machine parts