US1741733A - Alloy - Google Patents

Alloy Download PDF

Info

Publication number
US1741733A
US1741733A US138812A US13881226A US1741733A US 1741733 A US1741733 A US 1741733A US 138812 A US138812 A US 138812A US 13881226 A US13881226 A US 13881226A US 1741733 A US1741733 A US 1741733A
Authority
US
United States
Prior art keywords
per cent
lead
mercury
tin
copper
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
US138812A
Inventor
John V O Palm
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.)
Cleveland Graphite Bronze Co
Original Assignee
Cleveland Graphite Bronze 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 Cleveland Graphite Bronze Co filed Critical Cleveland Graphite Bronze Co
Priority to US138812A priority Critical patent/US1741733A/en
Application granted granted Critical
Publication of US1741733A publication Critical patent/US1741733A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C11/00Alloys based on lead
    • C22C11/06Alloys based on lead with tin as the next major constituent

Definitions

  • lhe present invention relating, as indicated, to alloys is particularly directed to a lead babbitt composition having properties and physical characteristics comparable to that of standard babbitt, but costing considerable less to manufacture.
  • a further object of the invention is the provision of'a lead babbitt composition having high ductility be worked by rolling and otherwise for the purpose of applying it to other metal articles as a surface bearing material, or to be rolled and formed intobearings and similar articles.
  • My improved composition consists of lead in a predominating amount with smaller amounts of copper, tin, mercury and anti-. mony.
  • I employ lead in an amount equal to 70 to 7 5 per cent of the total composition, copper to the extent of 5 or 6 per cent, tin about 12 per cent, mercury about 4 per cent and antimony from4 to 8 per cent. If a higher ductility is required the amount of antimony is reduced.
  • the above composition is entirely comparable in its physical properties toa standard babbitt and is approximately 50 per cent cheaper to manufacture. It is of course to be understood that the" specific proportion of ingredients referred to above may be varied within a. reasonable range without departing from the spirit of this invention. It also possesses.
  • a bearing alloy consisting of'70 to 75 per cent of lead, approximately 5 per cent copper, 12 per cent tin, 4 per cent mercury and 4 to 8 per cent of antimony.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Manufacture And Refinement Of Metals (AREA)

Description

permitting it to I plisliinent of the Patented Dec. 31, 1929 UNITED STATES PATENT, OFFICE JOHN V. 50. BALM, OF CLEVELAND fiEIGHT S, OHIO, ASSIGNOR TO THE CLEVELAND GRAPHITE BRONZE COMPANY,-OI CLEVELAND, OHIO, A CORPORATION OF OHIO ALLOY lt'o Drawing.
lhe present invention relating, as indicated, to alloys is particularly directed to a lead babbitt composition having properties and physical characteristics comparable to that of standard babbitt, but costing considerable less to manufacture. A further object of the invention is the provision of'a lead babbitt composition having high ductility be worked by rolling and otherwise for the purpose of applying it to other metal articles as a surface bearing material, or to be rolled and formed intobearings and similar articles. To the accomforegoing and related ends, said invention, then, consists of the means hereinafter fully described and particularly pointed out in the claims.
The following description sets forth in detail one approved combination of ingredients and method of making same embodying my invention, such disclosed ingredients'and procedure constituting, however, but one of various forms in which the principle of the invention may be used.
My improved composition consists of lead in a predominating amount with smaller amounts of copper, tin, mercury and anti-. mony. In a preferred embodiment of the invention I employ lead in an amount equal to 70 to 7 5 per cent of the total composition, copper to the extent of 5 or 6 per cent, tin about 12 per cent, mercury about 4 per cent and antimony from4 to 8 per cent. If a higher ductility is required the amount of antimony is reduced. The above composition is entirely comparable in its physical properties toa standard babbitt and is approximately 50 per cent cheaper to manufacture. It is of course to be understood that the" specific proportion of ingredients referred to above may be varied within a. reasonable range without departing from the spirit of this invention. It also possesses. the important property of not obtaining its full tensile strength and hardness for approximately 24 hours after casting, and it is possible that there is some amalgamating action occurring during this period by reason of the mercury content, which acts to reduce the size ofthe crystals and gives the same effect as .in cast- A iplication filed September 30, 1926. Serial No- 138,812.
ing an ordinary babbitt against a cold mold.
In my present composition I first mix copper and tin and to this molten composition add the antimony and subsequently the mercury and lead. For convenience the copper and tin are ordinarily alloyed first, as are the mercury and the lead.
Other modes of applying the principle of my invention may be employed instead of the one explained, change being made as regards the process herein disclosed or the materials employed in carrying out the process, provided the ingredient or ingredients stated by any of the following claims or the equivalent of such ingredient or ingredients be employed.
I therefore particularly point out and distipctly claim as my invention 1. A bearing alloy consisting of'70 to 75 per cent of lead, approximately 5 per cent copper, 12 per cent tin, 4 per cent mercury and 4 to 8 per cent of antimony.
2. An alloy consisting of 7 O to 75 per cent of lead, 5 to 6 per cent of copper, antimony 4 to 8 per cent, mercury approximately 4 per cent and the balance of tin.
Signed by me, this 28th day of September,
US138812A 1926-09-30 1926-09-30 Alloy Expired - Lifetime US1741733A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US138812A US1741733A (en) 1926-09-30 1926-09-30 Alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US138812A US1741733A (en) 1926-09-30 1926-09-30 Alloy

Publications (1)

Publication Number Publication Date
US1741733A true US1741733A (en) 1929-12-31

Family

ID=22483768

Family Applications (1)

Application Number Title Priority Date Filing Date
US138812A Expired - Lifetime US1741733A (en) 1926-09-30 1926-09-30 Alloy

Country Status (1)

Country Link
US (1) US1741733A (en)

Similar Documents

Publication Publication Date Title
US2128955A (en) Hot workable phosphor bronze
US1928747A (en) Nonferrous alloy
US2229463A (en) Alloy
US1741733A (en) Alloy
US2134905A (en) Manufacture of cast iron
US2105945A (en) Hot workable bronze
US3201234A (en) Alloy and method of producing the same
US2400566A (en) Alloy
US1016549A (en) Iron-nickel-copper alloy.
US2098081A (en) Aluminum alloy
US1932843A (en) Aluminum alloys
US1937465A (en) Bearing
US2144279A (en) Alloy
US1869378A (en) Britannia metal or pewter alloy
US1360347A (en) Lead alloy
US1745721A (en) Bearing metal
US2107223A (en) Bearing metal alloy
US1898390A (en) Chilled iron roll
US2105652A (en) Steel for permanent magnets
US1667641A (en) Bearing alloy
US933139A (en) Antifriction alloy.
US1518321A (en) Aluminum alloy
US1975112A (en) Beryllium alloy
US2210504A (en) Lead alloy bearing metal
US1932846A (en) Aluminum alloys