US2328580A - Ruthenium alloy pen point - Google Patents

Ruthenium alloy pen point Download PDF

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Publication number
US2328580A
US2328580A US423693A US42369341A US2328580A US 2328580 A US2328580 A US 2328580A US 423693 A US423693 A US 423693A US 42369341 A US42369341 A US 42369341A US 2328580 A US2328580 A US 2328580A
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United States
Prior art keywords
ruthenium
alloy
pen point
platinum
ruthenium alloy
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US423693A
Inventor
Pickus Milton Robert
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Parker Pen Co
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Parker Pen Co
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Publication date
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Priority to US423693A priority Critical patent/US2328580A/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B43WRITING OR DRAWING IMPLEMENTS; BUREAU ACCESSORIES
    • B43KIMPLEMENTS FOR WRITING OR DRAWING
    • B43K1/00Nibs; Writing-points
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C5/00Alloys based on noble metals
    • C22C5/04Alloys based on a platinum group metal

Definitions

  • Pen points are subjected to very serious corrosion and erosion influences and as a result must be hard, wear resistant, and extremely resistant to chemical corrosion.
  • the platinum group of metals is known for the high melting points of the members and for their chemical inertness. As a result all of the metals of this group have been tried for pen point purposes. Up to the present time, however, osmium has been the platinum metal almost universally employed, although it has been used in combination with many others of the group.
  • Ruthenium has hitherto not been successfully employed as a major constituent of a pen point material, nor has it been employed in a binary alloy even in minor proportions.
  • ruthenium is employed in an amount of at least approximately 85% of the total, and may be utilized to as high a proportion as approximately 98%.
  • a further advantage of the present invention lies in the fact that ruthenium may be employed in a binary alloy in the proportions stated.
  • a preferred alloy comprises from 85% to 98% by weight of ruthenium and from 2% to 15% of platinum metal.
  • the platinum metal forms a matrix binding together the ruthenium. It has been found important that the alloy be prepared under such conditions that the matrix will not greatly exceed 15% of the total. For example, if an alloy is prepared using 85% ruthenium and 15% platinum, and the individual constituents are alloyed by fusion, a considerable proportion of ruthenium will dissolve in the platinum, thereby increasing to a great extent the amount of matrix material, and the resulting alloy will be brittle and unsatisfactory for pen point purposes. The same thing is true of an alloy comprising 90% ruthenium and 10% platinum. If the proportion of platinum is made low enough, however, and fusion is carried on with great care, it is possible to produce a satisfactory alloy by fusion. However, under commercial-conditions fusion has not been found to be a suitable method of producing the alloy.
  • the alloys of the present invention are, therefore, preferably produced by powder metallurgy processes in which the constituents are ground to a fine state of division, thoroughly intermingled, compressed under extremely high pres-.
  • the treating time and temperature may be. considerably altered, but care should be taken not to produce a temperature so high that excessive amounts of matrix will be formed. If the alloy becomes excessively brittle, the treating time or temperature, or both, should be reduced.
  • An alloy of ruthenium and 10% platinum is suitably produced in the same manner, in this case the sintering being for one hour at 2950 1.
  • An alloy of ruthenium and 5% platinum may satisfactorily be produced by the same method, employing two hours of sintering at The platinum may be replaced in part by other metals which do not modify the characteristics of the alloy, and the term fplatinum metal" has been used to indicate a platinum which may be so modified.
  • a pen point consisting essentially of a nonvbrittle ruthenium alloy including at least substantially 85% ruthenium, said alloy containing at least approximately 2% of other platinum group metal, said alloy being characterized by substantial freedom of the matrix thereof from ruthenium.
  • a pen point consisting essentially of a nonbrittle alloy including from 85% to 98% 0t ruthenium, and 2% to 15% of platinum, the matrix metal in said alloy being substantially free from ruthenium.
  • a ruthenium alloy including substantially 85% to 98% ruthenium, and 2% to 15% platinum metal, the matrix metal in said alloy being substantially free from ruthenium.
  • An alloy consisting essentially of 85% to 98% ruthenium and 2% to 15% of platinum, the matrix metal in said alloy being substantially free from ruthenium.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Powder Metallurgy (AREA)

Description

Patented Sept. 7, 1943 RUTHENIUM ALLOY PEN rom'r Milton Robert Pickus, Janesville, Wis., assignor to The Parker Pen Company, a corporation of Wisconsin No Drawing. Application December 19, 1941, Serial No. 423,693
8 Claims. (01. 75-112) l'his invention relates to a pen point composed essentially of ruthenium alloy.
Pen points are subjected to very serious corrosion and erosion influences and as a result must be hard, wear resistant, and extremely resistant to chemical corrosion.
The platinum group of metals is known for the high melting points of the members and for their chemical inertness. As a result all of the metals of this group have been tried for pen point purposes. Up to the present time, however, osmium has been the platinum metal almost universally employed, although it has been used in combination with many others of the group.
Ruthenium has hitherto not been successfully employed as a major constituent of a pen point material, nor has it been employed in a binary alloy even in minor proportions. The
reason for this apparently has been that ruthenium, when used in pen point alloys, produced an extremely brittle metal which could not be worked in the manner required of pen point materials.
It has now been discovered that a very satisfactory pen point may be produced by the use of ruthenium, provided the proportion of ruthenium in the alloy is extremely high and particularly if the presence of a substantial proportion of matrix metal is avoided.
In the alloy of the present invention ruthenium is employed in an amount of at least approximately 85% of the total, and may be utilized to as high a proportion as approximately 98%.
A further advantage of the present invention lies in the fact that ruthenium may be employed in a binary alloy in the proportions stated.
A preferred alloy comprises from 85% to 98% by weight of ruthenium and from 2% to 15% of platinum metal. The platinum metal forms a matrix binding together the ruthenium. It has been found important that the alloy be prepared under such conditions that the matrix will not greatly exceed 15% of the total. For example, if an alloy is prepared using 85% ruthenium and 15% platinum, and the individual constituents are alloyed by fusion, a considerable proportion of ruthenium will dissolve in the platinum, thereby increasing to a great extent the amount of matrix material, and the resulting alloy will be brittle and unsatisfactory for pen point purposes. The same thing is true of an alloy comprising 90% ruthenium and 10% platinum. If the proportion of platinum is made low enough, however, and fusion is carried on with great care, it is possible to produce a satisfactory alloy by fusion. However, under commercial-conditions fusion has not been found to be a suitable method of producing the alloy.
The alloys of the present invention are, therefore, preferably produced by powder metallurgy processes in which the constituents are ground to a fine state of division, thoroughly intermingled, compressed under extremely high pres-.
The treating time and temperature may be. considerably altered, but care should be taken not to produce a temperature so high that excessive amounts of matrix will be formed. If the alloy becomes excessively brittle, the treating time or temperature, or both, should be reduced. An alloy of ruthenium and 10% platinum is suitably produced in the same manner, in this case the sintering being for one hour at 2950 1. An alloy of ruthenium and 5% platinum may satisfactorily be produced by the same method, employing two hours of sintering at The platinum may be replaced in part by other metals which do not modify the characteristics of the alloy, and the term fplatinum metal" has been used to indicate a platinum which may be so modified.
The foregoing detailed'description has been given for clearness of understanding only,-and no unnecessary limitations should be understood therefrom.
What 1 claim as new, and desire to secure by Letters Patent, is:
1. A pen point consisting essentially of a nonvbrittle ruthenium alloy including at least substantially 85% ruthenium, said alloy containing at least approximately 2% of other platinum group metal, said alloy being characterized by substantial freedom of the matrix thereof from ruthenium.
2. A pen point as set forth in claim 1, in which the alloy includes a substantial proportion of platinum.
3. A pen point consisting essentially of a nonbrittle alloy including from 85% to 98% 0t ruthenium, and 2% to 15% of platinum, the matrix metal in said alloy being substantially free from ruthenium.
4. A ruthenium alloy including substantially 85% to 98% ruthenium, and 2% to 15% platinum metal, the matrix metal in said alloy being substantially free from ruthenium.
5. An alloy consisting essentially of 85% to 98% ruthenium and 2% to 15% of platinum, the matrix metal in said alloy being substantially free from ruthenium.
6. An alloy consisting essentially of 85%
US423693A 1941-12-19 1941-12-19 Ruthenium alloy pen point Expired - Lifetime US2328580A (en)

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Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2536124A (en) * 1946-10-11 1951-01-02 Bolvin Camille Marian Francois Writing instrument
US3278280A (en) * 1964-03-16 1966-10-11 Int Nickel Co Workable ruthenium alloy and process for producing the same
US3362799A (en) * 1964-05-13 1968-01-09 Int Nickel Co Ductile ruthenium alloy and process for producing the same
US3957451A (en) * 1974-08-02 1976-05-18 General Motors Corporation Ruthenium powder metal alloy
US3977841A (en) * 1974-08-02 1976-08-31 General Motors Corporation Ruthenium powder metal alloy and method for making same
US8436520B2 (en) 2010-07-29 2013-05-07 Federal-Mogul Ignition Company Electrode material for use with a spark plug
US8471451B2 (en) 2011-01-05 2013-06-25 Federal-Mogul Ignition Company Ruthenium-based electrode material for a spark plug
US8575830B2 (en) 2011-01-27 2013-11-05 Federal-Mogul Ignition Company Electrode material for a spark plug
US8760044B2 (en) 2011-02-22 2014-06-24 Federal-Mogul Ignition Company Electrode material for a spark plug
US8766519B2 (en) 2011-06-28 2014-07-01 Federal-Mogul Ignition Company Electrode material for a spark plug
US8890399B2 (en) 2012-05-22 2014-11-18 Federal-Mogul Ignition Company Method of making ruthenium-based material for spark plug electrode
US8979606B2 (en) 2012-06-26 2015-03-17 Federal-Mogul Ignition Company Method of manufacturing a ruthenium-based spark plug electrode material into a desired form and a ruthenium-based material for use in a spark plug
US10044172B2 (en) 2012-04-27 2018-08-07 Federal-Mogul Ignition Company Electrode for spark plug comprising ruthenium-based material

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2536124A (en) * 1946-10-11 1951-01-02 Bolvin Camille Marian Francois Writing instrument
US3278280A (en) * 1964-03-16 1966-10-11 Int Nickel Co Workable ruthenium alloy and process for producing the same
US3362799A (en) * 1964-05-13 1968-01-09 Int Nickel Co Ductile ruthenium alloy and process for producing the same
US3957451A (en) * 1974-08-02 1976-05-18 General Motors Corporation Ruthenium powder metal alloy
US3977841A (en) * 1974-08-02 1976-08-31 General Motors Corporation Ruthenium powder metal alloy and method for making same
US8436520B2 (en) 2010-07-29 2013-05-07 Federal-Mogul Ignition Company Electrode material for use with a spark plug
US8471451B2 (en) 2011-01-05 2013-06-25 Federal-Mogul Ignition Company Ruthenium-based electrode material for a spark plug
US8575830B2 (en) 2011-01-27 2013-11-05 Federal-Mogul Ignition Company Electrode material for a spark plug
US8760044B2 (en) 2011-02-22 2014-06-24 Federal-Mogul Ignition Company Electrode material for a spark plug
US8766519B2 (en) 2011-06-28 2014-07-01 Federal-Mogul Ignition Company Electrode material for a spark plug
US10044172B2 (en) 2012-04-27 2018-08-07 Federal-Mogul Ignition Company Electrode for spark plug comprising ruthenium-based material
US8890399B2 (en) 2012-05-22 2014-11-18 Federal-Mogul Ignition Company Method of making ruthenium-based material for spark plug electrode
US8979606B2 (en) 2012-06-26 2015-03-17 Federal-Mogul Ignition Company Method of manufacturing a ruthenium-based spark plug electrode material into a desired form and a ruthenium-based material for use in a spark plug

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