US3627515A - Engine component steel containing small amounts of chromium and nickel - Google Patents

Engine component steel containing small amounts of chromium and nickel Download PDF

Info

Publication number
US3627515A
US3627515A US37015A US3627515DA US3627515A US 3627515 A US3627515 A US 3627515A US 37015 A US37015 A US 37015A US 3627515D A US3627515D A US 3627515DA US 3627515 A US3627515 A US 3627515A
Authority
US
United States
Prior art keywords
engine component
chromium
nickel
small amounts
steel containing
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
US37015A
Inventor
Kenneth E Kueny
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.)
Johnson Products Inc
Original Assignee
Johnson Products Inc
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 Johnson Products Inc filed Critical Johnson Products Inc
Application granted granted Critical
Publication of US3627515A publication Critical patent/US3627515A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L3/00Lift-valve, i.e. cut-off apparatus with closure members having at least a component of their opening and closing motion perpendicular to the closing faces; Parts or accessories thereof
    • F01L3/02Selecting particular materials for valve-members or valve-seats; Valve-members or valve-seats composed of two or more materials
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L7/00Rotary or oscillatory slide valve-gear or valve arrangements

Definitions

  • This invention relates to engine components, and more particularly to engine components having greatly superior wearability.
  • Element Percent by weight Total carbon 3.00-3.60 Silicon 2.00-3.00 Manganese 0.70-1.25 Phosphorous a 0.20 max. Sulfur a 0.10 max. Nickel 0.15-0.70 Chromium 0.40-l.25 Molybdenum 0 -070 Titanium 0 10-100 Tungsten O.50-l0.0 Iron Balance Impurity.
  • the controlled percentages of titanium and tungsten are essential to the composition. It is by carefully controlling the composition to this range that the surprisingly high wearability results.
  • Element Percent by weight Total carbon 3.50 Silicon 2.42 Manganese 0.82 Phosphorous a 0.09 Sulfur a 0.03 Nickel 0.21 Chromium 0.72 Molybdenum 0.34 Titanium 0.19 Tungsten 3.20 Iron Balance Impurity.
  • the complete engine component e.g. tappet, camshaft, rocker arm, or other
  • the complete engine component is formed of the novel alloy, but at least the bearing surfaces thereof are of the novel alloy.
  • the components may be cast by normal casting techniques wherein the material is melted by any standard melting method, then poured into suitable molds, such as sand molds, shell molds, carbon dioxide molds, or permanent molds, with or without chill plates as of carbon. It may be hardened by normal heat training techniques such as those conventionally used on hardenable iron for such components, a typical heat treatment including heating to 1575 F., holding forthirty minutes, then quenching in oil. It is conceivable that minor variations may be made within the concept presented, with the invent-ion being limited only by the scope of the appended claims and the reasonable equivalents thereto.
  • An internal combustion engine component comprising a body having at least a bearing surface of a hardenable ferrous alloy consisting essentially of the following composition:
  • the component of claim 1 being a tappet.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Valve-Gear Or Valve Arrangements (AREA)

Abstract

AN INTERNAL COMBUSTION ENGINE COMPONENT HAVING AT LEAST THE BEARING SURFACE OF A HARDENABLE FERROUS ALLOY CONTAINING BOTH TITANIUM AND TUNGSTEN IN CONTROLLED RANGES GIVING SYNERGISTIC RESULTS IN WEARABILITY.

Description

United States Patent Ofice ENGINE COMPONENT STEEL CONTAINING SMALL AMOUNTS OF CHROMIUM AND NICKEL Kenneth E. Kueny, North Muskegon, Mich., assignor to Johnson Products Inc., Muskegon, Mich. No Drawing. Filed May 7, 1970, Ser. No. 37,015 Int. Cl. C22c 39/20 US. Cl. 75-128 5 Claims ABSTRACT OF THE DISCLOSURE An internal combustion engine component having at least the bearing surface of a hardenable ferrous alloy containing both titanium and tungsten in controlled ranges giving synergistic results in wearability.
BACKGROUND OF THE INVENTION This invention relates to engine components, and more particularly to engine components having greatly superior wearability.
In my Patent 3,370,941 is disclosed a tungsten containing cast iron alloy having beneficial hardness qualities. This alloy has demonstrated markedly better characteristics compared to conventional hardenable iron, for high compression engines.
Consequently, this material has proven to be a significant advance in the auto industry.
SUMMARY OF THE INVENTION Subsequent to the invention in the above noted patent, it was discovered that by the addition of a controlled amount of titanium to the novel tungsten alloy, with modification of this alloy to controlled component ranges, unique synergistic wearabality results occur. The novel alloy is extremely effective in high compression engines. Its wearability is unexpectedly three times greater than even the alloy of the above mentioned patent, hence many times greater than conventional hardenable iron. Although my Patent 3,472,651 teaches of a titanium containing hardenable iron, it was never guessed that the controlled incorporation of titanium and tungsten would have the synergistic results experienced.
It therefore is an object of this invention to provide an engine component material having highly unusual wearability, many times greater than hardenable iron, yet capable of being readily founded by casting into sand molds, shell molds, CO molds or permanent molds. It has been found particularly useful for components such as tappets and camshafts, but can be used for others where friction wear is a problem.
DESCRIPTION OF THE PREFERRED EMBODIMENTS Basically the engine component alloy is a hardenable iron composition as follows:
Element: Percent by weight Total carbon 3.00-3.60 Silicon 2.00-3.00 Manganese 0.70-1.25 Phosphorous a 0.20 max. Sulfur a 0.10 max. Nickel 0.15-0.70 Chromium 0.40-l.25 Molybdenum 0 -070 Titanium 0 10-100 Tungsten O.50-l0.0 Iron Balance Impurity.
Patented Dec. 14, 1971 The phosphorous and sulfur elements are normal impurities which are almost invariably present in these ferrous alloys. They are not required.
The controlled percentages of titanium and tungsten are essential to the composition. It is by carefully controlling the composition to this range that the surprisingly high wearability results.
A preferred specific composition in the above noted range is as follows:
Element: Percent by weight Total carbon 3.50 Silicon 2.42 Manganese 0.82 Phosphorous a 0.09 Sulfur a 0.03 Nickel 0.21 Chromium 0.72 Molybdenum 0.34 Titanium 0.19 Tungsten 3.20 Iron Balance Impurity.
This composition, when tested for tappets and camshafts, for example, showed an excellent initial and retained hardness and demonstrated a wearability unexpectedly three times greater than the tungsten bearing hardenable iron alloy in the above identified Patent 3,370,941. Since such tungsten alloy has hardness and wearability characteristics markedly greater than conventional hardenable iron alloys, the value of these present synergistic results are clearly evident. The material retains its hardness at greatly elevated temperatures, even up to about 900 F.
Preferably the complete engine component, e.g. tappet, camshaft, rocker arm, or other, is formed of the novel alloy, but at least the bearing surfaces thereof are of the novel alloy.
The components may be cast by normal casting techniques wherein the material is melted by any standard melting method, then poured into suitable molds, such as sand molds, shell molds, carbon dioxide molds, or permanent molds, with or without chill plates as of carbon. It may be hardened by normal heat training techniques such as those conventionally used on hardenable iron for such components, a typical heat treatment including heating to 1575 F., holding forthirty minutes, then quenching in oil. It is conceivable that minor variations may be made within the concept presented, with the invent-ion being limited only by the scope of the appended claims and the reasonable equivalents thereto.
The embodiments of the invention in which an exclusive property or privilege is claimed are defined as follows.
1. An internal combustion engine component comprising a body having at least a bearing surface of a hardenable ferrous alloy consisting essentially of the following composition:
phorous impurities) Balance 2. The component of claim 1 being a tappet.
3. The component in claim 1 being a camshaft.
4. The component in claim 1 being a rocker arm.
5. The component in claim 1 substantially of the following composition:
Element: Percent by weight Carbon 3.50 Silicon 2.42 Manganese 0.82 Nickel 0.21
Chromium 0.72
Molybdenum 0.34 Titanium 3.20
Tungsten 0.19
Iron (plus minor sulfur and phosphorous impurities) Balance References Cited UNITED STATES PATENTS 10 HYLAND BIZOT, Primary Examiner PMOSO STATES PATENT @FFTCE @EETTTTQATE QT @QRREQTTGN- Patent Non 3,627,515 Dated December 14, 1971 n i l Kenneth E. Kueny It ceriii'iwji that error appears in the above-identified patent e124; than; said Letters Patent are hereby corrected as shown below:
Claim 5, line 11; delete 5;:20 and insert "0.19"
line 12; delete 0.19 and insert "3.20".
Signed and sealed this 15th day of January 197M.
( SEAL) Attest:
EDWARD M. FLEI'CHER,JR. RENE Da TEG-TMEYER Attest'ing Officer Acting Commissioner of Patents
US37015A 1970-05-07 1970-05-07 Engine component steel containing small amounts of chromium and nickel Expired - Lifetime US3627515A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US3701570A 1970-05-07 1970-05-07

Publications (1)

Publication Number Publication Date
US3627515A true US3627515A (en) 1971-12-14

Family

ID=21891980

Family Applications (1)

Application Number Title Priority Date Filing Date
US37015A Expired - Lifetime US3627515A (en) 1970-05-07 1970-05-07 Engine component steel containing small amounts of chromium and nickel

Country Status (5)

Country Link
US (1) US3627515A (en)
CA (1) CA951546A (en)
DE (1) DE2100653A1 (en)
FR (1) FR2089272A5 (en)
GB (1) GB1288183A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4124413A (en) * 1974-03-18 1978-11-07 Toyota Jidosha Kogyo Kabushiki Kaisha Wear and pitting resistant cast iron
US4153017A (en) * 1977-05-16 1979-05-08 Stanadyne, Inc. Alloyed chilled iron

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6483804A (en) * 1987-09-25 1989-03-29 Mazda Motor Tappet valve mechanism for engine

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3502058A (en) * 1966-02-24 1970-03-24 Earl A Thompson Rocker arm

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4124413A (en) * 1974-03-18 1978-11-07 Toyota Jidosha Kogyo Kabushiki Kaisha Wear and pitting resistant cast iron
US4153017A (en) * 1977-05-16 1979-05-08 Stanadyne, Inc. Alloyed chilled iron

Also Published As

Publication number Publication date
DE2100653A1 (en) 1971-11-25
FR2089272A5 (en) 1972-01-07
GB1288183A (en) 1972-09-06
CA951546A (en) 1974-07-23

Similar Documents

Publication Publication Date Title
US4435226A (en) Wear resistant cast iron alloy with spheroidal graphite separation and manufacturing method therefor
JPH0431018B2 (en)
US3627515A (en) Engine component steel containing small amounts of chromium and nickel
US3370941A (en) Tungsten-containing alloy cast iron useful for internal combustion engine parts
US3086858A (en) Hard cast alloy
US4482396A (en) Method for making pitting resistant cast iron product
US3472651A (en) Engine components of cast iron having ni,cr,and ti as alloying elements
JPS6365056A (en) Wear resistant sintered iron alloy
US3998664A (en) Cast iron
US4032334A (en) Tappet metallurgy
US2827373A (en) Ni-cr-co-mo valve seat insert
JPS5839907B2 (en) Surface damage resistant alloy cast iron
JPH0285338A (en) Ferrous sintered sliding material
US1542440A (en) Iron alloy
US1762109A (en) Cast-iron alloy
US2804414A (en) Chill iron alloy castings
US1587994A (en) Composition of matter for alloy of metals
SU897115A3 (en) Method of alloying iron-based alloy articles
JPS6024174B2 (en) Fe-based sintered alloy for valve seats
US3165401A (en) Alloy steel for cast parts resistant to high temperatures and corrosion
JPS597003B2 (en) Valve mechanism for internal combustion engines
US1533782A (en) Valve for internal-combustion engines
US3738829A (en) Nickel alloy for automotive valve seats
JPS60204843A (en) Manufacture of wear-resistant and lightweight rocker arm
US2174281A (en) Ferrous alloy