US3795510A - Valve components - Google Patents

Valve components Download PDF

Info

Publication number
US3795510A
US3795510A US00777557A US3795510DA US3795510A US 3795510 A US3795510 A US 3795510A US 00777557 A US00777557 A US 00777557A US 3795510D A US3795510D A US 3795510DA US 3795510 A US3795510 A US 3795510A
Authority
US
United States
Prior art keywords
alloys
iron
valve components
titanium
valve
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
US00777557A
Inventor
R Davies
T Johnston
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.)
Ford Motor Co
Original Assignee
Ford Motor 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 Ford Motor Co filed Critical Ford Motor Co
Application granted granted Critical
Publication of US3795510A publication Critical patent/US3795510A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/03Alloys based on nickel or cobalt based on nickel
    • C22C19/05Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/058Alloys based on nickel or cobalt based on nickel with chromium without Mo and W
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • General Engineering & Computer Science (AREA)
  • Powder Metallurgy (AREA)
  • Heat Treatment Of Steel (AREA)
  • Lift Valve (AREA)

Abstract

THIS INVENTION RELATES TO INTERNAL COMBUSTION ENGINE VALVE SYSTEM COMPONENTS WHICH ARE EXPOSED TO EXHAUST GAS AND MUST BE RESISTANT TO OXIDATION, SULFIDATION AND THE EFFECTS OF LEAD COMPOUNDS AT HIGH TEMPERATURES. A TYPICAL COMPOSITION OF SUCH A COMPONENT IS 20% CHROMIUM, 5.5% ALUMINUM, 2.5% TITANIUM, 7.5% IRON, 0.15% CARBON, REMAINDER NICKEL.

Description

March 5, 1974 DAVlEs ETAL 3,795,510
VALVE COMPONENTS Filed Nov. 21 1968 4 Sheets-Sheet 1 i W How W .0 l S83E18 O'IHIA RICHARD G DAV/ES THOMAS L. JOHNSTON INVENTORS' y W ATTORNEYS March 5, 1974 DAVlEs ETAL VALVE COMPONENTS 4 Sheets-Sheet 2 Filed Nov. 21 1968 m fir E WM N M Z J T 2 & T 0 A PM E A C0 NA /H S 00 RT m M L N L A R E H T 0 FORD ALLOY- AS CAST "moo 750 FIG. 2
w m m m m a s 4 z 0 0; G E0000; wmDOI OO 2 wmfiEhDm mom mwmmkm March 5, 1974 DAVIES EI'AL 3,795,510
VALVE COMPONENTS Filed Nov. 21 1968 4 Sheets-Sheet 5 25 PbO CRUCIBLE TEST AT 1675" F &
C i mmw uwfim wan" H m N "mun FIG.3
O 2 w v w 5 O March 5, 1974 w s ETAL VALVE COMPONENTS 4 Sheets-Sheet &
Filed Nov. 21
WEIGHT PERCENT IRON FIG. 4
RICHARD 6. DA V/ES THOMAS L. JOHNSTON INVENTORS 3,795,510 VALVE COMPONENTS Richard G. Davies, Dearborn, and Thomas L. Johnston,
Bloomfield Hills, Mich., assignors to Ford Motor Company, Dearborn, Mich.
Filed Nov. 21, 1968, Ser. No. 777,557 Int. Cl. C22c 19/00; F01i 3/.02
US. Cl. 75-171 1 Claim United States Patent 3,795,510 Patented Mar. 5, 1974 "Ice sure. This resistance to lead compound attack is a critical parameter for metals exposed to hot exhaust gas from leaded gasoline.
FIG. 4 has been presented to demonstate that the iron content of the claimed alloys can be increased to about 14% without loss of resistance to lead compound attack. This is economically important as it enables the alloy to be fabricated from more economical alloys such as ferrochromium and ferro-titanium. Iron is, of course, per se the cheapest constituent of the alloy. ABSTRACT OF THE DISCLOSURE It is important that these alloys have the maximum This invention relates to internal combustion engine possible amount of gamma prime dissolved in a gamma valve system components which are exposed to exhaust matrix at operating temperature; The amount of gamma gas and must be resistant to oxidation, sulfidation and prime should be at least twenty percent. The presence of the effects of lead compounds at high temperatures. A the titanium in this alloy permits this particular structure typical composition of such a component is chroto be obtained. mium, 5.5% aluminum, 2.5% titanium, 7.5% iron, 0.15% The following table is presented to illustrate the resistcarbon, remainder nickel. ance of a variety of alloys to attack by molten lead oxide.
This invention is predicated upon the discovery that 20 certain quaternary alloys of nickel, chromium, aluminum and titanium possess a combination of qualities highly TABLE 11 desirable in internal combustion engine valve components Composition wt percent Ba1ance Ni which are exposed to exhaust gas and must be resistant to oxidation, sufidation and the efiects of lead compounds 5,235?) at high temperatures. Cr e Al Ti dc l s- Attention is invited to a scholarly dissertation upon the 20 7,1 267 properties of this general type of alloys published in Journal of Metals, October 1956 at pages 1356 to 136 2 2 2 2 by A. Taylor. We have discovered that certain nickel 20 base, chromium, aluminum titanium alloys altered with a 338 $3 {3 as much as 14% iron are particularly attractive as internal 16 combustion engine valve system components. Particular i2 &8 $18 ;;2 reference is had to poppet valve heads and valve seat inserts, both of which are subject to the action of hot ex- 5; i318 21 haust gas contaminated with lead compounds. These alloys 22 4 0 9 are used in the as-cast condition. The cast poppet valve 2 212 jg heads were frictionally welded to a carbon steel valve from to economize the expensive alloying ingredients in the Nom'wAnanoys mmamwls head.
To document the properties of the alloys described in this specification, a typical such alloy designated V270 has been compared in detail with four other commercially We claim as our invention: popular and available high temperature alloys, one an 1. The as-cast nickel base internal combustion engine iron base alloy and the other three nickel base alloys. valve system component consisting essentially of 20% The chemical composition of these alloys are given on the chromium, 5.5% aluminum, 2.5% titanium, 7.5 iron, following table. 0.15% carbon, remainder nickel.
TABLE I Composition of- Alloy C N Mn Cr Co Mo Nb Fe Ti Al Ni Nimonic 80A.-. 0.06 0.10 19.5 1.1 2.5 1.3 Balance Inconel X750..- 0.04 0.70 15.0 .5 0.8 Balance 21-4N 0.53 0.40 9 0 21.0 3.75 lnco 7l3 0.12 12.5 Balance V270 0.15 20 Balance FIG. =1 has been presented to graphically illustrate the superior properties of the claimed alloys as compared to three popular competitive high temperature alloys. Note that the showing to the left of FIG. 1 relates to yield stress at room temperature While the showing to the right is at the much more critical temperature of 1600 R, which is approximately the maximum temperature now contemplated in internal combustion engine valve system components.
FIG. 2 is a comparable showing and relates to the stress required for rupture in 100 hours at 1600" F. The superior properties of the claimed alloys are clearly apparent insofar as creep rupture is concerned.
FIG. 3 relates to the resistance of the alloys to attack by hot lead compounds and is reported in weight loss of a standard specimen in grams per dcm. per hour of expo- References Cited UNITED STATES PATENTS 2,515,185 7/1950 Bieber et al. -171 2,766,455 10/1956 Betteridge et al. 75-171 X 3,145,124 8/1964 Hignett et a1 148-162 3,147,155 9/1964 Lamb 148-162 X FOREIGN PATENTS 493,718 6/1953 Canada 75-171 CHARLES N. LOVELL, Primary Examiner U.S. Cl. X.R.
US00777557A 1968-11-21 1968-11-21 Valve components Expired - Lifetime US3795510A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US77755768A 1968-11-21 1968-11-21

Publications (1)

Publication Number Publication Date
US3795510A true US3795510A (en) 1974-03-05

Family

ID=25110579

Family Applications (1)

Application Number Title Priority Date Filing Date
US00777557A Expired - Lifetime US3795510A (en) 1968-11-21 1968-11-21 Valve components

Country Status (4)

Country Link
US (1) US3795510A (en)
JP (1) JPS5415248B1 (en)
DE (1) DE1957823A1 (en)
GB (1) GB1227730A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4741080A (en) * 1987-02-20 1988-05-03 Eaton Corporation Process for providing valve members having varied microstructure
US4783966A (en) * 1987-09-01 1988-11-15 Aldrich Clare A Multi-staged internal combustion engine
EP0639652A1 (en) * 1993-07-27 1995-02-22 Ngk Insulators, Ltd. Ni-based alloys
USH1869H (en) * 1998-12-18 2000-10-03 Caterpillar Inc. Valve train components having an oxidation and corrosion-resistant thermal spray coating

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2648145B1 (en) * 1989-06-08 1991-10-04 Inst Francais Du Petrole USE OF NICKEL-BASED ALLOYS IN A PROCESS OF THERMAL CRACKING OF AN OIL LOAD AND REACTOR FOR IMPLEMENTING THE PROCESS

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4741080A (en) * 1987-02-20 1988-05-03 Eaton Corporation Process for providing valve members having varied microstructure
US4783966A (en) * 1987-09-01 1988-11-15 Aldrich Clare A Multi-staged internal combustion engine
EP0639652A1 (en) * 1993-07-27 1995-02-22 Ngk Insulators, Ltd. Ni-based alloys
USH1869H (en) * 1998-12-18 2000-10-03 Caterpillar Inc. Valve train components having an oxidation and corrosion-resistant thermal spray coating

Also Published As

Publication number Publication date
JPS5415248B1 (en) 1979-06-13
DE1957823A1 (en) 1970-06-04
GB1227730A (en) 1971-04-07

Similar Documents

Publication Publication Date Title
US4061495A (en) Platinum group metal-containing alloy
US4437913A (en) Cobalt base alloy
US3615376A (en) Cast nickel base alloy
US4207098A (en) Nickel-base superalloys
GB2219600A (en) Nickel-iron aluminides for use in oxidizing environments
US4533414A (en) Corrosion-resistance nickel alloy
US4882125A (en) Sulfidation/oxidation resistant alloys
US4288247A (en) Nickel-base superalloys
US3922168A (en) Intermetallic compound materials
US3972713A (en) Sulfidation resistant nickel-iron base alloy
US3918964A (en) Nickel-base alloys having a low coefficient of thermal expansion
US3795510A (en) Valve components
CA2080964A1 (en) Nickel aluminide base single crystal alloys and method
JPS629659B2 (en)
US3118763A (en) Cobalt base alloys
SE452633B (en) Nickel base alloy with gamma primer matrix
US3902899A (en) Austenitic castable high temperature alloy
US2575915A (en) Nickel base high-temperature alloy
US2891859A (en) Alloy steel
US3135602A (en) 45% iron base austenitic cr-ni alloy with 18-22% cr, 27-32% ni or (ni+co) plus strengthening additions
US3854941A (en) High temperature alloy
CN105886954A (en) Alloy for fan blade of aircraft engine
JPH07238349A (en) Heat resistant steel
US2981621A (en) High temperature nickel-iron base alloy
JPH0573815B2 (en)