US3078194A - Tappet with cast iron base and tubular steel body - Google Patents
Tappet with cast iron base and tubular steel body Download PDFInfo
- Publication number
- US3078194A US3078194A US517520A US51752055A US3078194A US 3078194 A US3078194 A US 3078194A US 517520 A US517520 A US 517520A US 51752055 A US51752055 A US 51752055A US 3078194 A US3078194 A US 3078194A
- Authority
- US
- United States
- Prior art keywords
- base
- tappet
- cast iron
- steel body
- tubular steel
- 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
Links
- 229910001018 Cast iron Inorganic materials 0.000 title claims description 17
- 229910000831 Steel Inorganic materials 0.000 title claims description 14
- 239000010959 steel Substances 0.000 title claims description 14
- 239000002245 particle Substances 0.000 claims description 25
- 229910001567 cementite Inorganic materials 0.000 claims description 23
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 21
- KSOKAHYVTMZFBJ-UHFFFAOYSA-N iron;methane Chemical compound C.[Fe].[Fe].[Fe] KSOKAHYVTMZFBJ-UHFFFAOYSA-N 0.000 claims description 21
- 229910002804 graphite Inorganic materials 0.000 claims description 14
- 239000010439 graphite Substances 0.000 claims description 14
- 229910045601 alloy Inorganic materials 0.000 claims description 13
- 239000000956 alloy Substances 0.000 claims description 13
- 238000010438 heat treatment Methods 0.000 claims description 8
- 229910052799 carbon Inorganic materials 0.000 claims description 7
- 229910000734 martensite Inorganic materials 0.000 claims description 6
- 239000011159 matrix material Substances 0.000 claims description 5
- 238000005266 casting Methods 0.000 description 27
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 8
- 238000005255 carburizing Methods 0.000 description 5
- 239000000470 constituent Substances 0.000 description 5
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 4
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 4
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 4
- 229910052804 chromium Inorganic materials 0.000 description 4
- 239000011651 chromium Substances 0.000 description 4
- 229910052742 iron Inorganic materials 0.000 description 4
- 229910052750 molybdenum Inorganic materials 0.000 description 4
- 239000011733 molybdenum Substances 0.000 description 4
- 238000010791 quenching Methods 0.000 description 4
- 230000000171 quenching effect Effects 0.000 description 4
- 238000005256 carbonitriding Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 239000003921 oil Substances 0.000 description 3
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 2
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 2
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 2
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 2
- 239000005864 Sulphur Substances 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 239000010949 copper Substances 0.000 description 2
- 230000003247 decreasing effect Effects 0.000 description 2
- 230000004927 fusion Effects 0.000 description 2
- 229910052748 manganese Inorganic materials 0.000 description 2
- 239000011572 manganese Substances 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 229910052759 nickel Inorganic materials 0.000 description 2
- 229910052698 phosphorus Inorganic materials 0.000 description 2
- 239000011574 phosphorus Substances 0.000 description 2
- 238000003303 reheating Methods 0.000 description 2
- 239000004576 sand Substances 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- 238000005275 alloying Methods 0.000 description 1
- 229910001566 austenite Inorganic materials 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000008014 freezing Effects 0.000 description 1
- 238000007710 freezing Methods 0.000 description 1
- 238000005304 joining Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 229910001562 pearlite Inorganic materials 0.000 description 1
- -1 that is Substances 0.000 description 1
- 230000001131 transforming effect Effects 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
- F01L1/00—Valve-gear or valve arrangements, e.g. lift-valve gear
- F01L1/12—Transmitting gear between valve drive and valve
- F01L1/14—Tappets; Push rods
Definitions
- This invention relates to a tappet and more particularly to a tappet comprising a cast iron base and a tubular steel body bonded, fused, welded, brazed or otherwise permanently joined together, such as shown in my Patent 2,887,098 of May 19, 1959.
- One of the objects of this invention is that of producing a tappet for an internal combustion engine wherein the cast iron base or wear surface which contacts the customary cam for operating such a tappet has excellent wear resistance properties and strength.
- This object is achieved in part by fabricating the base of the tappet independently of its body from. an alloy cast iron which is hardenable by heat treatment. By fabricating the base or wear face of the tappet separately from the tubular steel body one is able to control the rnicrostructure of the base and thereby achieve the above mentioned wear resistance properties and strength.
- My above mentioned copending applications show the preferred method for joining the tubular steel body to the cast iron base.
- the present invention is particularly concerned with a tappet such as shown in my copending applications wherein the cast iron base or button has a uniform microstructure across substantially the entire wear face of the tappet.
- This object is accomplished by fabricating the base from a cast iron alloy which is hardenable by heat treatment.
- the base of .the wear surface of the tappet can be made from any typical castiron alloy the elements of which are expressed in percentages by weight of the total composition; such Carbon d 2.9.
- the cast iron is left in the shell mold for only suflicient time to allow all of the metal in the castings to solidify. This, by way of example, is about two minutes.
- the castings are quickly removed from the molds and the base castings clipped off of the runners and immediately quenched at sufiicient rate to produce at least a partially complete martensitic structure commonly referred to as mottled iron. This may be done by air quenching when the cast bases are sufficiently separated or they may be dropped into a suitable liquid quenching media, such as oil.
- the castings are then introduced into a furnace at a temperature of l700-1800 F.
- This furnace must have sufficient heating capacity to 3,078,194 Patented Feb. 19, 1963 quickly bring the temperature of the base castings to the temperature of the furnace; for example, in approximately two and one-half to four minutes.
- the base castings should be distributed in the furnace so that they may be quickly heated to this temperature.
- the time they are held at this temperature of 1700-1800 F. is about eight minutes.
- the percentage of-carbide forming alloy constituents such as chromium and molybdenum .or even vanadium is varied, the length of time which they are held at this range of temperature will be varied to produce the desired result. 1
- the length of time that the alloy will be held at furnace temperature can be increased to produce the dev sired microstructure whereas if the amount of carbide forming alloy constituents is decreased over that stated in the above example, then the time that the base castings are held at furnace temperature will be correspondingly decreased-or the temperature decreased.
- the base castings are allowed to remain in this zone about twelve minutes which is sufiicient time to insure the transforming of the austenite content of the castings to pearlite.
- the base c ast-' ings may then be air cooled, or, if desired, transferred to a third zone in the furnace at around 750 F.'for a that- 1 ter of ten to fifteen minutes and then air cooled.
- FIG. 1 is a photomicrograph showing the structure of the casting as eastand quenched to room temperature.
- FIG. 2 shows the changesinthe structure brought about the time at heat in the 1700 1800 -F. zone. This photograph is taken from a'sp'eeimenthat was removed from this zone after having been in this zone for the specified time and then air cooled.
- FIG. 3 shows the structure of the base castingafter having been treated as above described in zone 1 (1700-1800 F.) and zone 2 (1300 F.), the specimen being taken out at that point and air cooled.
- Photomicrograph FlG. 4 shows the structure of the base casting after it has been heat treated in zones land 2 referred to above and then additionally treated in the furnace zone at 750 F. for a periodoften to fiftee minutes and then air cooled.
- the base casting is then joined to the tubular steel body, preferably as shown and de scribed in my above specified copending applications.
- the tappet as thus formed is then subjected to a final carburizing treatment in a gas carburizing or carbonitriding furnace at a temperature of from 1525 to 1550" F. and held at the temperature for a sufiicient time to produce a case depth in the steel tubing of around .012 to 0.16.
- the thus carburized or carbo-nitrided tappet is direct quenched in oil and drawn to a temperature of approximately 400 F. This final carburizing or carbonitriding treatment improves the fusion bonded joint.
- FIG. 5 shows the structure of the base after the final heat treatment in the carburizing or carbo-nitriding atmosphere.
- mottled areas are located on an average over the entire wear face of the base casting of approximately one mottled area per square inch at 100 diameter magnification, that is, about 10,000 mottled areas per square inch of actual surface.
- the average of mottled areas may range as high as one and one-half mottled areas per square inch at 100 diameter magnification, but preferably should average less than about one per square inch at 100 magnification.
- the unconnected cementite or iron carbide particles may, in the vicinity of high graphite concentration, be as low locally as approximately ten particles per square inch at 100 diameter magnification. In areas where there is a low concentration of graphite, the cementite particles may range as high in 190 particles per square inch at 100 diameter magnification.
- a highly desirable or preferred base casting will contain in the minimum areas of cementite particles of the order of 40-50 particles of cementite per square inch at 100 diameter magnification and in the maximum areas of cementite particles a concentration of the order of 120-440 cementite particles per square inch at 100 diameter magnification.
- the base casting after undergoing the treatment in zone 1 at 1700- 1800 F. for the time specified can be transferred into a zone at about 900 F. and maintained in this zone until the casting falls to a temperature of 1300 F. or a little below, whereupon the casting can be cooled in air to room temperature.
- a microstructure such as shown in the photomicrograph FIG. 6, is obtained which comprises substantially uniformly distributed discrete cementite particles in a martensitic matrix with some free graphite.
- the reheating step at 1550 F. can be accomplished simultaneously with the carburizing ofthe tappet after the base has been permanently joined to the tubular steel body.
- FIG. 7 is a photomicrograph having the same disclosure as that of FIG. but at a magnification of 1000 diameters.
- a valve tappet comprising a tubular steel body and a base of alloy cast ironwhich has been hardened by heat treatment characterized by a martensitic matrixhaving substantially uniformly distributed unconnected cementite particles predominantly with rounded contours, the number of discrete cementite particles being present within a range of from about 10 to 190 per square inch at 100. diameter magnification and a minor amount of the carbon in the alloy cast iron being present as free graphite.
- valve tappet as claimed in claim 2 wherein the cementite particles in their lowest concentration areas fall within a range of from 40 to 50 cementite particles per square inch at diameter magnification and in their highest concentration areas fall within a range of from to cementite particles per square inch at 100 diameter magnification.
- valve tappet as claimed in claim 4 wherein the carbon existing as free graphite is concentrated mostly in mottled areas.
- a valve tappet comprising a tubular steel body and a base of alloy cast iron which has been hardened by heat treatment characterized by a martensitic matrix having substantially uniformly distributed, unconnected, relatively small cementite particles predominantly with rounded corners and very small primary graphite particles, said graphite particles appearing primarily in generally isolated areas having a mettle-like pattern, said cementite particles being present in said mettle-like areas in a range of about at least 40 to 50 cementite particles per square inch at a 100 diameter magnification.
- a valve tappet as claimed in claim 8 wherein the cast iron alloy has substantially the following composition by weight: carbon 2.9%, silicon 2.10%, manganese .70%, chromium .70%, molybdenum 50%, copper 50%, nickel .25%, sulphur about .1% maximum, phosphorus about .2% maximum, and the balance iron.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Valve-Gear Or Valve Arrangements (AREA)
Description
Feb. 19, 1963 E. A. THOMPSON 3,078,194
TAPPET WITH CAST IRON BASE AND TUBULAR STEEL BODY 2 Sheets-Sheet 1 Filed June 23, 1955 Feb. 19, 1963 E. A. THOMPSON TAPPET WITH CAST IRON BASE AND TUBULAR STEEL BODY Filed June 23, 1955 2 Sheets-Sheet 2 FIG. 5
United States Patent 3,078,194 TAPPET WITH CAST IRON BASE AND TUBULAR STEEL BODY Earl A. Thompson, Ferndale, Mich. (1300 Hilton Road, Ferndale Station, Detroit 20, Mich.) Filed June 23, 1955, Ser. No. 517,520 9 Claims. (Cl. 148-31) This invention relates to a tappet and more particularly to a tappet comprising a cast iron base and a tubular steel body bonded, fused, welded, brazed or otherwise permanently joined together, such as shown in my Patent 2,887,098 of May 19, 1959.
One of the objects of this invention is that of producing a tappet for an internal combustion engine wherein the cast iron base or wear surface which contacts the customary cam for operating such a tappet has excellent wear resistance properties and strength. This object is achieved in part by fabricating the base of the tappet independently of its body from. an alloy cast iron which is hardenable by heat treatment. By fabricating the base or wear face of the tappet separately from the tubular steel body one is able to control the rnicrostructure of the base and thereby achieve the above mentioned wear resistance properties and strength.
My above mentioned copending applications show the preferred method for joining the tubular steel body to the cast iron base. The present invention is particularly concerned with a tappet such as shown in my copending applications wherein the cast iron base or button has a uniform microstructure across substantially the entire wear face of the tappet. This object is accomplished by fabricating the base from a cast iron alloy which is hardenable by heat treatment. By way of example, the base of .the wear surface of the tappet can be made from any typical castiron alloy the elements of which are expressed in percentages by weight of the total composition; such Carbon d 2.9.
Silicon 2.10.
Manganese .70. Chromium; .70.
Molybdenum .50.
Copper n .50.
Nickel .25. Sulphur About .1 maximum. Phosphorus; About .2 maximum. Iron Balance.
The percentages of these constituents will vary slightly depending on the control exercised in the foundry.
I prefer to melt the iron and alloying constituents in an electric furnace and cast a plurality of individual base castings or buttons in a shell mold. I prefer a shell mold over a sand mold because with a shell mold one can obtain a more uniform and rapid freezing rate than with an ordinary green sand mold. The cast iron is left in the shell mold for only suflicient time to allow all of the metal in the castings to solidify. This, by way of example, is about two minutes. At the end of this time the castings are quickly removed from the molds and the base castings clipped off of the runners and immediately quenched at sufiicient rate to produce at least a partially complete martensitic structure commonly referred to as mottled iron. This may be done by air quenching when the cast bases are sufficiently separated or they may be dropped into a suitable liquid quenching media, such as oil.
After a cleaning operation the castings are then introduced into a furnace at a temperature of l700-1800 F. This furnace must have sufficient heating capacity to 3,078,194 Patented Feb. 19, 1963 quickly bring the temperature of the base castings to the temperature of the furnace; for example, in approximately two and one-half to four minutes. The base castings should be distributed in the furnace so that they may be quickly heated to this temperature. Where the base castings are made from the above typical alloy, the time they are held at this temperature of 1700-1800 F. is about eight minutes. However, where the percentage of-carbide forming alloy constituents such as chromium and molybdenum .or even vanadium is varied, the length of time which they are held at this range of temperature will be varied to produce the desired result. 1
if the above analysis is varied to increase the carbide forming constituents, that is, chromium, molybdenum, then the length of time that the alloy will be held at furnace temperature can be increased to produce the dev sired microstructure whereas if the amount of carbide forming alloy constituents is decreased over that stated in the above example, then the time that the base castings are held at furnace temperature will be correspondingly decreased-or the temperature decreased.
After the base castings have been left in the furnace I at the 1700-l800 F. zone for the above specified time,
they are then immediately and quickly transferred to an adjacent zone in the furnace having a lower temperature of approximately 1300 F. The base castings are allowed to remain in this zone about twelve minutes which is sufiicient time to insure the transforming of the austenite content of the castings to pearlite. The base c ast-' ings may then be air cooled, or, if desired, transferred to a third zone in the furnace at around 750 F.'for a that- 1 ter of ten to fifteen minutes and then air cooled.
The above described casting procedure and heat treatment will bring out changes in the microstructure in the castings as illustrated in the attached photomicrographsi FIG. 1 is a photomicrograph showing the structure of the casting as eastand quenched to room temperature.
Photomicrograph FIG. 2 shows the changesinthe structure brought about the time at heat in the 1700 1800 -F. zone. This photograph is taken from a'sp'eeimenthat was removed from this zone after having been in this zone for the specified time and then air cooled.
Photomicrograph FIG. 3 shows the structure of the base castingafter having been treated as above described in zone 1 (1700-1800 F.) and zone 2 (1300 F.), the specimen being taken out at that point and air cooled.
Photomicrograph FlG. 4 shows the structure of the base casting after it has been heat treated in zones land 2 referred to above and then additionally treated in the furnace zone at 750 F. for a periodoften to fiftee minutes and then air cooled.
. After the base casting has been heat treated as above described to produce, the structure shown in hotomicrographs FIG. 3 or FIG. 4, the base casting is then joined to the tubular steel body, preferably as shown and de scribed in my above specified copending applications.
'- This produces a combined fusion bond and mechanical connection between the base casting and the tubular steel body. The tappet as thus formed is then subjected to a final carburizing treatment in a gas carburizing or carbonitriding furnace at a temperature of from 1525 to 1550" F. and held at the temperature for a sufiicient time to produce a case depth in the steel tubing of around .012 to 0.16. The thus carburized or carbo-nitrided tappet is direct quenched in oil and drawn to a temperature of approximately 400 F. This final carburizing or carbonitriding treatment improves the fusion bonded joint.
A photomicrograph FIG. 5 shows the structure of the base after the final heat treatment in the carburizing or carbo-nitriding atmosphere.
This quenching from 1550 F. produces a fully mattensitic matrix in the casting and further refines the shape and size of the cementite or iron carbide particles. It will be noted that the final microstructure of the base casting is characterized by uniformly distributed cementite particles with predominantly rounded contours and the matrix is martensitic. A minor amount of the carbon content exists as free graphite mostly concentrated in mottled areas.
A study of the final microstructure of the base casting shows that these mottled areas are located on an average over the entire wear face of the base casting of approximately one mottled area per square inch at 100 diameter magnification, that is, about 10,000 mottled areas per square inch of actual surface. The average of mottled areas may range as high as one and one-half mottled areas per square inch at 100 diameter magnification, but preferably should average less than about one per square inch at 100 magnification. The unconnected cementite or iron carbide particles may, in the vicinity of high graphite concentration, be as low locally as approximately ten particles per square inch at 100 diameter magnification. In areas where there is a low concentration of graphite, the cementite particles may range as high in 190 particles per square inch at 100 diameter magnification.
A highly desirable or preferred base casting will contain in the minimum areas of cementite particles of the order of 40-50 particles of cementite per square inch at 100 diameter magnification and in the maximum areas of cementite particles a concentration of the order of 120-440 cementite particles per square inch at 100 diameter magnification.
As a modification of the above method, the base casting after undergoing the treatment in zone 1 at 1700- 1800 F. for the time specified, can be transferred into a zone at about 900 F. and maintained in this zone until the casting falls to a temperature of 1300 F. or a little below, whereupon the casting can be cooled in air to room temperature. After reheating to 1550" F. and quenching in oil a microstructure, such as shown in the photomicrograph FIG. 6, is obtained which comprises substantially uniformly distributed discrete cementite particles in a martensitic matrix with some free graphite. The reheating step at 1550 F. can be accomplished simultaneously with the carburizing ofthe tappet after the base has been permanently joined to the tubular steel body.
FIG. 7 is a photomicrograph having the same disclosure as that of FIG. but at a magnification of 1000 diameters.
I claim:
1. A valve tappet comprising a tubular steel body and a base of alloy cast ironwhich has been hardened by heat treatment characterized by a martensitic matrixhaving substantially uniformly distributed unconnected cementite particles predominantly with rounded contours, the number of discrete cementite particles being present within a range of from about 10 to 190 per square inch at 100. diameter magnification and a minor amount of the carbon in the alloy cast iron being present as free graphite.
2. A valve tappet as claimed in claim 1 wherein the cementite particles have their lowest concentration in the vicinity of the areas of higher graphite concentration and their highest concentration in the vicinity of the areas of lowest graphite concentration.
3. A valve tappet as claimed in claim 2 wherein the carbon existing as free graphite is concentrated mostly in mottled areas.
4. The valve tappet as claimed in claim 2 wherein the cementite particles in their lowest concentration areas fall within a range of from 40 to 50 cementite particles per square inch at diameter magnification and in their highest concentration areas fall within a range of from to cementite particles per square inch at 100 diameter magnification.
5. A valve tappet as claimed in claim 3 wherein the mottled areas of free graphite are present in an average amount of less than about 1.5 per square inch at 100 diameter magnification.
6. The valve tappet as claimed in claim 4 wherein the carbon existing as free graphite is concentrated mostly in mottled areas.
7. A valve tappet comprising a tubular steel body and a base of alloy cast iron which has been hardened by heat treatment characterized by a martensitic matrix having substantially uniformly distributed, unconnected, relatively small cementite particles predominantly with rounded corners and very small primary graphite particles, said graphite particles appearing primarily in generally isolated areas having a mettle-like pattern, said cementite particles being present in said mettle-like areas in a range of about at least 40 to 50 cementite particles per square inch at a 100 diameter magnification.
8. A valve tappet as claimed in claim 7 wherein said cementite particles are present in the areas of lowest graphite concentration in an amount of about at least 90 particles per square inch at a 100 diameter magnification.
9. A valve tappet as claimed in claim 8 wherein the cast iron alloy has substantially the following composition by weight: carbon 2.9%, silicon 2.10%, manganese .70%, chromium .70%, molybdenum 50%, copper 50%, nickel .25%, sulphur about .1% maximum, phosphorus about .2% maximum, and the balance iron.
References Cited in the file of this patent UNITED STATES PATENTS 1,710,997 Rich Apr. 30, 1929 1,760,241 Lauenstein May 27, 1930 1,871,544 McCarroll Aug. 16, 1932 1,871,545 McCarroll Aug; 16, 1932 1,908,741 Fahrenwald May 16, 1933 1,915,157 Fahrenwald June 20, 1933 2,032,906 Biewind' Mar. 3, 1936 2,077,117 Lauenstein Apr. 13, 1937 2,155,215 Beament Apr. 18, 1939 2,192,645 Lauenstein Mar. 5, 1940 2,208,544 Lorig July 16, 1940 2,633,438 Uhle Mar. 31, 1953
Claims (1)
1. A VALVE TAPPET COMPRISING A TUBULAR STEEL BODY AND A BASE OF ALLOY CAST IRON WHICH HAS BEEN HARDENED BY HEAT TREATMENT CHARACTERIZED BY A MARTENSITIC MATRIX HAVING SUBSTANTIALLY UNIFORMLY DISTRIBUTED UNCONNECTED CEMENTITE PARICLES PREDOMINATLY WITH ROUNDED CONTOURS, THE NUMBER OF DISCRETE CEMENTITE PARTICLES BEING PRESENT WITHIN A RANGE OF FROM ABOUT 10 TO 190 PER SPUARE INCH AT 100 DIAMETER MAGNIFICATION AND A MINOR AMOUNT OF THE CARBON IN THE ALLOY CAST IRON BEING PRESENT AS FREE GRAPHITE.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US517520A US3078194A (en) | 1955-06-23 | 1955-06-23 | Tappet with cast iron base and tubular steel body |
| US685030A US2962397A (en) | 1955-06-23 | 1957-09-19 | Method of making tappets |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US517520A US3078194A (en) | 1955-06-23 | 1955-06-23 | Tappet with cast iron base and tubular steel body |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3078194A true US3078194A (en) | 1963-02-19 |
Family
ID=24060147
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US517520A Expired - Lifetime US3078194A (en) | 1955-06-23 | 1955-06-23 | Tappet with cast iron base and tubular steel body |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3078194A (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3502057A (en) * | 1966-02-24 | 1970-03-24 | Earl A Thompson | Alloy,article of manufacture,and process |
| EP0015520A1 (en) * | 1979-03-02 | 1980-09-17 | David T. Smith | Method of forming valve lifters |
| US5323742A (en) * | 1993-03-26 | 1994-06-28 | Fuji Oozx, Inc. | Shim structure in use for valve tappet of internal combustion engine |
| US20040074460A1 (en) * | 2002-10-18 | 2004-04-22 | Dhruva Mandal | Valve lifter body |
| US20050000314A1 (en) * | 2002-10-18 | 2005-01-06 | Dhruva Mandal | Roller follower body |
| US6871622B2 (en) | 2002-10-18 | 2005-03-29 | Maclean-Fogg Company | Leakdown plunger |
| US7028654B2 (en) | 2002-10-18 | 2006-04-18 | The Maclean-Fogg Company | Metering socket |
| US7191745B2 (en) | 2002-10-18 | 2007-03-20 | Maclean-Fogg Company | Valve operating assembly |
Citations (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1710997A (en) * | 1928-05-14 | 1929-04-30 | Wilcox Rich Corp | Process of making valve tappets |
| US1760241A (en) * | 1928-10-15 | 1930-05-27 | Link Belt Co | Metal |
| US1871544A (en) * | 1930-12-26 | 1932-08-16 | Ford Motor Co | Cast iron article and method of manufacturing thereof |
| US1871545A (en) * | 1931-01-19 | 1932-08-16 | Ford Motor Co | Method of manufacturing cast iron, and cast iron articles |
| US1908741A (en) * | 1929-07-06 | 1933-05-16 | Southern Wheel Company | Car wheel and method of making same |
| US1915157A (en) * | 1929-07-06 | 1933-06-20 | Southern Wheel Company | Car-wheel |
| US2032906A (en) * | 1931-12-10 | 1936-03-03 | Erik C Biewend | Valve tappet |
| US2077117A (en) * | 1933-04-07 | 1937-04-13 | Link Belt Co | Ferrous alloy and process of producing ferrous alloy |
| US2155215A (en) * | 1936-02-27 | 1939-04-18 | Beament Thomas Geoffrey | Method of producing composite wear-resisting bodies |
| US2192645A (en) * | 1935-06-07 | 1940-03-05 | Link Belt Co | Ferrous metal |
| US2208544A (en) * | 1938-05-04 | 1940-07-16 | Battelle Memorial Institute | Cast iron roll |
| US2633438A (en) * | 1950-09-07 | 1953-03-31 | Aralloy Company | Alloy and process |
-
1955
- 1955-06-23 US US517520A patent/US3078194A/en not_active Expired - Lifetime
Patent Citations (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1710997A (en) * | 1928-05-14 | 1929-04-30 | Wilcox Rich Corp | Process of making valve tappets |
| US1760241A (en) * | 1928-10-15 | 1930-05-27 | Link Belt Co | Metal |
| US1908741A (en) * | 1929-07-06 | 1933-05-16 | Southern Wheel Company | Car wheel and method of making same |
| US1915157A (en) * | 1929-07-06 | 1933-06-20 | Southern Wheel Company | Car-wheel |
| US1871544A (en) * | 1930-12-26 | 1932-08-16 | Ford Motor Co | Cast iron article and method of manufacturing thereof |
| US1871545A (en) * | 1931-01-19 | 1932-08-16 | Ford Motor Co | Method of manufacturing cast iron, and cast iron articles |
| US2032906A (en) * | 1931-12-10 | 1936-03-03 | Erik C Biewend | Valve tappet |
| US2077117A (en) * | 1933-04-07 | 1937-04-13 | Link Belt Co | Ferrous alloy and process of producing ferrous alloy |
| US2192645A (en) * | 1935-06-07 | 1940-03-05 | Link Belt Co | Ferrous metal |
| US2155215A (en) * | 1936-02-27 | 1939-04-18 | Beament Thomas Geoffrey | Method of producing composite wear-resisting bodies |
| US2208544A (en) * | 1938-05-04 | 1940-07-16 | Battelle Memorial Institute | Cast iron roll |
| US2633438A (en) * | 1950-09-07 | 1953-03-31 | Aralloy Company | Alloy and process |
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3502057A (en) * | 1966-02-24 | 1970-03-24 | Earl A Thompson | Alloy,article of manufacture,and process |
| EP0015520A1 (en) * | 1979-03-02 | 1980-09-17 | David T. Smith | Method of forming valve lifters |
| US5323742A (en) * | 1993-03-26 | 1994-06-28 | Fuji Oozx, Inc. | Shim structure in use for valve tappet of internal combustion engine |
| US20040074460A1 (en) * | 2002-10-18 | 2004-04-22 | Dhruva Mandal | Valve lifter body |
| US20050000314A1 (en) * | 2002-10-18 | 2005-01-06 | Dhruva Mandal | Roller follower body |
| US6871622B2 (en) | 2002-10-18 | 2005-03-29 | Maclean-Fogg Company | Leakdown plunger |
| US7028654B2 (en) | 2002-10-18 | 2006-04-18 | The Maclean-Fogg Company | Metering socket |
| US7128034B2 (en) | 2002-10-18 | 2006-10-31 | Maclean-Fogg Company | Valve lifter body |
| US7191745B2 (en) | 2002-10-18 | 2007-03-20 | Maclean-Fogg Company | Valve operating assembly |
| US7273026B2 (en) | 2002-10-18 | 2007-09-25 | Maclean-Fogg Company | Roller follower body |
| US7281329B2 (en) | 2002-10-18 | 2007-10-16 | Maclean-Fogg Company | Method for fabricating a roller follower assembly |
| US7284520B2 (en) | 2002-10-18 | 2007-10-23 | Maclean-Fogg Company | Valve lifter body and method of manufacture |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US4243414A (en) | Slidable members for prime movers | |
| US3078194A (en) | Tappet with cast iron base and tubular steel body | |
| US20150190864A1 (en) | Composite components formed by coating a mold with ceramic material | |
| JP3679508B2 (en) | Sintered parts manufacturing method and apparatus | |
| KR20140110612A (en) | Spline hub for a clutch and manufacturing method thereof | |
| US20120240755A1 (en) | Ballistic applications of composite materials | |
| Cull | Mechanical and metallurgical properties of powder forgings | |
| US20150158082A1 (en) | Composite components formed with loose ceramic material | |
| US3384515A (en) | Process of preparing improved cast iron articles | |
| CN101755060B (en) | Functionally graded powder metal components | |
| US3255513A (en) | Method of making a valve lifiter | |
| US2962397A (en) | Method of making tappets | |
| CN108950366A (en) | A kind of processing method for the spheroidal graphite cast-iron product that wearability is good | |
| US4482396A (en) | Method for making pitting resistant cast iron product | |
| JPS6347773B2 (en) | ||
| US3998664A (en) | Cast iron | |
| US3673004A (en) | Method of making piston rings | |
| US2875109A (en) | Method for the isothermal treatment of alloys after casting | |
| US1984458A (en) | Cast iron alloy articles | |
| US2352408A (en) | Method of producing ferrous castings having desired physical properties | |
| JPH0115576B2 (en) | ||
| US2192645A (en) | Ferrous metal | |
| JPH0679541A (en) | Method for forming torque transmitting shaft for induction hardening | |
| WO1998047648A3 (en) | Low-alloy cast iron tappet, apparatus, and process for its manufacturing | |
| JP4596577B2 (en) | Manufacturing method of billet for cold forging |