US2166634A - Process for making engine cylinders with an inner lining - Google Patents
Process for making engine cylinders with an inner lining Download PDFInfo
- Publication number
- US2166634A US2166634A US190960A US19096038A US2166634A US 2166634 A US2166634 A US 2166634A US 190960 A US190960 A US 190960A US 19096038 A US19096038 A US 19096038A US 2166634 A US2166634 A US 2166634A
- Authority
- US
- United States
- Prior art keywords
- cylinder
- metal
- inner lining
- engine cylinders
- layer
- 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
- 238000000034 method Methods 0.000 title description 6
- 229910052751 metal Inorganic materials 0.000 description 24
- 239000002184 metal Substances 0.000 description 24
- 239000010410 layer Substances 0.000 description 13
- 238000002844 melting Methods 0.000 description 6
- 230000008018 melting Effects 0.000 description 6
- 229910045601 alloy Inorganic materials 0.000 description 5
- 239000000956 alloy Substances 0.000 description 5
- 229910001338 liquidmetal Inorganic materials 0.000 description 4
- 229910001234 light alloy Inorganic materials 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical group [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 2
- 239000004411 aluminium Substances 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 230000004927 fusion Effects 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 102000007469 Actins Human genes 0.000 description 1
- 108010085238 Actins Proteins 0.000 description 1
- 229910001018 Cast iron Inorganic materials 0.000 description 1
- 241001052209 Cylinder Species 0.000 description 1
- 229920000914 Metallic fiber Polymers 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- BVKZGUZCCUSVTD-UHFFFAOYSA-N carbonic acid Chemical compound OC(O)=O BVKZGUZCCUSVTD-UHFFFAOYSA-N 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 239000002826 coolant Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 239000002344 surface layer Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D13/00—Centrifugal casting; Casting by using centrifugal force
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49229—Prime mover or fluid pump making
- Y10T29/4927—Cylinder, cylinder head or engine valve sleeve making
- Y10T29/49272—Cylinder, cylinder head or engine valve sleeve making with liner, coating, or sleeve
Definitions
- This invention relates to the cylinder of internal combustion engines and more particularly to cyl inders having an internal surface layer :of a harder metal than the cylinder, this lining being devised .to form the :slide way of the piston reciprocated in the cylinder.-
- An object of this invention is the-method for making the liner in an easy, effective and cheap I way.
- 1 .10 In lininga casting of light-alloy containing a considerable percentagefof' aluminium with a .melted harder metal or alloy ⁇ having a higher melting point with the aim of obtaining an uni-' form and'continuous thin layer the drawback '15 often arises that thealloy with the lower melting point is liquefied as the heat cannot be removed quickly'enough so that the two layers form a new 4 alloy uniform inits hardness and resistance to,
- the cylinder is fastened to a carrier having the form of a disk 3 which is arranged at the top end of a vertical hollow spindle 4 and rotatably mounted in bearings 5.
- a pulley 6 fixed on the said spindle 4 and a belt 1 or of a, similar driving appliance the spindle!- may be rotated.
- a shaft dcarrying a pouring funnel s at its upper end which funnel is provided with a slanting outlet spout l0.
- the device is made use of in the following way:
- the liquid metal to be applied to the inside surface of the engine cylinder [8 is put into the 46 funnel t rotated by the driving means-i2, i3 and then flowsthrough the outlet l0 against the inside wall of the cylinder l8 while the same is at the same time raised by the appliance l4, 05 so that the liquid metal being poured is applied to 60 the .cylinder wall in helical lines placed narrowly side by side. If a rapid rotation at the same time is imparted 'to the cylinder by the transmission means i, I the.
- the relative angular and axial displacements of both the cylinder and the funnel may be chosen tinuously, also a pressure fluid may be caused to act upon the contents of the said funnel.
- a pressure fluid may be caused to act upon the contents of the said funnel.
- the material to be used for the slide surface on which the piston runs may be a harder alloy melting at a higher temperature or a hard metal such as cast iron, steel, etc.
- the aluminium is preferably protected from burning; by an atmosphereof 'an inert gas, such as carbonic acid, being formed within and around the cylinder. which gas may at the same time also act as a cooling agent.
- an atmosphereof 'an inert gas such as carbonic acid
- the method of making an internal combustion cylinder with a light metal jacket'having radiating fins and a lining of metal of substantially greater hardness and of substantially higher melting point which comprises the steps of rotating a vertically disposed jacket, projecting a jet of the molten harder metal within and radially of said cylinder jacket, and against the inner periphery of the latter, eifecting relative rotation of said jet and said cylinder, and continuously moving said jet axially of said cylinder, said jet being so fine that the metal therefrom solidifies quickly on the inner surface of the cylinder as a helical strip, and fuses only the inner surface portion of the cylinder jacket on which it is projected, to form a thin-intermediate layer alloyed from said light metal and said harder metal, said jacket being rotated at such high speed, that adjacent turns of said helical strip are levelled off by centrifugal action to form a
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
Description
A. LEISAGE July 18,- 1939.
PROCESS FOR MAKING ENGINE CYLINDERS WITH AN INNER LINING Filed Feb. 17, 1938 'Paten tcd July 18, 1939 V UNITE-o STATES 'rmess roa Maxine ENGINE crnnvnnns wrrn AN nmna LINING Alfred Lesage, Schweinfurt, Germany Application February 17, 1938, Serial No. 190,960 a In Germany February 15 1937 1 Claim. (circa- 203 This invention relates to the cylinder of internal combustion engines and more particularly to cyl inders having an internal surface layer :of a harder metal than the cylinder, this lining being devised .to form the :slide way of the piston reciprocated in the cylinder.-
An object of this invention-is the-method for making the liner in an easy, effective and cheap I way. 1 .10 In lininga casting of light-alloy containing a considerable percentagefof' aluminium with a .melted harder metal or alloy} having a higher melting point with the aim of obtaining an uni-' form and'continuous thin layer the drawback '15 often arises that thealloy with the lower melting point is liquefied as the heat cannot be removed quickly'enough so that the two layers form a new 4 alloy uniform inits hardness and resistance to,
' wearing out, or the harder metal will enter the .20 light-metal to an uncontrollable extent. thereby generating furtherinconv'eniences.
' Thefnew objects will be attained by a method allowing the lining operation to be well and continuously regulated by the gradual formation of 25 the liner. It has been found'that a thin jet of the harder metal when applied to the inside surface of a light-alloy cylinder while advancing on the same in a lengthwise direction and peripherally, viz. along a helical line, will produce a me- 30 tall i'c layer of uniform depth because it cools down more quickly. The thinner the jet of moltenjmetal, themore uniform the layer pro duced, especially when being pressed against and distributed on the inside surface of the cylinder 35 byrcentrifugal force. With theaid of the method according to the present invention it is possible to apply such a thin metal jet in the fo'rmof metallic threads narrowly juxtaposed on the inside surface of a 40 cylinder and tocause the said threads tocombine into a continuous layer which firmly adheres to I v the saidcylinder. E
To this end a rapidly rotated pouring funnel containing the liquid metal and the bottom end,"
45 of which is provided witha smalloutlet nozzle is introduced into the cylinder which'is displaced at a suitable speed along its center line by me-' chanicallydriven means. Under the pressure resulting from gravity th e metal flows out as a '60 thin jetag'ainst the wallgof the cylinder in a helical line, The pressure-maybefincreased by a pressure fluid actin'g'upon the contents of the funnel; The jet may also be applied along a helical line when there is; imparted to the funnel a 65 movement ina lengthwisedirection and a rapid causes the liquid metal to-more strongly adhere to the'cylinder wall. The funnel may also be stationary while the cylinder at the same time has imparted. thereto the said longitudinal and 5 rotary movements in which case the centrifugal force acting on the metal flowing into the cyl in derv will result in the layer applied being dis-' tributed more uniformly and smoothened accordingly. Also thefunnel and the cylinder may be rotated simultaneously, and in general the relative rotation and rectilinear displacement maybe distributed between the funneiand the cylinder in any suitable way and proportion. a e
The accompanying drawing, forming a part'of this specification, by way of example showsan embodiment of the present invention, represent-' ing a device intended for producing the slide sur face for the piston of a light-alloy engine cylinder, the figure representing a. vertical section along the center line of the said device. I
For the production of the harder inside layer the cylinder is fastened to a carrier having the form of a disk 3 which is arranged at the top end of a vertical hollow spindle 4 and rotatably mounted in bearings 5. By means of a pulley 6 fixed on the said spindle 4 and a belt 1 or of a, similar driving appliance the spindle!- may be rotated. Within this spindle there is r'evolubly mounted a shaft dcarrying a pouring funnel s at its upper end which funnel is provided with a slanting outlet spout l0. The lower end-of the with apertures it through which-dropping molten 40 metal, if any, is thrown into the cup H where it collects. I r The device is made use of in the following way: The liquid metal to be applied to the inside surface of the engine cylinder [8 is put into the 46 funnel t rotated by the driving means-i2, i3 and then flowsthrough the outlet l0 against the inside wall of the cylinder l8 while the same is at the same time raised by the appliance l4, 05 so that the liquid metal being poured is applied to 60 the .cylinder wall in helical lines placed narrowly side by side. If a rapid rotation at the same time is imparted 'to the cylinder by the transmission means i, I the. harder metal applied thereto is pressed against the cylinder wall so tained within such a range that the molten metal as to effect a partial fusion of the light metal of the cylinder having a lower melting point so that a connection free from joints and affording a highly satisfactory conductivity for heat will be obtained. By the centrifugal force the juxtaposed helical threads of the molten harder metal will also at once be pressed against one another and combined into a layer uniformly cohering and having about the same thickness throughout. In this way it is possible to produce a comparatively thin layer on the inside wall of the cylinder which layer will by the partial fusion of the metal thereof not, only strongly ad here but also cool down so quickly that the cylinder itself will comprise several concentrical layers of'different metals or alloys with distinct degrees of hardness. By providing the cylinder with heat radiating flanges ll, the temperature of the cylinder during the admission of the molten metal to form the liner may be readily mainwill rapidly solidify; the molten metal will not unduly melt the cylinder and will not be so in.- stantly chilled as to prevent the desired partial melting and the'formation of the bonding alloy.
The relative angular and axial displacements of both the cylinder and the funnel may be chosen tinuously, also a pressure fluid may be caused to act upon the contents of the said funnel. When the process is being carried out, hea may be supplied or carried oif so that the temperature required for the application of the internal liner may be controlled at will.
The material to be used for the slide surface on which the piston runs may be a harder alloy melting at a higher temperature or a hard metal such as cast iron, steel, etc.
In case the inside layer is iron or steel the aluminium is preferably protected from burning; by an atmosphereof 'an inert gas, such as carbonic acid, being formed within and around the cylinder. which gas may at the same time also act as a cooling agent.
I claim: I
The method of making an internal combustion cylinder with a light metal jacket'having radiating fins and a lining of metal of substantially greater hardness and of substantially higher melting point, which comprises the steps of rotating a vertically disposed jacket, projecting a jet of the molten harder metal within and radially of said cylinder jacket, and against the inner periphery of the latter, eifecting relative rotation of said jet and said cylinder, and continuously moving said jet axially of said cylinder, said jet being so fine that the metal therefrom solidifies quickly on the inner surface of the cylinder as a helical strip, and fuses only the inner surface portion of the cylinder jacket on which it is projected, to form a thin-intermediate layer alloyed from said light metal and said harder metal, said jacket being rotated at such high speed, that adjacent turns of said helical strip are levelled off by centrifugal action to form a
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE2166634X | 1937-02-15 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2166634A true US2166634A (en) | 1939-07-18 |
Family
ID=7988192
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US190960A Expired - Lifetime US2166634A (en) | 1937-02-15 | 1938-02-17 | Process for making engine cylinders with an inner lining |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2166634A (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2534406A (en) * | 1944-09-22 | 1950-12-19 | Jr Harry M Bramberry | Coated metal article and method of making the same |
| US2588422A (en) * | 1947-12-19 | 1952-03-11 | Metallizing Engineering Co Inc | Application of spray metal linings for aluminum engine cylinders of or for reciprocating engines |
| US2676895A (en) * | 1949-12-29 | 1954-04-27 | American La France Foamite | Method and apparatus for applying coating material to the inside of a container |
| US2681260A (en) * | 1951-07-27 | 1954-06-15 | Norton Co | Cylinder and liner |
| US2792657A (en) * | 1946-05-16 | 1957-05-21 | Battelle Development Corp | Gun barrel coated with tantalum |
| US2844855A (en) * | 1953-11-05 | 1958-07-29 | Bristol Aero Engines Ltd | Method of producing castings with one or more internal passages |
| US3015153A (en) * | 1955-09-08 | 1962-01-02 | Hartford Nat Bank & Trust Co | Method of making a heat regenerator |
| US4365399A (en) * | 1978-07-12 | 1982-12-28 | Metal Leve S.A. Industria E Comercio | Manufacture of light weight pistons |
| US5320158A (en) * | 1993-01-15 | 1994-06-14 | Ford Motor Company | Method for manufacturing engine block having recessed cylinder bore liners |
-
1938
- 1938-02-17 US US190960A patent/US2166634A/en not_active Expired - Lifetime
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2534406A (en) * | 1944-09-22 | 1950-12-19 | Jr Harry M Bramberry | Coated metal article and method of making the same |
| US2792657A (en) * | 1946-05-16 | 1957-05-21 | Battelle Development Corp | Gun barrel coated with tantalum |
| US2588422A (en) * | 1947-12-19 | 1952-03-11 | Metallizing Engineering Co Inc | Application of spray metal linings for aluminum engine cylinders of or for reciprocating engines |
| US2676895A (en) * | 1949-12-29 | 1954-04-27 | American La France Foamite | Method and apparatus for applying coating material to the inside of a container |
| US2681260A (en) * | 1951-07-27 | 1954-06-15 | Norton Co | Cylinder and liner |
| US2844855A (en) * | 1953-11-05 | 1958-07-29 | Bristol Aero Engines Ltd | Method of producing castings with one or more internal passages |
| US3015153A (en) * | 1955-09-08 | 1962-01-02 | Hartford Nat Bank & Trust Co | Method of making a heat regenerator |
| US4365399A (en) * | 1978-07-12 | 1982-12-28 | Metal Leve S.A. Industria E Comercio | Manufacture of light weight pistons |
| US5320158A (en) * | 1993-01-15 | 1994-06-14 | Ford Motor Company | Method for manufacturing engine block having recessed cylinder bore liners |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US2166634A (en) | Process for making engine cylinders with an inner lining | |
| US3563300A (en) | Centrifugal casting of a composite roller | |
| US4824478A (en) | Method and apparatus for producing fine metal powder | |
| US3401736A (en) | Process for formation of non-abrasive refractory rubbing surface having high thermal conductivity by casting | |
| CN107243618A (en) | A kind of production method of compound high speed steel roll | |
| US20080251230A1 (en) | Strip Casting of Immiscible Metals | |
| US2129702A (en) | Process for making metal products | |
| US2307939A (en) | Metal product produced directly from molten metal | |
| US2129703A (en) | Apparatus for producing metal products | |
| US2157453A (en) | Process for the manufacture of bearings | |
| US1943720A (en) | Method of casting brake drums | |
| CN104475696A (en) | Centrifugal casting process suitable for tin bronze alloy material | |
| US2046369A (en) | Brake drum | |
| US1964647A (en) | Method of welding | |
| CN100333861C (en) | High temperature gradient layer-by-layer solidifying continuously casting process | |
| JP2003343343A (en) | Metallic cylindrical body and method of manufacture | |
| KR100758750B1 (en) | Cylinder liner for gasoline engine and its manufacturing method | |
| US1944461A (en) | Method of centrifugal casting | |
| CN106756293B (en) | A kind of preparation method of ferro-silicon-aluminium copper magnesium alloy | |
| US1040517A (en) | Process for casting molten metal in molds. | |
| JP4509335B2 (en) | Method for producing cylindrical metal cast-in member | |
| JPH0437122B2 (en) | ||
| RU2840420C1 (en) | Method of producing thick-walled centrifugally cast tubular billets | |
| PL31686B1 (en) | ||
| JPH07107167B2 (en) | Method and apparatus for producing rapidly solidified metal powder |