CN105127433A - An exhaust valve spindle for an internal combustion engine, and a method of manufacturing - Google Patents
An exhaust valve spindle for an internal combustion engine, and a method of manufacturing Download PDFInfo
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- CN105127433A CN105127433A CN201510511006.XA CN201510511006A CN105127433A CN 105127433 A CN105127433 A CN 105127433A CN 201510511006 A CN201510511006 A CN 201510511006A CN 105127433 A CN105127433 A CN 105127433A
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
- B22F7/06—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
- B22F7/08—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools with one or more parts not made from powder
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J5/00—Methods for forging, hammering, or pressing; Special equipment or accessories therefor
- B21J5/002—Hybrid process, e.g. forging following casting
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J5/00—Methods for forging, hammering, or pressing; Special equipment or accessories therefor
- B21J5/06—Methods for forging, hammering, or pressing; Special equipment or accessories therefor for performing particular operations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21K—MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
- B21K1/00—Making machine elements
- B21K1/20—Making machine elements valve parts
- B21K1/22—Making machine elements valve parts poppet valves, e.g. for internal-combustion engines
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21K—MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
- B21K1/00—Making machine elements
- B21K1/20—Making machine elements valve parts
- B21K1/24—Making machine elements valve parts valve bodies; valve seats
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/12—Both compacting and sintering
- B22F3/14—Both compacting and sintering simultaneously
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/17—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces by forging
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
- B22F5/008—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of engine cylinder parts or of piston parts other than piston rings
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- 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
- F01L3/00—Lift-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
- F01L3/02—Selecting particular materials for valve-members or valve-seats; Valve-members or valve-seats composed of two or more materials
- F01L3/04—Coated valve members or valve-seats
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Chemical & Material Sciences (AREA)
- General Engineering & Computer Science (AREA)
- Composite Materials (AREA)
- Materials Engineering (AREA)
- Combustion & Propulsion (AREA)
- Forging (AREA)
- Powder Metallurgy (AREA)
Abstract
An exhaust valve spindle (1) for an internal combustion engine, particularly a two-stroke crosshead engine, which exhaust valve spindle comprises a valve head (3) with a base portion (4) of an alloyed steel, and an outer facing (5) forming the surface of the valve spindle towards a combustion chamber. The outer facing (5) has been formed from particulate starting material of a hot-corrosion-resistant alloy being nickel-based, chromium- based or cobalt-based, where said particulate starting material has been united to a coherent layer. At least at the transition zone to the base portion (4) the particles in the particulate material of the outer facing (5) have been deformed into oval or elongate shapes by shear strain caused by forging the outer facing and the base portion, and that the forged outer facing (5) has a density of at least 98.0%.
Description
The application is the divisional application of patent application case (denomination of invention is " exhasut valve stem and manufacture method thereof for internal combustion engine " for international filing date on October 29th, 2010, application number 201080048506.X).
Technical field
The present invention relates to a kind of exhasut valve stem for internal combustion engine, especially, relate to a kind of exhasut valve stem for two stroke cross-head engine, wherein exhasut valve stem comprises the valve head of the base part with steel alloy, with the outer surface on the surface towards combustion chamber of formation valve rod, this outer surface is formed by the particulate parent material of the hot-corrosion-resistant alloy for Ni-based, chromium base or cobalt-based, and wherein said particulate parent material is adhered to adhesion coating.
Background technology
United States Patent (USP) 6,173,702 describe this known exhasut valve stem, wherein anticorrosive outer surface is arranged on base part by powder metallurgy process, and wherein the microparticle material of corrosion-resisant alloy to be arranged in the mould of base part and by HIP process (high temperature insostatic pressing (HIP) power) and base portion adheres.This mould is drained to remove air or gas as much as possible.HIP process performs in room, and this room also can be set under stress by heating.In order to utilize this room in an efficient way, fill base part or other parts as much as possible, and these targets all experience identical HIP process in indoor.When starting to process, this room is heated and is pressed onto HIP condition, and then these conditions are kept the cycle of needs, are usually at least 8 to 12 hours.
In HIP processing procedure, pressure affects microparticle material as isostatic pressure (pressure is completely even in all directions), and when microparticle material is compressed on base part, the volume of microparticle material reduces equably in all directions.In the microstructure that outer surface produces, when observe take out from the valve rod completed grind with polishing sample time, can see that particulate remains and has the spherical of circular contour.This sample is have taken in the accompanying drawing of Fig. 1 and 10.
Lower valve head surface has large area, and therefore such as when changing engine load, and especially when engine starts or stop, under being exposed on sizable thermal stress.Thermal shock is the heaviest in the center on surface, part because burning gases have maximum temperature near the centre of combustion chamber, part because when valve cuts out the base region of valve head on the wherein upper surface of outer rim tactile with water-cooled stationary valve seated connection near cool.Cold peripheral material prevents the thermal expansion of thermal center (-tre) material, and therefore produces sizable thermal stress.Except the large thermal stress caused by described heat affecting, change slowly, to the intensity of outer surface and quality, there is very high requirement.
HIP process is known, and to provide the outer surface of high-quality microstructure and meticulous adhesion, but HIP process is very time-consuming, and the long process time of high temperature also produces unaccommodated Metallurgical processing: as spread from an alloy to the parts of other alloy.
Summary of the invention
The outer surface that the present invention is intended to obtain high strength also obtains the microstructure had in the outer surface of robust construction, and this robust construction is specially the robust construction near the transition region of base part.
By the observation to this exhasut valve stem according to the present invention, be characterised in that at least at the transition region place to base part, particulate in the microparticle material of outer surface is deformed into ellipse or elongated shape by the shear strain caused by forging outer surface and base part, and the outer surface after forging has the density of at least 98.0%.
The shear strain produced by forging causes powder particle relative to the displacement of other powder particle, particulate is rubbed relative to each other and penetrates the oxidation film layer that may be present on microparticle surfaces.Any oxidation film layer is all thin, because microparticle material is manufactured by atomization in oxygenless gas usually, but in storing process, some oxides will inevitably be formed on particulate.Shear strain makes particle deforms become can show as the non-spherical shape of ellipse or elongated shape.In forging process, microparticle material is compressed into compacted zone, and particulate is merged into the sticky material being bonded to adjacent layer, and when microparticle material is directly positioned on base part, this sticky material is base part.The density of at least 98.0% can also be represented as the gas porosity of maximum 2%.
The shear strain produced by forging causes microparticle material to flow at least in radial directions, these radial direction are perpendicular to the axial direction of exhasut valve stem, and therefore these radial direction are parallel with the lower surface of valve head and parallel with the general plane transition region between the material of outer surface and the material of base part.Shear strain and the radial motion produced in material near transition region to guarantee that in deformation process generation between the materials effectively combines and guarantees that particulate rubs in a very effective manner relative to each other and combines in deformation process, and the microstructure of generation only has very small amount of internal failure point in this microstructure.Therefore, the material combined in transitional region has firm microstructure and can save the geometry locking between outer surface and base part completely.
In a preferred embodiment, the transition region between outer surface and base part is extending from the inner region extended to the central area of valve head of the lug area of valve head along at least one straight plane.In lug area, outer surface can have increase portion, and this increase portion upwards extends and peripherally surrounds base part, outer surface self is had comprise the pan shape of the upstanding wall at peripheral place.Transition region a distance of distance flange start along straight plane towards valve head in the middle of extend, and this planar extent has the following advantages: no matter the thickness of outer surface or shape can not be suddenlyd change and how microparticle material therefore in outer surface is processed and large local all can not occur changes in forging process.The process that microparticle material experience near plane transition region is roughly the same with in regional area, and when one or more plane domain reaches central area from lug area inside, this one or more plane domain covers most of regions of valve head.
Possibly: outer surface is directly positioned on base part.Optionally, at least one alloy buffer layer is positioned between base part and outer surface.When using this cushion, the alloy of cushion is by having the steel alloy that is different from base part and the 3rd alloy being different from the synthetic of the hot-corrosion-resistant alloy of outer surface is made.Difference in synthetic represents that the alloy analysis of cushion is different in the amount (percentage of weight) of alloy compositions or one or more alloy compositions.Such as, cushion can be have the steel alloy of different phosphorus content or have the steel alloy of other group component of difference of such as chromium, iron or nickel.Therefore term synthetic is represented as alloy analysis.The location of the cushion between the base part of steel alloy and outer surface has steel alloy and only directly contacts with the material of cushion and the effect directly do not contacted with outer field corrosion-resisant alloy.Cushion is done in order to reduce or to prevent alloy compositions to be diffused into base part from outer surface, and vice versa.
Preferably, cushion is selected from following group, the alloy that this group comprises steel, austenitic steel, nickel-base alloy and is made up of iron aside from unavoidable impurities or nickel.These alloys are considered to can be compatible with the alloy of the steel of base part and outer surface.
In an embodiment, the steel alloy of base part is austenitic stainless steel.For many years, accepted whole valve rod to be all made up of alloy nimonic (NIMONIC) 80A (particulate metal of registration mark).But, specific alloy so can easily use far away from as austenitic stainless steel, and stainless steel also has high strength and is all considered to very good execution, particularly concerning arrange two stroke cross-head engine, can in the face of combustion chamber surface on stainless aspect of performance improve corrosion resistance.But stainless steel has quite high carbon content.Cushion absorbs the carbon of diffusion, makes the major part for air bleeding valve use stainless advantage not weakened by the hot corrosion resistance of air bleeding valve that completes and the high request of long-term ductility.
In a preferred embodiment, cushion has the thickness of at least 2 millimeters.Even if this thickness enough guarantees that carbon can not diffuse through cushion when cushion is made up of the alloy with carbide structure performance, the carbon be wherein diffused in described layer can be converted to carbide and therefore not make the carbon activity of described layer increase.
The invention still further relates to the method manufactured for the exhasut valve stem of internal combustion engine, described exhasut valve stem comprises the valve head with steel alloy base part, with the outer surface that the stem surface towards combustion chamber is formed, this outer surface is made up of the particulate parent material of the hot-corrosion-resistant alloy for Ni-based, chromium base or cobalt-based.
According to the present invention, the feature of described method is: when the microparticle material of hot-corrosion-resistant alloy is maintained in the shell of base portion office, microparticle material is heated to forging temperature and is forged, by this, microparticle material is subject to shear strain, this shear strain makes particle deforms become elongated or elliptical shape, and described forging makes microparticle material be compressed to the density of at least 98.0%, and make outer surface and base portion adheres or with make outer surface and cushion and base portion adheres.
Compared with HIP process, forging occurs very fast, and therefore when valve portion is in the forging temperature of increase, alloying component only has the very short time for from an alloy diffusion to adjacent alloys.As mentioned above, forge and microparticle material is pressed together, and shear strain makes particulate move along the direction being parallel to transition region and make the particulate in microparticle material rub relative to each other and merge.In motion process, rubbing and merging any oxide-film initial representation is particulate division, and directly contact with the clean alloy material of the particle from other interparticle from the clean alloy material of the particle of any one interparticle, and therefore, particle can be connected to microstructure level effectively.
In an example, the microparticle material in shell is arranged on and extends in the roughly equal thick layer the region of the middle section of valve head from the lug area inside of valve head.When the layer of microparticle material has roughly equal thickness in shell, and apply roughly equal forging condition, cause outer surface to have roughly equal thickness.Therefore transition region between outer surface and base part extends along valve head separately straight plane in the radial direction.
In another example, the microparticle material in shell is arranged on and extends in the layer of thickness increase of the longitudinal center's axis towards valve the region of the middle section of valve head from the lug area inside of valve head.The generally planar surface of lower surface due to valve head, the lower surface of base part can be made with recessed middle section, and this recessed middle section allows outer surface to have comparatively heavy thickness.Therefore transition region between outer surface and base part can extend along several straight plane, or transition region can have the shape of slight curvature.Compared with the consumption of microparticle material, outer surface provides the air bleeding valve of long life at the thickness of the increase at the middle section place of valve head lower surface, because the middle section place using the highest material unaccounted-for (MUF) in maximum temperature influence process and in operation to appear at valve head lower surface.If exhasut valve stem is used for using within the engine, wherein material unaccounted-for (MUF) expects to be that outer surface can increase the thickness on the direction of lug area alternatively, or increases the thickness at this regional area place near lug area or in other regional area.
Feature according to another method of the present invention is: the microparticle material of hot-corrosion-resistant alloy in inert environments by thermojet to form preformed part, this preformed part and base part are heated to forging temperature and are forged, by this, microparticle material is subject to shear strain, this shear strain makes particle deforms become elongated or elliptical shape, described forging makes microparticle material be compressed to the density of at least 98.0%, and make outer surface and base portion adheres or with make outer surface and cushion and base portion adheres.
According to this method, first microparticle material is formed as the preformed part with enough shape stabilities, is located on base part to allow microparticle material as single main body.Microparticle material directly equally can be injected on described base part.When microparticle material does not have interconnected pore, can avoid using shell.When using shell, machining must be stopped after completing forging.Although the microparticle material in preformed part had irregular shape before forging, forging is as produced identical impact with the description that the method mentioned at first is associated, unless the particulate producing distortion has very irregular shape.
No matter profit how, and preferably before forging, the material of outer surface is emptied to and is less than 1X10
-4the pressure of bar.This emptying gas that makes is removed from the space in microparticle material to be forged, and this contributes to the compression of material.Although the gas being present in the material kind of outer surface is the oxygenless gas of such as inert gas, is more advantageously in fact have the least possible gas.Therefore, the material being preferably outer surface is emptied to and is less than 1X10
-7the pressure of bar.
If use the cushion of the 3rd alloy, this 3rd alloy has the synthetic of the hot-corrosion-resistant alloy (the second alloy) being different from base part steel alloy (the first alloy) and being different from outer surface.3rd alloy was applied to the surface of described base part be preferably positioned at the described surface of base part at the material of outer surface before.3rd alloy can be applied to the material of outer surface alternatively.But the surface of base part is generally rule and smooth surface, and the 3rd alloy can be applied in extraordinary control mode on this smooth surface, be in particular the amount about material and the coating from material well controlled with equivalent way.
Can forge with more than one step, to obtain the valve head with outer surface.After the forging step that base part and outer surface bond, the base part of bonding and outer surface can be forged to obtain net shape with at least one subsequent step.Such as, if base part and outer surface have cylinder form when the first forging step bonding, then the head portion of valve will be favourable after forging in a subsequent step.
Diffusing through transition region to reduce, preferably within the time being less than 10 minutes, performing forging, and the base segments with outer surface is cooled after forging immediately.
In another improvement of method, after completing forging, valve stem part friction welding is on base part.An advantage is that when not having valve stem part, the amount that must be heated to the material of forging temperature is less.Another advantage is: base part can be fully closed and be supported on replace having the shaft portion extending to sidepiece in the face of away from the mould on the sidepiece of outer surface.
Forging valve head or the whole valve with valve head and axle optionally can be subject to the last heat treatment of such as tempering or annealing.Heat treatment can make alloy compositions be diffused in transition region and can metallurgical binding between reinforcement material.
Accompanying drawing explanation
Example is described in more detail at the accompanying drawing referring to highly signal according to an embodiment of the invention, wherein:
What Fig. 1 took out from valve rod grinds the microcosmic picture with polishing sample, wherein provides outer surface by the hot isotatic pressing HIP process of prior art,
Fig. 2 illustrates according to of the present invention with the cross section partial view of the exhasut valve stem of air bleeding valve form,
Fig. 3 and 4 is schematic diagrames of the forging according to valve head of the present invention,
Fig. 5 is the view according to valve head of the present invention and valve rod,
Fig. 6 and 7 is the microcosmic pictures with polishing sample that grind taken out from valve rod, wherein according to the invention provides outer surface,
Fig. 8 and 9 is top view and the side view of test specimen respectively,
What Figure 10 took out from valve rod grinds the microcosmic picture with polishing sample, wherein provides outer surface by the hot isotatic pressing HIP process of prior art, and
Figure 11 is maintained at the microparticle material in shell before illustrating the forging according to method of the present invention.
Detailed description of the invention
In Fig. 1 and Figure 10, sample takes out from HIP compressed microparticles material, and can see the annular shape cutting through particulate.This demonstrates the spherical form that particulate keeps them in compression process.The typical characteristics of HIP compression is particulate is spherical, and this is the result applying isostatic pressure in compression process.This isostatic pressure makes microparticle material shrink around the mode of material internal movement in processing procedure with wherein particulate.Very orderlyly this process, and the mutual alignment wherein in particulate is kept.In order to more clearly understand the microstructure of prior art, three circles are added to the picture in Figure 10, to draw the profile of three particulates shown in picture.
Fig. 2 illustrates the schematic structure of the exhasut valve stem 1 for the air bleeding valve of two stroke cross-head engine.Externally visibly, and valve right-hand part is found out in the diagram location of outer surface 5 and the cross section of the example of degree in the left side of valve.Valve rod comprises valve shaft 2 and valve head 3, and only the bottom of valve shaft 2 is shown in Figure 2, and valve head 3 has base part 4 and outer surface 5.The arrow A that the axial direction of air bleeding valve passes through the direction of the line C extended in the center of axle illustrates illustrates, and arrow R illustrates the radial direction perpendicular to described axial direction.
Valve seat 6 at the upper surface place of valve head 3 is by the hot-corrosion-resistant alloy manufacture being suitable for the indenture vestige structure offset on base sealing surface.The alloy of this set is especially known in applicant WO97/47862 and be illustrated, its by relative to the alloy arranged to be herein incorporated with reference to mode.
When exhasut valve stem is installed within the engine, the outer surface 5 on valve head be prevent the material of air bleeding valve from burnouting and formed towards combustion chamber prone surperficial 7 corrosion and heat resistant material layer.Corrosion and heat resistant material is formed by the particulate parent material of the alloy of Ni-based, chromium base or cobalt-based.When power operation, exhasut valve stem moves the engine cycle of suitable number of times between the closed position and the open position, static valve seat in closing position in valve seat 6 adjacent rows air valve shell (not showing), exhasut valve stem 1 moves down in the open position, and valve seat 6 is positioned at a distance apart from static valve seat.Exhasut valve stem 1 and cylinder buss limit the combustion chamber of internal combustion engine together with cylinder head (not showing), and the heat occurred when being therefore exposed to burning and corrosive environment.
Utilize the internal combustion engine of exhasut valve stem can be four-stroke engine or two stroke cross-head engine.Two-cycle engine can be the MAN diesel engine of such as MC or ME type, can be maybe to bend the RTA type of (flex) by such as RTA
make, or the two-cycle engine be made up of Mitsubishi.For this two stroke cross-head engine, the diameter of piston can in the scope of 250 to 1100 millimeters, and the external diameter of valve head can in the scope of 120 to 600 millimeters, and usually minimum be 170 millimeters.
Have a clear understanding of from these sizes, the surface towards the exhasut valve stem of combustion chamber has larger area, and this causes the larger thermal stress in outer surface 5 and between outer surface and base part interface zone respectively.In an embodiment of the present invention, outer surface 5 is firmly connected to the base part 4 plane domain that the lug area from exhasut valve stem towards valve head extends.
Exhasut valve stem 1 can also be used in less engine, the four-stroke engine of such as middling speed or high-speed type, and exhasut valve stem especially can be applicable in two stroke cross-head engine, this two stroke cross-head engine is big-block engine, and wherein load weighs and importantly needs continued operation when not losing efficacy.
In one embodiment, outer surface 5 is applied directly on the surface of base part 4.In another embodiment of exhasut valve stem, one in the sample of shooting from Fig. 6 and 7 is intercepted, and cushion 9 is positioned between base part 4 and outer surface 5.Cushion 9 can for being applied to the roughly pure-nickel-layer on base part surface aside from unavoidable impurities.Nickel dam can be applied to described surface in a different manner, such as, be provided as the microparticle material be arranged on the top of base part.Nickel dam is set up before can also arranging the microparticle material of outer surface on the top of cushion in a separate step.In this independent step, base part can be arranged in electroplating bath, and the nickel precipitated by electronickelling forms the layer with thickness, this thickness in the scope of 30 to 150 μm, preferably in the scope of 30 to 70 μm.Electrodeposited coating has the advantage of the very compacted zone of pure nickel.Electrodeposited coating has the metallurgical binding to base part.
In another embodiment, cushion is made up of iron aside from unavoidable impurities.Be that cushion does not have or only has very small amount of carbide form by pure iron or nickel or the advantage of cushion that almost pure iron or nickel are made.When in this case, the carbide structure in cushion is suppressed, and the carbon increased in cushion to the carbon diffusion in cushion is active, and therefore carbon will be limited to the further diffusion in described layer.Carbon only has very little dissolubility in iron and nickel.As an example, the dissolubility of carbon in nickel is less than 0.1% at the temperature place of 500 DEG C according to Weight computation, even if therefore when a small amount of carbon is diffused in cushion, cushion is also active by the carbon of acquisition 100%, and therefore in fact anti-blocking to the further diffusion in described layer.
In another example, cushion 9 can be made up of steel or austenitic steel.Cushion can be steel plate.As example more specifically, base part 4 is formed by forging valve steel (the SNCrW-alloy 1 in table 1), and outer surface 5 is performed by alloy 671, and No. W.-1.4332 alloys that steel plate is selected by the alloy from table 2 are formed.As another example, cushion 9 can be provided as the microparticle material of alloy UNSS31603 and outer surface 5 is made up of the microparticle material of alloy 671.Base part 4 is made up of forged steel.In this case, the microparticle material of cushion and the microparticle material of outer surface are adhered in the binding material on base part 4 in forging process.
As embodiment, cushion can be made up of nickel-base alloy.Such alloy is particularly suitable for being combined preferably with the alloy of outer surface, and it can have the chromium content being starkly lower than outer surface, the chromium content such as calculated by weight is less than 25%, such as there is the alloy IN625 of the chromium of 20 to 23%, there is the Xite alloy (alloyINCOLOY) 600 of chromium from 19 to 23%, or there is the alloy IN718 of chromium of 10 to 25%, or there is the alloy 105 of nimonic nickel-base alloy (NIMONICAlloy) of chromium of about 15%, or there is the alloy (alloyRene) 220 of chromium of 10 to 25%.Because more substantial nickel tends to prevent Carbon diffusion, cushion can also be made up of the alloy that nickel is abundanter.
Microparticle material can with multiple different modes manufacture well known in the prior art.Such as, granular materials can by making to be ejected into the atomization of liquid of the melted alloy of the suitable synthetic had in the room of inert environments and manufactured, and by this, material is quenched and condenses as the particulate with very fine dendrite structure.Microparticle material can also be called powder.
Microparticle material can manufacture by making to be ejected into the melted alloy atomization of liquid of the suitable synthetic had in the room of inert environments alternatively, and wherein the injection of atomized particles is directed to collide and to be deposited on solid portion.Solid portion can be cooled, and in this case, particulate is manufactured into the preformed part be separated with solid portion.Particulate can be combined with solid portion alternatively, and is used as base part 4, makes preformed part directly be attached to base part.
Suitable material for base part 4 comprises stainless steel.The example of this material provides in following table 1.No. W.-is the DIN number for alloy.The percentage illustrated is by weight percentage.
table 1
Suitable material for optional buffer layer comprises the steel illustrated in table 2 below.No. W.-is the DIN number for alloy.The percentage illustrated is by weight percentage.
table 2
Another suitable material for cushion is alloy UNSS31603, and it comprises the manganese of 0.5-1.0%, the chromium of 16.5 – 18%, the nickel of 11.5 – 14%, the molybdenum of 2.5 – 3.0%, the nitrogen of 0 – 0.1%, the oxygen of 0 – 0.025%, the carbon of 0 – 0.03% and Balance Iron.When cushion is made up of board-like material, then not there is any requirement to nitrogen and oxygen content usually.But when cushion is made up of microparticle material, then preferably the content of nitrogen is 0.1% to the maximum, and preferably the content of oxygen mostly is 0.03% most..
Suitable material for outer surface is known in the technology of air bleeding valve, and example is stellite (Stellite) 6, the alloy of the type of the chromium of 50% and the nickel of 50%, comprise the chromium of 48-52%, the niobium of 1.4-1.7%, the carbon of maximum 0.1%, the titanium of maximum 0.16%, the carbon+nitrogen of maximum 0.2%, maximum 0.5% silicon, the iron of maximum 1.0%, the magnesium of maximum 0.3 and balance the alloy of IN657 type of nickel.Another example be have 40 to 51% chromium, 0 to 0.1% carbon, be less than 1.0% silicon, 0 to 5.0% manganese, be less than 1.0% molybdenum, 0.05% to be less than 0.5% boron, 0 to 1.0% aluminium, 0 to 1.5% titanium, 0 to 0.2% zirconium, the niobium of 0.5 to 3.0%, the total content of the cobalt of maximum 5.0% and iron, the oxygen of maximum 0.2%, the nitrogen of maximum 0.3 and balance the alloy of synthetic 40 of nickel.Provide in article " Reviewofoperatingexperiencewithcurrentvalvematerials " in the book " Dieselenginecombustionchambermaterialsforheavyfueloperat ion " of the London association of marine engineer institute published in nineteen ninety as other suitable surface alloy of outer surface.
And if cushion 9 is applied to base part surface and is produced by the some words of base part 4 of forging by arranging valve head in forging position.The microparticle material of outer surface 5 can be set up in several different mode.In an example shown in Figure 11, outer surface is provided as the microparticle material in the shell 12 remaining on base part 4 place, and the base part simultaneously with shell and microparticle material is arranged on as forging in the mould part of preparation.Shell 12 on base part and the configuration of microparticle material can act in a number of different ways.Shell to can be soldered on base part and is provided with barrel bolt, and this barrel bolt is used for microparticle material to be filled in shell, then for connecting vacuum equipment, and then removes or closes before forging.Alternatively, shell 12 has deposited in shell at microparticle material and has been fixed to base part 4.This fixing can passing through utilizes welding or as another example, pass through vacuum welding.As another alternative embodiment, shell can be fixed to base part, and is filled in shell by microparticle material subsequently, and finally performs welding.When using vacuum welding, shell can have cup-shaped and inside is provided with coarse-pitch thread, and threaded engagement is threadably screwed on base part by this coarse-pitch thread.Solder is provided on described screw thread.Then heat and fix and can be performed in vacuum oven.In another example, the microparticle material of outer surface 8 is provided as the preformed part be positioned on base part 4, as shown in Figure 3.The structure of this preformed part is described in more detail below.
Before forging has the base part 4 of the microparticle material of outer surface 5, cushion 9 and shell 12 may be heated to forging temperature, and this forging temperature is preferably in the temperature range of 950 DEG C to 1100 DEG C.Heating part to be introduced in the forging press with part of the lower die 10 and part of the upper die 11 and can be mechanically driven or in hydraulically powered driving mechanism.The driving of forging press makes a mould part move towards other mould part, and remains on the material mechanically deform in this moving process in mould part.Need active force so that the size based on valve head performs forging.For the valve head of the diameter of about 490 millimeters, can perform effective forging operation, wherein forging press can carry the compression stress in the scope of about 250 to 400MN.For the valve head of small diameter, the compression stress of use can be less, and such as, for the air bleeding valve of valve head diameter with 150 millimeters, compression stress is 35MN.Forging operation preferably performed in 10 minutes, and more preferably performed in 3 minutes.In forging process, the microparticle material of outer surface 5 is compressed usually, makes the thickness of outer surface be reduced to 30 to 70% of the original depth of microparticle material.If when the preformed part of densification is used, density can be quite high before forging, and in this case, the thickness of outer surface can reduce to 30 to 95% of the original depth of microparticle material.Microparticle material is reduced on thickness, and making the density of the generation of outer surface minimum is 98.0%.When by using forging to compress so far, microparticle material obtains suitable density.Certainly, more preferably further compressed microparticles material, makes density be at least 99.0%, or density more preferably at least 99.5%, and is most preferably compressed to the density of 100%.
In forging process, microparticle material is subject to shear strain, and this shear strain makes particulate change position and make material deformation.This strain is the distortion of the dimensional measurement of the relative displacement represented between the particulate in material.Shear strain causes particulate to change position, and it makes particle deforms when particulate interacts.Shear strain is parallel to the surface action by forging impact.Forge along impact surface 7 on the axial direction of exhasut valve stem, the axial direction of this exhasut valve stem is perpendicular to this surface, and therefore shear strain is parallel to this surface action, and this surface is positioned at the radial direction of exhasut valve stem.In the outer field process of compression, shear strain makes particulate radially move, and particulate is relative to each other rubbed, and promotes particulate and make particle deforms become the non-spherical shape of such as rectangle, elliptical shape or irregular shape.When completing forging, the valve head after forging is removed and by Air flow or be otherwise cooled from mould.
Preferably, the effect strain in the material of outer surface is at least 0.3.Effective strain is calculated with traditional approach disclosed in basic textbook, " the FormelsamglingI such as, delivered by GertHedner in the 222-223 page to publish for 1978 in the publication 104 of " Manufacturingengineeringandtechnology " that delivered by Kalpakjian and Schmid of the 5th edition that published by PrenticeHall in 2006 or the RoyalSwedishTechnicalUniversity in Stockholm
".More preferably, effective strain is minimum is 0.4.This guarantees the very effective and firm bonding between the particulate of outer surface and the material of base part or cushion.
Described below the first method manufacturing exhasut valve stem.Exhasut valve stem has valve head and outer surface, and this valve head comprises the base part be made up of steel alloy, and outer surface forms the surface towards combustion chamber of valve rod.The base part be made up of steel alloy is such as produced by material is forged into suitable shape.Particulate parent material for the formation of outer surface is produced.Material is made up of hot-corrosion-resistant alloy.Particulate parent material is sealed in shell, and the inside of this shell has the shape of the outer surface of formation.In other words, shell is produced for being removed after forging valve head.When the microparticle material of hot-corrosion-resistant alloy is maintained in the shell of base portion office, microparticle material and base part are heated to forging temperature and are positioned in a mould part, are usually located in part of the lower die 10.Then material is forged, and by this, microparticle material is subject to shear strain, and this shear strain makes particle deforms be elongated or elliptical shape.Meanwhile, microparticle material is compressed to have the density of at least 98.0% and is adhered to base part or cushion and base part.
The second method manufacturing exhasut valve stem is that the microparticle material of thermojet hot-corrosion-resistant alloy is to form preformed part.Preformed part can be formed directly on base part in course of injection, or this preformed part can be separately formed, and is positioned on base part, to be heated to forging temperature.Then, preformed part and base part and optionally cushion can be forged into air bleeding valve part.In forging process, microparticle material is subject to shear strain, this shear strain makes particle deforms become elongated or elliptical shape, described forging compressed microparticles material with the density with at least 98.0%, and make outer surface and base part or with cushion and base portion adheres.
The thermojet of microparticle material can by providing the ejector dryer nozzle with molten alloy and being ejected on base part 4 as atomized particles by alloy and occurring, in base part 4, particulate is partly bonded, and remains non-densifie state.There is base part thermojet being applied to preformed part and be heated to forging temperature, and be arranged in the above-mentioned mould mentioned, and be then swaged to densifie state.
Preferably: the microparticle material for the preparation of outer surface was drained before forging, to reduce the amount of oxygen being present in particulate.In this fashion, the oxide-film structure on particulate is counteracted.
During forging, outer surface 5 is compressed into less thickness, such as compared with original depth less about 25% thickness.Meanwhile, the density of material in outer surface is from being approximately increased to close to 100% around 65%.The density preferably produced is at least 98.0%.
By the valve head with outer surface 5 that the valve head 3 of any one method manufacture above-mentioned is on the surface pointing to combustion chamber.Valve head can have valve shaft, if the base part of valve head 34 and valve shaft 2 are integrally formed, or alternatively, if be considered to more convenient words, valve head can also be produced when not having valve shaft 2.In the latter cases, valve shaft must be installed on valve head after the manufacture completing valve head.The valve head that Fig. 5 has illustrated and valve shaft 2.These two parts can be connected by the friction welding of known way.In this friction welding, the single part being generally valve head is held stationary, and first the other parts of such as valve shaft are rotated, and then move axially to have in the adjacency section of valve head, make these two parts together friction welding (FW) be connected into independent exhasut valve stem.
The firm microstructure obtained causes the firm combining of the material in transitional region.According to the present invention, this combination can be tested.In order to test the intensity of tearing of the material in relative shear load, special test sample is that basis is produced at the sample cut out from air bleeding valve.Test specimen has the shape shown in Fig. 8 and 9.Distance d=25.4 millimeter between the center of the width w=9.0 millimeter of test specimen, length I=40.0 millimeter, pulling eye, the thickness t=3.5 millimeter of base part, and there is the thickness T of outer surface.The thickness of outer surface is measured and be set to thickness T.Then cut from both sides by groove g1, g2 of integral material, this groove has the width of at least 2 millimeters and has separated part in the longitudinal direction, and this causes with the overlapping layer of the layer combined more less than the detect thickness t of outer surface.
Eight examples are performed, and in table 3 result are shown.Be clear that: the shearing strength of acquisition is in high level.This level is corresponding with the shearing strength of solid material.Therefore the combination obtained according to the present invention can not cause the weakening of material.
table 3
In another embodiment, the microparticle material of hot-corrosion-resistant alloy mixes with the particulate of such as ceramic material zirconia (ZrO2) insulating materials.Insulating materials can have higher concentration at the proximity of outer surface, and preferably, does not have insulating materials in the transition region between outer surface and base part.The microparticle material of outer surface can comprise the insulating materials of calculate by weight 5 to 60%, and the amount of insulating materials is no more than 40% of outer surface weight.
The details of the above-mentioned embodiment mentioned can be attached in other embodiment in the scope of the application's claim.In addition, the change in the details of above-described embodiment can be had in the scope of the application's claim.Such as valve seat 6 can be made up of the alloy identical with valve head, and cushion 9 can terminate at valve seat 6 place and have or vertical region in maximum gauge place (in the region below valve seat 6).
Any one in the above-mentioned embodiment mentioned all is subject to the finished heat treatment of such as tempering or annealing.Such as, heat treatment can have the durability degree in the scope of 2 to 6 hours, and carries out at temperature in the scope of 800 to 1050 DEG C.Other temperature can also be had.
Exhasut valve stem is important engine section, and may manufacture details and can be stored in the label be embedded in exhasut valve stem for the information of documentation identification and concrete exhasut valve stem.Label is preferably long-range write and readable RFID type, even preferably comprises the independent code data providing traceability.If suitable, concrete bar can be provided with more than one label.Described label can be positioned at the position in exhasut valve stem, fully shields heat and other mark infringement parameter in this position.
Claims (11)
1. one kind manufactures the method for the exhasut valve stem being used for internal combustion engine, described exhasut valve stem comprises valve head and outer surface, described valve head has the base part of steel alloy, and described outer surface forms the surface towards combustion chamber of valve rod, described outer surface is formed by the particulate parent material of hot-corrosion-resistant alloy, the particulate parent material of described hot-corrosion-resistant alloy is Ni-based, chromium base or cobalt-based, it is characterized in that, when the microparticle material of described hot-corrosion-resistant alloy is maintained in the shell of described base portion office, described microparticle material is heated to forging temperature and is forged, by this, described microparticle material stands shear strain, this shear strain makes described particle deforms become elongated or elliptical shape, described microparticle material is compressed to the density of at least 98.0% by described forging, and make described outer surface and described base part or with described outer surface and and described base part between cushion be combined.
2. the method for manufacture exhasut valve stem according to claim 1, it is characterized in that, extend in the region of the middle section of described valve head in the lug area inside from described valve head, described microparticle material is in the housing arranged in the layer with roughly equal thickness.
3. the method for manufacture exhasut valve stem according to claim 1, it is characterized in that, extend in the region of the middle section of described valve head in the lug area inside from described valve head, described microparticle material is in the housing arranged on to have to be increased in the layer of thickness towards the center of described valve.
4. one kind manufactures the method for the exhasut valve stem being used for internal combustion engine, described exhasut valve stem comprises valve head and outer surface, described valve head has the base part of steel alloy, and described outer surface forms the surface towards combustion chamber of valve rod, described outer surface is formed by the particulate parent material of hot-corrosion-resistant alloy, the particulate parent material of described hot-corrosion-resistant alloy is Ni-based, chromium base or cobalt-based, it is characterized in that, when the microparticle material of described hot-corrosion-resistant alloy by thermojet to form preformed part, described preformed part and described base part are heated to forging temperature and are forged, by this, described microparticle material stands shear strain, this shear strain makes described particle deforms become elongated or elliptical shape, described microparticle material is compressed to the density of at least 98.0% by described forging, and make described outer surface and described base part or with described outer surface and and described base part between cushion be combined.
5. the method for the manufacture exhasut valve stem according to claim 1 or 4, is characterized in that, before forging, the described material of described outer surface is emptied to and is less than 1x10
-4the pressure of bar.
6. the method for the manufacture exhasut valve stem according to claim 1 or 4, it is characterized in that, 3rd alloy buffer layer was applied to the described surface of described base part before the material of described outer surface is positioned at the described surface of described base part, and wherein said 3rd alloy buffer layer has the synthetic of the steel alloy being different from described base part and the described hot-corrosion-resistant alloy being different from described outer surface.
7. the method for manufacture exhasut valve stem according to claim 6, is characterized in that, described cushion is selected from following group, and described group comprises steel, austenitic steel, nickel-base alloy and make alloy by iron aside from unavoidable impurities or nickel.
8. the method for the manufacture exhasut valve stem according to claim 1 or 4, it is characterized in that, after the forging step making described base part and described outer surface combine, in conjunction with base part and outer surface forged to obtain net shape at least one subsequent step.
9. the method for the manufacture exhasut valve stem according to claim 1 or 4, is characterized in that, described forging is performed within the time being less than 10 minutes, and the described base part with described outer surface is cooled immediately after described forging.
10. the method for manufacture exhasut valve stem according to claim 8, is characterized in that, described forging is performed within the time being less than 2 minutes.
The method of 11. manufacture exhasut valve stems according to claim 1 or 4, it is characterized in that, valve spindle part is friction welded on described base part after completing forging.
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| DKPA200970184 | 2009-10-30 | ||
| DKPA200970184A DK177071B1 (en) | 2009-10-30 | 2009-10-30 | Exhaust valve spindle for an internal combustion engine and a method of manufacture thereof |
| CN201080048506.XA CN102667077B (en) | 2009-10-30 | 2010-10-29 | For the exhasut valve stem of two stroke cross-head |
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| JP (1) | JP4701309B2 (en) |
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| KR101238126B1 (en) | 2011-12-23 | 2013-02-27 | 주식회사 케이,에스,피 | Manufacturing process for exhaust valve spindle with defferent materials |
| DK177487B1 (en) * | 2012-07-06 | 2013-07-15 | Man Diesel & Turbo Deutschland | An exhaust valve spindle for an exhaust valve in an internal combustion engine |
| EP2781284A1 (en) | 2013-03-18 | 2014-09-24 | Sandvik Intellectual Property AB | A method for manufacturing a valve spindle |
| KR101821082B1 (en) * | 2014-03-28 | 2018-01-22 | 아사히 가세이 가부시키가이샤 | Exhaust valve stem for internal combustion engine and method for manufacturing same |
| DE102015220891A1 (en) * | 2015-10-26 | 2017-04-27 | Federal-Mogul Valvetrain Gmbh | Internally cooled valve for internal combustion engines and method and apparatus for its manufacture |
| CN105507978A (en) * | 2015-12-15 | 2016-04-20 | 苏州爱盟机械有限公司 | Vehicle engine valve |
| CN116732390B (en) * | 2023-06-30 | 2024-02-09 | 江西宝顺昌特种合金制造有限公司 | 80A alloy and preparation method thereof |
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| JP4701309B2 (en) | 2011-06-15 |
| ES2651311T3 (en) | 2018-01-25 |
| KR20120075485A (en) | 2012-07-06 |
| EP2494158A1 (en) | 2012-09-05 |
| EP2494158B1 (en) | 2017-10-18 |
| EP2494158A4 (en) | 2017-05-03 |
| WO2011050815A1 (en) | 2011-05-05 |
| KR101435401B1 (en) | 2014-08-28 |
| CN102667077B (en) | 2015-09-02 |
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| JP2011094605A (en) | 2011-05-12 |
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