JPH0286946A - Combination of sliding surface layers - Google Patents
Combination of sliding surface layersInfo
- Publication number
- JPH0286946A JPH0286946A JP23816588A JP23816588A JPH0286946A JP H0286946 A JPH0286946 A JP H0286946A JP 23816588 A JP23816588 A JP 23816588A JP 23816588 A JP23816588 A JP 23816588A JP H0286946 A JPH0286946 A JP H0286946A
- Authority
- JP
- Japan
- Prior art keywords
- nickel
- silicon nitride
- dispersed
- surface layer
- plating 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.)
- Pending
Links
- 239000002344 surface layer Substances 0.000 title claims abstract description 47
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims abstract description 57
- 229910052759 nickel Inorganic materials 0.000 claims abstract description 30
- 229910052581 Si3N4 Inorganic materials 0.000 claims abstract description 26
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 claims abstract description 26
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 claims abstract description 17
- 229910052698 phosphorus Inorganic materials 0.000 claims abstract description 17
- 239000011574 phosphorus Substances 0.000 claims abstract description 17
- 229910017052 cobalt Inorganic materials 0.000 claims abstract description 16
- 239000010941 cobalt Substances 0.000 claims abstract description 16
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims abstract description 16
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 9
- 239000000956 alloy Substances 0.000 claims abstract description 9
- 239000002245 particle Substances 0.000 claims description 42
- 239000011159 matrix material Substances 0.000 claims description 7
- 239000006185 dispersion Substances 0.000 claims description 5
- 238000002485 combustion reaction Methods 0.000 abstract description 8
- 238000005299 abrasion Methods 0.000 abstract description 3
- 239000000126 substance Substances 0.000 abstract 2
- 238000007747 plating Methods 0.000 description 54
- 239000010410 layer Substances 0.000 description 44
- 239000002131 composite material Substances 0.000 description 14
- 239000000463 material Substances 0.000 description 13
- 229910000838 Al alloy Inorganic materials 0.000 description 9
- 230000000694 effects Effects 0.000 description 9
- 238000010438 heat treatment Methods 0.000 description 8
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 8
- 229910010271 silicon carbide Inorganic materials 0.000 description 8
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 7
- 230000013011 mating Effects 0.000 description 6
- 239000000203 mixture Substances 0.000 description 6
- 239000000446 fuel Substances 0.000 description 5
- 229910001018 Cast iron Inorganic materials 0.000 description 4
- 229910000990 Ni alloy Inorganic materials 0.000 description 4
- 229910052804 chromium Inorganic materials 0.000 description 4
- 239000011651 chromium Substances 0.000 description 4
- 239000010687 lubricating oil Substances 0.000 description 4
- 239000003921 oil Substances 0.000 description 4
- 230000007423 decrease Effects 0.000 description 3
- 230000002093 peripheral effect Effects 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 2
- IGOJDKCIHXGPTI-UHFFFAOYSA-N [P].[Co].[Ni] Chemical compound [P].[Co].[Ni] IGOJDKCIHXGPTI-UHFFFAOYSA-N 0.000 description 2
- 239000003082 abrasive agent Substances 0.000 description 2
- 239000000428 dust Substances 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 230000001050 lubricating effect Effects 0.000 description 2
- 230000014759 maintenance of location Effects 0.000 description 2
- 239000010705 motor oil Substances 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- 230000009467 reduction Effects 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- KWSLGOVYXMQPPX-UHFFFAOYSA-N 5-[3-(trifluoromethyl)phenyl]-2h-tetrazole Chemical compound FC(F)(F)C1=CC=CC(C2=NNN=N2)=C1 KWSLGOVYXMQPPX-UHFFFAOYSA-N 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910000669 Chrome steel Inorganic materials 0.000 description 1
- 241001629511 Litchi Species 0.000 description 1
- 229910021586 Nickel(II) chloride Inorganic materials 0.000 description 1
- 229910001315 Tool steel Inorganic materials 0.000 description 1
- 238000002441 X-ray diffraction Methods 0.000 description 1
- 230000002159 abnormal effect Effects 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 238000003483 aging Methods 0.000 description 1
- 239000007864 aqueous solution Substances 0.000 description 1
- KGBXLFKZBHKPEV-UHFFFAOYSA-N boric acid Chemical compound OB(O)O KGBXLFKZBHKPEV-UHFFFAOYSA-N 0.000 description 1
- 239000004327 boric acid Substances 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 229910000361 cobalt sulfate Inorganic materials 0.000 description 1
- 229940044175 cobalt sulfate Drugs 0.000 description 1
- KTVIXTQDYHMGHF-UHFFFAOYSA-L cobalt(2+) sulfate Chemical compound [Co+2].[O-]S([O-])(=O)=O KTVIXTQDYHMGHF-UHFFFAOYSA-L 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000001000 micrograph Methods 0.000 description 1
- 150000002815 nickel Chemical class 0.000 description 1
- QMMRZOWCJAIUJA-UHFFFAOYSA-L nickel dichloride Chemical compound Cl[Ni]Cl QMMRZOWCJAIUJA-UHFFFAOYSA-L 0.000 description 1
- LGQLOGILCSXPEA-UHFFFAOYSA-L nickel sulfate Chemical compound [Ni+2].[O-]S([O-])(=O)=O LGQLOGILCSXPEA-UHFFFAOYSA-L 0.000 description 1
- 229910000363 nickel(II) sulfate Inorganic materials 0.000 description 1
- 238000005498 polishing Methods 0.000 description 1
- 231100000241 scar Toxicity 0.000 description 1
- 229910001379 sodium hypophosphite Inorganic materials 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 238000010998 test method Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 239000013585 weight reducing agent Substances 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F1/00—Cylinders; Cylinder heads
- F02F1/004—Cylinder liners
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2203/00—Non-metallic inorganic materials
- F05C2203/04—Phosphor
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Pistons, Piston Rings, And Cylinders (AREA)
Abstract
Description
【発明の詳細な説明】
イ、産業上の利用分野
本発明は、摺動表面層の組合せに関し、例えば内燃機関
のピストンリング表面層とシリンダ表面層との組合せに
関する。DETAILED DESCRIPTION OF THE INVENTION A. Field of Industrial Application The present invention relates to a combination of sliding surface layers, for example, a combination of a piston ring surface layer and a cylinder surface layer of an internal combustion engine.
口、従来技術
近年、内燃機関はその高出力化のために、高圧縮比、高
速回転が図られ、これに伴って例えばピストンリングや
シリンダライナ等の摺動部品は高温に曝されて潤滑油膜
が薄くなり、金属接触の機会が多くなって異常摩耗や甚
だしくは焼付を起こすことがある。そのため、これらの
摺動部品には、従来に増して一層の耐摩耗性、耐焼付性
が要求されるようになってきている。In recent years, internal combustion engines have been designed to have high compression ratios and high speed rotation in order to increase their output, and as a result, sliding parts such as piston rings and cylinder liners are exposed to high temperatures and develop a lubricating oil film. becomes thinner, increasing the chance of metal-to-metal contact, which may cause abnormal wear or even seizure. Therefore, these sliding parts are required to have even higher wear resistance and seizure resistance than ever before.
これら摺動部品に耐摩耗性を付与するために、古くから
摺動部品に硬質クロムめっきを施すことが行われている
。硬質クロムめっき層は硬度が高く、それ自身の摩耗、
相手摺動部品の摩耗共に少なく、優れた耐摩耗性を備え
てはいるが、保油性がないために摺動中に焼付を起こし
易いという問題点を有している。特に、硬質クロムめっ
き層同士の組合せでは焼付が甚だしい。In order to impart wear resistance to these sliding parts, hard chrome plating has been practiced for a long time. The hard chrome plating layer has high hardness and its own wear,
Although it has excellent wear resistance with less wear on mating sliding parts, it has the problem of being susceptible to seizure during sliding due to lack of oil retention. In particular, the combination of hard chrome plating layers causes severe seizure.
耐焼付性の改善された表面層として、硬質クロムめっき
層に替えてニッケルめっき層の採用が考えられるが、ニ
ッケルめっき層の耐摩耗性は満足し得るものではない。As a surface layer with improved seizure resistance, a nickel plating layer may be used in place of the hard chromium plating layer, but the wear resistance of the nickel plating layer is not satisfactory.
そこで、近年、耐摩耗性を改善しためっき層として、ニ
ッケル基地中に耐摩耗粒子、例えば炭化珪素粒子を分散
させてなる複合めっき層が注目されるようになってきて
いる。Therefore, in recent years, a composite plating layer in which wear-resistant particles, such as silicon carbide particles, are dispersed in a nickel base has been attracting attention as a plating layer with improved wear resistance.
上記複合めっき層の耐摩耗性を改善しようとして耐摩耗
粒子の分散量を増加してい(と、相手摺動部材を摩耗さ
せるようになる上に、めっき層の機械的強度が弱くなる
。他方、上記複合めっき層のニッケル基地中に燐を含有
させ、熱処理によってめっき層の硬度を高め、耐摩耗性
を改善すると共に耐蝕性を改善することが考えられるが
、耐摩耗性改善のために燐含有量を増加させていくと、
基地を脆化させてめっき層の機械的強度、とりわけ衝撃
強度が低下するようになる。これらのようにめっき層の
機械的強度が低下すると、内燃機関の運転中にめっき層
が局部的に剥離するようになり、この剥離部分がアブレ
イシブ材となって却って摩耗が進行するようになる。In an attempt to improve the abrasion resistance of the composite plating layer, the amount of dispersion of wear-resistant particles is increased (and this results in abrasion of the mating sliding member and weakens the mechanical strength of the plating layer.On the other hand, It is conceivable to incorporate phosphorus into the nickel base of the above composite plating layer and increase the hardness of the plating layer through heat treatment to improve wear resistance and corrosion resistance. As the amount increases,
The base becomes brittle and the mechanical strength of the plating layer, especially the impact strength, decreases. If the mechanical strength of the plating layer decreases as described above, the plating layer will locally peel off during operation of the internal combustion engine, and this peeled off portion will turn into an abrasive material, causing wear to progress.
シリンダの材料には鋳鉄が広く採用されているが、最近
、内燃機関の軽量化及びこれによる燃費低減の要請から
、アルミニウム合金製のシリンダが注目されるようにな
ってきている。アルミニウム合金は、鋳鉄に較べて摩耗
し易いため、アルミニウム合金製シリンダには、摺動面
に鋳鉄製シリンダスリーブを嵌め込んだものが使用され
ている。Although cast iron is widely used as a material for cylinders, cylinders made of aluminum alloys have recently been attracting attention due to the demand for lighter internal combustion engines and the resulting reduction in fuel consumption. Since aluminum alloy wears more easily than cast iron, aluminum alloy cylinders are used that have cast iron cylinder sleeves fitted onto the sliding surfaces.
この方法では、原価高となる上に、軽量化が充分には達
成されず、燃費の低減も充分ではない。それで、アルミ
ニウム合金製シリンダの内周面に、ピストンリングと同
様に炭化珪素粒子を分散させたニッケル複合めっき層を
形成したものが提案されている。This method increases the cost, does not achieve sufficient weight reduction, and does not sufficiently reduce fuel consumption. Therefore, it has been proposed that a nickel composite plating layer in which silicon carbide particles are dispersed is formed on the inner circumferential surface of an aluminum alloy cylinder, similar to a piston ring.
このニッケル複合めっき層は、炭化珪素粒子がハードス
ポット(第一摺動面と呼ばれる。)を形成し、ニッケル
の基地が僅か摩耗して凹部(第二摺動面と呼ばれる。)
を形成し、この第二摺動面によって保油性が付与されて
耐摩耗性を改善する。In this nickel composite plating layer, the silicon carbide particles form hard spots (referred to as the first sliding surface), and the nickel base is slightly abraded and recessed (referred to as the second sliding surface).
This second sliding surface provides oil retention and improves wear resistance.
ところが、炭化珪素は極めて硬質でかつ結晶の端部が鋭
利なため、摺動によって相手材のピストンリングを摩耗
させるという欠点がある。例えば、外周面Gご硬質クロ
ムめっき層又は窒化層を設けたピストンリングと組合せ
て使用した場合、ピストンリングを摩耗させる。また、
シリンダと同様の炭化珪素分散ニッケルめっきを施した
ピストンリングと組合せて使用した場合、焼付が発生し
易い。However, since silicon carbide is extremely hard and has sharp crystal edges, it has the disadvantage that the mating piston ring wears out due to sliding. For example, when used in combination with a piston ring provided with a hard chromium plating layer or a nitrided layer on the outer peripheral surface G, the piston ring will wear out. Also,
When used in combination with a piston ring coated with silicon carbide dispersed nickel plating similar to the cylinder, seizure is likely to occur.
このように、ピストンリング、シリンダ双方共摩耗が少
なくかつ焼付を起こし難い表面層の組合せが望まれるの
であるが、現在迄のところ、この要請に応える好ましい
表面層の組合せは見出されていない。Thus, there is a desire for a combination of surface layers that causes less wear on both the piston ring and the cylinder and is less likely to cause seizure, but to date no preferred combination of surface layers that meets this demand has been found.
ハ1発明の目的
本発明は、苛酷な摺動条件下にあっても、互いに摺動す
る摺動表面層の双方共摩耗が少なくかつ焼付を起こし難
い、摺動表面層の組合せを提供することを目的としてい
る。C1 Purpose of the Invention The present invention provides a combination of sliding surface layers in which both of the sliding surface layers that slide against each other have less wear and are less likely to seize even under severe sliding conditions. It is an object.
二0発明の構成
本発明は、2〜15重量%燐、10〜40重量%コバル
ト、残部が実質的にニッケルからなる合金基地中に平均
粒径0.5〜10μmの窒化珪素粒子が5〜40容積%
分散した第一の表面層と、2〜15重量%燐、10〜4
0重量%コバルト、残部が実質的にニッケルからなる合
金基地中に平均粒径0.5〜10μmの窒化珪素粒子が
5〜30容積%分散した第二の表面層とが互いに摺動す
る、摺動表面層の組合せに係る。20 Structure of the Invention The present invention is characterized in that silicon nitride particles with an average particle size of 0.5 to 10 μm are contained in an alloy matrix consisting of 2 to 15% by weight of phosphorus, 10 to 40% by weight of cobalt, and the remainder substantially nickel. 40 volume%
a dispersed first surface layer and 2 to 15 wt% phosphorus, 10 to 4
A second surface layer in which silicon nitride particles having an average particle size of 0.5 to 10 μm are dispersed in an alloy matrix of 5 to 30 volume % and having an average particle size of 0.5 to 10 μm in an alloy base consisting of 0 weight % cobalt and the remainder substantially nickel slide against each other. It concerns the combination of dynamic surface layers.
水1発明の作用効果
潤滑材として作用する黒鉛を組織中に含有する鋳鉄以外
では、一般に同種の材料を組合せて摺動させると、摩耗
や焼付が甚だしくなるものである。Water 1 Functions and Effects of the Invention Except for cast iron, which contains graphite in its structure that acts as a lubricant, if similar materials are combined and slid together, wear and seizure will generally be severe.
ところが、本発明に基づく表面層の組合せでは、同種の
組成の表面層の組合せであるにも拘らず、耐摩耗性、耐
焼付性が極めて良好である。However, the combination of surface layers based on the present invention has extremely good wear resistance and seizure resistance, even though the surface layers have the same composition.
以下、表面層を構成する基地及びこの基地中に分散させ
る分散粒子について説明する。The base constituting the surface layer and the dispersed particles dispersed in the base will be explained below.
ニッケルは、後述するように、窒化珪素粒子と共にNi
3Siを生成し、更に燐と共にNi1Pを生成し、耐摩
耗性、耐焼付性に寄与する。As described later, nickel is used together with silicon nitride particles.
It generates 3Si and further generates Ni1P together with phosphorus, contributing to wear resistance and seizure resistance.
コバルトはニッケル中に固溶して硬度を上げ、耐摩耗性
、耐焼付性を改善すると共に表面層の圧壊強度及び疲労
強度を向上させる。基地中のコバルト含有量が10重量
%以上で上記の効果が顕著になる。また上記コバルト含
有量が40重量%を超えると相対的にニッケル含有量が
少なくなって、後述するNi、Si及びNL、Pの生成
量が少なく表面層の機械的強度が十分には改善されず、
その結果、耐摩耗性、耐焼付性改善の効果が不十分にな
る。従って基地中のコバルト含有量は40重量%以下と
する。Cobalt dissolves in nickel to increase hardness, improve wear resistance and seizure resistance, and improve the crushing strength and fatigue strength of the surface layer. The above effect becomes remarkable when the cobalt content in the base is 10% by weight or more. Furthermore, if the cobalt content exceeds 40% by weight, the nickel content will be relatively low, and the amount of Ni, Si, NL, and P produced, which will be described later, will be small, and the mechanical strength of the surface layer will not be sufficiently improved. ,
As a result, the effect of improving wear resistance and seizure resistance becomes insufficient. Therefore, the cobalt content in the base should be 40% by weight or less.
燐は、熱処理によって基地の硬度を上げて耐摩耗性、耐
焼付性改善に寄与する。即ち、ニッケルと燐とが反応し
て基地中にNi3Pの相が生成し、時効硬化に於ける析
出相による機械的強度改善に類似したメカニズムによっ
て基地の硬度を上げ、これによって耐摩耗性改善に寄与
する。かくして基地の硬度は650〜800HMVに上
昇し、後述する窒化珪素粒子による耐摩耗性改善や炭化
珪素繊維の機械的強度改善による耐摩耗性、耐焼付性改
善に加えて耐摩耗性、耐焼付性が更に改善される。Phosphorus increases the hardness of the base through heat treatment and contributes to improving wear resistance and seizure resistance. In other words, nickel and phosphorus react to form a Ni3P phase in the base, increasing the hardness of the base through a mechanism similar to the mechanical strength improvement caused by the precipitated phase during age hardening, thereby improving wear resistance. Contribute. In this way, the hardness of the base increases to 650 to 800 HMV, and in addition to the improved wear resistance and seizure resistance due to the improved wear resistance due to silicon nitride particles and the mechanical strength improvement of silicon carbide fibers, which will be described later. is further improved.
但し、この表面層と組合せる相手摺動表面層の窒化珪素
分散量は、5〜30容積%とする。両表面層の窒化珪素
粒子分散量が共に30容積%を超えると両表面層の摩耗
が増大する。熱処理は400℃に加熱の熱処理で良い。However, the amount of silicon nitride dispersed in the mating sliding surface layer to be combined with this surface layer is 5 to 30% by volume. When the amount of silicon nitride particles dispersed in both surface layers exceeds 30% by volume, wear of both surface layers increases. The heat treatment may be performed by heating to 400°C.
基地中の燐含有量が2重量%未満では上記の効果が顕著
ではなく、これが15重量%を超えると基地が脆くなっ
て表面層の衝撃強度や母材への被着性が悪(なり、その
結果、耐摩耗性、耐焼付性も劣化する。If the phosphorus content in the base is less than 2% by weight, the above effects will not be noticeable, and if it exceeds 15% by weight, the base will become brittle and the impact strength of the surface layer and adhesion to the base material will be poor. As a result, wear resistance and seizure resistance also deteriorate.
窒化珪素粒子は基地中に分散してハードスポットを形成
し、耐摩耗性、耐焼付性改善に寄与する。The silicon nitride particles are dispersed in the matrix and form hard spots, contributing to improved wear resistance and seizure resistance.
然し、炭化珪素のような鋭い端面を持たず、相手摺動面
を摩耗させる作用は少ない。その粒径は、0.5μm未
満では微細過ぎて耐摩耗性、耐焼付性改善の効果が顕著
ではなく、これが10,17mを超えて大きくなるとこ
の粒子がアブレイシブ材として作用し、却って互いに摺
動相手材の摩耗が進行するようになる。また粒子の分散
量は、5容積%未満では耐摩耗性、耐焼付性改善の効果
が顕著ではなく、これが40容積%を超えると表面層の
機械的強度が低下して却って耐摩耗性が劣化するように
なる。従って、基地中に粒径0.5〜10μmの窒化珪
素粒子を5〜40容積%分散させる。窒化珪素の粒子を
基地中に分散させると、400”c加熱の熱処理を施す
ことによって粒子表面にNi、Siが生成して基地と粒
子との接着効果が顕れ、表面層の機械的強度が一層改善
される。加熱温度が高過ぎると前記の接着効果が低減す
る。例えば600℃に4分間加熱すると窒化珪素粒子の
略全量がNL3Siになってしまう。また窒化珪素の粒
子による前記の耐摩耗性、耐焼付性改善の効果もなくな
ってしまう。However, unlike silicon carbide, it does not have sharp end faces and has little effect on abrading the mating sliding surface. If the particle size is less than 0.5 μm, it is too fine and the effect of improving wear resistance and seizure resistance is not significant. If it exceeds 10.17 m, the particles act as an abrasive material and instead slide against each other. Wear of the mating material progresses. Furthermore, if the dispersion amount of particles is less than 5% by volume, the effect of improving wear resistance and seizure resistance will not be significant, and if it exceeds 40% by volume, the mechanical strength of the surface layer will decrease and the wear resistance will deteriorate. I come to do it. Therefore, 5 to 40 volume % of silicon nitride particles having a particle size of 0.5 to 10 μm are dispersed in the matrix. When silicon nitride particles are dispersed in the base, Ni and Si are generated on the particle surface by heat treatment at 400"C, which creates an adhesive effect between the base and the particles, further increasing the mechanical strength of the surface layer. If the heating temperature is too high, the above-mentioned adhesion effect will be reduced.For example, if heated to 600°C for 4 minutes, almost all of the silicon nitride particles will become NL3Si.Also, the above-mentioned wear resistance due to the silicon nitride particles will be improved. , the effect of improving seizure resistance is also lost.
へ、実施例 以下、本発明の詳細な説明する。To, Example The present invention will be explained in detail below.
ピストンリング用材料として使用されている合金工具鋼
鋼材5KD61から断面5 M X 5 +uの角柱状
試料を採取し、試料の正方形端面にニッケルのストライ
クめっき層を介して厚さ100μmのめっき層を形成し
、400℃に5時間加熱の熱処理を施してからめっき層
表面を研磨仕上げし、試験片とした。A prismatic sample with a cross section of 5 M x 5 + u was taken from alloy tool steel 5KD61, which is used as a material for piston rings, and a 100 μm thick plating layer was formed on the square end surface of the sample via a nickel strike plating layer. After heat treatment at 400° C. for 5 hours, the surface of the plating layer was polished to obtain a test piece.
めっき浴としては、硫酸ニッケル、塩化ニッケル、硫酸
コバルト、次亜燐酸ソーダ及び硼酸からなる水溶液(め
っき液)に窒化珪素粉末を懸濁させためっき浴を使用し
、これらの配合量及び窒化珪素粉末の粒径を変化させて
めっき層の組成及び組織を変化させた。As a plating bath, a plating bath in which silicon nitride powder is suspended in an aqueous solution (plating solution) consisting of nickel sulfate, nickel chloride, cobalt sulfate, sodium hypophosphite, and boric acid is used, and the proportions of these and the silicon nitride powder are The composition and structure of the plating layer were changed by changing the particle size of the plating layer.
めっき浴の温度は50〜53℃、電流密度は8A/dt
J、めっき時間は2.5時間、めっき浴のp Hは浴組
成に応じて2.0〜3.0の間の所定の値とした。The temperature of the plating bath is 50-53℃, the current density is 8A/dt
J, the plating time was 2.5 hours, and the pH of the plating bath was set to a predetermined value between 2.0 and 3.0 depending on the bath composition.
これら試験片に対する摺動相手材としては、シリンダ用
アルミニウム合金A390の円板(直径80n1厚さ1
0fi)の表面に上記と同様にして次のようなめっき層
を形成させ、研磨仕上げを施した。As a sliding partner material for these test pieces, a circular plate of aluminum alloy A390 for cylinders (diameter 80n, thickness 1
The following plating layer was formed on the surface of 0fi) in the same manner as described above, and a polishing finish was applied.
このめっき層は、30重量%コバルト、5重量%燐、残
部が実質的にニッケルからなる基地中に、平均粒径0.
8μmの窒化珪素粒子が20容積%分散した組織のめっ
き層である。This plating layer is formed in a base consisting of 30% by weight cobalt, 5% by weight phosphorus, and the remainder substantially nickel, with an average grain size of 0.
The plating layer has a structure in which 20% by volume of silicon nitride particles of 8 μm are dispersed.
上記角柱試験片と円板試験片とを互いに摺動させ、焼付
試験及び摩耗試験を行った。試験方法は次の通りである
。The above-mentioned prismatic test piece and disc test piece were slid against each other, and a seizure test and a wear test were conducted. The test method is as follows.
塊仕拭鍍
試験装置は第9図及び第9図のX−X線に沿う矢視側面
図である第10図に概要を図解的に示すものであって、
ステータホルダ1に取外し可能に取付けられた前記円板
試験片2の中央には裏側から注油孔3を通じて潤滑油が
注油される。ステータホルダ1には図示しない油圧装置
によって図に於いて右方へ向けて所定圧力で押圧力Pが
作用するようにしである。円板試験片2に相対向してロ
ータ4があり、図示しない駆動装置によって所定速度で
回転するようにしである。ロータ4の円板試験片2に対
する端面に取付けられた試験片保持具4aには正方形端
面を摺動面として角柱試験片5が同心円上に等間隔に4
個取外し可能に、かつ円板試験片2に対して摺動自在に
取付けである。The lump-wiping plating test device is schematically shown in FIG. 9 and FIG. 10, which is a side view taken along the line X-X in FIG.
Lubricating oil is applied to the center of the disk test piece 2, which is removably attached to the stator holder 1, from the back side through an oil filling hole 3. A pressing force P is applied to the stator holder 1 by a hydraulic device (not shown) at a predetermined pressure toward the right in the figure. A rotor 4 is disposed opposite to the disk test piece 2, and is rotated at a predetermined speed by a drive device (not shown). A test piece holder 4a attached to the end face of the rotor 4 with respect to the disc test piece 2 has four prismatic test pieces 5 concentrically arranged at equal intervals with the square end face as a sliding surface.
It is attached so that it can be removed individually and slidably relative to the disk test piece 2.
このような装置において、ステータ1に所定の押圧力P
をかけ、所定の面圧で円板試験片2の表面層(めっき層
)2aと角柱試験片5の表面層(めっき層)5aとが接
触するようにしておいて、注油孔3から摺動面に所定給
油速度で給油しながらロータ4を回転させる。一定時間
毎にステータ1に作用する圧力を段階的に増加してゆき
、ロータ4の回転によって角柱試験片5と円板試験片2
との摩擦によってステータ1に生ずるトルク(摩擦力に
よって生ずるトルク)Tをスピンドル6を介してロート
セルフに作用せしめ、その変化を動歪計8で読み取り、
記録計9に記録させる。トルクTが急激に上昇するとき
に焼付が生じたものとし、その大小を以て耐焼付性の良
否を判断する。In such a device, a predetermined pressing force P is applied to the stator 1.
The surface layer (plating layer) 2a of the disk test piece 2 and the surface layer (plating layer) 5a of the prismatic test piece 5 are brought into contact with each other with a predetermined surface pressure, and the oil is slid from the oiling hole 3. The rotor 4 is rotated while lubricating the surface at a predetermined lubricating speed. The pressure applied to the stator 1 is increased stepwise at regular intervals, and the rotation of the rotor 4 causes the prismatic test piece 5 and the disc test piece 2 to be separated.
Torque T generated on the stator 1 due to friction with the stator (torque generated by frictional force) is applied to the rotor self via the spindle 6, and the change is read by the dynamic strain meter 8,
Record it on recorder 9. It is assumed that seizure has occurred when the torque T increases rapidly, and the quality of the seizure resistance is determined based on the magnitude of the increase.
試験条件は次に示す通りである。The test conditions are as follows.
摩擦速度= 8 m/sec
潤滑油 :加鉛ガソリンを燃料とする実機試験に供した
モータオイル5AE30
にダスト(3132種を0.2 g / I!添加した
もの(温度80℃))を
400a+ j! / win給油
接触圧カニ試験開始時40kg/cIK、その後3分間
経過毎に10kg/cjずつ上昇
輩用広腋
第9図、第10図の試験装置を使用し、次のような試験
条件で摩耗試験を行った。Friction speed = 8 m/sec Lubricating oil: 400a+j of dust (0.2 g/I! of type 3132 added (temperature 80°C)) to motor oil 5AE30, which was used in an actual machine test using leaded gasoline as fuel. ! / Win refueling contact pressure Crab test: 40kg/cIK at the start, then increased by 10kg/cJ every 3 minutes We conducted a test.
摩擦速度ば5 n’L / 3B(、接触圧力は100
kg/cdに一定、摩擦距離は1100k、潤滑油は加
鉛ガソリンを燃料としての実機テストに使用済みのエン
ジンオイルS A E N130にダスト(3132種
)を0.2 g / 1添加したもので温度80℃、そ
の他の試験条件は前記焼付試験に於けると同じである。Friction speed is 5 n'L / 3B (, contact pressure is 100
kg/cd constant, the friction distance is 1100k, and the lubricating oil is engine oil S A E N130, which has been used in actual machine tests using leaded gasoline as fuel, and dust (type 3132) is added at 0.2 g/1. The temperature was 80° C. and the other test conditions were the same as in the above-mentioned baking test.
摩耗量は次のようにして測定した。角柱試験片について
は、試験後に試験片を取り外し、摩耗による高さ寸法の
減少を測定した。円板試験片については、摩耗によって
生じた円環状の摩耗痕の深さを測定した。The amount of wear was measured as follows. Regarding the prismatic test piece, the test piece was removed after the test and the reduction in height due to wear was measured. Regarding the disk test piece, the depth of the annular wear scar caused by wear was measured.
試験結果は、第4図〜第7図に示す通りであった。The test results were as shown in FIGS. 4 to 7.
上記と同様にして、角柱試験片の表面層を4.5重量%
燐、27重量%コバルトのニッケル合金基地中に平均粒
径0.8μmの窒化珪素粒子を39容積%分散させたも
のとし、円板試験片の表面層を5重量%燐、30重景%
コバルト、残部ニッケルのニッケル合金基地中に平均粒
径0.8μmの窒化珪素粒子の分散量を5〜30容積%
の範囲で変化させ、同様の試験を行った。試験結果は第
8図に示す通りであった。In the same manner as above, the surface layer of the prismatic specimen was reduced to 4.5% by weight.
It is assumed that 39% by volume of silicon nitride particles with an average particle size of 0.8 μm are dispersed in a nickel alloy base of phosphorus and 27% by weight cobalt, and the surface layer of the disk specimen is 5% by weight phosphorus and 30% by weight.
Dispersion amount of silicon nitride particles with an average particle size of 0.8 μm in a nickel alloy base of cobalt and balance nickel is 5 to 30% by volume.
A similar test was conducted by changing the value within the range of . The test results were as shown in FIG.
第4図〜第8図から、互いに摺動する表面層の基地は、
2〜15重量%燐、10〜40重量%コバルトのニッケ
ル合金とし、これらの基地中に分散させる窒化珪素粒子
は、一方の表面層では平均粒径を0.5〜10μm、分
散量を5〜40容積%とし、他方の表面層では平均粒径
を0.5〜10μm、分散量を5〜30容積%とするの
が、良い結果が得られることが理解できる。From Figures 4 to 8, the bases of the surface layers that slide against each other are
A nickel alloy containing 2 to 15% by weight of phosphorus and 10 to 40% by weight of cobalt is used, and the silicon nitride particles dispersed in these bases have an average particle size of 0.5 to 10 μm and a dispersion amount of 5 to 10 μm in one surface layer. It can be seen that good results can be obtained by setting the average particle diameter to 0.5 to 10 μm and dispersing amount to 5 to 30 volume % in the other surface layer.
大檄拭腋
次に、ピストンリングの外周面とシリンダライチ内周面
とに本発明に基づく表面層を形成させ、これらを内燃機
関に組付けて実機試験を行った結果について説明する。Next, the results of an actual machine test in which a surface layer based on the present invention was formed on the outer circumferential surface of a piston ring and the inner circumferential surface of a cylinder litchi were assembled into an internal combustion engine will be described.
呼び径78m、幅1.5鶴、厚さ3.2fiの鋼製第一
圧力リングに、第一工程として外周面に通例のニッケル
ストライクめっきを施して厚さ108mのニッケルめっ
き層を形成した0次に第二工程として下記第1表に示す
浴組成及びめっき条件で窒化珪素粒子を分散させた厚さ
110μmのニッケルーコバルト−燐複合めっき層を前
記ニッケルめっき層上番こ形成した。The first steel pressure ring has a nominal diameter of 78 m, a width of 1.5 m, and a thickness of 3.2 m. As a first step, the outer circumferential surface is subjected to conventional nickel strike plating to form a 108 m thick nickel plating layer. Next, as a second step, a nickel-cobalt-phosphorus composite plating layer having a thickness of 110 μm in which silicon nitride particles were dispersed was formed on the nickel plating layer using the bath composition and plating conditions shown in Table 1 below.
第1表
シリンダライナはボア径78Mのアルミニウム合金A3
90製とし、ボア内周面に下記第2表に示す浴組成及び
めっき条件で窒化珪素粒子を分散させた厚さ120μm
のニッケルーコバルト−燐複合めっき層を形成した。Table 1 Cylinder liner is aluminum alloy A3 with bore diameter 78M
90, and silicon nitride particles were dispersed on the inner peripheral surface of the bore according to the bath composition and plating conditions shown in Table 2 below, and the thickness was 120 μm.
A nickel-cobalt-phosphorus composite plating layer was formed.
第2表
この複合めっき層の基地中の燐の量は445重量%、コ
バルトの量は30重量%、窒化珪素粒子の分散量は15
容積%であった。Table 2 The amount of phosphorus in the matrix of this composite plating layer is 445% by weight, the amount of cobalt is 30% by weight, and the amount of silicon nitride particles dispersed is 15% by weight.
It was % by volume.
第三工程としてピストンリングを400℃に1時間加熱
し、基地を硬化させた。この処理によって複合めっき層
の硬度はマイクロビッカース硬度800〜900となっ
た。In the third step, the piston ring was heated to 400° C. for 1 hour to harden the base. As a result of this treatment, the hardness of the composite plating layer became 800 to 900 on the micro Vickers hardness.
第1図はピストンリングの拡大断面図で、鋼の母材11
の外周面にニッケルめっき層12を介して複合めっき層
13が形成されている。第2図はシリンダライナの断面
図で、ボアにはアルミニウム合金の母材14上に複合め
っき層15が形成されている。Figure 1 is an enlarged sectional view of the piston ring, showing the steel base material 11.
A composite plating layer 13 is formed on the outer peripheral surface of the nickel plating layer 12 with a nickel plating layer 12 interposed therebetween. FIG. 2 is a sectional view of the cylinder liner, in which a composite plating layer 15 is formed on a base material 14 of aluminum alloy in the bore.
第3図はピストンリングの複合めっき層(第1図の13
)の組織を示す顕微鏡写真(倍率400倍)である。ニ
ッケル合金の基地中に、灰色を呈する窒化珪素粒子が均
一に分散しているのが観察される。なお、熱処理によっ
て基地に析出したNis P相、Ni3St相は、極め
て微細であって写真には顕われていないが、これらの相
の存在はX線回折試験によって確認されている。シリン
ダライナの複合めっき層(第2図の15)も第3図の組
織と実質的に同じであった。Figure 3 shows the composite plating layer of the piston ring (13 in Figure 1).
) is a micrograph (magnification: 400 times) showing the structure of. Gray silicon nitride particles are observed to be uniformly dispersed in the nickel alloy matrix. Note that the Nis P phase and Ni3St phase precipitated on the base by the heat treatment are extremely fine and are not visible in the photograph, but the existence of these phases has been confirmed by an X-ray diffraction test. The composite plating layer (15 in FIG. 2) of the cylinder liner also had substantially the same structure as that in FIG. 3.
上記ピストンリング及びシリンダライナを4サイクル、
水冷4気筒のガソリンに組付け、高鉛ガソリンを燃料と
して回転数860Orpm、全負荷、100時間のベン
チテストを行い、ピストンリング外周面及び上死点での
シリンダライナ内周面の摩耗量を測定した。4 cycles of the above piston ring and cylinder liner,
Assembled into a water-cooled 4-cylinder gasoline engine, a bench test was performed at 860 rpm, full load, and 100 hours using high-lead gasoline as fuel, and the amount of wear on the outer circumferential surface of the piston ring and the inner circumferential surface of the cylinder liner at top dead center was measured. did.
比較のために、シリンダライナは上記と同様のものを使
用し、ピストンリング表面層として硬質クロムめっき層
、17クロム鋼に形成した窒化層、又は炭化珪素粒子を
分散させた上記と同様のニッケル複合めっき層を形成し
たピストンリングの組合せについて同様の試験を行った
。For comparison, the same cylinder liner as above was used, and the piston ring surface layer was a hard chromium plating layer, a nitrided layer formed on 17 chromium steel, or a nickel composite similar to the above with silicon carbide particles dispersed. A similar test was conducted on a combination of piston rings on which a plating layer was formed.
試験結果は第11図に示す通りであった。摩耗量は、硬
質クロムめっき層を形成したピストンリングを使用した
ときの摩耗量に対する百分率で表しである。同図から、
実施例のピストンリングとシリンダライナとの組合せは
、比較の組合せに対して耐摩耗性が著しく改善されてい
る。17クロム鋼に窒化処理を施したピストンリングを
使用した場合は、摩耗量はかなり小さくなってはいるが
、軽いスカッフ(焼付き)が発生していた。これに対し
、実施例ではスカッフ発生の痕跡は認められなかった。The test results were as shown in FIG. The amount of wear is expressed as a percentage of the amount of wear when using a piston ring with a hard chromium plating layer formed thereon. From the same figure,
The combination of the piston ring and cylinder liner of the example has significantly improved wear resistance compared to the comparative combination. When piston rings made of 17 chrome steel were used, the amount of wear was considerably reduced, but slight scuffing (seizure) occurred. On the other hand, in Examples, no trace of scuffing was observed.
以上の結果から、本発明を内燃機関やコンプレッサ等の
ピストンリングとシリンダライナとの組合せに適用する
と、耐久性が著しく改善されることが理解できる。また
、シリンダライナの母材は任意の材料とでき、これをア
ルミニウム合金とすることにより内燃機関の軽量化を図
ることができる。この場合、シリンダブロックもアルミ
ニウム合金製とするのが効果的である。From the above results, it can be seen that when the present invention is applied to a combination of a piston ring and a cylinder liner of an internal combustion engine, a compressor, etc., the durability is significantly improved. Further, the base material of the cylinder liner can be made of any material, and by using an aluminum alloy as the base material, it is possible to reduce the weight of the internal combustion engine. In this case, it is effective to make the cylinder block also made of aluminum alloy.
図面はいずれも本発明の実施例を示すものであって−
第1図はピストンリングの拡大断面図、第2図はシリン
ダライナの断面図、
第3図はピストンリングの表面層の金属組織を示す顕微
鏡写真、
第4図、第5図、第6図、第7図及び第8図は表面層の
組成と耐摩耗性又は耐焼付性との関係を示すグラフ、
第9図は焼付試験、摩耗試験の装置の要部を示す一部破
砕正面図、
第10図は第9図のX−X線矢視側面図、第11図は実
機試験の結果を示すグラフである。
なお、図面に示された符号において、
2 ・・・・円板試験片
5 ・・・・角柱試験片
11・・・・ピストンリング母材
14・・−・シリンダライナ母材
2a、5a、13.15
・・・・表面層
である。The drawings all show embodiments of the present invention - Fig. 1 is an enlarged sectional view of a piston ring, Fig. 2 is a sectional view of a cylinder liner, and Fig. 3 shows a metallographic structure of the surface layer of the piston ring. 4, 5, 6, 7, and 8 are graphs showing the relationship between the composition of the surface layer and wear resistance or seizure resistance. FIG. 9 is a seizure test. FIG. 10 is a partially fragmented front view showing the main parts of the wear test device, FIG. 10 is a side view taken along the line X--X in FIG. 9, and FIG. 11 is a graph showing the results of the actual machine test. In addition, in the symbols shown in the drawings, 2...Disc test piece 5...Prismatic test piece 11...Piston ring base material 14...Cylinder liner base material 2a, 5a, 13 .15...Surface layer.
Claims (1)
部が実質的にニッケルからなる合金基地中に平均粒径0
.5〜10μmの窒化珪素粒子が5〜40容積%分散し
た第一の表面層と、2〜15重量%燐、10〜40重量
%コバルト、残部が実質的にニッケルからなる合金基地
中に平均粒径0.5〜10μmの窒化珪素粒子が5〜3
0容積%分散した第二の表面層とが互いに摺動する、摺
動表面層の組合せ。1.2 to 15% by weight phosphorus, 10 to 40% by weight cobalt, and the balance substantially nickel in an alloy matrix with an average grain size of 0.
.. A first surface layer in which silicon nitride particles of 5 to 10 μm are dispersed in an amount of 5 to 40% by volume, and an alloy base consisting of 2 to 15% by weight of phosphorus, 10 to 40% by weight of cobalt, and the remainder substantially nickel with average particles dispersed therein. 5 to 3 silicon nitride particles with a diameter of 0.5 to 10 μm
A combination of sliding surface layers in which a second surface layer with 0 volume % dispersion slides on each other.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP23816588A JPH0286946A (en) | 1988-09-22 | 1988-09-22 | Combination of sliding surface layers |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP23816588A JPH0286946A (en) | 1988-09-22 | 1988-09-22 | Combination of sliding surface layers |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH0286946A true JPH0286946A (en) | 1990-03-27 |
Family
ID=17026152
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP23816588A Pending JPH0286946A (en) | 1988-09-22 | 1988-09-22 | Combination of sliding surface layers |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0286946A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100595429C (en) | 2008-02-20 | 2010-03-24 | 江苏爱吉斯海珠机械有限公司 | Ocean-going ship engine cylinder liner and cylinder liner material |
-
1988
- 1988-09-22 JP JP23816588A patent/JPH0286946A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100595429C (en) | 2008-02-20 | 2010-03-24 | 江苏爱吉斯海珠机械有限公司 | Ocean-going ship engine cylinder liner and cylinder liner material |
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