JP2002021898A - Bonded structure of metallic material and friction material - Google Patents

Bonded structure of metallic material and friction material

Info

Publication number
JP2002021898A
JP2002021898A JP2000203128A JP2000203128A JP2002021898A JP 2002021898 A JP2002021898 A JP 2002021898A JP 2000203128 A JP2000203128 A JP 2000203128A JP 2000203128 A JP2000203128 A JP 2000203128A JP 2002021898 A JP2002021898 A JP 2002021898A
Authority
JP
Japan
Prior art keywords
adhesive
friction material
friction
metal material
bonding
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.)
Granted
Application number
JP2000203128A
Other languages
Japanese (ja)
Other versions
JP4588846B2 (en
Inventor
Takao Nakagawa
隆夫 中川
Toshiyuki Kanesaka
敏行 金坂
Noriko Hashimoto
徳子 橋本
Eiichi Kijima
栄一 木島
Takuhiro Tsuruoka
卓弘 鶴岡
Takashi Suzuki
隆司 鈴木
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Across Co Ltd
Isuzu Motors Ltd
Acros Corp
Original Assignee
Across Co Ltd
Isuzu Motors Ltd
Acros Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Across Co Ltd, Isuzu Motors Ltd, Acros Corp filed Critical Across Co Ltd
Priority to JP2000203128A priority Critical patent/JP4588846B2/en
Publication of JP2002021898A publication Critical patent/JP2002021898A/en
Application granted granted Critical
Publication of JP4588846B2 publication Critical patent/JP4588846B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

PROBLEM TO BE SOLVED: To provide bonded structure wherein a metallic material and a friction material different in the coefficient of linear expansion or surface roughness from the metallic material can be firmly bonded without the possibility of separation. SOLUTION: In this bonded structure of the metallic material 1 and the friction material 2 different in the coefficient of linear expansion or surface roughness from the metallic material 1, an adhesive cushion layer 6 with an adhesive 5 impregnated in unwoven fabric 4 formed of short carbon fiber 3 or the like is interposed between adhesive faces 1a, 2a of the metallic material 1 and friction material 2, and pressure-bonded and hardened by heating. A friction material 24 formed of a carbon fiber reinforced carbon composite sheet material is stuck to an inner peripheral surface 23 of a metal ring 29 through the adhesive cushion layer 6 formed of the unwoven fabric 4 of short carbon fiber 3 or the like impregnated with a phenol resin adhesive 5, and the friction material 24 is pressed to the metal ring 29 side and hardened by heating while compressing the adhesive cushion layer 6, to form a synchronizer ring.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】本発明は、金属材と摩擦材の
接着構造に係り、特に、金属材と、その金属材と線膨脹
係数又は表面粗度が異なる摩擦材の接着構造に関するも
のである。
The present invention relates to a bonding structure between a metal material and a friction material, and more particularly to a bonding structure between a metal material and a friction material having a different linear expansion coefficient or surface roughness from the metal material. .

【0002】[0002]

【従来の技術】使用環境が厳しく、高強度・高耐久性を
要求される自動車用の駆動系部品(例えば、トランスミ
ッション部品等)においては、主として金属、特に鋳鉄
材料が多用されているが、各部品毎に、要求される摺動
性、摩擦性等の各種特性が異なるため、材料改質又は特
性の異なる数種の材料を接合することによって、要求さ
れる各種特性を確保している。
2. Description of the Related Art Metals, especially cast iron materials, are mainly used in automobile drive system parts (for example, transmission parts, etc.) which are required to be used in a harsh environment and have high strength and high durability. Since various required characteristics such as slidability and frictional characteristics are different for each part, required various characteristics are secured by material modification or joining of several kinds of materials having different characteristics.

【0003】トランスミッション部品の一つであるシン
クロナイザ・リングは、図3に示すように、金属製(鋳
鉄製)のリング部31とコーン部32とを備えており、
このコーン部32の内周面33が、トランスミッション
のメインギヤ(図示せず)のコーン部外周面と摩擦係合
することによって、回転速度の異なる二つのギヤ(図示
せず)が同期する。
As shown in FIG. 3, a synchronizer ring, which is one of transmission components, includes a metal (cast iron) ring portion 31 and a cone portion 32.
When the inner peripheral surface 33 of the cone portion 32 frictionally engages with the outer peripheral surface of the cone portion of the main gear (not shown) of the transmission, two gears (not shown) having different rotation speeds are synchronized.

【0004】ここで、シンクロナイザ・リング30のコ
ーン部32の摩擦係合面(内周面33)は、トランスミ
ッションのメインギヤの摩擦係合面(コーン部外周面)
と摩擦係合されるため、十分な摩擦係数と耐摩耗性を有
している必要がある。このため、通常、コーン部32の
摩擦係合面に摩擦材(図示せず)を設けている。従来の
摩擦材としては、コーン部の摩擦係合面に設けられるC
u−Zn製ライナやMoの溶射被膜等が挙げられる。
Here, the frictional engagement surface (inner peripheral surface 33) of the cone portion 32 of the synchronizer ring 30 is the frictional engagement surface (cone outer peripheral surface) of the main gear of the transmission.
Therefore, it is necessary to have a sufficient friction coefficient and abrasion resistance. For this reason, a friction material (not shown) is usually provided on the friction engagement surface of the cone portion 32. As a conventional friction material, C is provided on a friction engagement surface of a cone portion.
Examples thereof include a u-Zn liner and a thermal spray coating of Mo.

【0005】近年、コーン部32の摩擦係合面に金属製
摩擦材を接合させたシンクロナイザ・リングの他に、金
属では出せない特性を付与すべく、コーン部32の摩擦
係合面に樹脂製(フェノール樹脂製)摩擦材を接合(接
着)し、より高強度接着性、熱膨張吸収性、耐高温性、
耐油性などの高性能な表面特性を確保したシンクロナイ
ザ・リングが提案されている。しかし、シンクロナイザ
・リングを含むトランスミッション部品は、トランスミ
ッションオイル中に浸漬されていると共に、このトラン
スミッションオイルは、車両の走行中、最高約140℃
にも達する。また、エンジン始動直後や、潤滑油が十分
に回らないような時には、摩擦材が破損する等の問題が
発生する。そこで、樹脂製摩擦材の代わりに、耐熱・耐
摩耗性に優れた炭素繊維強化炭素複合材料(以下、C−
Cコンポジットと示す)からなる摩擦材をコーン部32
の摩擦係合面に接合(接着)することが検討されてい
る。
In recent years, in addition to a synchronizer ring in which a friction material made of metal is joined to the friction engagement surface of the cone portion 32, a resin engagement surface of the cone portion 32 has (Made of phenolic resin) Friction material is joined (adhered) to provide higher strength adhesiveness, thermal expansion absorption, high temperature resistance,
Synchronizer rings that ensure high-performance surface characteristics such as oil resistance have been proposed. However, the transmission components, including the synchronizer ring, are immersed in the transmission oil and the transmission oil can be up to about 140 ° C during vehicle operation.
Also reach. Immediately after the start of the engine or when the lubricating oil does not rotate sufficiently, problems such as breakage of the friction material occur. Therefore, instead of a resin friction material, a carbon fiber reinforced carbon composite material (hereinafter referred to as C-
A friction material made of a C composite
It has been studied to join (adhere) to the frictional engagement surface of the.

【0006】[0006]

【発明が解決しようとする課題】ところで、従来の金属
製摩擦材を接合したシンクロナイザ・リングにおいて
は、金属材と金属製摩擦材(例えば、Cu−Zn材又は
Mo材等)の金属同士(同種材料間)の接合であるた
め、両材料の熱的特性差および表面粗度差が問題になる
ことは殆どなかった。
By the way, in a synchronizer ring in which a conventional metal friction material is joined, a metal material and a metal friction material (for example, Cu-Zn material or Mo material, etc.) are mutually connected (the same kind). (Material-to-material) bonding, there was almost no problem with differences in thermal characteristics and surface roughness between the two materials.

【0007】これに対して、C−Cコンポジット製の摩
擦材を用いたシンクロナイザ・リングにおいては、金属
材と摩擦材の接着が異種材料間であるため、両材料の熱
的特性差および表面粗度差に起因する不具合が生じるこ
とが有る。
On the other hand, in a synchronizer ring using a friction material made of a CC composite, the difference between the thermal characteristics and the surface roughness of the two materials is caused by the adhesion between the metal material and the friction material between different materials. Problems due to the difference may occur.

【0008】すなわち、金属材とC−Cコンポジット製
の摩擦材とでは、線膨張係数が大きく異なることから、
両材料の接着部が高温に晒されると、接着界面に剪断応
力が働く。その結果、接着部が剪断破壊され、両材料が
剥離してしまうという現象を引き起こす。
That is, since the coefficient of linear expansion differs greatly between a metal material and a friction material made of a CC composite,
When the bond between the two materials is exposed to high temperatures, a shear stress acts on the bond interface. As a result, a phenomenon occurs in which the bonded portion is sheared and broken, and both materials are peeled off.

【0009】また、金属材とC−Cコンポジット製摩擦
材とでは、表面処理加工の加工精度が異なることから、
両材料の表面粗度が異なっている。このため、ミクロ的
には接着面間のクリアランスが不均一となることから、
両材料の接着面において接着不良などの問題が生じるお
それがあり、両材料を強固に接着することは非常に困難
である。
Further, since the processing accuracy of the surface treatment differs between the metal material and the friction material made of the CC composite,
The surface roughness of both materials is different. For this reason, microscopically, the clearance between the bonding surfaces becomes non-uniform,
There is a possibility that a problem such as poor bonding may occur on the bonding surface of both materials, and it is very difficult to firmly bond both materials.

【0010】以上の事情を考慮して創案された本発明の
目的は、金属材と、その金属材と線膨脹係数又は表面粗
度が異なる摩擦材とを、剥離のおそれなく強固に接着す
ることができる接着構造及びその接着方法を提供するこ
とにある。
An object of the present invention, which has been made in view of the above circumstances, is to firmly bond a metal material and a friction material having a different linear expansion coefficient or surface roughness from the metal material without fear of peeling. An object of the present invention is to provide a bonding structure and a bonding method thereof.

【0011】[0011]

【課題を解決するための手段】上記目的を達成すべく本
発明に係る金属材と摩擦材の接着構造は、金属材と、そ
の金属材と線膨脹係数又は表面粗度が異なる摩擦材との
接着構造において、炭素短繊維等からなる不織布に接着
剤を含浸させた接着クッション層を上記金属材と摩擦材
の接着面間に介在させると共に圧着させて加熱硬化させ
たものである。
In order to achieve the above object, the bonding structure of a metal material and a friction material according to the present invention comprises a metal material and a friction material having a different linear expansion coefficient or surface roughness from the metal material. In the adhesive structure, an adhesive cushion layer obtained by impregnating an adhesive into a nonwoven fabric made of short carbon fiber or the like is interposed between the adhesive surfaces of the metal material and the friction material, and is pressed and heat-cured.

【0012】また、上記金属材が鋳鉄、上記摩擦材が炭
素繊維強化炭素複合材で構成されていてもよい。
Further, the metal material may be made of cast iron, and the friction material may be made of a carbon fiber reinforced carbon composite material.

【0013】さらに、上記金属材及び上記摩擦材の各接
着面に、フェノール樹脂系等の接着剤からなる接着層を
予め形成して接着クッション層を介在させていてもよ
い。
Furthermore, an adhesive layer made of an adhesive such as a phenolic resin may be previously formed on each of the adhesive surfaces of the metal material and the friction material, and an adhesive cushion layer may be interposed.

【0014】また、上記金属材及び上記摩擦材の各接着
面に、フェノール樹脂系等の接着剤を予め塗布してお
き、その後、金属材と摩擦材の接着面間に上記接着クッ
ション材を介在させていてもよい。
An adhesive such as a phenolic resin is previously applied to each of the bonding surfaces of the metal material and the friction material, and then the bonding cushion material is interposed between the bonding surfaces of the metal material and the friction material. You may let it.

【0015】さらに、上記金属が変速装置のシンクロナ
イザ・リングであってもよい。
Furthermore, the metal may be a synchronizer ring of a transmission.

【0016】また、上記摩擦材が、上記金属リングの内
周面の周方向に亘って設けられた多数の炭素繊維強化炭
素複合シート片で構成されていてもよい。
Further, the friction material may be composed of a large number of carbon fiber reinforced carbon composite sheet pieces provided in a circumferential direction of an inner peripheral surface of the metal ring.

【0017】以上の接着構造によれば、金属材と摩擦材
の接着面間に設けた接着クッション層が、両材料の線膨
脹係数の違いに起因する伸び率の相違を緩衝、又は両材
料の表面粗度の違いに起因する接着面間の不均一なクリ
アランスを吸収するため、両材料の線膨脹係数又は表面
粗度が異なっていても、両材料を剥離のおそれなく強固
に接着することができる。
According to the above-described bonding structure, the bonding cushion layer provided between the bonding surfaces of the metal material and the friction material buffers the difference in elongation caused by the difference in the linear expansion coefficient between the two materials, or reduces the difference between the two materials. In order to absorb the uneven clearance between the bonding surfaces due to the difference in surface roughness, even if both materials have different linear expansion coefficients or surface roughness, both materials can be firmly bonded without fear of peeling. it can.

【0018】また、シンクロナイザ・リングの摩擦材
を、耐熱性及び耐摩耗性に優れたC−Cコンポジットで
形成することで、シンクロナイザ・リングの耐久性・信
頼性がより向上する。また、金属リングと摩擦材(C−
Cコンポジット)とは、線膨脹係数及び表面粗度が異な
っているものの、金属リングと摩擦材との間に介在させ
た接着クッション層が、両材料の線膨脹係数の違いに起
因する伸び率の相違を緩衝し、両材料の表面粗度の違い
に起因する接着面間の不均一なクリアランスを吸収す
る。このため、金属リングから摩擦材が剥離するおそれ
がないと共に、金属リングと摩擦材とを強固に接着する
ことができる。
Further, by forming the friction material of the synchronizer ring with a CC composite having excellent heat resistance and wear resistance, the durability and reliability of the synchronizer ring are further improved. In addition, metal ring and friction material (C-
C composite) means that although the coefficient of linear expansion and the surface roughness are different, the adhesive cushion layer interposed between the metal ring and the friction material causes the elongation of the material due to the difference in the coefficient of linear expansion between the two materials. Buffers for differences and absorbs uneven clearance between the bonded surfaces due to differences in surface roughness between the two materials. Therefore, there is no possibility that the friction material is separated from the metal ring, and the metal ring and the friction material can be firmly bonded.

【0019】[0019]

【発明の実施の形態】以下、本発明の好適一実施の形態
を添付図面に基いて説明する。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS A preferred embodiment of the present invention will be described below with reference to the accompanying drawings.

【0020】一般に、異種材料間の接着(即ち、金属材
と、その金属材と線膨脹係数又は表面粗度が大きく異な
る摩擦材との接着)を行う場合、ゴム状弾性を有する接
着剤を用いたり、接着層の層厚を厚くすることにより、
前述した接着界面における剪断応力を緩和し、線膨張係
数の違いに起因する材料の剥離を防ぐことができる。
Generally, when bonding between different materials (that is, bonding between a metal material and a friction material having a significantly different coefficient of linear expansion or surface roughness from the metal material), an adhesive having rubber-like elasticity is used. Or by increasing the thickness of the adhesive layer,
The above-described shear stress at the bonding interface can be reduced, and peeling of the material due to a difference in linear expansion coefficient can be prevented.

【0021】しかしながら、例えば、シンクロナイザ・
リングの摩擦係合面等のように、大きな応力が負荷され
る部位においては、接着部が十分な接着強度を有してい
ることも重要となってくる。このため、ゴム状弾性を有
する接着剤による接着では十分な接着強度を得ることが
できず(一般的に、ゴム状弾性を有する接着剤の接着強
度は低い)、接着部が剪断破壊される又は接着層自体が
壊れるおそれがある。また、低ゴム状弾性タイプの硬い
接着剤を用いて接着層を厚く形成した場合においても、
接着剤自体が脆いことから、結果として両材料の剥離を
招くおそれがある。
However, for example, a synchronizer
In a portion where a large stress is applied, such as a friction engagement surface of a ring, it is also important that the bonding portion has a sufficient bonding strength. For this reason, sufficient bonding strength cannot be obtained by bonding with an adhesive having rubber-like elasticity (generally, the bonding strength of the adhesive having rubber-like elasticity is low), and the bonding portion is sheared or broken. The adhesive layer itself may be broken. Also, even when the adhesive layer is formed thick using a low rubber-like elastic type hard adhesive,
Since the adhesive itself is brittle, there is a possibility that both materials will be peeled off as a result.

【0022】このため、異種材料間の接着部を有するシ
ンクロナイザ・リングの摩擦係合面において、十分な接
着強度を確保するには、低ゴム状弾性タイプの硬い接着
剤を用いると共に接着層を薄く形成する必要があるが、
前述した異種材料間の接着条件と矛盾してしまう。
For this reason, in order to secure sufficient adhesive strength on the frictional engagement surface of the synchronizer ring having an adhesive portion between dissimilar materials, a low rubber-like elastic type hard adhesive is used and the adhesive layer is made thin. Need to be formed,
This is inconsistent with the bonding conditions between different materials described above.

【0023】また、シンクロナイザ・リングの摩擦係合
面に、金属製リング材と線膨脹係数又は表面粗度が大き
く異なる摩擦材(例えば、C−Cコンポジット製摩擦
材)を接着するための接着剤には、高強度接着性、熱膨
張吸収性、クリアランス吸収性、耐高温性、耐油性等の
特性が要求される。現在、高強度接着性及び耐高温性が
要求される条件下で使用されている接着剤として、耐熱
性、耐油性に優れるフェノール樹脂系接着剤があり、こ
のフェノール樹脂系接着剤を、シンクロナイザ・リング
の摩擦係合面における金属材とC−Cコンポジット製摩
擦材との接着に適用することが検討されている。フェノ
ール樹脂系接着剤は加熱硬化時にガス(気泡)が発生す
るが、このガスを接着層から放出させないと、ガスによ
る接着層の破壊が生じ、接着強度の低下を招く。このた
め、通常、加熱硬化の際に5〜15kgf/cm2 程度
で加圧し、ガス抜きが行われる。
An adhesive for adhering a friction material (for example, a C-C composite friction material) having a significantly different linear expansion coefficient or surface roughness from the metal ring material to the friction engagement surface of the synchronizer ring. Are required to have properties such as high-strength adhesiveness, thermal expansion absorption, clearance absorption, high-temperature resistance, and oil resistance. At present, there is a phenolic resin adhesive having excellent heat resistance and oil resistance as an adhesive used under conditions requiring high-strength adhesiveness and high temperature resistance. It has been studied to apply the present invention to adhesion between a metal material and a C-C composite friction material on a friction engagement surface of a ring. The phenolic resin adhesive generates gas (bubbles) at the time of heat curing, but if this gas is not released from the adhesive layer, the gas will destroy the adhesive layer, resulting in a decrease in adhesive strength. For this reason, usually, pressure is applied at about 5 to 15 kgf / cm 2 during heat curing to degas.

【0024】ここで、両材料の接着面間には、前述した
ように、表面粗度の違いに起因する不均一なクリアラン
スが存在していることから、両材料の接着に用いる接着
剤には、この不均一なクリアランスを充填(吸収)する
役割も期待される。しかし、フェノール樹脂系接着剤に
おいて、クリアランス吸収のために加熱硬化の際の圧力
を減じると、接着強度が十分に発現しなくなることか
ら、クリアランス吸収と高接着強度の両方の達成は困難
である。よって、シンクロナイザ・リングの摩擦係合面
に、フェノール樹脂系接着剤をそのまま適用することは
困難であった。
Here, as described above, there is an uneven clearance between the bonding surfaces of the two materials due to the difference in the surface roughness. The role of filling (absorbing) the uneven clearance is also expected. However, in a phenolic resin-based adhesive, if the pressure at the time of heat curing is reduced to absorb the clearance, the adhesive strength will not be sufficiently exhibited, so that it is difficult to achieve both the clearance absorption and the high adhesive strength. Therefore, it has been difficult to apply the phenol resin-based adhesive as it is to the frictional engagement surface of the synchronizer ring.

【0025】本発明者らは、金属材と摩擦材の接着のた
めの接着剤として耐熱性及び耐油性に優れるフェノール
樹脂系接着剤を用いると共に、接着層の層厚はできるだ
け薄くし、また、その接着層に、金属材と摩擦材の線膨
脹係数の違いに起因する伸び率の相違を緩衝、又は両材
料の表面粗度の違いに起因する接着面間の不均一なクリ
アランスを吸収する緩衝・吸収機能を持たせるべく、鋭
意研究を行った。
The present inventors used a phenolic resin adhesive having excellent heat resistance and oil resistance as an adhesive for bonding a metal material and a friction material, and made the thickness of the adhesive layer as thin as possible. The adhesive layer buffers the difference in elongation caused by the difference in linear expansion coefficient between the metal material and the friction material, or absorbs the uneven clearance between the bonded surfaces caused by the difference in the surface roughness of both materials.・ Dedicated research was conducted to provide an absorption function.

【0026】本発明に係る金属材と摩擦材の接着構造の
断面模式図を図1に示す。ここで、図1(b)は、図1
(a)の要部Aの拡大図である本発明に係る金属材と摩
擦材の接着構造は、図1に示すように、炭素短繊維(又
はガラス短繊維)3からなる不織布4にフェノール樹脂
系接着剤(又はアクリル樹脂系接着剤)5を含浸させた
接着クッション層6を、金属材1と摩擦材2との接着面
1a,2a間に介在させると共に圧着させて加熱硬化
(又は硬化)させたものである。
FIG. 1 is a schematic cross-sectional view of a bonding structure between a metal material and a friction material according to the present invention. Here, FIG.
As shown in FIG. 1, the bonding structure of the metal material and the friction material according to the present invention, which is an enlarged view of the main part A of FIG. An adhesive cushion layer 6 impregnated with a system-based adhesive (or an acrylic resin-based adhesive) 5 is interposed between the bonding surfaces 1a and 2a of the metal material 1 and the friction material 2 and pressed and heat-cured (or cured). It was made.

【0027】また、金属材1及び摩擦材2の各接着面1
a,2aに、フェノール樹脂系接着剤(又はアクリル樹
脂系接着剤)からなる接着層(図示せず)を予め形成し
て接着クッション層6を介在させてもよい。
Each of the bonding surfaces 1 of the metal material 1 and the friction material 2
An adhesive layer (not shown) made of a phenol resin-based adhesive (or an acrylic resin-based adhesive) may be formed in advance on a and 2a, and the adhesive cushion layer 6 may be interposed.

【0028】ここで、金属材1としては特に限定するも
のではなく、例えば、Fe合金、Al又はAl合金、T
i又はTi合金などが挙げられるが、特に鋳鉄が好まし
い。
Here, the metal material 1 is not particularly limited, and may be, for example, Fe alloy, Al or Al alloy, T
Although i or Ti alloy is mentioned, cast iron is particularly preferable.

【0029】摩擦材2としては、金属材1と線膨脹係数
が異なる材料であれば、金属材又は非金属材のどちらで
あってもよいが、耐熱性及び耐摩耗性に優れたC−Cコ
ンポジットが特に好ましい。
The friction material 2 may be either a metal material or a non-metal material as long as the material has a different linear expansion coefficient from the metal material 1. However, the friction material 2 is a C--C material having excellent heat resistance and wear resistance. Composites are particularly preferred.

【0030】摩擦材2としてC−Cコンポジットを用い
る場合、C−Cコンポジットを構成する炭素繊維(炭素
長繊維)としては、繊維長は特に指定しないが、繊維径
Dが0.002〜0.010mm、好ましくは0.00
5〜0.007mmのものが挙げられる。また、C−C
コンポジットにおける炭素繊維の配向性は、所望の摩擦
係数に応じて適宜設定されるものであって、特に限定す
るものではなく、この配向性を調節することによってC
−Cコンポジットの摩擦係数を任意に調節することが可
能となる。
When a CC composite is used as the friction material 2, the carbon fiber (carbon long fiber) constituting the CC composite is not particularly limited in fiber length, but has a fiber diameter D of 0.002-0. 010 mm, preferably 0.00
One having a thickness of 5 to 0.007 mm is exemplified. Also, C-C
The orientation of the carbon fibers in the composite is appropriately set in accordance with the desired coefficient of friction, and is not particularly limited.
It is possible to arbitrarily adjust the friction coefficient of the -C composite.

【0031】炭素短繊維(又はガラス短繊維)3として
は、不織布を形成可能な繊維であれば特に限定するもの
ではないが、クリアランス吸収性を考慮すると、繊維長
Lが10〜20mm、好ましくは14〜16mm、繊維
径Dが0.5〜1.0μm、好ましくは0.6〜0.8
μmのものが挙げられる。
The short carbon fiber (or short glass fiber) 3 is not particularly limited as long as it is a fiber capable of forming a nonwoven fabric. However, considering the clearance absorbency, the fiber length L is preferably 10 to 20 mm, and more preferably 10 to 20 mm. 14 to 16 mm, fiber diameter D is 0.5 to 1.0 μm, preferably 0.6 to 0.8
μm.

【0032】不織布4の布厚は、あまり薄いとフェノー
ル樹脂系接着剤(又はアクリル樹脂系接着剤)5の含浸
が不可能であり、逆に、あまり厚いと接着クッション層
6の層厚が厚くなるため、1.5〜2.5mmが好まし
く、2mm前後が特に好ましい。また、不織布4の密度
は、あまり低いとフェノール樹脂系接着剤5の含浸が不
可能であり、逆に、あまり高いとフェノール樹脂系接着
剤5が含浸しにくくなるため、目付量2.5〜3.5m
g/cm2 が好ましい。
If the thickness of the nonwoven fabric 4 is too small, it is impossible to impregnate the phenolic resin adhesive (or the acrylic resin adhesive) 5, and if it is too thick, the thickness of the adhesive cushion layer 6 is too large. Therefore, the thickness is preferably 1.5 to 2.5 mm, and particularly preferably about 2 mm. On the other hand, if the density of the nonwoven fabric 4 is too low, the impregnation of the phenolic resin adhesive 5 is impossible, and if the density is too high, the impregnation of the phenolic resin adhesive 5 becomes difficult. 3.5m
g / cm 2 is preferred.

【0033】不織布4に含浸させる接着剤5としてはフ
ェノール樹脂系、エポキシ樹脂系、ポリエステル樹脂
系、又はアクリル樹脂系などの接着剤であっても良い
が、高温での接着強度が要求される場合はフェノール樹
脂系接着剤の方が好ましい。
The adhesive 5 to be impregnated into the nonwoven fabric 4 may be a phenol resin-based, epoxy resin-based, polyester resin-based, or acrylic resin-based adhesive. Is preferably a phenolic resin adhesive.

【0034】次に、本発明に係る金属材と摩擦材の接着
方法を図1を用いて説明する。
Next, a method of bonding a metal material and a friction material according to the present invention will be described with reference to FIG.

【0035】図1(b)に示す炭素短繊維3の不織布4
にフェノール樹脂系接着剤5を含浸させ、予め接着クッ
ション材(図示せず)を形成しておく。この接着クッシ
ョン材を、60〜100℃×10〜60min、好まし
くは70〜90℃×20〜40minの温度条件で加熱
して予備硬化を行い、フェノール樹脂系接着剤5中の溶
剤を揮発させる。
The nonwoven fabric 4 of the short carbon fiber 3 shown in FIG.
Is impregnated with a phenolic resin-based adhesive 5 to form an adhesive cushion material (not shown) in advance. This adhesive cushion material is heated at a temperature of 60 to 100 ° C. × 10 to 60 min, preferably 70 to 90 ° C. × 20 to 40 min to perform pre-curing, thereby evaporating the solvent in the phenolic resin adhesive 5.

【0036】この予備硬化後の接着クッション材を、金
属材1と、その金属材1と線膨脹係数又は表面粗度が大
きく異なる摩擦材2の接着面1a,2a間に介在させ
る。この介在に先立って、金属材1及び摩擦材2の各接
着面1a,2aにもフェノール樹脂系接着剤を予め塗布
しておくと共に、予備硬化を行っておくとよい。両材料
1,2の各接着面1a,2aに塗布するフェノール樹脂
系接着剤としては、接着クッション材に含浸させるフェ
ノール樹脂系接着剤5よりも粘度の高いものが好まし
い。
The adhesive cushion material after the pre-curing is interposed between the metal material 1 and the adhesive surfaces 1a, 2a of the friction material 2 having a significantly different linear expansion coefficient or surface roughness from the metal material 1. Prior to this interposition, it is preferable to apply a phenol resin-based adhesive to each of the bonding surfaces 1a and 2a of the metal material 1 and the friction material 2 in advance, and to perform preliminary curing. The phenolic resin-based adhesive applied to each of the bonding surfaces 1a and 2a of both materials 1 and 2 is preferably one having a higher viscosity than the phenolic resin-based adhesive 5 impregnated in the adhesive cushioning material.

【0037】その後、金属材1と摩擦材2を、約0.5
〜1.5MPa(5〜15kgf/cm2 )の圧力で押
圧し、接着クッション材を圧縮しながらフェノール樹脂
系接着剤5を130〜230℃×30〜90min、好
ましくは160〜200℃×40〜80minの温度条
件で加熱硬化させる。これによって、図1(a)に示す
ように、金属材1と摩擦材2とが、接着クッション層6
を介して接着される。
After that, the metal material 1 and the friction material 2 are
The phenolic resin-based adhesive 5 is pressed at 130 to 230 ° C. × 30 to 90 min, preferably 160 to 200 ° C. × 40 to 40 mm while compressing the adhesive cushion material by pressing at a pressure of 1.5 to 1.5 MPa (5 to 15 kgf / cm 2 ). Heat and cure under a temperature condition of 80 min. As a result, as shown in FIG. 1A, the metal material 1 and the friction material 2
Glued through.

【0038】ここで、接着クッション層6をミクロ的に
見ると、図1(b)に示す炭素短繊維3a,3b,3c
で囲まれた領域Bは非常に微小であり、この微小領域B
が、硬い接着剤であるフェノール樹脂系接着剤5で充填
されていると共に、接着クッション層6の水平方向及び
層厚方向にランダムに配置されている。別の見方をすれ
ば、微小領域Bは、硬い接着剤による微小な接着領域と
見なすことができることから、接着クッション層6にお
ける炭素短繊維3群はフェノール樹脂系接着剤5で互い
に強固に接着(固着)され、結果的に、両材料1,2が
強固に接着される。一方、接着クッション層6をマクロ
的に見ると、フェノール樹脂系接着剤5の接着層が炭素
短繊維3群で繊維補強されていることから、接着クッシ
ョン層6は、全方向に対して僅かながら動き(伸縮)に
余裕があり、硬く、かつ、“しなやか”な(靱性の高
い)層となる。
Here, when the adhesive cushion layer 6 is viewed microscopically, the short carbon fibers 3a, 3b, 3c shown in FIG.
The region B surrounded by is very small.
Are filled with a phenol resin-based adhesive 5 which is a hard adhesive, and are randomly arranged in the horizontal direction and the layer thickness direction of the adhesive cushion layer 6. From another point of view, since the minute region B can be regarded as a minute adhesive region made of a hard adhesive, the short carbon fibers 3 in the adhesive cushion layer 6 are strongly adhered to each other by the phenol resin adhesive 5 ( As a result, both materials 1 and 2 are firmly bonded. On the other hand, macroscopically, the adhesive cushion layer 6 is slightly reinforced in all directions because the adhesive layer of the phenolic resin-based adhesive 5 is fiber-reinforced by the short carbon fiber 3 group. It is a hard and “flexible” (high toughness) layer that has room for movement (expansion and contraction).

【0039】通常、フェノール樹脂系接着剤5の接着層
は硬く、非常に脆いことから、フェノール樹脂系接着剤
5のみで形成した層厚の厚い接着層を、シンクロナイザ
・リングの摩擦係合面等のように大きな応力が負荷され
る部位に適用することは困難であった。これに対して、
接着クッション層6は、炭素短繊維3群を含んでいる
分、層厚が厚くなっているものの、前述のように硬く、
かつ、靱性の高い層であることから、大きな応力が負荷
されても壊れるおそれがない。また、層厚が厚いことに
より、両材料1,2の線膨張係数の違いに起因する剪断
応力を、接着クッション層6全体に分散することがで
き、異材接合時に懸念される剥離現象を防止することが
可能となる。
Usually, since the adhesive layer of the phenolic resin adhesive 5 is hard and very brittle, a thick adhesive layer formed only of the phenolic resin adhesive 5 is used for the frictional engagement surface of the synchronizer ring. However, it is difficult to apply the method to a part where a large stress is applied as described above. On the contrary,
Although the adhesive cushion layer 6 is thick as much as it includes the short carbon fiber 3 group, it is hard as described above,
And since it is a layer with high toughness, there is no possibility of breakage even when a large stress is applied. In addition, since the layer thickness is large, the shear stress caused by the difference in the linear expansion coefficient between the two materials 1 and 2 can be dispersed throughout the adhesive cushion layer 6, thereby preventing a peeling phenomenon that is a concern at the time of joining dissimilar materials. It becomes possible.

【0040】また、両材料1,2の接着面1a,2a
を、接着クッション材を介在させて接着する際に、十分
な圧力で圧着しながら加熱硬化させているため、十分な
接着強度を得ることができる。
The bonding surfaces 1a, 2a of the two materials 1, 2
Is bonded by interposing an adhesive cushion material, and is heated and cured while being pressed with a sufficient pressure, so that a sufficient bonding strength can be obtained.

【0041】さらに、接着クッション材は、面圧を加え
ることにより所定の範囲内で面形状の変形が自在である
ことから、前述のように十分な圧力で圧着を行っても、
接着クッション材が、両材料1,2の接着面1a,2a
間の不均一なクリアランスを充填(吸収)するように変
形し、かつ、炭素短繊維3自身の圧縮剛性により接着ク
ッション材が所定の範囲を超えて圧縮変形することはな
い。このため、両材料1,2の接着面1a,2a間に、
両材料1,2の表面粗度の違いに起因する不均一なクリ
アランスが存在しても、金属材1と接着クッション層6
との間及び摩擦材2と接着クッション層6との間に接着
不良などの問題が生じるおそれはない。
Further, since the surface of the adhesive cushion material can be freely deformed within a predetermined range by applying a surface pressure, even if the pressure is applied under a sufficient pressure as described above,
The bonding cushion material is used as the bonding surface 1a, 2a
The adhesive cushion material is not deformed so as to fill (absorb) the uneven clearance therebetween and the compression stiffness of the short carbon fiber 3 itself exceeds a predetermined range. For this reason, between the bonding surfaces 1a, 2a of both materials 1, 2,
Even if there is uneven clearance due to the difference in surface roughness between the two materials 1 and 2, the metal material 1 and the adhesive cushion layer 6
And between the friction material 2 and the adhesive cushion layer 6, there is no possibility of a problem such as poor adhesion.

【0042】また更に、金属材1と摩擦材2の組合わせ
としては、両者とも表面の粗い金属材からなる金属材1
と摩擦材2、表面の粗い金属材からなる金属材1とC−
Cコンポジットからなる摩擦材2であってもよく、この
場合、金属材1又は摩擦材2の表面処理が不要となるこ
とから、製造工程が簡易となると共に製造コストの削減
を図ることができる。
Further, as a combination of the metal material 1 and the friction material 2, both of the metal materials 1 made of a metal material having a rough surface are used.
And friction material 2, metal material 1 made of metal material having a rough surface and C-
The friction material 2 made of a C composite may be used. In this case, since the surface treatment of the metal material 1 or the friction material 2 becomes unnecessary, the manufacturing process can be simplified and the manufacturing cost can be reduced.

【0043】以上のことから、かかる金属材と摩擦材の
接着構造及びその接着方法によれば、金属材と摩擦材と
を、損壊・剥離のおそれなく強固に接着することができ
る。
As described above, according to the bonding structure of the metal material and the friction material and the method of bonding the metal material and the friction material, the metal material and the friction material can be firmly bonded without fear of damage or peeling.

【0044】尚、本実施の形態においては、フェノール
樹脂系接着剤を用いた場合について説明を行ったが、ア
クリル樹脂系接着剤を用いても略同様の効果が得られる
ことは言うまでもない。
In this embodiment, the case where the phenol resin-based adhesive is used has been described. However, it is needless to say that substantially the same effect can be obtained by using the acrylic resin-based adhesive.

【0045】次に、本発明の他の実施の形態を添付図面
に基いて説明する。
Next, another embodiment of the present invention will be described with reference to the accompanying drawings.

【0046】本発明に係るシンクロナイザ・リングの好
適一実施の形態の斜視図を図2に示す。
FIG. 2 is a perspective view of a preferred embodiment of the synchronizer ring according to the present invention.

【0047】図2に示すように、本発明に係るシンクロ
ナイザ・リング20は、金属製(鋳鉄製)のリング部2
1とコーン部22とを備えたリング本体(金属リング)
29の、コーン部22の内周面に、図1に示したフェノ
ール樹脂系接着剤5を含浸させた炭素短繊維(又はガラ
ス短繊維)3の不織布4からなる接着クッション層6を
介して、炭素繊維強化炭素複合シート(以下、C−Cシ
ートと示す)材からなる摩擦材24を貼り付け、その摩
擦材24をコーン部22側に押圧させて接着クッション
層6を圧縮させながら加熱硬化させたものである。
As shown in FIG. 2, the synchronizer ring 20 according to the present invention comprises a metal (cast iron) ring portion 2.
Ring body (metal ring) provided with 1 and cone portion 22
29, an adhesive cushion layer 6 made of a nonwoven fabric 4 of carbon short fibers (or glass short fibers) 3 impregnated with the phenolic resin adhesive 5 shown in FIG. A friction material 24 made of a carbon fiber reinforced carbon composite sheet (hereinafter, referred to as a CC sheet) material is adhered, and the friction material 24 is pressed toward the cone portion 22 to be heated and cured while compressing the adhesive cushion layer 6. It is a thing.

【0048】摩擦材24は、コーン部22の内周面の周
方向に亘って設けられた多数のC−Cシート片25で構
成されており、各C−Cシート片25は、隣接するC−
Cシート片25と所定の間隔を有して設けられている。
また、摩擦材24は、必要に応じて軸方向(図2中では
上下方向)に多段に設けても良い(図2中では2段)。
ここで、各C−Cシート片25の非貼付面(摩擦係合
面)には、コーン部22の内周面の周方向に沿って油切
り溝(図示せず)が形成されている。
The friction material 24 is composed of a large number of CC sheet pieces 25 provided over the inner peripheral surface of the cone portion 22 in the circumferential direction. −
It is provided with a predetermined interval from the C sheet piece 25.
The friction material 24 may be provided in multiple stages in the axial direction (vertical direction in FIG. 2) as needed (two stages in FIG. 2).
Here, an oil cut groove (not shown) is formed on the non-sticking surface (friction engagement surface) of each CC sheet piece 25 along the circumferential direction of the inner peripheral surface of the cone portion 22.

【0049】次に、本発明に係るシンクロナイザ・リン
グ20の製造方法を図2を用いて説明する。
Next, a method of manufacturing the synchronizer ring 20 according to the present invention will be described with reference to FIG.

【0050】先ず、既知の方法等を用いて製作したC−
Cコンポジットのブロック体から、ダイヤモンドカッタ
等を用いて多数のC−Cシート片25を切出す。また、
図1(b)に示す炭素短繊維3の不織布4にフェノール
樹脂系接着剤5を含浸させ、接着クッション材(図示せ
ず)を形成する。
First, a C-C manufactured using a known method or the like is used.
A large number of CC sheet pieces 25 are cut out of the C composite block using a diamond cutter or the like. Also,
A nonwoven fabric 4 of short carbon fibers 3 shown in FIG. 1B is impregnated with a phenolic resin-based adhesive 5 to form an adhesive cushion material (not shown).

【0051】次に、各C−Cシート片25の貼付面およ
びリング本体29のコーン部22の内周面23に、粘度
が比較的高いフェノール樹脂系接着剤を塗布した後、接
着クッション材、各C−Cシート片25、及びリング本
体29をそれぞれ炉内に入れて所定の温度条件で加熱
し、フェノール樹脂系接着剤の予備硬化を行い、フェノ
ール樹脂系接着剤中の溶剤を揮発させる。
Next, a phenol resin-based adhesive having a relatively high viscosity is applied to the attachment surface of each CC sheet piece 25 and the inner peripheral surface 23 of the cone portion 22 of the ring main body 29, and then, an adhesive cushion material, Each of the CC sheet pieces 25 and the ring main body 29 are placed in a furnace and heated under a predetermined temperature condition, and the phenol resin-based adhesive is pre-cured, thereby evaporating the solvent in the phenol resin-based adhesive.

【0052】予備硬化後、接着クッション材を、C−C
シート片25と同一形状に切断する。その後、コーン部
22の内周面23の周方向に亘って、接着クッション材
を介して各C−Cシート片25を貼付ける。
After pre-curing, the adhesive cushioning material was replaced with CC
The sheet piece 25 is cut into the same shape. After that, each CC sheet piece 25 is attached via an adhesive cushion material over the circumferential direction of the inner peripheral surface 23 of the cone portion 22.

【0053】その後、コーン部22の内周面23内に型
ピン(図示せず)を嵌め合わせ、型ピンによって各C−
Cシート片25をコーン部22の内周面23に所定の圧
力で押し付ける。この状態でリング本体29を炉内に入
れて所定の温度条件で加熱し、フェノール樹脂系接着剤
を加熱硬化させる。この時、接着クッション材が、コー
ン部22の内周面23とC−Cシート片25の接着面間
のクリアランスを充填(吸収)するように変形し、か
つ、炭素短繊維3自身の圧縮剛性により接着クッション
材が所定の範囲を超えて圧縮変形することはない。この
ため、コーン部22の内周面23とC−Cシート片25
の接着面間の不均一なクリアランスを、接着クッション
材で完全に充填することができる。
Thereafter, a mold pin (not shown) is fitted into the inner peripheral surface 23 of the cone portion 22, and each of the C-
The C sheet piece 25 is pressed against the inner peripheral surface 23 of the cone portion 22 with a predetermined pressure. In this state, the ring main body 29 is placed in a furnace and heated under a predetermined temperature condition to heat and harden the phenol resin-based adhesive. At this time, the adhesive cushion material is deformed so as to fill (absorb) the clearance between the inner peripheral surface 23 of the cone portion 22 and the adhesive surface of the CC sheet piece 25, and the compression rigidity of the short carbon fiber 3 itself. As a result, the adhesive cushion material is not compressed and deformed beyond a predetermined range. For this reason, the inner peripheral surface 23 of the cone portion 22 and the CC sheet piece 25
The non-uniform clearance between the bonding surfaces can be completely filled with the bonding cushion material.

【0054】コーン部22の内周面23に接着クッショ
ン材を介して各C−Cシート片25を接着することで、
コーン部22の内周面23に摩擦材24を有したシンク
ロナイザ・リング20が得られる。
By bonding each CC sheet piece 25 to the inner peripheral surface 23 of the cone portion 22 via an adhesive cushion material,
The synchronizer ring 20 having the friction material 24 on the inner peripheral surface 23 of the cone portion 22 is obtained.

【0055】本実施の形態に係るシンクロナイザ・リン
グによれば、シンクロナイザ・リング20の摩擦材24
を、耐熱性及び耐摩耗性に優れたC−Cコンポジットで
形成することで、長期使用後の高温油中においても安定
して優れた耐摩耗性を発揮し、従来のシンクロナイザ・
リングと比較して耐久性・信頼性に優れる。
According to the synchronizer ring according to the present embodiment, the friction material 24 of the synchronizer ring 20 is used.
Is made of a C-C composite having excellent heat resistance and wear resistance, and exhibits excellent wear resistance stably even in high-temperature oil after long-term use.
Superior in durability and reliability compared to rings.

【0056】また、リング本体29と摩擦材24との間
に接着クッション材を介在させ、この接着クッション材
を所定の圧力で圧着すると共に、所定の温度条件で加熱
硬化させることで、リング本体29と摩擦材24とを接
着クッション層6を介して十分な接着強度で接着するこ
とができる。また、この接着クッション層6は、前述し
たように、炭素短繊維3群で繊維強化されたフェノール
樹脂系接着剤5の接着層であり、硬く、かつ、靱性の高
い層である。このため、この接着クッション層6に、摩
擦係合による多大な応力が負荷されても、層が損壊する
おそれはない。
Further, an adhesive cushion material is interposed between the ring body 29 and the friction material 24, and the adhesive cushion material is press-bonded at a predetermined pressure and is cured by heating under a predetermined temperature condition. And the friction material 24 can be bonded through the bonding cushion layer 6 with a sufficient bonding strength. Further, as described above, the adhesive cushion layer 6 is an adhesive layer of the phenol resin-based adhesive 5 fiber-reinforced with the short carbon fiber 3 group, and is a hard and highly tough layer. Therefore, even if a large stress due to frictional engagement is applied to the adhesive cushion layer 6, the layer is not likely to be damaged.

【0057】さらに、鋳鉄からなるリング本体29とC
−Cコンポジットからなる摩擦材24とは、異種材料で
あり、線膨脹係数及び表面粗度が大きく異なっているも
のの、接着クッション材を介して接着することで、リン
グ本体29と摩擦材24の線膨脹係数の違いに起因する
伸び率の相違を緩衝し、リング本体29と摩擦材24の
表面粗度の違いに起因する接着面間の不均一なクリアラ
ンスを吸収することができる。このため、リング本体2
9と摩擦材24との接着面に、線膨脹係数の違いに起因
する剪断応力が負荷されてもリング本体29から摩擦材
24が剥離するおそれがない。また、リング本体29と
摩擦材24との接着面間の不均一なクリアランスは接着
クッション材で完全に充填されるため、リング本体29
と接着クッション層6との間及び摩擦材24と接着クッ
ション層6との間において接着不良が生じるおそれはな
い。
Further, a ring body 29 made of cast iron and C
The friction material 24 made of a C-composite is a dissimilar material and has a large difference in linear expansion coefficient and surface roughness. The difference in elongation caused by the difference in expansion coefficient can be buffered, and the uneven clearance between the bonding surfaces caused by the difference in surface roughness between the ring main body 29 and the friction material 24 can be absorbed. For this reason, the ring body 2
Even if a shear stress caused by a difference in linear expansion coefficient is applied to the bonding surface between the friction material 9 and the friction material 24, there is no possibility that the friction material 24 is separated from the ring main body 29. Further, the uneven clearance between the bonding surfaces of the ring main body 29 and the friction material 24 is completely filled with the adhesive cushion material.
There is no risk that poor adhesion will occur between the adhesive cushion layer 6 and the friction material 24 and the adhesive cushion layer 6.

【0058】[0058]

【実施例】鋳鉄からなる金属材とC−Cコンポジットか
らなる摩擦材との接着強度、および鋳鉄からなる金属材
同士の接着強度を確認すべく、引張り試験機を用いて剪
断強度を測定する。ここで、金属材と摩擦材とを接着し
たものについて剪断強度を測定する際、摩擦材を引張り
試験機で引張ると、C−Cコンポジットが非常に脆い材
料であることから摩擦材が損壊してしまい、金属材と摩
擦材とを接着したものについては、引張り試験を行うこ
とができない。よって、この場合、摩擦材を金属材で挟
んで接着したものを引張り試験に供し、金属材同士を引
張ることにした。
EXAMPLE In order to confirm the adhesive strength between a metal material made of cast iron and a friction material made of a C-C composite, and the adhesive strength between metal materials made of cast iron, the shear strength is measured using a tensile tester. Here, when measuring the shear strength of a bonded metal material and a friction material, when the friction material is pulled with a tensile tester, the friction material is damaged because the C-C composite is a very brittle material. Thus, a tensile test cannot be performed on a metal material and a friction material bonded together. Therefore, in this case, the friction material was sandwiched between metal materials and bonded, and subjected to a tensile test to pull the metal materials together.

【0059】<試験1>幅25mm、厚さ0.8mm、
長さ100mmの鋳鉄材(SPCC−SD(JIS規格))を
2枚作製した後、各鋳鉄材の接着部表面に浸炭処理を施
し、その後、ショットブラストにより接着部の表面調整
を行い、表面粗度を50μRzとする。この鋳鉄材の
内、片方の鋳鉄材の接着部を幅方向にV字状に折曲げ、
図4に示すように、折曲がった第1部材41と、真直な
第2部材42を作製する。ここで、第1部材41の谷側
の面41aの最大深さは0.5mmとして不均一なクリ
アランスとした。
<Test 1> Width 25 mm, thickness 0.8 mm,
After preparing two cast iron materials (SPCC-SD (JIS standard)) with a length of 100 mm, the surface of the bonded part of each cast iron material is carburized, and then the surface of the bonded part is adjusted by shot blasting, and the surface roughness is adjusted. The degree is 50 μRz. Among these cast iron materials, one of the cast iron materials is bent in a V-shape in the width direction,
As shown in FIG. 4, a bent first member 41 and a straight second member 42 are manufactured. Here, the maximum depth of the valley-side surface 41a of the first member 41 was set to 0.5 mm to provide an uneven clearance.

【0060】また、繊維径Dが0.006mm(6μ
m)の炭素繊維を用いてC−Cコンポジットを形成し、
このC−Cコンポジットをスライスして、縦25mm、
横25mm、厚さ0.7mmの摩擦材43(図5,図6
参照)を作製する。摩擦材については、表面研磨を行う
ことができないことから、表面粗度は可成りと粗くなっ
ている(表面粗度は測定不可であり、ばらつきが大き
い)。
The fiber diameter D is 0.006 mm (6 μm).
m) forming a CC composite using the carbon fibers of
Slice this C-C composite, 25mm in length,
A friction material 43 having a width of 25 mm and a thickness of 0.7 mm (see FIGS. 5 and 6)
Reference). Since the surface of the friction material cannot be polished, the surface roughness is considerably large (the surface roughness cannot be measured and has large variations).

【0061】さらに、繊維長Lが15mm、繊維径Dが
0.8μmの炭素短繊維を用いて、厚さ2mm、目付量
3.0×10-3g/cm2 の不織布を作製する。この不
織布にフェノール樹脂系接着剤(ハマタイトA−344
−B(横浜ゴム(株)製))を含浸させ、縦25mm、
横25mm、厚さ2.0mmの接着クッション材44
(図5参照)を作製する。
Further, a non-woven fabric having a thickness of 2 mm and a basis weight of 3.0 × 10 −3 g / cm 2 is prepared using short carbon fibers having a fiber length L of 15 mm and a fiber diameter D of 0.8 μm. A phenolic resin adhesive (hamatite A-344) is applied to this nonwoven fabric.
-B (Yokohama Rubber Co., Ltd.)), 25 mm long,
Adhesive cushion material 44 25mm wide and 2.0mm thick
(See FIG. 5).

【0062】(実施例1)図5に示すように、第1部材
41及び第2部材42の各接着部表面、および摩擦43
材の両面に、フェノール樹脂系接着剤(ハマタイトY−
3600(横浜ゴム(株)製))45を塗布した後、第
1部材41、第2部材42、摩擦材43、および接着ク
ッション材44を80℃×30minの温度条件で加熱
し、フェノール樹脂系接着剤45及び接着クッション材
44に含浸させたフェノール樹脂系接着剤を予備硬化さ
せる。
(Example 1) As shown in FIG. 5, the surfaces of the bonding portions of the first member 41 and the second member 42 and the friction 43
Phenolic resin-based adhesive (hamatite Y-
After applying 3600 (manufactured by Yokohama Rubber Co., Ltd.) 45, the first member 41, the second member 42, the friction material 43, and the adhesive cushioning material 44 are heated under a temperature condition of 80 ° C. × 30 min to form a phenol resin-based material. The phenol resin-based adhesive impregnated in the adhesive 45 and the adhesive cushioning material 44 is pre-cured.

【0063】次に、第1部材41及び第2部材42の各
接着部表面を対向させて重ねる際、各接着部表面間に、
摩擦材43を接着クッション材44,44で挟んだもの
を介在させる。
Next, when the surfaces of the bonding portions of the first member 41 and the second member 42 are overlapped with each other,
A friction material 43 sandwiched between adhesive cushioning materials 44, 44 is interposed.

【0064】その後、第1部材41及び第2部材42を
0.98MPa(10kgf/cm2 )の圧力で圧着さ
せると共に180℃×60minの温度条件で加熱し、
フェノール樹脂系接着剤45及び接着クッション材44
に含浸させたフェノール樹脂系接着剤を加熱硬化させて
試料1を作製する。
Then, the first member 41 and the second member 42 are pressed at a pressure of 0.98 MPa (10 kgf / cm 2 ) and heated at a temperature of 180 ° C. × 60 min.
Phenolic resin adhesive 45 and adhesive cushioning material 44
The phenol resin-based adhesive impregnated in the sample is cured by heating to prepare a sample 1.

【0065】(比較例1)図6に示すように、第1部材
41、第2部材42、及び摩擦材43の各接着部表面
に、フェノール樹脂系接着剤(ハマタイトY−3600
(横浜ゴム(株)製))45を塗布した後、第1部材4
1、第2部材42、及び摩擦材43を80℃×30mi
nの温度条件で加熱し、フェノール樹脂系接着剤45を
予備硬化させる。
(Comparative Example 1) As shown in FIG. 6, a phenol resin-based adhesive (hamatite Y-3600) was applied to the surface of each of the bonding portions of the first member 41, the second member 42, and the friction material 43.
After applying (Yokohama Rubber Co., Ltd.) 45, the first member 4
1, the second member 42 and the friction material 43 are set at 80 ° C. × 30 mi.
Heating is performed under the temperature condition of n, and the phenol resin-based adhesive 45 is pre-cured.

【0066】次に、第1部材41及び第2部材42の各
接着部表面を対向させて重ねる際、各接着部表面間に摩
擦材43を介在させる。その後、第1部材41及び第2
部材42を0.98MPa(10kgf/cm2 )の圧
力で圧着させると共に180℃×60minの温度条件
で加熱し、フェノール樹脂系接着剤45を加熱硬化させ
て試料2を作製する。
Next, when the surfaces of the bonding portions of the first member 41 and the second member 42 are superposed on each other, a friction material 43 is interposed between the surfaces of the bonding portions. Thereafter, the first member 41 and the second
The member 42 is pressed under a pressure of 0.98 MPa (10 kgf / cm 2 ) and heated under a temperature condition of 180 ° C. × 60 min to heat and cure the phenolic resin-based adhesive 45 to prepare a sample 2.

【0067】<試験2>試験1と同様にして、第1部材
41及び第2部材42を作製する。また、試験1と同様
にして作製した不織布に、アクリル樹脂系接着剤(ハー
ドロックG55(電気化学(株)製))を含浸させ、縦
25mm、横25mm、厚さ2.0mmの接着クッショ
ン材74(図7参照)を作製する。
<Test 2> In the same manner as in Test 1, a first member 41 and a second member 42 are manufactured. In addition, the nonwoven fabric prepared in the same manner as in Test 1 was impregnated with an acrylic resin-based adhesive (Hard Rock G55 (manufactured by Denki Kagaku Co., Ltd.)) to provide an adhesive cushion material having a length of 25 mm, a width of 25 mm, and a thickness of 2.0 mm. 74 (see FIG. 7).

【0068】(実施例2)図7に示すように、第1部材
41及び第2部材42の各接着部表面を対向させて重ね
る際、各接着部表面間に、接着クッション材74を介在
させる。
(Embodiment 2) As shown in FIG. 7, when the surfaces of the bonding portions of the first member 41 and the second member 42 face each other, an adhesive cushion member 74 is interposed between the surfaces of the bonding portions. .

【0069】その後、第1部材41及び第2部材42を
クリップで固定すると共に室温で24時間放置し、接着
クッション材74に含浸させたアクリル樹脂系接着剤を
硬化させて試料3を作製する。
Thereafter, the first member 41 and the second member 42 are fixed with clips and left at room temperature for 24 hours to cure the acrylic resin-based adhesive impregnated in the adhesive cushion material 74, thereby preparing the sample 3.

【0070】(比較例2)図8に示すように、第1部材
41及び第2部材42の各接着部表面に、アクリル樹脂
系接着剤(ハードロックG55(電気化学(株)製))
81を塗布した後、第1部材41及び第2部材42の各
接着部表面を対向させて重ねる。その後、第1部材41
及び第2部材42をクリップで固定すると共に室温で2
4時間放置し、アクリル樹脂系接着剤81を硬化させて
試料4を作製する。
Comparative Example 2 As shown in FIG. 8, an acrylic resin-based adhesive (Hard Rock G55 (manufactured by Denki Kagaku Co., Ltd.))
After 81 is applied, the surfaces of the bonding portions of the first member 41 and the second member 42 are overlapped so as to face each other. Then, the first member 41
And fix the second member 42 with a clip and
The sample 4 is prepared by allowing the acrylic resin-based adhesive 81 to cure for 4 hours.

【0071】ここで、見方を変えると、試料3,4は、
金属材と、その金属材と線膨脹係数は同じであるが表面
粗度が異なる摩擦材との接着構造と見ることができる。
Here, from a different point of view, Samples 3 and 4 are:
It can be seen as a bonding structure between a metal material and a friction material having the same linear expansion coefficient as the metal material but different surface roughness.

【0072】<試験3>幅25mm、厚さ0.8mm、
長さ100mmの鋳鉄材(SPCC−SD(JIS規格))を
2枚作製した後、各鋳鉄材の接着部表面に浸炭処理を施
し、その後、ショットブラストにより接着部の表面調整
を行い、表面粗度を50μRzとする。この鋳鉄材の
内、片方の鋳鉄材の接着部を幅方向にアーチ状に曲げ、
図9に示すように、折曲がった第1部材91と、真直な
第2部材92を作製する。ここで、第1部材91の凹側
の面91aの最大深さは0.5mmである。
<Test 3> 25 mm wide, 0.8 mm thick,
After preparing two cast iron materials (SPCC-SD (JIS standard)) with a length of 100 mm, the surface of the bonded part of each cast iron material is carburized, and then the surface of the bonded part is adjusted by shot blasting, and the surface roughness is adjusted. The degree is 50 μRz. Of this cast iron material, the adhesive part of one cast iron material is bent into an arch shape in the width direction,
As shown in FIG. 9, a bent first member 91 and a straight second member 92 are manufactured. Here, the maximum depth of the concave surface 91a of the first member 91 is 0.5 mm.

【0073】その他は、試験1と同様にして摩擦材43
(図10,図11参照)及び接着クッション材44(図
10参照)を作製する。
Other than the above, the friction material 43 was made in the same manner as in Test 1.
(See FIGS. 10 and 11) and an adhesive cushion material 44 (see FIG. 10).

【0074】(実施例3)図10に示すように、第1部
材91及び第2部材92の各接着部表面、および摩擦4
3材の両面に、フェノール樹脂系接着剤(ハマタイトY
−3600(横浜ゴム(株)製))45を塗布した後、
第1部材91、第2部材92、摩擦材43、および接着
クッション材44を80℃×30minの温度条件で加
熱し、フェノール樹脂系接着剤45及び接着クッション
材44に含浸させたフェノール樹脂系接着剤を予備硬化
させる。
(Embodiment 3) As shown in FIG. 10, the surfaces of the bonding portions of the first member 91 and the second member 92 and the friction
A phenolic resin-based adhesive (hamatite Y
-3600 (produced by Yokohama Rubber Co., Ltd.) 45
The first member 91, the second member 92, the friction material 43, and the adhesive cushion material 44 are heated at a temperature of 80 ° C. × 30 min to impregnate the phenol resin adhesive 45 and the adhesive cushion material 44 with the phenol resin adhesive. Pre-curing agent.

【0075】次に、第1部材91及び第2部材92の各
接着部表面を対向させて重ねる際、各接着部表面間に、
摩擦材43を接着クッション材44,44で挟んだもの
を介在させる。
Next, when the surfaces of the bonding portions of the first member 91 and the second member 92 are overlapped with each other,
A friction material 43 sandwiched between adhesive cushioning materials 44, 44 is interposed.

【0076】その後、第1部材91及び第2部材92を
0.98MPa(10kgf/cm2 )の圧力で圧着さ
せると共に180℃×60minの温度条件で加熱し、
フェノール樹脂系接着剤45及び接着クッション材44
に含浸させたフェノール樹脂系接着剤を加熱硬化させて
試料5を作製する。
Then, the first member 91 and the second member 92 are pressed at a pressure of 0.98 MPa (10 kgf / cm 2 ) and heated at a temperature of 180 ° C. × 60 min.
Phenolic resin adhesive 45 and adhesive cushioning material 44
The sample 5 is prepared by heating and curing the phenol resin-based adhesive impregnated in the resin.

【0077】(比較例3)図11に示すように、第1部
材91、第2部材92、及び摩擦材43の各接着部表面
に、フェノール樹脂系接着剤(ハマタイトY−3600
(横浜ゴム(株)製))45を塗布した後、第1部材9
1、第2部材92、及び摩擦材43を80℃×30mi
nの温度条件で加熱し、フェノール樹脂系接着剤45を
予備硬化させる。
(Comparative Example 3) As shown in FIG. 11, a phenolic resin-based adhesive (hamatite Y-3600) was applied to the surfaces of the first member 91, the second member 92, and the friction material 43 at the respective bonding portions.
(Yokohama Rubber Co., Ltd.) After applying 45, the first member 9
1. The second member 92 and the friction material 43 were heated at 80 ° C. × 30 mi.
Heating is performed under the temperature condition of n, and the phenol resin-based adhesive 45 is pre-cured.

【0078】次に、第1部材91及び第2部材92の各
接着部表面を対向させて重ねる際、各接着部表面間に摩
擦材43を介在させる。その後、第1部材91及び第2
部材92を0.98MPa(10kgf/cm2 )の圧
力で圧着させると共に180℃×60minの温度条件
で加熱し、フェノール樹脂系接着剤45を加熱硬化させ
て試料6を作製する。
Next, when the surfaces of the bonding portions of the first member 91 and the second member 92 are superposed on each other, the friction material 43 is interposed between the surfaces of the bonding portions. Thereafter, the first member 91 and the second
The member 92 is pressed under a pressure of 0.98 MPa (10 kgf / cm 2 ) and heated under a temperature condition of 180 ° C. × 60 min to heat and cure the phenolic resin adhesive 45 to prepare a sample 6.

【0079】<試験4>試験3と同様にして、第1部材
91及び第2部材92(図12,図13参照)、および
接着クッション材44(図12参照)を作製する。
<Test 4> In the same manner as in Test 3, a first member 91 and a second member 92 (see FIGS. 12 and 13) and an adhesive cushion material 44 (see FIG. 12) are manufactured.

【0080】(実施例4)図12に示すように、第1部
材91及び第2部材92の各接着部表面に、フェノール
樹脂系接着剤(ハマタイトY−3600(横浜ゴム
(株)製))45を塗布した後、第1部材91、第2部
材92、および接着クッション材44を80℃×30m
inの温度条件で加熱し、フェノール樹脂系接着剤45
及び接着クッション材44に含浸させたフェノール樹脂
系接着剤を予備硬化させる。
(Embodiment 4) As shown in FIG. 12, a phenolic resin-based adhesive (Hamatite Y-3600 (manufactured by Yokohama Rubber Co., Ltd.)) was applied to the surface of each of the bonding portions of the first member 91 and the second member 92. 45, the first member 91, the second member 92, and the adhesive cushioning material 44 were heated to 80 ° C. × 30 m
in phenol resin adhesive 45
Then, the phenol resin adhesive impregnated in the adhesive cushion material 44 is pre-cured.

【0081】次に、第1部材91及び第2部材92の各
接着部表面を対向させて重ねる際、各接着部表面間に、
接着クッション材44を介在させる。その後は実施例3
と同様にして、フェノール樹脂系接着剤45及び接着ク
ッション材44に含浸させたフェノール樹脂系接着剤を
加熱硬化させて試料7を作製する。
Next, when the surfaces of the bonding portions of the first member 91 and the second member 92 are overlapped with each other,
An adhesive cushion member 44 is interposed. Then, Example 3
In the same manner as in the above, the phenol resin-based adhesive 45 and the phenol resin-based adhesive impregnated in the adhesive cushioning material 44 are cured by heating to prepare a sample 7.

【0082】(比較例4)図13に示すように、第1部
材91及び第2部材92の各接着部表面に、フェノール
樹脂系接着剤(ハマタイトY−3600(横浜ゴム
(株)製))45を塗布した後、第1部材91、第2部
材92を80℃×30minの温度条件で加熱し、フェ
ノール樹脂系接着剤45を予備硬化させる。
(Comparative Example 4) As shown in FIG. 13, a phenolic resin-based adhesive (Hamatite Y-3600 (manufactured by Yokohama Rubber Co., Ltd.)) was applied to the surfaces of the bonded portions of the first member 91 and the second member 92. After applying 45, the first member 91 and the second member 92 are heated under a temperature condition of 80 ° C. × 30 minutes to pre-cure the phenolic resin-based adhesive 45.

【0083】次に、第1部材91及び第2部材92の各
接着部表面を対向させて重ねた後、第1部材91及び第
2部材92を0.98MPa(10kgf/cm2 )の
圧力で圧着させると共に180℃×60minの温度条
件で加熱し、フェノール樹脂系接着剤45を加熱硬化さ
せて試料8を作製する。
Next, after the surfaces of the bonding portions of the first member 91 and the second member 92 are superposed on each other, the first member 91 and the second member 92 are pressed at a pressure of 0.98 MPa (10 kgf / cm 2 ). The sample 8 is produced by pressure bonding and heating at a temperature of 180 ° C. × 60 min to heat and cure the phenolic resin adhesive 45.

【0084】ここで、見方を変えると、試料3,4は、
金属材と、その金属材と線膨脹係数は同じであるが表面
粗度が異なる摩擦材との接着構造と見ることができる。
Here, from a different point of view, Samples 3 and 4 are:
It can be seen as a bonding structure between a metal material and a friction material having the same linear expansion coefficient as the metal material but different surface roughness.

【0085】実施例1〜4及び比較例1〜4で得られた
試料1〜8について、第1部材41,91及び第2部材
42,92を、インストロン型引張り試験機を用いて、
図4、図9に示す矢印方向に引張り、室温大気中におけ
る剪断強度を測定した。
For the samples 1 to 8 obtained in Examples 1 to 4 and Comparative Examples 1 to 4, the first members 41 and 91 and the second members 42 and 92 were subjected to an Instron type tensile tester.
Pulling was performed in the direction of the arrow shown in FIGS. 4 and 9, and the shear strength in the air at room temperature was measured.

【0086】従来の金属材と摩擦材の接着構造を有する
比較例1,3の試料2,6では、第1部材41,91と
摩擦材43との間および第2部材42,92と摩擦材4
3との間に介在するのが、フェノール樹脂系接着剤45
の接着層である。この接着層は、硬く、脆い層であるた
め、引張りに伴って接着層が変形する際の許容範囲が狭
い(小さい)。また、この接着層は接着強度を発現させ
るために加圧が必要であるが、接着の際に加圧を行う
と、第1部材41,91と摩擦材43との間および第2
部材42,92と摩擦材43との間の不均一なクリアラ
ンスを吸収できなくなってしまう。このため、第1部材
41,91と摩擦材43との間および第2部材42,9
2と摩擦材43との間に接着不良が生じてしまう。これ
らの理由によって、試料2,6の剪断強度(接着強度)
は5MPaと低い値となってしまう。
In Samples 2 and 6 of Comparative Examples 1 and 3 having a conventional structure of bonding a metal material and a friction material, the friction members 43 between the first members 41 and 91 and the friction material 43 and the friction members 43 and the second members 42 and 92 were used. 4
And the phenolic resin-based adhesive 45
Is an adhesive layer. Since this adhesive layer is a hard and brittle layer, the allowable range when the adhesive layer is deformed due to tension is narrow (small). The adhesive layer needs to be pressurized in order to develop adhesive strength. However, when pressure is applied during the bonding, the pressure between the first members 41 and 91 and the friction material 43 and the second
The uneven clearance between the members 42 and 92 and the friction material 43 cannot be absorbed. Therefore, between the first members 41 and 91 and the friction material 43 and between the second members 42 and 9
Adhesion failure occurs between the friction material 2 and the friction material 43. For these reasons, the shear strength (adhesive strength) of Samples 2 and 6
Is as low as 5 MPa.

【0087】これに対して、本発明の金属材と摩擦材の
接着構造を有する実施例1,3の試料1,5では、第1
部材41,91と摩擦材43との間および第2部材4
2,92と摩擦材43との間に介在するのが、接着クッ
ション層である。この接着クッション層は、硬く、か
つ、靱性の高い層であるため、引張りに伴って接着クッ
ション層が変形する際の許容範囲が広い(大きい)。ま
た、フェノール樹脂系接着剤の接着強度を発現させるた
めに加圧を行っても、この接着クッション層は、ある一
定の範囲を超えて圧縮されることがないため、第1部材
41,91と摩擦材43との間および第2部材42,9
2と摩擦材43との間の不均一なクリアランスを略完全
に吸収することができる。このため、第1部材41,9
1と摩擦材43との間および第2部材42,92と摩擦
材43との間に接着不良が生じるおそれはない。これら
の理由によって、試料1,3の剪断強度(接着強度)
は、試料2,6の3倍以上の17MPaと非常に高い値
となる。
On the other hand, in the samples 1 and 5 of Examples 1 and 3 having the bonding structure of the metal material and the friction material of the present invention, the first
Between the members 41 and 91 and the friction material 43 and the second member 4
An adhesive cushion layer is interposed between the friction members 43 and the friction members 43. Since this adhesive cushion layer is a layer that is hard and has high toughness, the allowable range when the adhesive cushion layer is deformed due to tension is wide (large). Also, even if pressure is applied to develop the adhesive strength of the phenolic resin-based adhesive, the adhesive cushion layer is not compressed beyond a certain range, so that the first members 41 and 91 are not compressed. Between the friction member 43 and the second members 42, 9
The uneven clearance between the friction material 2 and the friction material 43 can be almost completely absorbed. For this reason, the first members 41, 9
There is no risk of poor adhesion between the first member and the friction member 43 and between the second members 42 and 92 and the friction member 43. For these reasons, the shear strength (adhesive strength) of samples 1 and 3
Is a very high value of 17 MPa, which is three times or more that of the samples 2 and 6.

【0088】また、実施例2,4の試料3,7および比
較例2,4の試料4,8は、同種材料間の接着であるた
め、第1部材41,91と第2部材42,92との間に
歪みが生じることはなく、接着後の第1部材41,91
と第2部材42,92とは略一体のものと見なすことが
できる。
Samples 3 and 7 of Examples 2 and 4 and Samples 4 and 8 of Comparative Examples 2 and 4 are adhesives between the same materials, and therefore, the first members 41 and 91 and the second members 42 and 92 are used. No distortion occurs between the first members 41 and 91 after bonding.
And the second members 42 and 92 can be regarded as substantially integral.

【0089】このため、従来の金属材と摩擦材の接着構
造を有する比較例2,4の試料4,8では、試料2,6
と比較すると、第1部材41,91と第2部材42,9
2との間に歪みがない分、剪断強度(接着強度)は若干
高いが、試料2,6と同様の理由で、剪断強度(接着強
度)が7MPaと依然として低い。
For this reason, in Samples 4 and 8 of Comparative Examples 2 and 4 having a conventional structure of bonding a metal material and a friction material, Samples 2 and 6
, The first members 41 and 91 and the second members 42 and 9
Although the shear strength (adhesive strength) is slightly higher because there is no distortion between the two, the shear strength (adhesive strength) is still low at 7 MPa for the same reason as in Samples 2 and 6.

【0090】これに対して、本発明の金属材と摩擦材の
接着構造を有する実施例2,4の試料3,7では、試料
1,3と同様の理由で、剪断強度(接着強度)が試料
4,8の3倍の21MPaと非常に高い値となる。
On the other hand, in the samples 3 and 7 of Examples 2 and 4 having the bonding structure of the metal material and the friction material according to the present invention, the shear strength (adhesion strength) was reduced for the same reason as in the samples 1 and 3. This is a very high value of 21 MPa, which is three times that of Samples 4 and 8.

【0091】即ち、本発明に係る金属材と摩擦材の接着
構造を有するものは、従来の金属材と摩擦材の接着構造
を有するものと比較して、接着強度が大幅に向上するこ
とが確認できた。
That is, it was confirmed that the adhesive having the structure of bonding a metal material and a friction material according to the present invention greatly improved the adhesive strength as compared with the conventional structure having an adhesion structure of a metal material and a friction material. did it.

【0092】以上、本発明の実施の形態は、上述した実
施の形態に限定されるものではなく、他にも種々のもの
が想定されることは言うまでもない。
As described above, the embodiments of the present invention are not limited to the above-described embodiments, and it is needless to say that various other embodiments are also conceivable.

【0093】尚、本発明に係る金属材と摩擦材の接着構
造は、上述したようにシンクロナイザ・リングのみにそ
の用途が限定されるものではなく、その他の多大な応力
が負荷される摩擦部に適用することができることは言う
までもなく、例えば、ブレーキシュー、ブレーキパッ
ド、シリンダライナ等が想定される。
[0093] The bonding structure of the metal material and the friction material according to the present invention is not limited to the synchronizer ring as described above, but may be applied to other frictional parts to which a large amount of stress is applied. It goes without saying that a brake shoe, a brake pad, a cylinder liner, and the like are assumed, of course.

【0094】[0094]

【発明の効果】以上要するに本発明によれば、金属材
と、その金属材と線膨脹係数又は表面粗度が大きく異な
る摩擦材との接着面間に、炭素短繊維等からなる不織布
にフェノール樹脂系接着剤又はアクリル樹脂系接着材を
含浸させた接着クッション層を介在させると共に圧着さ
せて硬化させたことで、金属材と摩擦材とを強固に接着
することができるという優れた効果を発揮する。
In summary, according to the present invention, a phenolic resin is applied to a nonwoven fabric made of short carbon fibers or the like between a metal material and a friction material having a greatly different linear expansion coefficient or surface roughness from the metal material. An excellent effect that the metal material and the friction material can be firmly adhered to each other by interposing the adhesive cushion layer impregnated with the adhesive or the acrylic resin adhesive, and pressing and curing the adhesive material. .

【図面の簡単な説明】[Brief description of the drawings]

【図1】本発明に係る金属材と摩擦材の接着構造の断面
模式図である。
FIG. 1 is a schematic cross-sectional view of a bonding structure between a metal material and a friction material according to the present invention.

【図2】本発明に係るシンクロナイザ・リングの好適一
実施の形態を示す斜視図である。
FIG. 2 is a perspective view showing a preferred embodiment of a synchronizer ring according to the present invention.

【図3】従来のシンクロナイザ・リングの一形態を示す
斜視図である。
FIG. 3 is a perspective view showing an embodiment of a conventional synchronizer ring.

【図4】試験1,2に用いた第一部材及び第二部材の斜
視図である。
FIG. 4 is a perspective view of a first member and a second member used in tests 1 and 2.

【図5】実施例1における試料1の接着部断面図であ
る。
FIG. 5 is a sectional view of a bonding portion of a sample 1 in Example 1.

【図6】比較例1における試料2の接着部断面図であ
る。
FIG. 6 is a cross-sectional view of a bonding portion of Sample 2 in Comparative Example 1.

【図7】実施例2における試料3の接着部断面図であ
る。
FIG. 7 is a sectional view of a bonding portion of a sample 3 in Example 2.

【図8】比較例2における試料4の接着部断面図であ
る。
FIG. 8 is a cross-sectional view of a bonding portion of Sample 4 in Comparative Example 2.

【図9】試験3,4に用いた第一部材及び第二部材の斜
視図である。
FIG. 9 is a perspective view of a first member and a second member used in tests 3 and 4.

【図10】実施例3における試料5の接着部断面図であ
る。
FIG. 10 is a cross-sectional view of a bonding portion of a sample 5 according to a third embodiment.

【図11】比較例3における試料6の接着部断面図であ
る。
11 is a cross-sectional view of a bonding portion of a sample 6 in Comparative Example 3. FIG.

【図12】実施例4における試料7の接着部断面図であ
る。
FIG. 12 is a sectional view of a bonded portion of a sample 7 in Example 4.

【図13】比較例4における試料8の接着部断面図であ
る。
FIG. 13 is a cross-sectional view of a bonding portion of Sample 8 in Comparative Example 4.

【符号の説明】[Explanation of symbols]

1 金属材 2 摩擦材 3 炭素短繊維(又はガラス短繊維) 4 不織布 5 フェノール樹脂系接着剤(又はアクリル樹脂系接着
剤) 6 接着クッション層 20 シンクロナイザ・リング 21 リング部(金属リング) 22 コーン部(金属リング) 23 コーン部の内周面(金属リングの内周面) 24 摩擦材 25 C−Cシート片(炭素繊維強化炭素複合シート
片) 29 リング本体(金属リング)
DESCRIPTION OF SYMBOLS 1 Metal material 2 Friction material 3 Short carbon fiber (or short glass fiber) 4 Nonwoven fabric 5 Phenol resin adhesive (or acrylic resin adhesive) 6 Adhesive cushion layer 20 Synchronizer ring 21 Ring part (metal ring) 22 Cone part (Metal ring) 23 Inner peripheral surface of cone part (Inner peripheral surface of metal ring) 24 Friction material 25 CC sheet piece (Carbon fiber reinforced carbon composite sheet piece) 29 Ring body (Metal ring)

───────────────────────────────────────────────────── フロントページの続き (72)発明者 金坂 敏行 神奈川県藤沢市土棚8番地 いすゞ自動車 株式会社藤沢工場内 (72)発明者 橋本 徳子 神奈川県藤沢市土棚8番地 いすゞ自動車 株式会社藤沢工場内 (72)発明者 木島 栄一 神奈川県藤沢市土棚8番地 いすゞ自動車 株式会社藤沢工場内 (72)発明者 鶴岡 卓弘 神奈川県川崎市川崎区殿町3丁目25番1号 いすゞ自動車株式会社川崎工場内 (72)発明者 鈴木 隆司 神奈川県川崎市川崎区殿町3丁目25番1号 いすゞ自動車株式会社川崎工場内 Fターム(参考) 3J056 AA14 AA53 AA61 BA02 BC01 BE01 BE17 CA03 CA12 EA03 EA26 EA30 FA07 GA05 GA12 3J058 BA47 DD13 GA03 GA27 GA42 GA55 GA68 GA93 GA94 4F100 AB01A AB08A AD11B AD11C AK33C BA03 BA07 BA10A BA10B CB00C DC21B DG01B DG01C DG15C EC012 EC182 EJ082 EJ422 GB32 JK16B JL11  ──────────────────────────────────────────────────続 き Continuing on the front page (72) Inventor Toshiyuki Kanasaka 8 Dosana, Fujisawa-shi, Kanagawa Prefecture Isuzu Motors Fujisawa Plant Co., Ltd. (72) Inventor Tokiko Hashimoto 8 Isuzu-Mura, Fujisawa City, Kanagawa Prefecture Isuzu Motors Fujisawa Plant, Inc. (72) Inventor Eiichi Kijima 8 Tozai, Fujisawa-shi, Kanagawa Prefecture Isuzu Motors Fujisawa Co., Ltd. (72) Inventor Takuoka Tsuruoka 3- 25-1, Tonomachi, Kawasaki-ku, Kawasaki-shi, Kanagawa Prefecture Isuzu Motors Kawasaki Plant (72) Inventor Takashi Suzuki 3-25-1, Tonomachi, Kawasaki-ku, Kawasaki-shi, Kanagawa Prefecture F-term in the Kawasaki Plant of Isuzu Motor Co., Ltd. (Reference) 3J056 AA14 AA53 AA61 BA02 BC01 BE01 BE17 CA03 CA12 EA03 EA26 EA30 FA07 GA05 GA12 3J058 BA47 DD13 GA03 GA27 GA42 GA55 GA68 GA93 GA94 4F100 AB01A AB08A AD11B AD11C AK33C BA03 BA07 BA10A BA1 0B CB00C DC21B DG01B DG01C DG15C EC012 EC182 EJ082 EJ422 GB32 JK16B JL11

Claims (6)

【特許請求の範囲】[Claims] 【請求項1】 金属材と、その金属材と線膨脹係数が異
なる摩擦材との接着構造において、炭素短繊維等からな
る不織布に接着剤を含浸させた接着クッション層を上記
金属材と摩擦材の接着面間に介在させると共に圧着させ
て加熱硬化させたことを特徴とする金属材と摩擦材の接
着構造。
In a bonding structure of a metal material and a friction material having a different linear expansion coefficient from the metal material, an adhesive cushion layer obtained by impregnating an adhesive into a non-woven fabric made of short carbon fiber or the like is provided with the metal material and the friction material. An adhesive structure between a metal material and a friction material, wherein the metal material and the friction material are interposed between the adhesive surfaces and are pressed and heat-cured.
【請求項2】 上記接着剤がフェノール樹脂系接着剤で
ある請求項1記載の金属材と摩擦材の接着構造。
2. The bonding structure according to claim 1, wherein said adhesive is a phenolic resin adhesive.
【請求項3】 上記金属材が鋳鉄、上記摩擦材が炭素繊
維強化炭素複合材で構成された請求項1又は請求項2に
記載の金属材と摩擦材の接着構造。
3. The bonding structure between a metal material and a friction material according to claim 1, wherein the metal material is cast iron, and the friction material is a carbon fiber reinforced carbon composite material.
【請求項4】 上記金属材及び上記摩擦材の各接着面
に、フェノール樹脂系接着剤からなる接着層を予め形成
して接着クッション層を介在させる請求項1から請求項
3いずれかに記載の金属材と摩擦材の接着構造。
4. The method according to claim 1, wherein an adhesive layer made of a phenolic resin adhesive is previously formed on each of the adhesive surfaces of the metal material and the friction material, and an adhesive cushion layer is interposed therebetween. Adhesion structure of metal material and friction material.
【請求項5】 上記金属が、変速装置のシンクロナイザ
・リングである請求項1から請求項4いずれかに記載の
金属材と摩擦材の接着構造。
5. The bonding structure between a metal material and a friction material according to claim 1, wherein the metal is a synchronizer ring of a transmission.
【請求項6】 上記摩擦材が、上記金属リングの内周面
の周方向に亘って設けられた多数の炭素繊維強化炭素複
合シート片で構成される請求項5記載の金属材と摩擦材
の接着構造。
6. The metal material and the friction material according to claim 5, wherein the friction material is constituted by a plurality of carbon fiber reinforced carbon composite sheet pieces provided in a circumferential direction of an inner peripheral surface of the metal ring. Adhesive structure.
JP2000203128A 2000-06-30 2000-06-30 Bonding structure of metal ring and friction material Expired - Fee Related JP4588846B2 (en)

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2004111479A1 (en) * 2003-06-10 2004-12-23 Oiles Corporation Synchronizer ring
KR100769848B1 (en) 2006-08-29 2007-10-25 국방과학연구소 Method to increase adhesive strength for metal tube and carbon fiber/epoxy resin layer and thereof increasing structure
CN109578468A (en) * 2017-09-29 2019-04-05 罗伯特·博世有限公司 The Brake pad component of increasing material manufacturing with controlled compressibility factor

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JPH11210792A (en) * 1998-01-23 1999-08-03 Sumitomo Electric Ind Ltd Disk brake pad and its manufacture
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JPS62115536U (en) * 1986-01-13 1987-07-22
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JPH01172634A (en) * 1987-12-26 1989-07-07 Nsk Warner Kk Synchronizer ring and shaping device and method thereof
JPH01292088A (en) * 1988-05-19 1989-11-24 Sumitomo Electric Ind Ltd Sheetlike adhesive and friction material assembly
JPH07197948A (en) * 1993-11-29 1995-08-01 Ntn Corp Synchronizer ring
JPH09316209A (en) * 1996-05-30 1997-12-09 Nisshinbo Ind Inc Friction material molded product and intermediate layer material
JPH11210792A (en) * 1998-01-23 1999-08-03 Sumitomo Electric Ind Ltd Disk brake pad and its manufacture
JP2000094589A (en) * 1998-07-21 2000-04-04 Nagoya Oil Chem Co Ltd Molding material

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2004111479A1 (en) * 2003-06-10 2004-12-23 Oiles Corporation Synchronizer ring
JPWO2004111479A1 (en) * 2003-06-10 2006-07-20 オイレス工業株式会社 Synchronizer ring
US7361395B2 (en) 2003-06-10 2008-04-22 Oiles Corporation Synchronizer ring
KR100769848B1 (en) 2006-08-29 2007-10-25 국방과학연구소 Method to increase adhesive strength for metal tube and carbon fiber/epoxy resin layer and thereof increasing structure
CN109578468A (en) * 2017-09-29 2019-04-05 罗伯特·博世有限公司 The Brake pad component of increasing material manufacturing with controlled compressibility factor
CN109578468B (en) * 2017-09-29 2022-11-04 罗伯特·博世有限公司 Additive manufactured brake pad assembly with controlled compression factor

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