JP2629500B2 - Sliding member of hermetic compressor - Google Patents

Sliding member of hermetic compressor

Info

Publication number
JP2629500B2
JP2629500B2 JP3270795A JP27079591A JP2629500B2 JP 2629500 B2 JP2629500 B2 JP 2629500B2 JP 3270795 A JP3270795 A JP 3270795A JP 27079591 A JP27079591 A JP 27079591A JP 2629500 B2 JP2629500 B2 JP 2629500B2
Authority
JP
Japan
Prior art keywords
boron
treatment
layer
base material
hermetic compressor
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
JP3270795A
Other languages
Japanese (ja)
Other versions
JPH05106582A (en
Inventor
哲哉 望月
進 川口
隆行 花木
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.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric 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 Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Priority to JP3270795A priority Critical patent/JP2629500B2/en
Publication of JPH05106582A publication Critical patent/JPH05106582A/en
Application granted granted Critical
Publication of JP2629500B2 publication Critical patent/JP2629500B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Description

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

【0001】[0001]

【産業上の利用分野】この発明は、冷凍・空調用に使用
する密閉形圧縮機の摺動部品に関するものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a sliding part of a hermetic compressor used for refrigeration and air conditioning.

【0002】[0002]

【従来の技術】図4は例えば特開昭63−159685
号公報に示された従来の鉄系金属の表面にボロン硬化層
を形成したベーン形圧縮機の摺動部材(ベーン)であ
り、図において、101は母材、102はボロン硬化
層、102aはボロン硬化層の表面に設けられたミクロ
孔部である。
2. Description of the Related Art FIG.
Is a sliding member (vane) of a conventional vane type compressor in which a boron hardened layer is formed on the surface of an iron-based metal, in which reference numeral 101 denotes a base material, 102 denotes a boron hardened layer, and 102a denotes a boron hardened layer. Micropores provided on the surface of the boron hardened layer.

【0003】ボロン硬化層2を形成した摺動部品は、表
面のボロン硬化層2の硬度が1200〜1800HVと
高く、またミクロ孔部2aに潤滑油が入り込むため潤滑
性能に優れており、耐摩耗性に優れ、かつ相手材の摩耗
も防止でき、圧縮機の寿命を長くし、又焼付きを防止す
ることができる。
[0003] The sliding parts having the hardened boron layer 2 have a high hardness of 1200 to 1800 HV on the surface of the hardened boron layer 2 and have excellent lubricating performance due to lubricating oil entering the micropores 2a. It is excellent in performance and can prevent wear of the partner material, prolong the life of the compressor and prevent seizure.

【0004】[0004]

【発明が解決しようとする課題】密閉形圧縮機の摺動部
品は、もれ損失を低下させるため相手部品、例えばベー
ンとベーンスロット、軸と軸受などのすきまは数μmの
嵌合寸法管理が必要である。このため、摺動部品に表面
処理を実施する場合、表面処理前後の寸法変化が大きな
問題となる。表面処理により寸法変化の無い場合は、仕
上げ加工後に表面処理を実施して、そのまま使用するこ
とができるが、表面層のFeにボロンBを浸透させるボ
ロン処理の場合、ボロン硬化層の厚さの約1/10程度
のボロン硬化層のふくれとともに800〜1000℃の
処理温度により、母材のボロン処理前の熱処理状態によ
っては、母材の組織変化、応力解放等により大きな寸法
変化を生じる場合があり、密閉形圧縮機の摺動部品とし
て使用する場合は、ボロン処理後に表面の硬度1500
HV程度の硬いボロン硬化層に仕上げ加工を施さなくて
はならない。従来例においては、固体法で浸ボロン処理
を施し、表面に厚さ約30μmのFeB(ホウ化第1
鉄)層と厚さ約70μmのFe2 B(ホウ化第2鉄)層
の2層からなる厚さ約100μmのボロン硬化層200
を形成し、このボロン硬化層を約数十μm、GC砥粒に
よるラッピングと仕上げにダイヤモンドラッピングにて
加工している。この時、ボロン硬化層の硬度は1500
HVと極めて高いため、特殊な仕上加工用の砥石や専用
の設備が必要となり、既存の鉄系材料を仕上げる場合と
比べて、加工が困難でまたコストもかかるという問題点
があった。また、厚さ100μm程度のボロン硬化層を
形成するためには3〜10時間という長い処理時間が必
要で、実用的でなく、ボロン処理にかかるコストの低減
の面からも、処理時間の短縮が望まれていた。加えて、
処理時間の短縮及び前述したボロン処理後の加工をなく
すことを目的として、ボロン処理層を必要低限まで薄く
した場合、使用時のボロン層のはく離が発生するという
問題点もある。
For the sliding parts of a hermetic compressor, in order to reduce leakage loss, mating dimensions of mating parts such as vanes and vane slots, shafts and bearings are controlled by several μm. is necessary. For this reason, when performing surface treatment on a sliding component, a dimensional change before and after the surface treatment becomes a serious problem. If there is no dimensional change due to the surface treatment, the surface treatment can be performed after the finish processing and used as it is. However, in the case of the boron treatment in which boron B is penetrated into Fe of the surface layer, the thickness of the boron hardened layer is reduced. Due to the treatment temperature of 800 to 1000 ° C. together with the boron swelling of the boron hardened layer of about 1/10, depending on the heat treatment state before the boron treatment of the base material, a large dimensional change may occur due to structural change of the base material, stress release, and the like. Yes, when used as sliding parts for hermetic compressors, surface hardness after boron treatment is 1500
A finishing process must be applied to the hardened boron layer of about HV. In a conventional example, boron is immersed by a solid method, and a surface of about 30 μm-thick FeB (first boride) is applied.
A hardened boron layer 200 having a thickness of about 100 μm, comprising two layers of an iron (Fe) layer and a Fe 2 B (ferric boride) layer having a thickness of about 70 μm.
This boron hardened layer is processed by diamond lapping for lapping and finishing with GC abrasive grains of about several tens μm. At this time, the hardness of the boron hardened layer is 1500
Since the HV is extremely high, a special grindstone for finishing and special equipment are required, and there is a problem that the processing is more difficult and costly as compared with the case of finishing an existing iron-based material. Further, a long processing time of 3 to 10 hours is required to form a boron cured layer having a thickness of about 100 μm, which is not practical, and the processing time can be reduced from the viewpoint of reducing the cost of boron processing. Was desired. in addition,
When the boron-treated layer is made as thin as necessary for the purpose of shortening the treatment time and eliminating the above-mentioned processing after the boron treatment, there is also a problem that the boron layer is peeled off during use.

【0005】この発明は上記のような問題点を解消する
ためになされたもので、ボロン処理前後の寸法変化が小
さく、ボロン処理前に仕上げ加工を施し、そのまま使用
することができ、また、ボロン処理時間が短く、薄いボ
ロン硬化層においてもはく離の可能性が小さい、経済的
でかつ信頼性の高い密閉型圧縮機の摺動部材を得ること
を目的とする。
The present invention has been made in order to solve the above-mentioned problems. The dimensional change before and after the boron treatment is small, and it is possible to perform finishing before the boron treatment and use it as it is. It is an object of the present invention to obtain an economical and highly reliable sliding member of a hermetic compressor having a short processing time and a small possibility of peeling even in a thin boron hardened layer.

【0006】[0006]

【課題を解決するための手段】この発明に係る密閉型圧
縮機の摺動部材は、Cr、Mo、W、Vなどの合金元素
含有率が低い鉄系材料に、焼入れ・焼戻し処理及び仕上
げ加工後にFe2 B単層から成るボロン硬化層を表面の
一部または全体に浸漬処理するものである。
SUMMARY OF THE INVENTION A sliding member of a hermetic compressor according to the present invention is formed by quenching / tempering and finishing a ferrous material having a low content of alloying elements such as Cr, Mo, W and V. Thereafter, a boron hardened layer composed of a single layer of Fe 2 B is immersed in part or all of the surface.

【0007】[0007]

【作用】この発明における密閉型圧縮機の摺動部材は、
母材に含有されるCの量によって決まる焼戻し後の母材
硬度を、仕上げ加工のできる最低限の硬度を保ち、か
つ、ボロン処理時の加熱による組織変化及び応力解放に
よる母材の寸法変化を最小にするように焼入れ及び焼戻
し温度をコントロールし、また、Fe2 B単層によるボ
ロン硬化層の厚さを従来例と比べて薄くする両方の効果
により、ボロン処理前後の寸法変化が小さくなるため、
ボロン処理前に仕上げ加工を施し、そのまま使用するこ
とができる。また、Fe2 B単層を溶融塩浸漬法により
従来例と比べて薄く表面に浸透させるボロン浸漬処理で
あり、加えてCr、Mo、W、Vなどの合金元素含有率
の低い鉄系材料を使用するため合金の含有によって起こ
るボロン処理時間の増大も発生せず2〜3時間の短時間
でボロン処理が実施できる。また、Cr、Mo、W、V
などの合金元素含有率が低い鉄系材料であるため主にC
r等の含有によって起こるボロン硬化層と母材層の境界
部のくさび状ボロン化合物生成効果をおさえる現象が発
生せず、くさび状にボロン加工物が生成するため、従来
と比べて薄いボロン硬化層でもはく離の可能性が小さく
なる。
The sliding member of the hermetic compressor according to the present invention comprises:
The hardness of the base material after tempering, which is determined by the amount of C contained in the base material, is kept at the minimum hardness that can be finished, and the dimensional change of the base material due to the structural change due to heating and the stress release during the boron treatment. Since the quenching and tempering temperatures are controlled to minimize the thickness and the thickness of the boron hardened layer made of a single layer of Fe 2 B is made thinner compared to the conventional example, the dimensional change before and after the boron treatment is reduced. ,
Finish processing can be performed before boron treatment and used as it is. In addition, a boron immersion treatment in which the Fe 2 B single layer is penetrated into the surface thinly by a molten salt immersion method as compared with the conventional example, and in addition, an iron-based material having a low content of alloying elements such as Cr, Mo, W, and V is used. Since the alloy is used, the boron treatment time does not increase due to the inclusion of the alloy, and the boron treatment can be performed in a short time of 2 to 3 hours. Also, Cr, Mo, W, V
Mainly because it is a ferrous material with a low content of alloying elements such as
Since the phenomenon that suppresses the effect of forming the wedge-shaped boron compound at the boundary between the boron-hardened layer and the base material layer caused by the inclusion of r and the like does not occur, and a boron-processed product is generated in a wedge-like shape, the boron-hardened layer is thinner than before. However, the possibility of peeling is reduced.

【0008】[0008]

【実施例】実施例1. 以下この発明の一実施例を図1について、例えば母材を
SK−5とした場合について説明する。図1において、
1はSK−5の母材である。SK−5材はC含有率0.
8%の炭素工具鋼で、合金Cr0.30%以下、Ni
0.25%以下、Cu0.25%以下、Mo、W、Vは
含有されていないキルド鋼である。母材は850℃40
minの焼入れ後、550℃2Hrの焼戻し処理により
硬度はHRC37程度となったものを仕上げ加工してあ
る。2はFe2 B単層による厚さ約30μmのボロン硬
化層であり、母材との境界部にはくさび状ボロン加
3が生成している。この実施例でのボロン処理は、処理
温度800℃、処理時間2〜3Hrの溶融塩浸漬法であ
る。
[Embodiment 1] One embodiment of the present invention will be described below with reference to FIG. 1 where, for example, the base material is SK-5. In FIG.
1 is a base material of SK-5. SK-5 has a C content of 0.
8% carbon tool steel, alloy Cr 0.30% or less, Ni
0.25% or less, Cu 0.25% or less, Mo, W, V are killed steels not containing. Base material is 850 ℃ 40
After quenching for a minimum of 550 ° C. for 2 hours, a material having a hardness of about HRC37 by tempering at 2 hours is finished. 2 is a boron cured layer having a thickness of about 30μm by Fe 2 B monolayer, the boundary between the base material is generated by the wedge-shaped boron additive compound 3. The boron treatment in this embodiment is a molten salt immersion method at a treatment temperature of 800 ° C. and a treatment time of 2 to 3 hours.

【0009】本実施例の場合、SK−5K金属材料的特
性より、焼入れ後の焼戻し温度による母材1の硬度とボ
ロン処理時の800℃の加熱及びボロン層の生成による
ふくれのためのボロン処理前後の寸法変化量は、焼戻し
温度により支配され、図2に示すような関係になる。図
2において、焼戻し温度230℃のポイントは今回のボ
ロン処理と同一の条件にて比較のために行なったもの
で、母材はSUJ−2である。仕上げ加工のために必要
な最低限の硬度は、一般にHRC30程度であり、今回
の実施例のものでは焼戻し温度550〜600℃でHR
C35〜40、また比較用のSUJ−2ではHRC60
程度となっており、どちらも仕上げ加工が可能な硬度と
なっている。しかし、ボロン処理後の寸法変化は今回の
実施例の場合3μm程度に対し、比較用のSUJ−2で
は30μm程度の大きな寸法変化が生じている。これは
図3に示すように共析炭素鋼の焼戻しに対する寸法変化
の特性より、今回の実施例のように、550〜600℃
の焼戻し温度で処理された場合(X点)その後、ボロン
処理時に800℃程度の加熱を受けても(D点)母材1
の特性はX点に戻り寸法変化はほとんど発生せず、図2
に示したように、ボロン硬化層2の厚さ30μmの約1
/10のふくれとして3μmの寸法変化のみを生じてい
る。これに対して比較用のSUJ−2は、焼戻し温度が
230℃で、Y点で処理されたことになり、ボロン処理
時に800℃の加熱をされるとZ点に戻るためY−Zの
寸法変化として、約30μmを生じてしまうこととな
る。また、実施例のSK−5の場合、合金元素の含有が
ほとんど無いため、合金の含有によるボロン処理時間の
アップが発生せず、かつ、約30μmという薄いボロン
硬化層であるため、ボロン処理時間は従来例の3〜10
時間と比較して、2〜3時間と大幅に短縮することがで
きる。この時、母材に合金元素、特にCr等の含有がほ
とんど無いため、ボロン硬化層と母材層の境界部にくさ
び状ボロン化合物を十分に成生するので、従来と比べて
薄いボロン硬化層でもはく離の可能性が小さいものとな
り、信頼性の向上もはかれている。
In the case of the present embodiment, the hardness of the base material 1 according to the tempering temperature after quenching, the heating at 800 ° C. during the boron treatment, and the boron treatment for blistering due to the formation of the boron layer, from the characteristics of the SK-5K metal material. The amount of dimensional change before and after is governed by the tempering temperature and has a relationship as shown in FIG. In FIG. 2, the point at a tempering temperature of 230 ° C. is for comparison under the same conditions as in the present boron treatment, and the base material is SUJ-2. The minimum hardness required for finish processing is generally about HRC30, and in this embodiment, the temper temperature is 550 to 600 ° C and the HR is
C35-40, and HRC60 in SUJ-2 for comparison
And both have a hardness that allows finishing. However, the dimensional change after the boron treatment is as large as about 3 μm in the present embodiment, whereas the dimensional change in the comparative SUJ-2 is as large as about 30 μm. This is based on the dimensional change characteristics of eutectoid carbon steel with respect to tempering as shown in FIG.
(Point X), the base material 1 may be heated at about 800 ° C. during boron treatment (point D).
2 returns to the point X and almost no dimensional change occurs.
As shown in FIG.
As a result, only a dimensional change of 3 μm is caused as blisters of / 10. On the other hand, SUJ-2 for comparison has a tempering temperature of 230 ° C. and is treated at the Y point. When heated at 800 ° C. during the boron treatment, the temperature returns to the Z point. As a change, about 30 μm is generated. Moreover, in the case of SK-5 embodiment, since almost no content of alloying elements, since does not occur up boron processing time by containing alloy, and a thin boron hardened layer of approximately 30 [mu] m, boron processing time Are 3 to 10 of the conventional example.
Compared to the time, it can be significantly reduced to 2-3 hours. At this time, since the base material contains almost no alloying elements, especially Cr, etc., a sufficient amount of a wedge-shaped boron compound is formed at the boundary between the boron hardened layer and the base material layer. However, the possibility of peeling has become smaller, and reliability has been improved.

【0010】[0010]

【発明の効果】以上のように、この発明による密閉形圧
縮機の摺動部材は、合金元素含有率が低い鉄系材料に、
焼入れ・焼戻し処理及び仕上げ加工時にFe2 B単層か
ら成るボロン硬化層を表面の一または全体に浸漬処理
したもので、ボロン処理前後の寸法変化が小さく、ボロ
ン処理前に仕上げ加工を施し、そのまま使用することが
でき、また、ボロン処理時間が短く、薄いボロン硬化層
においてもはく離の可能性が小さい、経済的でかつ信頼
性の高い密閉形圧縮機の摺動部材が得られる。
As described above, the sliding member of the hermetic compressor according to the present invention can be used for an iron-based material having a low alloy element content.
Which was a boron hardened layer consisting of Fe 2 B monolayer during quenching and tempering and finishing was immersed in a part or whole of the surface, small dimensional change before and after boron treatment, subjected to finishing before the boron treatment, An economical and highly reliable sliding member of a hermetic compressor that can be used as it is, has a short boron treatment time, and has a small possibility of peeling even in a thin boron hardened layer can be obtained.

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

【図1】この発明の一実施例による摺動部品の要部断面
図である。
FIG. 1 is a sectional view of a main part of a sliding component according to an embodiment of the present invention.

【図2】この発明の一実施例による摺動部品の焼戻し温
度と硬度及びボロン処理前後の寸法変化を示す説明図で
ある。
FIG. 2 is an explanatory diagram showing a tempering temperature and hardness of a sliding component and a dimensional change before and after boron treatment according to an embodiment of the present invention.

【図3】この発明の一実施例による摺動部品の共析炭素
鋼の焼戻しに対する寸法変化の特性を示す説明図であ
る。
FIG. 3 is an explanatory view showing a dimensional change characteristic of a sliding component according to an embodiment of the present invention with respect to tempering of eutectoid carbon steel.

【図4】従来の摺動部品(ベーン)の要部断面図であ
る。
FIG. 4 is a sectional view of a main part of a conventional sliding component (vane).

【符号の説明】[Explanation of symbols]

1 合金元素含有率の低い鉄系材料による母材 2 Fe2 B単層によるボロン硬化層 2a ミクロ孔部 3 くさび状ボロン化合物Base material 2 Fe 2 B boron cured layer 2a micropores 3 wedge-shaped boron compounds according monolayer by low iron-based material 1 alloying element content

Claims (1)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】 合金元素含有率の低い鉄系材料と、この
鉄系材料の焼入れ・焼戻し処理及び仕上げ加工後に、そ
の表面に浸漬処理されたFe2 B単層から成るボロン硬
化層とを備えたことを特徴とする密閉形圧縮機の摺動部
材。
An iron-based material having a low alloying element content, and a hardened boron layer made of a single layer of Fe 2 B immersed on the surface of the iron-based material after quenching / tempering and finishing. A sliding member for a hermetic compressor.
JP3270795A 1991-10-18 1991-10-18 Sliding member of hermetic compressor Expired - Lifetime JP2629500B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3270795A JP2629500B2 (en) 1991-10-18 1991-10-18 Sliding member of hermetic compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3270795A JP2629500B2 (en) 1991-10-18 1991-10-18 Sliding member of hermetic compressor

Publications (2)

Publication Number Publication Date
JPH05106582A JPH05106582A (en) 1993-04-27
JP2629500B2 true JP2629500B2 (en) 1997-07-09

Family

ID=17491117

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3270795A Expired - Lifetime JP2629500B2 (en) 1991-10-18 1991-10-18 Sliding member of hermetic compressor

Country Status (1)

Country Link
JP (1) JP2629500B2 (en)

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS56108803A (en) * 1980-01-30 1981-08-28 Toshiba Corp Ferrous sintered parts

Also Published As

Publication number Publication date
JPH05106582A (en) 1993-04-27

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