JP2852623B2 - Gas compressor - Google Patents
Gas compressorInfo
- Publication number
- JP2852623B2 JP2852623B2 JP7001482A JP148295A JP2852623B2 JP 2852623 B2 JP2852623 B2 JP 2852623B2 JP 7001482 A JP7001482 A JP 7001482A JP 148295 A JP148295 A JP 148295A JP 2852623 B2 JP2852623 B2 JP 2852623B2
- Authority
- JP
- Japan
- Prior art keywords
- rotor
- face
- gas compressor
- aluminum rotor
- plastic flow
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 230000006835 compression Effects 0.000 claims description 11
- 238000007906 compression Methods 0.000 claims description 11
- 230000003014 reinforcing effect Effects 0.000 claims description 9
- 230000002093 peripheral effect Effects 0.000 claims description 8
- 239000003507 refrigerant Substances 0.000 claims description 5
- 238000003754 machining Methods 0.000 claims description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 46
- 229910052782 aluminium Inorganic materials 0.000 description 46
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 40
- 229910052742 iron Inorganic materials 0.000 description 20
- 229910000831 Steel Inorganic materials 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000010687 lubricating oil Substances 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
Landscapes
- Applications Or Details Of Rotary Compressors (AREA)
- Rotary Pumps (AREA)
Description
【0001】[0001]
【産業上の利用分野】この発明はカーエアコン等に用い
られる気体圧縮機に関し、特にアルミ製ロータの強度向
上を図るのに好適なものである。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a gas compressor used for a car air conditioner and the like, and is particularly suitable for improving the strength of an aluminum rotor.
【0002】[0002]
【従来の技術】従来より、この種の軽量型の気体圧縮機
としては例えば図4に示す如く内周楕円状のシリンダ1
内に断面円形状のアルミ製ロータ2(以下、アルミロー
タという。)を回転可能に収納したものが知られてお
り、アルミロータ2にはその両端面を貫く貫通穴2aを
介して鉄製シャフト3(以下、鉄シャフトという。)が
一体に設けられている。2. Description of the Related Art Conventionally, as a lightweight gas compressor of this type, for example, as shown in FIG.
An aluminum rotor 2 (hereinafter, referred to as an aluminum rotor) having a circular cross section is rotatably housed therein, and the aluminum rotor 2 is provided with a steel shaft 3 through a through hole 2a penetrating both end surfaces thereof. (Hereinafter, referred to as an iron shaft).
【0003】アルミロータ2と鉄シャフト3を一体化す
る際は、図6(a)に示すようにアルミロータ2の貫通
穴2aに鉄製シャフト3を挿入した上で、アルミロータ
2の端面2bをダイス100で加圧し、これによりアル
ミロータ2の一部を鉄シャフト3の外周溝部3aに塑性
流動させ、この塑性流動部Aを介してアルミロータ2と
鉄シャフト3とを締結する。When the aluminum rotor 2 and the iron shaft 3 are integrated, the iron shaft 3 is inserted into the through hole 2a of the aluminum rotor 2 as shown in FIG. Pressing is performed by the die 100, whereby a part of the aluminum rotor 2 is plastically flown into the outer peripheral groove 3a of the iron shaft 3, and the aluminum rotor 2 and the iron shaft 3 are fastened through the plastic flow part A.
【0004】このため、アルミロータ2の端面2bと鉄
シャフト3の外周溝部3aとの位置およびその形状は重
要であり、塑性流動したアルミロータ2の一部を鉄シャ
フト3の外周溝部3a溝に充満させてアルミロータ2と
鉄シャフト3の高い締結強度を得るにはアルミロータ2
と鉄シャフト3の位置およびその形状を図6(a)に示
すように設けるのが最適である。For this reason, the position and shape of the end face 2b of the aluminum rotor 2 and the outer peripheral groove 3a of the iron shaft 3 are important, and a part of the plastically flowed aluminum rotor 2 is transferred to the outer peripheral groove 3a of the iron shaft 3. To obtain high fastening strength between the aluminum rotor 2 and the iron shaft 3 by filling
It is optimal to provide the position of the iron shaft 3 and its shape as shown in FIG.
【0005】また、上記の如くアルミロータ2と鉄シャ
フト3を締結した後、アルミロータ2は端面2bに切削
加工および研削加工等の機械加工を施して図6(b)に
示すような所望の形状に形成する。After the aluminum rotor 2 and the iron shaft 3 are fastened to each other as described above, the aluminum rotor 2 is subjected to machining such as cutting and grinding on the end face 2b to obtain a desired surface as shown in FIG. Form into shape.
【0006】なお、図4に示すように、シリンダ1は一
対のサイドブロック4,4間に配設され、一対のサイド
ブロック4,4はシリンダ1の端面にそれぞれ取り付け
られており、また鉄シャフト3はサイドブロック4,4
の軸受部5,5により支持されている。As shown in FIG. 4, the cylinder 1 is disposed between a pair of side blocks 4 and 4, and the pair of side blocks 4 and 4 are attached to end surfaces of the cylinder 1, respectively. 3 is the side block 4, 4
Are supported by the bearing portions 5, 5.
【0007】また、図5に示すように、アルミロータ2
にはその径方向にベーン溝6,6…が形成され、ベーン
溝6,6にはベーン7,7…が装着されており、ベーン
7,7…はアルミロータ2の外周面からシリンダ1の内
壁に向かって出没自在に設けられ、かつシリンダ1の内
壁に付勢され、この種の付勢力はアルミロータ2の回転
による遠心力、およびベーン溝6,6に供給される潤滑
油の背圧により得られる。Further, as shown in FIG.
Are formed in the radial direction thereof, and vanes 7, 7,... Are mounted in the vane grooves 6, 6, and the vanes 7, 7,. It is provided so as to be able to protrude and retract toward the inner wall and is urged against the inner wall of the cylinder 1. This kind of urging force is caused by centrifugal force due to rotation of the aluminum rotor 2 and back pressure of lubricating oil supplied to the vane grooves 6, 6. Is obtained by
【0008】このような気体圧縮機においては、鉄シャ
フト3が回転し、この回転トルクがアルミロータ2に伝
達され、アルミロータ2が回転すると、シリンダ1、ア
ルミロータ2、一対のサイドブロック4,4およびベー
ン7,7…により仕切られた圧縮作業室8,8…の容量
が変化し、これにより吸入室9の冷媒ガスを圧縮して吐
出室10に吐出する。In such a gas compressor, the iron shaft 3 rotates, and this rotational torque is transmitted to the aluminum rotor 2, and when the aluminum rotor 2 rotates, the cylinder 1, the aluminum rotor 2, a pair of side blocks 4, 4 and the capacity of the compression working chambers 8, 8, ... divided by the vanes 7, 7, ..., thereby compress the refrigerant gas in the suction chamber 9 and discharge it to the discharge chamber 10.
【0009】[0009]
【発明が解決しようとする課題】しかしながら、上記の
ような従来の気体圧縮機にあっては、アルミロータ2と
鉄シャフト3を締結した後、アルミロータ2の端面2b
に機械加工を施してアルミロータ2を図6(b)に示す
ような形状に形成すると、塑性流動部Aに極端な薄肉部
ができるため、これによりアルミロータ2の強度が低下
する等の問題点がある。However, in the conventional gas compressor as described above, after the aluminum rotor 2 and the iron shaft 3 are fastened, the end face 2b of the aluminum rotor 2 is closed.
When the aluminum rotor 2 is formed into a shape as shown in FIG. 6 (b) by machining, the plastic flow portion A has an extremely thin portion, which causes a problem such as a decrease in the strength of the aluminum rotor 2. There is a point.
【0010】なお、鉄シャフト3における外周溝部3a
の位置およびその形状については前述の通り塑性流動の
面から一義的に決められており、塑性流動を無視してそ
れらを変更することはアルミロータ2と鉄シャフト3間
の締結強度の低下を招くことから許されないため、塑性
流動部Aに薄肉部ができない位置に外周溝部3aを設け
る、あるいは塑性流動部Aに薄肉部ができない形状に外
周溝部3aを形成することはできない。The outer circumferential groove 3a of the iron shaft 3
As described above, the position and shape of the shaft are uniquely determined from the viewpoint of plastic flow, and changing them while ignoring the plastic flow causes a decrease in the fastening strength between the aluminum rotor 2 and the iron shaft 3. Therefore, the outer peripheral groove 3a cannot be provided at a position where a thin portion cannot be formed in the plastic flow portion A, or the outer peripheral groove 3a cannot be formed in a shape where a thin portion cannot be formed in the plastic flow portion A.
【0011】この発明は上述の事情に鑑みてなされたも
ので、その目的とするところはアルミロータの強度向上
を図るのに好適な気体圧縮機を提供することにある。The present invention has been made in view of the above circumstances, and an object of the present invention is to provide a gas compressor suitable for improving the strength of an aluminum rotor.
【0012】[0012]
【課題を解決するための手段】上記目的を達成するため
に、請求項1記載の発明は、一対のサイドブロック、両
サイドブロック間に配設したシリンダ、上記シリンダ内
に回転可能に収納したロータ、上記ロータの外周面から
上記シリンダの内壁に向かって出没自在なベーン、およ
びこれらにより仕切られた圧縮作業室を備え、上記ロー
タの回転による圧縮作業室の容量変化で冷媒ガスを圧縮
する気体圧縮機において、上記ロータと、上記ロータに
回転トルクを伝達するためのシャフトとを締結するた
め、上記ロータの貫通穴の開口周縁にあたる上記ロータ
の端面をダイスで加圧して塑性変形することによって、
上記シャフトの外周溝部に上記ロータの一部を塑性流動
して塑性流動部を形成し、上記ダイスによる加圧変形部
分に切削加工および研削加工などの機械加工を施し除去
するとき、上記塑性流動部が最大限残余し補強でき、上
記ロータの端面側に拡がるテーパ部となるように加工し
た補強部が形成されてなることを特徴とする。To achieve the above object, according to the solution to ## invention of claim 1, wherein, and rotatably accommodated a pair of side blocks, cylinder disposed between the two side blocks, in the cylinder rotor , from the outer peripheral surface of the rotor
Retractable vane towards the inner wall of the cylinder, and includes a compression working chamber which is partitioned by these, in the gas compressor for compressing a refrigerant gas in a volume change of the compression working chamber due to the rotation of the low <br/> data , The rotor and the rotor
For fastening the shaft for transmitting the rotational torque
The rotor corresponding to the opening periphery of the through hole of the rotor
By pressurizing the end face with a die and plastically deforming it,
Plastic flow of part of the rotor into the outer circumferential groove of the shaft
To form a plastic flow part, and pressurized and deformed by the die
Machined and machined such as cutting and grinding
When the plastic flow part can be reinforced as much as possible,
Work so that it becomes a tapered part that spreads to the end face side of the rotor.
Characterized in that the reinforcing portion is formed .
【0013】請求項2記載の発明は、上記ロータの端面
側に拡がる上記テーパ部が円弧状となしたことを特徴と
する。According to a second aspect of the present invention , an end face of the rotor is provided.
The tapered portion expanding to the side has an arc shape .
【0014】請求項3記載の発明は、上記ロータの端面
側に拡がる上記テーパ部が上記ロータの端面より突出す
るように設けた段部からなることを特徴とする。According to a third aspect of the present invention , an end face of the rotor is provided.
The tapered portion expanding to the side protrudes from the end face of the rotor.
It is characterized by comprising a step provided so that it may be.
【0015】[0015]
【0016】[0016]
【作用】この発明によれば、補強部により塑性流動部が
補強されることから、特にこの種の塑性流動部を介し鉄
シャフトとの締結を行うアルミロータの不具合、すなわ
ち塑性流動部からアルミロータが破損するのを防止でき
る。According to the present invention, since the plastic flow portion is reinforced by the reinforcing portion, in particular, the problem of the aluminum rotor that is fastened to the iron shaft through this type of plastic flow portion, that is, the aluminum flow from the plastic flow portion to the aluminum rotor. Can be prevented from being damaged.
【0017】[0017]
【実施例】以下、この発明に係る気体圧縮機の実施例に
ついて図1ないし図3を基に詳細に説明する。DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS An embodiment of a gas compressor according to the present invention will be described below in detail with reference to FIGS.
【0018】なお、気体圧縮機の基本的な構成、例えば
一対のサイドブロック4,4、シリンダ1、アルミロー
タ2、およびベーン7,7…により仕切られた圧縮作業
室8,8…を備えること、並びにロータ2の回転による
圧縮作業室8,8…の容量変化で冷媒ガスを圧縮するこ
と等は従来と同様なため、それと同一部材には同一符号
を付し、その詳細説明は省略する。It is to be noted that a basic configuration of the gas compressor is provided, for example, to include a pair of side blocks 4, 4, a cylinder 1, an aluminum rotor 2, and compression working chambers 8, 8, ... partitioned by vanes 7, 7, .... , And the compression of the refrigerant gas by the change of the capacity of the compression working chambers 8, 8,... Due to the rotation of the rotor 2 is the same as in the prior art.
【0019】この気体圧縮機は図1に示す如くアルミロ
ータ2の端面2b側に補強部としてテーパ部11が設け
られている。As shown in FIG. 1, this gas compressor is provided with a tapered portion 11 as a reinforcing portion on the end face 2b side of the aluminum rotor 2.
【0020】テーパ部11はアルミロータ2の貫通穴2
aの周縁に位置し、かつアルミロータ2と鉄シャフト3
とを締結する塑性流動部Aに一体に形成され、この塑性
流動部Aを補強する。The tapered portion 11 is a through hole 2 of the aluminum rotor 2.
a, the aluminum rotor 2 and the iron shaft 3
Are formed integrally with the plastic flow portion A, which reinforces the plastic flow portion A.
【0021】また、テーパ部11はアルミロータ2の端
面2b側で拡がりが最大となるように設けられている。The tapered portion 11 is provided so as to maximize the expansion on the end face 2b side of the aluminum rotor 2.
【0022】上記のようなテーパ部11を形成するため
には、先ずアルミロータ2の一部を鉄シャフト3の外周
溝部3aに塑性流動させ、この塑性流動部Aを介してア
ルミロータ2と鉄シャフト3を締結する(図6(a)参
照)。その後、アルミロータ2の端面2bに切削加工等
の機械加工を施すとき、アルミロータ2の端面2bと鉄
シャフト3との境、すなわち貫通穴2aの周縁をテーパ
部11として残せばよい。In order to form the tapered portion 11 as described above, first, a part of the aluminum rotor 2 is plastically flowed into the outer circumferential groove 3a of the iron shaft 3, and the aluminum rotor 2 and the iron rotor 2 are formed through the plastic flow portion A. fastening the shaft 3 (see FIG. 6 (a)). Thereafter, when machining such as cutting is performed on the end face 2 b of the aluminum rotor 2, the boundary between the end face 2 b of the aluminum rotor 2 and the iron shaft 3, that is, the peripheral edge of the through hole 2 a may be left as the tapered portion 11.
【0023】次に、上記の如く構成された気体圧縮機の
動作を図1に基づき説明する。Next, the operation of the gas compressor configured as described above will be described with reference to FIG.
【0024】この気体圧縮機によれば、従来と同様にア
ルミロータ2の回転による圧縮作業室8,8…の容量変
化で冷媒ガスを圧縮する際、その圧縮力がアルミロータ
2に加わるが、塑性流動部Aはテーパ部11により補強
されているので、塑性流動部Aからアルミロータが破損
するのを防止でき、アルミロータ2を使用した気体圧縮
機の長期にわたる運転が可能となる。According to this gas compressor, the compression force is applied to the aluminum rotor 2 when compressing the refrigerant gas by changing the capacity of the compression working chambers 8, 8... Since the plastic flow portion A is reinforced by the tapered portion 11, the aluminum rotor can be prevented from being damaged from the plastic flow portion A, and the gas compressor using the aluminum rotor 2 can be operated for a long time.
【0025】したがって、上記実施例の気体圧縮機によ
れば、テーパ部11により塑性流動部Aを補強し、これ
により塑性流動部Aからアルミロータ2が破損するのを
防止したものであるため、アルミロータ2の強度が高
く、耐久性に優れる。Therefore, according to the gas compressor of the above embodiment, the plastic flow portion A is reinforced by the tapered portion 11, thereby preventing the aluminum rotor 2 from being damaged from the plastic flow portion A. The strength of the aluminum rotor 2 is high and the durability is excellent.
【0026】なお、上記実施例では補強部をテーパ部1
1から構成したが、これに代えて補強部は図2に示すよ
うな円弧部12または図3に示すような段部13として
構成してもよい。このとき円弧部12はテーパ部11と
同じくアルミロータ2の端面側で拡がりが最大となるよ
うに設け、また段部13はアルミロータ2の端面より突
出するように設ける。このような円弧部12および段部
13からなる補強部にあっても、テーパ部11と同様な
効果、すなわちアルミロータ2の耐久性向上を図れる。In the above embodiment, the reinforcing portion is formed by the tapered portion 1.
1, the reinforcing portion may be configured as a circular arc portion 12 as shown in FIG. 2 or a step portion 13 as shown in FIG. At this time, the circular arc portion 12 is provided so as to maximize the spread on the end face side of the aluminum rotor 2 like the tapered portion 11, and the step portion 13 is provided so as to protrude from the end face of the aluminum rotor 2. Even in the reinforcing portion including the arc portion 12 and the step portion 13, the same effect as that of the tapered portion 11, that is, the durability of the aluminum rotor 2 can be improved.
【0027】[0027]
【発明の効果】この発明に係る気体圧縮機にあっては、
上記の如くロータとこれに回転トルクを伝達するシャフ
トとを締結するロータ端面側の塑性流動部に、補強部を
設けたため、補強部により塑性流動部が補強されるの
で、特にこの種の塑性流動部を介し鉄シャフトとの締結
を行うアルミロータの不具合、すなわち塑性流動部から
アルミロータが破損するのを防止でき、アルミロータの
強度向上を図るのに好適である。In the gas compressor according to the present invention,
As described above, since the reinforcing portion is provided in the plastic flow portion on the rotor end surface side for fastening the rotor and the shaft transmitting the rotational torque to the rotor, the plastic flow portion is reinforced by the reinforcing portion. It is possible to prevent the problem of the aluminum rotor that is fastened to the iron shaft via the portion, that is, to prevent the aluminum rotor from being damaged from the plastic flow portion, and it is suitable for improving the strength of the aluminum rotor.
【0028】[0028]
【図1】この発明に係る気体圧縮機の要部を示す断面
図。FIG. 1 is a sectional view showing a main part of a gas compressor according to the present invention.
【図2】この発明の他の実施例を示す断面図。FIG. 2 is a sectional view showing another embodiment of the present invention.
【図3】この発明の他の実施例を示す断面図。FIG. 3 is a sectional view showing another embodiment of the present invention.
【図4】従来の気体圧縮機の断面図。FIG. 4 is a sectional view of a conventional gas compressor.
【図5】図4のIII−III線断面図。FIG. 5 is a sectional view taken along line III-III of FIG. 4 ;
【図6】図4に示す気体圧縮機のロータとシャフトとの
締結部分の説明図。FIG. 6 is an explanatory diagram of a fastening portion between a rotor and a shaft of the gas compressor shown in FIG. 4 ;
A 塑性流動部 1 シリンダ 2 ロータ 3 シャフト 4 サイドブロック 7 ベーン 8 圧縮作業室 11 テーパ部 12 円弧部 13 段部 A plastic flow section 1 cylinder 2 rotor 3 shaft 4 side block 7 vane 8 compression working chamber 11 taper section 12 arc section 13 step section
フロントページの続き (56)参考文献 特開 平5−33788(JP,A) 特開 昭63−268525(JP,A) (58)調査した分野(Int.Cl.6,DB名) F04C 18/30 - 18/352 F04C 2/30 - 2/352 F04C 29/00 - 29/10 B21D 39/04Continuation of the front page (56) References JP-A-5-33788 (JP, A) JP-A-63-268525 (JP, A) (58) Fields investigated (Int. Cl. 6 , DB name) F04C 18 / 30-18/352 F04C 2/30-2/352 F04C 29/00-29/10 B21D 39/04
Claims (3)
ク間に配設したシリンダ、上記シリンダ内に回転可能に
収納したロータ、上記ロータの外周面から上記シリンダ
の内壁に向かって出没自在なベーン、およびこれらによ
り仕切られた圧縮作業室を備え、上記ロータの回転によ
る圧縮作業室の容量変化で冷媒ガスを圧縮する気体圧縮
機において、上記ロータと、上記ロータに回転トルクを伝達するため
のシャフトとを締結するため、上記ロータの貫通穴の開
口周縁にあたる上記ロータの端面をダイスで加圧して塑
性変形することによって、上記シャフトの外周溝部に上
記ロータの一部を塑性流動して塑性流動部を形成し、上
記ダイスによる加圧変形部分に切削加工および研削加工
などの機械加工を施し除去するとき、上記塑性流動部が
最大限残余し補強でき、上記ロータの端面側に拡がるテ
ーパ部となるように加工した補強部が形成されてなる こ
とを特徴とする気体圧縮機。1. A pair of side blocks, cylinder disposed between the two side blocks, rotor rotatably housed in the cylinder, the rotor outer circumferential surface retractably toward the inner wall of the cylinder from the vane, and includes a compression working chamber which is partitioned by these, in the gas compressor for compressing a refrigerant gas in a volume change of the compression working chamber due to the rotation of the rotor, in order to transmit and the rotor, the rotational torque to the rotor
To open the through hole of the rotor
Press the end face of the rotor corresponding to the peripheral edge of the rotor with a die to
The upper part of the shaft is deformed by
A part of the rotor plastically flows to form a plastic flow part,
Cutting and grinding on the pressurized deformed part with the die
When removing by machining such as
The tape can be reinforced as much as possible, and it extends to the end face of the rotor.
A gas compressor characterized by having a reinforcing portion processed so as to be a tapered portion .
部が円弧状となしたことを特徴とする請求項1記載の気
体圧縮機。2. The taper extending toward the end face of the rotor.
The gas compressor according to claim 1, wherein the portion has an arc shape .
部が上記ロータの端面より突出するように設けた段部か
らなることを特徴とする請求項1記載の気体圧縮機。3. The taper expanding toward the end face of the rotor.
The gas compressor according to claim 1, wherein the portion comprises a step portion provided so as to protrude from an end face of the rotor .
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7001482A JP2852623B2 (en) | 1995-01-09 | 1995-01-09 | Gas compressor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7001482A JP2852623B2 (en) | 1995-01-09 | 1995-01-09 | Gas compressor |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH08189486A JPH08189486A (en) | 1996-07-23 |
| JP2852623B2 true JP2852623B2 (en) | 1999-02-03 |
Family
ID=11502665
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP7001482A Expired - Lifetime JP2852623B2 (en) | 1995-01-09 | 1995-01-09 | Gas compressor |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP2852623B2 (en) |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2740585B2 (en) * | 1991-07-26 | 1998-04-15 | カルソニック株式会社 | Method of manufacturing rotary compressor |
-
1995
- 1995-01-09 JP JP7001482A patent/JP2852623B2/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| JPH08189486A (en) | 1996-07-23 |
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