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JP2990907B2 - Scroll compressor - Google Patents
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JP2990907B2 - Scroll compressor - Google Patents

Scroll compressor

Info

Publication number
JP2990907B2
JP2990907B2 JP3330193A JP33019391A JP2990907B2 JP 2990907 B2 JP2990907 B2 JP 2990907B2 JP 3330193 A JP3330193 A JP 3330193A JP 33019391 A JP33019391 A JP 33019391A JP 2990907 B2 JP2990907 B2 JP 2990907B2
Authority
JP
Japan
Prior art keywords
blade
spiral
winding
spiral blade
swirling
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
JP3330193A
Other languages
Japanese (ja)
Other versions
JPH05164067A (en
Inventor
澤井  清
道生 山村
正太郎 伊東
定夫 河原
学 阪井
靖 饗場
修一 山本
正浩 坪川
能宣 小嶋
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.)
Panasonic Holdings Corp
Original Assignee
Matsushita Electric Industrial Co Ltd
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 Matsushita Electric Industrial Co Ltd filed Critical Matsushita Electric Industrial Co Ltd
Priority to JP3330193A priority Critical patent/JP2990907B2/en
Publication of JPH05164067A publication Critical patent/JPH05164067A/en
Application granted granted Critical
Publication of JP2990907B2 publication Critical patent/JP2990907B2/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】本発明は、冷暖房、あるいは冷蔵
庫等の冷却装置に用いられるスクロール圧縮機に関す
る。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a scroll compressor used for a cooling device such as a cooling and heating system or a refrigerator.

【0002】[0002]

【従来の技術】従来のスクロール圧縮機における羽根形
状は、特開平1−216091号公報(図7)に記載の
旋回渦巻羽根102のように、中心部の巻始め部を除い
てその渦巻は巻終り端まで一様なインボリュート曲線で
構成され、均一な羽根厚さtとなっていた。
2. Description of the Related Art The blade shape of a conventional scroll compressor is similar to that of a swirling spiral blade 102 described in Japanese Patent Application Laid-Open No. 1-216091 (FIG. 7) except for the spiral portion except for the winding start portion at the center. The blade had a uniform involute curve up to the end and had a uniform blade thickness t.

【0003】また、羽根高さについては、巻始め部から
巻終り端まで一定の高さHとなっていた。
[0003] Further, the blade height is constant H from the start of winding to the end of winding.

【0004】[0004]

【発明が解決しようとする課題】前記従来技術は、渦巻
羽根の厚みが羽根全体にわたって均一であるため、巻終
り部は他の部分に比較して強度が弱いという問題があっ
た。すなわち、羽根が一様なインボリュート曲線で構成
されているため、高回転数での運転時に、旋回渦巻部品
に働く大きな遠心力によって、一方の羽根が他方の羽根
の壁面に接触する場合が発生し、たまたまその接触が羽
根の巻終り部で生じると羽根が破損してしまうという問
題が生じていた。
In the above prior art, there is a problem that the strength of the end portion of the spiral is lower than that of other portions because the thickness of the spiral blade is uniform over the entire blade. In other words, since the blades are configured with a uniform involute curve, one of the blades may come into contact with the wall surface of the other blade due to the large centrifugal force acting on the swirling spiral parts during operation at a high rotation speed. However, if the contact happens to occur at the end of the winding of the blade, the blade is damaged.

【0005】また、羽根高さが巻始め部から巻終り端ま
で一定の高さとなっているため、除霜運転のような特殊
な圧力・温度条件下での温度歪や圧力歪によって、一方
の羽根の軸方向先端部が他方の渦巻部品の端板に接触摺
動し、その結果、強度の弱い巻終り部が破損してしまう
という問題が発生していた。
[0005] Further, since the blade height is constant from the start of winding to the end of winding, one of the blades may be subjected to temperature distortion or pressure distortion under special pressure and temperature conditions such as defrosting operation. The tip of the blade in the axial direction slides in contact with the end plate of the other spiral part, and as a result, a problem has occurred in that the end part having a weak strength is damaged.

【0006】[0006]

【課題を解決するための手段】前記目的を達成するた
め、本発明では、固定渦巻羽根あるいは旋回渦巻羽根の
巻終り部の羽根高さを段階的に僅かに減少させるか、あ
るいは、一方の渦巻羽根の巻終り部先端が相対する他方
の渦巻部品の端板の肉厚を、段階的に僅かに減少させて
いる。
In order to achieve the above object, according to the present invention, a fixed swirl vane or a swirl swirl vane is provided.
Decrease the blade height at the end of the winding step by step
Or, the tip of the end of one spiral blade is opposite to the other.
The thickness of the end plate of the spiral part
I have.

【0007】[0007]

【0008】[0008]

【作用】上記手段による作用は、いかに記すとおりであ
る。固定渦巻羽根あるいは旋回渦巻羽根の巻終り部の羽
根高さのみ段階的に僅かに減少させるか、あるいは、一
方の渦巻羽根の巻終り部先端が相対する他方の渦巻部品
の端板の肉厚を、段階的に僅かに減少させており、従来
に比較して実質的な羽根の軸方向先端隙間については増
加させていないので、通常運転時の性能は変化すること
がないままで、特殊な圧力温度条件での運転中に渦巻部
品に温度歪や圧力歪が生じても、渦巻羽根の巻終り先端
部は相対する渦巻羽根の鏡板に接触摺動することはなく
なって、軸方向接触による羽根の破損が発生しなくな
る。
The operation of the above means is as follows. Wings at the end of fixed or swirling swirl vanes
Only the root height may be reduced slightly in steps, or
The other spiral part where the end of the winding end of one spiral blade is opposite
The thickness of the end plate has been reduced slightly step by step.
The actual clearance at the tip of the blade in the axial direction is
Performance during normal operation may vary
During operation under special pressure and temperature conditions
Even if temperature distortion or pressure distortion occurs in the product, the end of the spiral blade end
The part does not slide on the end plate of the spiral blade
To prevent blade damage due to axial contact.
You.

【0009】[0009]

【0010】[0010]

【実施例】以下、本発明の実施例を図面に基づいて説明
する。図1〜図6は本発明の一実施例を示すものであ
る。これらの図に示すスクロール圧縮機は、旋回渦巻部
品1と固定渦巻部品5とを備えている。旋回渦巻部品1
は、円盤状の端板2の片側に渦巻状(本実施例ではイン
ボリュート曲線形状)の旋回渦巻羽根3を備え、端板2
の他方側には被駆動軸4を備えている。固定渦巻部品5
は、端板6上に、前記旋回渦巻羽根4と渦巻方向が逆方
向の固定渦巻羽根7を備え、さらに、端板6の中心部に
は吐出穴8を、端板6の外周部付近には吸入口9を備え
ている。スクロール圧縮部は、これら2つの旋回渦巻羽
根3と固定渦巻羽根7を位相を180度ずらして噛み合
わせて構成し、複数の圧縮室10を備えている。また、
スクロール圧縮機においては、圧縮室10の洩れ経路と
して半径方向隙間と軸方向隙間が存在するが、圧縮中の
冷媒ガスの洩れを最小限にするために、これら両隙間を
極小に設定している。
Embodiments of the present invention will be described below with reference to the drawings. 1 to 6 show one embodiment of the present invention. The scroll compressor shown in these figures includes a revolving spiral part 1 and a fixed spiral part 5. Swirling spiral parts 1
Is provided with a spiral (in this embodiment, an involute curve) swirling spiral blade 3 on one side of a disk-shaped end plate 2.
Is provided with a driven shaft 4 on the other side. Fixed spiral parts 5
Is provided with a fixed spiral blade 7 on the end plate 6, the spiral direction of which is opposite to that of the swirling spiral blade 4. Further, a discharge hole 8 is provided at the center of the end plate 6, and near the outer peripheral portion of the end plate 6. Has an inlet 9. The scroll compression unit is configured by meshing the two orbiting spiral blades 3 and the fixed spiral blade 7 with a phase shift of 180 degrees, and includes a plurality of compression chambers 10. Also,
In the scroll compressor, there are a radial gap and an axial gap as a leakage path of the compression chamber 10, but in order to minimize leakage of the refrigerant gas during compression, these two gaps are set to be extremely small. .

【0011】ところで、本発明の実施例では、図2に示
すように旋回渦巻羽根3の巻終り部301の内壁面を厚
さδrだけ落して、巻終り部301の羽根厚さ(te)
を他の部分(t)より薄くしている。即ちte=t−δ
rの関係に設定している。スクロール圧縮機を高い回転
数で運転すると、旋回渦巻部品1には回転数の2乗に比
例して増加した遠心力が働き、この遠心力によって旋回
渦巻部品1の旋回半径は、軸受隙間(例えば、被駆動軸
4の軸受部隙間)内でわずかに拡大する。この旋回半径
の拡大効果によって、旋回渦巻羽根1と固定渦巻羽根7
の半径方向隙間がなくなってしまい、2つの羽根の壁面
と壁面がいずれかの場所で接触する場合が生じる。しか
しながら、本実施例においては、旋回渦巻羽根1の巻終
り部301の内壁面のみδr落しているので、この巻終
り部301が相手の固定渦巻羽根7の壁面に接触するこ
とは決して起きない。一般に渦巻羽根の巻終り部は余切
れているため、強度的に弱いが、この手段により、巻終
り部羽根壁面の接触を回避することができ、羽根の破損
を防止することができることとなる。
[0011] In the embodiment of the present invention, dropped by a thickness [delta] r the inner wall surface of the winding end portion 301 of the orbiting wrap element 3 as shown in FIG. 2, the blades of winding end portion 301 thickness (te)
Is thinner than the other part (t). That is, te = t−δ
The relationship is set to r . When the scroll compressor is operated at a high rotational speed, a centrifugal force that increases in proportion to the square of the rotational speed acts on the orbiting spiral component 1, and the centrifugal force causes the orbiting radius of the orbiting spiral component 1 to be reduced by a bearing clearance (for example, a bearing gap). , And slightly increases in the bearing gap of the driven shaft 4). Due to the effect of increasing the turning radius, the turning swirl blade 1 and the fixed swirl blade 7
The gap in the radial direction disappears, and the wall surfaces of the two blades may come into contact with each other at any place. However, in the present embodiment, since the dropped internal wall surface only [delta] r of the orbiting wrap element 1 of the winding end portion 301, it will never happen that the winding end portion 301 contacts the wall surface of the fixed wrap element 7 of the mating . In general, the end portion of the spiral blade is partially cut off, so that the spiral blade is weak in strength. However, by this means, it is possible to avoid contact with the blade wall surface at the end portion of the spiral blade, thereby preventing breakage of the blade.

【0012】図2においては、巻終り部301の内壁落
し形状を最外端に向って除々に大きくしている。実験に
よれば、羽根の高さをH,羽根厚さをtとすると、内壁
落し部の長さA,最外端の落し量δrは次の値が適切で
ある。
In FIG. 2, the shape of the inner wall of the winding end portion 301 is gradually increased toward the outermost end. According to an experiment, when the height of the blade H, the blade thickness and t, the length A of the inner wall down portion, drop amount [delta] r of the outermost end next value is appropriate.

【0013】A =(2〜3)×H δr=(3/1000〜10/1000)×t また、図3には、巻終り部301の最外端部のみ内壁を
大きく落す実施例を示している。図3の形状は巻終り部
301の強度は余り低下させることなく、羽根の破損防
止に関しては、図2に示した形状と同等の効果を有する
ものである。
A = (2-3) × H δ r = (3/1000 to 10/1000) × t FIG. 3 shows an embodiment in which only the outermost end of the winding end portion 301 has the inner wall largely dropped. Is shown. The shape shown in FIG. 3 does not significantly reduce the strength of the winding end portion 301, and has the same effect as the shape shown in FIG.

【0014】ここで、B=(0.5〜1)×Hが適切な
値である。また、羽根巻終り部壁面の接触を回避する手
段は、上記の方法に限定されるものではなく、図4に示
す様に、一方の羽根(旋回渦巻羽根3)の内壁面と接近
する他方の羽根(固定渦巻羽根7)の外壁面をδrだけ
落しても、全く同じ効果が得られる。図4では、固定渦
巻羽根7の旋回渦巻羽根巻終り相当部701を長さAに
わたってδrだけ厚さを減じている。
Here, B = (0.5-1) × H is an appropriate value. The means for avoiding the contact with the end wall surface of the blade end is not limited to the above-described method, and as shown in FIG. 4, the other approaching the inner wall surface of one blade (rotating spiral blade 3). It is dropped outer wall surface of the blade (fixed wrap element 7) by [delta] r, obtained exactly the same effect. In Figure 4, it is subtracted [delta] r by the thickness over the length A swirl swirl vane winding end equivalent 701 of the fixed wrap element 7.

【0015】一方、図5には、旋回渦巻羽根3の巻終り
部301の軸方向先端面の段落し形状を示している。一
般に、スクロール圧縮機では羽根の先端隙間が性能に及
ぼす影響は半径方向隙間に比較して1桁高く、従って、
羽根先端隙間は、組立時極小(一部接触)に設定されて
いる。しかしながら、両渦巻部品に働く圧力と温度は様
々に変化し、それらによる圧力歪,温度歪によって先端
面が接触摺動する場合も生じている。前述のように、羽
根の巻終り部の強度は弱いので、羽根の軸方向先端面が
強い接触を繰り返すと、巻終り部301から羽根の破損
が生じてしまう。図5に示した、巻終り部301の軸方
向先端面の段落し形状は、この破損を防止するもので、
様々な運転条件下での圧力歪や温度歪から渦巻羽根を保
護するものである。実験によれば、羽根の高さをHとす
ると、段落し部長さA,B,段落し量δaは次の値が適
切である。
On the other hand, FIG. 5 shows a stepped shape of the axial end surface of the winding end portion 301 of the swirling spiral blade 3. Generally, in a scroll compressor, the effect of the blade tip clearance on performance is one order of magnitude higher than the radial clearance, and therefore,
The blade tip clearance is set to a minimum (partial contact) during assembly. However, the pressure and temperature acting on the two spiral components vary, and the tip surface may slide in contact due to the resulting pressure and temperature distortions. As described above, since the strength of the winding end portion of the blade is weak, if the axial end surface of the blade repeats strong contact, the blade is damaged from the winding end portion 301. The stepped shape of the axial end surface of the winding end portion 301 shown in FIG. 5 prevents this breakage,
It protects the swirl vanes from pressure distortion and temperature distortion under various operating conditions. According to an experiment, when the height of the blade and H, paragraphs and director of A, B, paragraph and the amount [delta] a has the following values are appropriate.

【0016】 A =(2〜3)×H,B=(0.5〜1)×H δa=(1/1000〜3/1000)×H この様に、巻終り部301のみ羽根の高さを低くして
も、この部分からの冷媒の洩れは少く、性能にはほとん
ど影響を与えない。
A = (2 to 3) × H, B = (0.5 to 1) × H δ a = (1/1000 to 3/1000) × H In this manner, only the end of the winding end 301 has the height of the blade. Even if the height is reduced, the leakage of the refrigerant from this portion is small, and the performance is hardly affected.

【0017】また、一方の羽根(旋回渦巻羽根)の巻終
り部の軸方向接触の回避手段は、上記方法に限定される
ものではなく、他方の羽根(固定渦巻部品)の端板の厚
みを減じる手段でも、全く同様の効果を得ることができ
る。図6はこれを示したもので、旋回渦巻羽根3の巻終
り部301の先端面と相対する部分(旋回渦巻羽根、巻
終り部先端面と相対する面702)をδaだけ端板6の
厚さを減じている。
The means for avoiding axial contact of the end of one of the blades (the swirling spiral blades) is not limited to the above-described method, and the thickness of the end plate of the other blade (the fixed spiral part) may be reduced. Exactly the same effect can be obtained even with the reducing means. FIG. 6 shows this distal end surface that faces the portion of the winding end portion 301 of the orbiting wrap element 3 (swirl spiral vanes, the winding end portion distal end face opposite face 702) [delta] a only of the end plate 6 The thickness has been reduced.

【0018】[0018]

【発明の効果】本発明によれば、固定渦巻羽根あるいは
旋回渦巻羽根の巻終り部の羽根高さのみ段階的に僅かに
減少させるか、あるいは、一方の渦巻羽根の巻終り部先
端が相対する他方の渦巻部品の端板の肉厚を、段階的に
僅かに減少させており、従来に比較して実質的な羽根の
軸方向先端隙間については増加させていないので、通常
運転時の性能は変化することがないままで、特殊な圧力
温度条件での運転中に渦巻部品に温度歪や圧力歪が生じ
ても、渦巻羽根の巻終り先端部は相対する渦巻羽根の鏡
板に接触摺動することはなくなって、軸方向接触による
羽根の破損が発生しなくなるという効果が得られる。
According to the present invention, a fixed spiral blade or
Only the blade height at the end of the winding of the swirling spiral blade is slightly reduced in steps.
Decrease or decrease the end of one spiral blade
The thickness of the end plate of the other spiral part whose end is opposite
It is slightly reduced, and the actual blade
Since the axial tip clearance is not increased,
During operation, the performance remains unchanged and special pressure
Temperature and pressure distortions occur in spiral components during operation under temperature conditions
However, the end of the end of the spiral blade is the mirror of the opposing spiral blade
No longer slides in contact with the plate.
The effect that breakage of the blade does not occur is obtained.

【0019】[0019]

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

【図1】本発明の一実施例におけるスクロール圧縮機の
要部断面図
FIG. 1 is a sectional view of a main part of a scroll compressor according to an embodiment of the present invention.

【図2】同要部斜視図FIG. 2 is a perspective view of the main part.

【図3】同要部斜視図FIG. 3 is a perspective view of the main part.

【図4】同要部平面図FIG. 4 is a plan view of the main part.

【図5】同要部斜視図FIG. 5 is a perspective view of the main part.

【図6】(a)は同要部平面図 (b)は同要部断面図FIG. 6A is a plan view of the main part, and FIG. 6B is a sectional view of the main part.

【図7】(a)は従来のスクロール圧縮機の旋回渦巻部
品の平面図 (b)は同断面図
FIG. 7A is a plan view of a swirling spiral part of a conventional scroll compressor, and FIG.

【符号の説明】[Explanation of symbols]

1 旋回渦巻部品 3 旋回渦巻羽根 5 固定渦巻部品 7 固定渦巻羽根 301 巻終り部 701 旋回渦巻羽根巻終り部相当部 702 旋回渦巻羽根巻終り部先端面と相対する面 REFERENCE SIGNS LIST 1 swirl spiral part 3 swirl spiral blade 5 fixed swirl part 7 fixed spiral swirler 301 end-of-turn part 701 part corresponding to end part of swirl-spiral blade end 702 surface facing end face of end of swirl-spiral blade end

───────────────────────────────────────────────────── フロントページの続き (72)発明者 河原 定夫 大阪府門真市大字門真1006番地 松下電 器産業株式会社内 (72)発明者 阪井 学 大阪府門真市大字門真1006番地 松下電 器産業株式会社内 (72)発明者 饗場 靖 大阪府門真市大字門真1006番地 松下電 器産業株式会社内 (72)発明者 山本 修一 大阪府門真市大字門真1006番地 松下電 器産業株式会社内 (72)発明者 坪川 正浩 大阪府門真市大字門真1006番地 松下電 器産業株式会社内 (72)発明者 小嶋 能宣 大阪府門真市大字門真1006番地 松下電 器産業株式会社内 (56)参考文献 特開 平3−264789(JP,A) 特開 平2−264178(JP,A) (58)調査した分野(Int.Cl.6,DB名) F04C 18/02 311 ──────────────────────────────────────────────────の Continuing on the front page (72) Inventor Sadao Kawahara 1006 Kadoma Kadoma, Osaka Pref. Matsushita Electric Industrial Co., Ltd. (72) Inventor Manabu Sakai 1006 Odakadoma Kadoma, Osaka Pref. Matsushita Electric Industrial Co., Ltd. (72) Inventor Yasushi Aiba 1006 Kadoma, Kadoma, Osaka Prefecture Inside Matsushita Electric Industrial Co., Ltd. (72) Inventor Shuichi Yamamoto 1006 Odaka, Kazuma, Kadoma, Osaka Prefecture Inside Matsushita Electric Industrial Co., Ltd. (72) Inventor Masahiro Tsubokawa 1006 Kadoma, Kazuma, Osaka Prefecture Matsushita Electric Industrial Co., Ltd. (72) Inventor Nobuyoshi Kojima 1006, Kadoma Kadoma, Kadoma City, Osaka Prefecture Matsushita Electric Industrial Co., Ltd. (56) References JP-A Hei 3- 264789 (JP, A) JP-A-2-264178 (JP, A) (58) Fields investigated (Int. Cl. 6 , DB name) F04C 18/02 311

Claims (2)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】端板に固定渦巻羽根を有する固定渦巻部品
と、端板に旋回渦巻羽根を有する旋回渦巻部品とを噛み
合わせて複数の圧縮空間を形成し、前記旋回渦巻部品の
自転拘束部品を備えて自転を防止し、旋回運動のみをさ
せることによって、前記圧縮空間を渦巻の中心に向かっ
て容積を減少させながら移動させるスクロール型圧縮機
であって、前記固定渦巻羽根と前記旋回渦巻羽根が軸方
向で接触しないように、前記固定渦巻羽根あるいは前記
旋回渦巻羽根の巻終り部の羽根高さを段階的に僅かに減
少させるか、あるいは、一方の渦巻羽根の巻終り部先端
が相対する他方の渦巻部品の端板の肉厚を、段階的に僅
かに減少させてなるスクロール圧縮機。
1. A plurality of compression spaces are formed by engaging a fixed spiral component having a fixed spiral blade on an end plate with a swirling spiral component having a swirling spiral blade on an end plate to rotate the rotating spiral component. A scroll compressor that moves the compression space toward the center of the spiral while reducing the volume by preventing rotation and performing only swirling motion, wherein the fixed spiral blade and the spiral spiral blade are arranged. Is the axis
In order not to contact in the same direction, the blade height at the end of the winding of the fixed spiral blade or the swirling spiral blade is slightly reduced in a stepwise manner, or the end of the winding end of one spiral blade is opposed to the other. A scroll compressor in which the thickness of the end plate of the spiral part is slightly reduced stepwise.
【請求項2】羽根の高さをH、段落し部長さをA,B、
段落し量をδaとした A=(2〜3)×H B=(0.5〜1)×H δa=(1/1000〜3/1000)×H とすることを特徴とした請求項1記載のスクロール圧縮
機。
2. The height of the blade is H, the length of the section is A, B,
When the .delta.a paragraph and amount, claims and characterized in that the A = (2~3) × H B = (0.5~1) × H δa = (1 / 1000~3 / 1000) × H Item 1 scroll compression
Machine.
JP3330193A 1991-12-13 1991-12-13 Scroll compressor Expired - Lifetime JP2990907B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3330193A JP2990907B2 (en) 1991-12-13 1991-12-13 Scroll compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3330193A JP2990907B2 (en) 1991-12-13 1991-12-13 Scroll compressor

Publications (2)

Publication Number Publication Date
JPH05164067A JPH05164067A (en) 1993-06-29
JP2990907B2 true JP2990907B2 (en) 1999-12-13

Family

ID=18229875

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3330193A Expired - Lifetime JP2990907B2 (en) 1991-12-13 1991-12-13 Scroll compressor

Country Status (1)

Country Link
JP (1) JP2990907B2 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3046486B2 (en) * 1993-12-28 2000-05-29 株式会社日立製作所 Scroll type fluid machine
US5421707A (en) * 1994-03-07 1995-06-06 General Motors Corporation Scroll type machine with improved wrap radially outer tip
JP4043144B2 (en) * 1999-06-08 2008-02-06 三菱重工業株式会社 Scroll compressor
JP5428522B2 (en) * 2009-05-22 2014-02-26 パナソニック株式会社 Scroll compressor
JP5348003B2 (en) * 2010-02-12 2013-11-20 パナソニック株式会社 Scroll compressor
JP5984377B2 (en) * 2011-12-22 2016-09-06 三菱重工業株式会社 Scroll compressor

Also Published As

Publication number Publication date
JPH05164067A (en) 1993-06-29

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