JPH0742944B2 - Scroll machine blades - Google Patents

Scroll machine blades

Info

Publication number
JPH0742944B2
JPH0742944B2 JP9370988A JP9370988A JPH0742944B2 JP H0742944 B2 JPH0742944 B2 JP H0742944B2 JP 9370988 A JP9370988 A JP 9370988A JP 9370988 A JP9370988 A JP 9370988A JP H0742944 B2 JPH0742944 B2 JP H0742944B2
Authority
JP
Japan
Prior art keywords
blade
swirl
spiral
fixed
vane
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
JP9370988A
Other languages
Japanese (ja)
Other versions
JPH01267380A (en
Inventor
弘之 福原
繁 村松
正信 関
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 JP9370988A priority Critical patent/JPH0742944B2/en
Publication of JPH01267380A publication Critical patent/JPH01267380A/en
Publication of JPH0742944B2 publication Critical patent/JPH0742944B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C18/00Rotary-piston pumps specially adapted for elastic fluids
    • F04C18/02Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents
    • F04C18/0207Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents both members having co-operating elements in spiral form
    • F04C18/0246Details concerning the involute wraps or their base, e.g. geometry
    • F04C18/0269Details concerning the involute wraps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C18/00Rotary-piston pumps specially adapted for elastic fluids
    • F04C18/02Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents
    • F04C18/0207Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents both members having co-operating elements in spiral form
    • F04C18/0246Details concerning the involute wraps or their base, e.g. geometry
    • F04C18/0269Details concerning the involute wraps
    • F04C18/0284Details of the wrap tips

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Rotary Pumps (AREA)

Description

【発明の詳細な説明】 産業上の利用分野 この発明は空調機、冷蔵庫等の冷凍のスクロール圧縮機
およびポンプ等のスクロールポンプとして利用されるス
クロール機械に関するものである。
Description: TECHNICAL FIELD The present invention relates to a scroll machine used as a scroll scroll compressor such as a refrigeration scroll compressor such as an air conditioner and a refrigerator and a pump.

従来の技術 スクロール圧縮機の圧縮機構について第2図、第3図を
用いて説明する。
2. Description of the Related Art A compression mechanism of a scroll compressor will be described with reference to FIGS. 2 and 3.

電動機要素4の回転に伴うクランク軸5の回転運動は、
偏芯軸受11、旋回渦巻羽根軸12を介して旋回渦巻羽根部
品8に伝達されるが、自転拘束部品13の作用により旋回
渦巻羽根部品8は、自転することなく固定渦巻羽根部品
7のインボリュートまたは類似曲線の中心を旋回の中心
として旋回運動する。
The rotational movement of the crankshaft 5 accompanying the rotation of the electric motor element 4 is
It is transmitted to the swirling spiral vane component 8 via the eccentric bearing 11 and the swirling spiral vane shaft 12, but due to the action of the rotation restraint component 13, the swirling spiral vane component 8 does not rotate and the involute of the fixed spiral vane component 7 or A turning motion is performed with the center of the similar curve as the center of turning.

このとき、旋回渦巻羽根部品8の羽根8aの巻き終り端8
a′が固定渦巻羽根部品7の羽根7aと、また固定渦巻羽
根部品7の羽根7aの巻き終り端7a′が旋回渦巻羽根部品
8の羽根8aに各々接触している状態が吸入完了である。
At this time, the winding end end 8 of the blade 8a of the swirling spiral blade component 8 is
The suction is completed when a'is in contact with the blade 7a of the fixed spiral blade part 7 and the winding end 7a 'of the blade 7a of the fixed spiral blade part 7 is in contact with the blade 8a of the swirl spiral blade part 8, respectively.

そして、旋回渦巻羽根部品8の公転運動に伴い、羽根7a
と羽根8a同士の2つの接触点がインボリュートの中心に
近づくに従い、圧縮室9の圧力が上昇し、吐出口26より
吐出される。
Then, along with the revolution movement of the swirling spiral blade component 8, the blade 7a
As the two contact points between the blades 8a and the blades 8a approach the center of the involute, the pressure in the compression chamber 9 rises and is discharged from the discharge port 26.

次に、ラップ上端の形状について説明する。Next, the shape of the upper end of the wrap will be described.

スクロール型圧縮機には、第4図に示すように、固定お
よび旋回渦巻羽根部品7,8の羽根の先端に面取り7c,8cを
設けている。これは圧縮機として用いる場合、理想形状
は第5図に示す様に、鏡板7c,8bおよび羽根7a,8aの各シ
ール面が隙間なく相対運動することが望ましいが、現在
の成形技術では、羽根7a,8aと鏡板7b,8bの接線部を理想
形状にすることは困難である。
As shown in FIG. 4, the scroll compressor is provided with chamfers 7c and 8c at the tips of the blades of the fixed and orbiting spiral vane components 7 and 8. When this is used as a compressor, it is desirable that the sealing surfaces of the end plates 7c, 8b and the blades 7a, 8a move relative to each other without a gap as shown in FIG. It is difficult to make the tangent portions of 7a, 8a and the end plates 7b, 8b into ideal shapes.

従って、羽根7a,8aと鏡板7b,8bの交線部には、第6図に
示すように羽根側面および鏡板部を加工した時に残留す
るわずかな突出27が生じ、これと相対する羽根上端と側
面の陵線部との干渉を避ける為に、羽根先端に面取りを
設ける必要がある。
Therefore, at the intersection of the blades 7a, 8a and the end plates 7b, 8b, as shown in FIG. 6, a slight protrusion 27 remains when the side surfaces of the blades and the end plate portion are processed, and the upper end of the blade opposite to this is formed. In order to avoid interference with the side ridges, it is necessary to provide chamfers at the blade tips.

発明が解決しようとする課題 羽根7a,8aと鏡板7b,8bの接線部のわずかな突出を含む羽
根7a,8aと鏡板7b,8bと羽根7a,8a先端の面取りに囲まれ
た隙間28は小さい程気体又は液体の洩れが少なく、効率
が上がることは容易に理解出来るが、成形上の突出27の
保証を考慮した場合、羽根先端面取りは、極小に形成す
ることは困難であった。
Problems to be Solved by the Invention The gap 28 surrounded by the chamfers of the vanes 7a, 8a and the vanes 7a, 8a and the vanes 7a, 8a and the vanes 7a, 8a including a slight protrusion of the tangent portion of the vanes 7a, 8a and the vanes 7a, 8b is small. Although it is easy to understand that the gas or liquid leaks less and the efficiency is improved, it is difficult to form the blade tip chamfer to the minimum in consideration of the guarantee of the protrusion 27 on molding.

また、羽根7a,8a先端の面取りを極めて小さくすること
が可能であっても、圧縮機組立の取扱いによっては、特
に羽根外周部上端は外部に接する可能性が高いため、打
痕等による変形が発生しやすい。羽根7a,8a先端面取部
に打痕等による変形が発生した場合、羽根7a,8aおよび
鏡板7b,8bによって構成される圧縮室9が、打痕等によ
る変形の為に、第7図の(a)および(b)に示すよう
に変形し、気体又は流体の洩れが多くなる。
Further, even if the chamfering of the tips of the blades 7a, 8a can be made extremely small, there is a high possibility that the upper end of the outer peripheral portion of the blade comes into contact with the outside depending on the handling of the compressor assembly. Likely to happen. When the tip chamfered portions of the blades 7a, 8a are deformed due to dents or the like, the compression chamber 9 constituted by the blades 7a, 8a and the end plates 7b, 8b is deformed due to dents or the like, so It deforms as shown in (a) and (b), and gas or fluid leaks more.

加えて、変形の為に固定渦巻羽根部品7と旋回渦巻羽根
部品8の鏡板7b,8bおよび羽根7a,8aの間において、局部
的な接触が起こり、これに起因する異常音や異常摩耗が
発生し、最悪の場合、圧縮機内又はポンプを破壊する場
合がある。
In addition, due to the deformation, local contact occurs between the end plates 7b, 8b and the blades 7a, 8a of the fixed spiral vane component 7 and the swirling spiral vane component 8, resulting in abnormal noise and abnormal wear. However, in the worst case, the inside of the compressor or the pump may be destroyed.

本発明は、上述した点を解決して、羽根と鏡板の接線部
と、羽根先端面取りに囲まれた隙間28からの洩れを実用
上少なくし、かつ打痕等による羽根先端の変形を実用上
無くし、洩れの減少、異常音、異常摩耗、および破壊と
いった現象より解放することを目的とする。
The present invention solves the above-mentioned problems, practically reduces the leakage from the tangent portion between the blade and the end plate, and the gap 28 surrounded by the chamfering of the blade tip, and practically prevents the deformation of the blade tip due to a dent or the like. The purpose is to eliminate the phenomena such as leakage reduction, abnormal noise, abnormal wear, and destruction.

課題を解決するための手段 この目的を達成するために本発明は、圧縮室又はポンプ
室を構成する前記固定渦巻羽根と旋回渦巻羽根の各先端
部に面取り部を設け、羽根外壁側において、前記固定も
しくは旋回渦巻羽根の少なくとも一方の面取り部の面取
りの大きさを羽根の巻き終わりほど大きく羽根の巻き始
めほど小さく形成するとともに、前記固定もしくは旋回
渦巻羽根の巻回方向に垂直な断面において、面取り部の
面取りの大きさを前記羽根外壁側よりも羽根内壁側を常
に小さく形成したのである。
Means for Solving the Problems In order to achieve this object, the present invention provides a chamfered portion at each tip of the fixed spiral vane and the swirl spiral vane forming a compression chamber or a pump chamber, and at the vane outer wall side, The chamfered size of at least one chamfered portion of the fixed or swirling spiral blade is formed so as to be larger at the end of winding of the blade and smaller at the beginning of winding of the blade, and chamfered in a cross section perpendicular to the winding direction of the fixed or swirling spiral blade. The chamfered portion is formed so that the inner wall side of the blade is always smaller than the outer wall side of the blade.

作 用 スクロール圧縮機の圧縮機構は、前述のごとく、中心に
近づくほど圧縮室9の圧力が上昇する。従って、中心に
近づくほど、隣接圧縮空間との圧力差が大きくなる。
As described above, in the compression mechanism of the working scroll compressor, the pressure in the compression chamber 9 increases as it approaches the center. Therefore, the closer to the center, the larger the pressure difference with the adjacent compression space.

従って、羽根の巻き始め30bでは、羽根外壁側31aおよび
羽根内壁側31b共、圧縮効率に及ぼす影響が大きい為、
羽根上端の面取りの大きさを極力小さくすることによる
効率向上の効果は大である。一方、羽根上端の打痕等に
よる変形は主に羽根外壁側31aの羽根の巻き終わり30aで
発生しやすいものであり、特に障害とならない。また、
羽根外壁側31aの羽根巻き終わり30aでは、渦巻上端の面
取りの大きさを大きくすることにより、羽根上端の打痕
等による変形を防止することが出来、製造上の取扱いが
容易となる。一方、羽根巻き終わり30aでは、隣接圧縮
室の圧力差は小さく、効率に及ぼす影響は非常に小さ
い。
Therefore, at the blade start 30b, both the blade outer wall side 31a and the blade inner wall side 31b have a great influence on the compression efficiency.
The effect of improving the efficiency is great by reducing the chamfered size of the upper end of the blade as much as possible. On the other hand, deformation due to dents or the like on the upper end of the blade is likely to occur mainly at the end 30a of the blade on the outer wall side 31a of the blade, and is not a particular obstacle. Also,
At the blade end 30a on the blade outer wall side 31a, by increasing the chamfering size of the spiral upper end, it is possible to prevent deformation of the upper end of the blade due to dents or the like, and it is easy to handle in manufacturing. On the other hand, at the blade winding end 30a, the pressure difference between the adjacent compression chambers is small, and the influence on the efficiency is very small.

実 施 例 以下、本発明の一実施例を添付図面にもとづいて説明す
る。
Example Hereinafter, one example of the present invention will be described with reference to the accompanying drawings.

まず第2図により本発明も含む一般的な密閉型スクロー
ル圧縮機の概略構造について説明する。
First, a schematic structure of a general hermetic scroll compressor including the present invention will be described with reference to FIG.

同図において、密閉容器1の内部に固定子2と回転子3
からなる電動機要素4および、この電動機要素4により
クランク軸5を介して駆動される圧縮機要素6が配設さ
れている。固定渦巻羽根部品7と旋回渦巻羽根部品8が
噛み合い、複数個の圧縮室9を形成し、電動機要素4の
駆動がクランク軸5、偏芯軸受11、旋回渦巻羽根軸12と
伝達されて旋回渦巻羽根部品8が旋回する。旋回渦巻羽
根部品8は自転拘束部品13で自転を拘束されている。
In the figure, a stator 2 and a rotor 3 are provided inside a closed container 1.
And a compressor element 6 driven by the electric motor element 4 via a crankshaft 5. The fixed spiral vane component 7 and the swirl spiral vane component 8 mesh with each other to form a plurality of compression chambers 9, and the drive of the electric motor element 4 is transmitted to the crankshaft 5, the eccentric bearing 11, and the swirl spiral vane shaft 12 to form the swirl spiral. The blade component 8 turns. The swirling spiral blade component 8 is restrained from rotating by a rotation restraining component 13.

吸入管24から密閉容器1内に入った冷媒ガスは、吸入口
25より圧縮機要素6に吸入され、圧縮室9で圧縮されて
吐出口26より吐出される。
Refrigerant gas that enters the closed container 1 from the suction pipe 24 is sucked into the suction port.
It is sucked into the compressor element 6 from 25, compressed in the compression chamber 9 and discharged from the discharge port 26.

第1図は、本発明の一例を説明する旋回渦巻羽根部品の
詳細図である。
FIG. 1 is a detailed view of a swirling spiral blade component for explaining an example of the present invention.

旋回渦巻羽根部品8は、鏡板8bと渦巻き状の羽根8aより
構成されている。そして羽根8aの上端には両コーナに面
取り8cが施されている。この面取りの度合いは、羽根外
壁側31aにおいては、羽根の巻き終り外周30aでは面取り
度合が大きく、巻き始め30bでは面取り度合を小さくし
ている。この度合いは、巻き終わりから巻き始めに向け
て一連して徐々に面取り度合いが変化している。
The swirling spiral blade component 8 is composed of an end plate 8b and a spiral blade 8a. Then, chamfers 8c are provided on both corners at the upper ends of the blades 8a. Regarding the degree of chamfering, on the blade outer wall side 31a, the chamfering degree is large at the winding end outer periphery 30a and is small at the winding start 30b. The degree of chamfer gradually changes from the end of winding to the beginning of winding.

羽根内壁側31bにおいては、その面取り度合いは、相対
する部分の羽根外壁側31aの面取り度合いより常に小さ
く形成している。すなわち、旋回渦巻羽根部品8の渦巻
の巻回方向に垂直な断面を見た場合、その面取り度合は
羽根外壁側31aより羽根内壁側31bが常に小さくなってい
ることになる。ただ、羽根内壁側31bの大きさは、巻き
終わりから巻き始めにかけて必ずしも変化する必要はな
く一様であってもよい(渦巻中心部では内外周とも略同
等としてよい)。
The chamfering degree on the blade inner wall side 31b is always smaller than the chamfering degree on the blade outer wall side 31a of the opposing portion. That is, when the cross section of the swirling spiral blade component 8 perpendicular to the spiral winding direction is viewed, the chamfering degree is always smaller on the blade inner wall side 31a than on the blade outer wall side 31a. However, the size of the blade inner wall side 31b does not necessarily have to change from the winding end to the winding start, and may be uniform (the inner and outer circumferences may be substantially equal at the center of the spiral).

上記構成において、圧縮機が駆動されると、圧縮室9の
圧力は、渦巻の中心に近づくに従い、圧力が上昇し、隣
接圧縮室との圧力差は大きくなってゆく。従って、羽根
の巻き始め30bでは、羽根外壁側31aおよび羽根内壁側31
b共、効率に及ぼす影響が大きい為、羽根上端の面取り
の大きさを小さくする必要があるが、羽根上端の打痕等
による変形は、主に羽根外壁側31aの羽根の巻き終わり3
0aであり、特に障害とはならない。また、羽根外壁側31
aの羽根の巻き終わり30aでは、渦巻上端の面取りの大き
さを大きくすることにより、羽根上端の打痕等による変
形を防止することが出来、製造上の取扱いが容易とな
る。しかし羽根の巻き終わり30aでは、隣接圧縮室の圧
力差は小さく、効率に及ぼす影響は非常に小さい。
In the above structure, when the compressor is driven, the pressure in the compression chamber 9 increases as it approaches the center of the spiral, and the pressure difference between the compression chamber 9 and the adjacent compression chamber increases. Therefore, at the blade winding start 30b, the blade outer wall side 31a and the blade inner wall side 31a
Both b have a large effect on efficiency, so it is necessary to reduce the chamfer size at the upper end of the blade, but deformation due to dents etc. at the upper end of the blade is mainly due to the end of winding 3 of the blade on the outer wall side 31a of the blade.
It is 0a, which does not cause any obstacle. Also, the blade outer wall side 31
At the end 30a of the blade of a, by increasing the chamfering size of the upper end of the spiral, it is possible to prevent the upper end of the blade from being deformed due to dents or the like, which facilitates the handling in manufacturing. However, at the winding end 30a of the blade, the pressure difference between the adjacent compression chambers is small and the influence on the efficiency is very small.

なお、羽根外壁側の上端の面取りの大きさを、羽根の巻
き角度を一定のブロックに分け、そのブロック毎に巻き
終わり30aほど大きく、巻き始め30bほど小さくなるよう
に段階的に面取りを行っても同様の効果が得られる。
In addition, the chamfering size of the upper end on the outer wall side of the blade is divided into blocks in which the winding angle of the blade is fixed, and each block is chamfered stepwise so that the winding end is larger by 30a and the winding start is smaller by 30b. Also has the same effect.

いずれの実施例についても、カムやギアあるいはNCを使
用した加工設備で成形することが出来るが特にNCを使用
した加工設備の場合、羽根上端の面取りの成形の調整は
容易である。
In any of the examples, the molding can be performed with the processing equipment using the cam, the gear, or the NC, but particularly in the case of the processing equipment using the NC, it is easy to adjust the shaping of the chamfering of the upper end of the blade.

また、本実施例においては旋回渦巻羽根部品8について
説明したが、固定渦巻羽根部品7についても同様に実施
できることはいうまでもない。
Further, although the swirling spiral blade component 8 has been described in the present embodiment, it goes without saying that the fixed spiral blade component 7 can be similarly implemented.

さらに、本実施例については、スクロール圧縮機として
説明したが、ポンプ、膨脹機等の機械としても同様に実
施できることはいうまでもない。
Furthermore, although the present embodiment has been described as a scroll compressor, it goes without saying that it can be similarly implemented as a machine such as a pump or an expander.

発明の効果 以上の様に本発明によれば、スクロール機械において、
圧縮室又はポンプ室を構成する前記固定渦巻羽根と旋回
渦巻羽根の各先端部に面取り部を設け、羽根外壁側にお
いて、前記固定もしくは旋回渦巻羽根の少なくとも一方
の面取り部の面取りの大きさを羽根の巻き終わりほど大
きく羽根の巻き始めほど小さく形成するとともに、前記
固定もしくは旋回渦巻羽根の巻回方向に垂直な断面にお
いて、面取り部の面取りの大きさを前記羽根外壁側より
も羽根内壁側を常に小さく形成したにより、洩れの少な
い高効率の圧縮機又はポンプを実現することが出来た。
併せて、渦巻上面の打痕等による変形を防止出来る為、
大幅な生産性の向上が図れ、低コストにすることが出
来、かつ、異常音、異常摩耗、機構破壊といった問題点
に対し、信頼性の向上を実現するこが出来る。
As described above, according to the present invention, in the scroll machine,
A chamfered portion is provided at each tip of the fixed spiral vane and the swirl spiral vane forming the compression chamber or the pump chamber, and the chamfered size of at least one chamfered portion of the fixed or swirl spiral vane is set on the outer wall side of the vane. In the section perpendicular to the winding direction of the fixed or swirling spiral blade, the chamfered portion of the chamfered portion is always larger on the blade inner wall side than on the blade outer wall side. By making it small, it was possible to realize a highly efficient compressor or pump with little leakage.
At the same time, it is possible to prevent deformation due to dents on the top surface of the spiral,
The productivity can be greatly improved, the cost can be reduced, and the reliability can be improved with respect to problems such as abnormal noise, abnormal wear, and mechanical destruction.

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

第1図は本発明の一実施例におけるスクロール圧縮機の
旋回渦巻羽根の斜視図、第2図は密閉型スクロール圧縮
機の縦断面図、第3図は同圧縮機の固定および旋回渦巻
羽根の組立図、第4図は従来例を示す渦巻羽根部の縦断
面図、第5図は理想形状の渦巻羽根部を示す縦断面図、
第6図は一般的な渦巻羽根部の縦断面図、第7図(a)
・(b)は従来の羽根において変形を起した異なる例の
縦断面図である。 1……密閉容器、2……固定子、3……回転子、4……
電動機要素、5……クランク軸、6……圧縮機要素、7
……固定渦巻羽根部品、7a……羽根、7b……鏡板、8…
…旋回渦巻羽根部品、8a……羽根、8b……鏡板、8c……
面取り、9……圧縮機、11……偏芯軸受、12……旋回渦
巻羽根軸、13……自転拘束部品、30a……羽根外周、30b
……羽根内周。
FIG. 1 is a perspective view of a swirling spiral blade of a scroll compressor according to an embodiment of the present invention, FIG. 2 is a vertical sectional view of a hermetic scroll compressor, and FIG. 3 is a fixed and swirling spiral blade of the compressor. FIG. 4 is an assembly view, FIG. 4 is a vertical cross-sectional view of a spiral vane portion showing a conventional example, and FIG. 5 is a vertical cross-sectional view showing a spiral vane portion of an ideal shape.
FIG. 6 is a vertical cross-sectional view of a general spiral blade portion, FIG. 7 (a)
(B) is a vertical cross-sectional view of another example in which the conventional blade is deformed. 1 ... airtight container, 2 ... stator, 3 ... rotor, 4 ...
Electric motor element, 5 ... Crankshaft, 6 ... Compressor element, 7
...... Fixed spiral blade parts, 7a ...... Wings, 7b ...... End plate, 8 ...
… Swirl spiral blade component, 8a …… Blade, 8b …… End plate, 8c ……
Chamfer, 9 ... Compressor, 11 ... Eccentric bearing, 12 ... Swirl spiral blade shaft, 13 ... Rotation restraint parts, 30a ... Blade outer circumference, 30b
...... The inner circumference of the blade.

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】第1の鏡板、およびその第1の鏡板の一面
上に凸設された第1の渦巻部を有し、ハウジングに固定
配置された固定渦巻羽根と、この固定渦巻羽根と向き合
って配置された第2の鏡板、およびその第2の鏡板上に
凸設されて前記第1の渦巻部と角度をずらせて噛み合
い、その第1の渦巻部との間に空間を形成する第2の渦
巻部を有する旋回渦巻羽根と、その旋回渦巻羽根に自転
を防止しながら固定渦巻羽根の中心周りに旋回運動を行
なわせる駆動機構とを具備し、前記旋回渦巻羽根の旋回
運動により、流体を圧縮又は吸引するスクロール機械に
おいて、圧縮室又はポンプ室を構成する前記固定渦巻羽
根と旋回渦巻羽根の各先端部に面取り部を設け、羽根外
壁側において、前記固定もしくは旋回渦巻羽根の少なく
とも一方の面取り部の面取りの大きさを羽根の巻き終わ
りほど大きく羽根の巻き始めほど小さく形成するととも
に、前記固定もしくは旋回渦巻羽根の巻回方向に垂直な
断面において、面取り部の面取りの大きさを前記羽根外
壁側よりも羽根内壁側を常に小さく形成したスクロール
機械の羽根。
1. A fixed scroll vane fixed to a housing, which has a first end plate and a first swirl portion projecting from one surface of the first end plate, and faces the fixed end swirl blade. And a second end plate which is provided on the second end plate so as to project from the second end plate and meshes with the first spiral part at a different angle to form a space between the second spiral plate and the first spiral part. A swirl spiral blade having a swirl part of the swirl and a drive mechanism for causing the swirl swirl blade to swivel around the center of the fixed swirl blade while preventing rotation of the swirl swirl blade. In a scroll machine that compresses or sucks, a chamfer is provided at each tip of the fixed spiral vane and the swirl spiral vane that form a compression chamber or a pump chamber, and at least one chamfer of the fixed or swirl spiral vane is provided on the outer wall side of the vane. Department The chamfer is formed to have a size larger toward the end of the blade and smaller toward the start of the blade, and the chamfer of the chamfered portion in the cross section perpendicular to the winding direction of the fixed or swirl spiral vane is larger than the vane outer wall side. Is a blade for scroll machines whose inner wall is always small.
JP9370988A 1988-04-15 1988-04-15 Scroll machine blades Expired - Lifetime JPH0742944B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP9370988A JPH0742944B2 (en) 1988-04-15 1988-04-15 Scroll machine blades

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP9370988A JPH0742944B2 (en) 1988-04-15 1988-04-15 Scroll machine blades

Publications (2)

Publication Number Publication Date
JPH01267380A JPH01267380A (en) 1989-10-25
JPH0742944B2 true JPH0742944B2 (en) 1995-05-15

Family

ID=14089944

Family Applications (1)

Application Number Title Priority Date Filing Date
JP9370988A Expired - Lifetime JPH0742944B2 (en) 1988-04-15 1988-04-15 Scroll machine blades

Country Status (1)

Country Link
JP (1) JPH0742944B2 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3046523B2 (en) * 1995-05-23 2000-05-29 株式会社豊田自動織機製作所 Scroll compressor
CN108087964A (en) * 2016-11-22 2018-05-29 苏州三星电子有限公司 A kind of regulating device and air-cooled ducted air conditioner of controllable air-cooled ducted air conditioner outlet air trend

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6176185U (en) * 1984-10-26 1986-05-22

Also Published As

Publication number Publication date
JPH01267380A (en) 1989-10-25

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