JPH0427787A - Scroll blade and manufacture thereof - Google Patents

Scroll blade and manufacture thereof

Info

Publication number
JPH0427787A
JPH0427787A JP13258290A JP13258290A JPH0427787A JP H0427787 A JPH0427787 A JP H0427787A JP 13258290 A JP13258290 A JP 13258290A JP 13258290 A JP13258290 A JP 13258290A JP H0427787 A JPH0427787 A JP H0427787A
Authority
JP
Japan
Prior art keywords
reinforcing member
scroll
end plate
wing
blade
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.)
Pending
Application number
JP13258290A
Other languages
Japanese (ja)
Inventor
Tsutomu Ichikawa
勤 市川
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.)
Toshiba Corp
Original Assignee
Toshiba 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 Toshiba Corp filed Critical Toshiba Corp
Priority to JP13258290A priority Critical patent/JPH0427787A/en
Publication of JPH0427787A publication Critical patent/JPH0427787A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To increase rigidity and make a scroll blade lightweight by covering a reinforcing member provided over and end plate section and a balde section with and base material so that the thickness of the reinforcing member of the blade section is made thicker at the root section than at the tip section. CONSTITUTION:A reinforcing member 42a made of a metal material is provided over the end plate section 40 and blade section 41 of a rotary scroll blade 4. The reinforcing member 42a is covered with a base material 43 made of a synthetic resin material. The thickness t1 at the root section of the reinforcing member 42a of the blade section 41 is made thicker than the thickness t2 at the tip section. The force of compression gas is applied to the blade section 41 in the height direction during the compression action, and its stress is larger at the root section than at the tip section. The thickness t1 at the root section of the reinforcing member 42 of the blade section 41 is made thicker than the thickness t2 at the tip section, the root section has large rigidity, and the reinforcing member 42a made of a synthetic resin material can be made lightweight.

Description

【発明の詳細な説明】 [発明の目的コ (産業上の利用分野) 本発明は、たとえば空気調和機の冷凍サイクルを構成す
るスクロール型圧縮機に係り、特にその圧縮機構部を構
成するスクロール翼と、スクロール翼の製造方法の改良
に関する。
DETAILED DESCRIPTION OF THE INVENTION [Purpose of the Invention (Industrial Application Field) The present invention relates to a scroll compressor that constitutes a refrigeration cycle of an air conditioner, for example, and particularly relates to a scroll type compressor that constitutes a compression mechanism thereof. and an improvement in a method for manufacturing scroll blades.

(従来の技術) たとえば空気調和機の冷凍サイクルを構成する圧縮機と
して用いられる、通常のロータリ式圧縮機と比較して、
運動騒音が極めて低く、かつ圧縮効率のよいスクロール
式の密閉形圧縮機が多用される傾向にある。
(Prior art) For example, compared to a normal rotary compressor used as a compressor that constitutes the refrigeration cycle of an air conditioner,
Scroll-type hermetic compressors, which have extremely low motion noise and high compression efficiency, are increasingly being used.

このスクロール型圧縮機は、たとえ第9図に示すように
構成される。すなわち、1は密閉ケースであり、この密
閉ケース1内に支持フレーム2が、密閉ケース1内を上
下部に仕切るように設けられる。上記支持フレーム2の
上部には、固定スクロール翼3と旋回スクロール翼4と
を噛合して圧縮室Sを形成するとともに固定スクロール
翼3側の吐出側空間部を囲繞し、内部に吐出室5を形成
するバルブカバー5とからなるスクロール圧縮機構部7
が設けられる。上記支持フレーム2の下部には、ステー
タ8とロータ9とからなる電動機部10が設けられる。
This scroll compressor is constructed as shown in FIG. That is, 1 is a closed case, and a support frame 2 is provided in this closed case 1 so as to partition the inside of the closed case 1 into upper and lower parts. In the upper part of the support frame 2, a fixed scroll blade 3 and an orbiting scroll blade 4 are meshed to form a compression chamber S, and a discharge side space on the side of the fixed scroll blade 3 is surrounded, and a discharge chamber 5 is formed inside. A scroll compression mechanism section 7 consisting of a valve cover 5 formed
will be provided. An electric motor section 10 consisting of a stator 8 and a rotor 9 is provided at the lower part of the support frame 2 .

これらスクロール圧縮機構部7と電動機部10とは、主
軸11を介して連設される。
These scroll compression mechanism section 7 and electric motor section 10 are connected via a main shaft 11.

このようにして、構成される密閉形圧縮機において、電
動機部10に通電してスクロール式圧縮機構部7を駆動
し、吸込管12から被圧縮流体である、たとえば低圧の
冷媒ガスを導入して密閉ケース1内に充満させる。この
冷媒ガスは上記スクロール圧縮機構部7に吸込まれ、旋
回スクロール翼4の旋回運動にともなって圧縮される。
In the hermetic compressor constructed in this manner, the electric motor section 10 is energized to drive the scroll compression mechanism section 7, and a fluid to be compressed, such as low-pressure refrigerant gas, is introduced from the suction pipe 12. Fill the airtight case 1. This refrigerant gas is sucked into the scroll compression mechanism 7 and compressed as the orbiting scroll blades 4 rotate.

所定圧まで上昇したところで吐出室5に吐出され、さら
に吐出管13を介して外部機器に導かれる。上記電動機
部10は負荷に応じた最適な運転周波数に制御され、最
適な条件での空気調和が可能である。
Once the pressure has risen to a predetermined level, it is discharged into the discharge chamber 5 and further guided to external equipment via the discharge pipe 13. The electric motor section 10 is controlled to an optimal operating frequency according to the load, and air conditioning can be performed under optimal conditions.

(発明が解決しようとする課題) ところで、上記固定スクロール翼3および旋回スクロー
ル翼4ともに、従来、金属材料で形成されていた。その
ため、それぞれ重量が重くなるとともに、特に上記旋回
スクロール翼4は軽快な旋回運動が望まれるのに対して
、振動が発生、し易い不具合があった。このような振動
を少しでも減衰させるため、たとえばバランスウェイト
14を大型化しているが、そのため圧縮機全体の小型化
の障害となっているとともに、高速運転時の大きな遠心
力による軸受負荷の増大を招(などの不具合が発生する
(Problems to be Solved by the Invention) By the way, both the fixed scroll blade 3 and the orbiting scroll blade 4 have conventionally been formed of a metal material. As a result, each of these blades is heavy in weight, and while the orbiting scroll blade 4 in particular is desired to have a light orbiting motion, there is a problem in that vibrations are likely to occur. In order to attenuate such vibrations, for example, the balance weight 14 is made larger, but this is an obstacle to downsizing the entire compressor, and it also prevents an increase in bearing load due to large centrifugal force during high-speed operation. Problems such as ``Invitation'' occur.

スクロール翼に係わる先願として、実開昭608493
号公報、特開昭59−79088号公報、特開昭61−
294180号公報、特開昭62−284980号公報
などの考案あるいは発明がある。これらは全て、スクロ
ール翼の表面を、スクロール翼の母材とは異なる材料で
被覆してなり、耐摩耗性向上を目的としている。
As a prior application related to scroll blades, Utility Model Application No. 608493
Publication No. 1988-79088, Japanese Patent Publication No. 1988-7908-
There are ideas and inventions such as Japanese Patent Application Laid-open No. 294180 and Japanese Patent Application Laid-Open No. 62-284980. In all of these, the surface of the scroll blade is coated with a material different from the base material of the scroll blade, and the purpose is to improve wear resistance.

しかしながら、これらのものは、いずれもスクロール翼
の大部分を占める母材か金属材料であるため、軽量化の
効果か小さい。
However, since all of these materials are base materials or metal materials that occupy the majority of the scroll blades, the weight reduction effect is small.

また、特開昭61−38187号公報に開示されるよう
に、スクロール翼を、合成樹脂を主体とする材料により
成形し、それぞれのスクロール翼の摺接部に耐摩耗性の
材料を一体的に備えたものも知られている。
Furthermore, as disclosed in Japanese Patent Application Laid-Open No. 61-38187, the scroll blades are molded from a material mainly composed of synthetic resin, and a wear-resistant material is integrally applied to the sliding contact portion of each scroll blade. It is also known that it is equipped with

このようなスクロール翼であれば、軽量化が可能である
。しかしながら、合成樹脂材料は金属材料と比較して強
度か弱いため、圧縮荷重による変形や、疲労破壊などの
問題かある。そしてさらに、合成樹脂材料は金属材料に
比べて熱膨張係数が高く、冷媒ガスに対する圧縮作用に
ともなってガスが高温化すると、熱膨張して変形する恐
れがある。
With such a scroll blade, it is possible to reduce the weight. However, since synthetic resin materials have lower strength than metal materials, they may suffer from problems such as deformation due to compressive loads and fatigue failure. Furthermore, synthetic resin materials have a higher coefficient of thermal expansion than metal materials, and when the gas becomes hot due to the compressive action on the refrigerant gas, there is a risk of thermal expansion and deformation.

さらにまた、上記スクロール翼を製造するには、多量生
産を考慮して射8成形による方法が採用されるであろう
が、この種方法によると合成樹脂材を一旦高温化してか
ら射出し、その後、強制冷却あるいは自然冷却をしなけ
ればならない。合成樹脂材料は熱膨張係数が高く、した
がって熱収縮量が大である。そのため射8後の冷却にと
もなう熱収縮で完成寸法が設定寸法よりも小さくなる恐
れがあり、製造方法が極めて難しい。
Furthermore, in order to manufacture the above-mentioned scroll blades, a method using injection molding would be adopted in consideration of mass production, but according to this type of method, the synthetic resin material is first heated to a high temperature, then injected, and then , forced cooling or natural cooling must be used. Synthetic resin materials have a high coefficient of thermal expansion and therefore have a large amount of thermal contraction. Therefore, there is a risk that the completed dimensions will be smaller than the set dimensions due to heat shrinkage due to cooling after irradiation, and the manufacturing method is extremely difficult.

なお、スクロール翼の変形防止、破壊防止を目的として
、たとえば実開昭61−17492号公報や実開平1−
88086号公報が開示されている。すなわち、実開昭
61−17492号公報は、スクロール部材よりも強度
・剛性が高く熱膨張係数が同等の材質からなるビンやね
じ等の補強部材を固着したことを特徴としている。実開
平188086号公報は、単一材料からなるスクロール
部材に、上記単一材料よりも強度の高い補強材を渦巻体
の中心近傍に内設したことを特徴としている。
In addition, for the purpose of preventing deformation and destruction of scroll blades, for example, Japanese Utility Model Application Publication No. 17492/1982 and Japanese Utility Model Application No. 1/1999
No. 88086 is disclosed. That is, Japanese Utility Model Application No. 61-17492 is characterized in that a reinforcing member such as a bottle or a screw made of a material having higher strength and rigidity and the same coefficient of thermal expansion as the scroll member is fixed thereto. Japanese Utility Model Application Publication No. 188086 is characterized in that a scroll member made of a single material is provided with a reinforcing material having higher strength than the single material in the vicinity of the center of the spiral body.

しかしながら、上記補強部材や補強材に対する形状が充
分考慮されておらず、スクロール翼を合成樹脂材料で形
成することは困難であった。
However, sufficient consideration has not been given to the reinforcing member and the shape of the reinforcing material, and it has been difficult to form the scroll blade from a synthetic resin material.

本発明は上記事情に着目してなされたものであり、その
目的とするところは、金属材料からなる補強部材を合成
樹脂材からなる母材で覆うことにより、剛性を増大化し
て耐久性の向上を図るとともに軽量化を得られ、高精度
で製造可能なスクロール翼およびその製造方法を提供し
ようとするものである。
The present invention has been made in view of the above circumstances, and its purpose is to increase rigidity and improve durability by covering a reinforcing member made of a metal material with a base material made of a synthetic resin material. It is an object of the present invention to provide a scroll blade that is lightweight, can be manufactured with high precision, and a manufacturing method thereof.

[発明の構成] (課題を解決するための手段および作用)すなわち、第
1の発明は、スクロール型圧縮機に備えられ、鏡板部と
、この鏡板部の一端部に立設された渦巻状の翼部とから
なるスクロール翼において、上記鏡板部と翼部とに亘っ
て金属材料からなる補強部材を設け、この補強部材を合
成樹脂材料からなる母材で覆ってなり、上記翼部の補強
部材は、その根元部の肉厚を先端部の肉厚よりも厚くし
たことを特徴とするスクロール翼である。
[Structure of the Invention] (Means and Effects for Solving the Problems) That is, the first invention is provided in a scroll type compressor, and includes an end plate portion and a spiral spiral erected at one end of the end plate portion. In the scroll wing consisting of a wing section, a reinforcing member made of a metal material is provided across the mirror plate section and the wing section, and this reinforcing member is covered with a base material made of a synthetic resin material, and the reinforcing member of the wing section is is a scroll blade characterized by having a thicker wall at its root than at its tip.

圧縮作用時に、翼部に対してその高さ方向に亘って圧縮
ガスの力が加わり、その応力は先端部より根元部が大に
なる。しかるに、翼部の補強部材の根元部の肉厚を先端
部の肉厚よりも厚くしたので、根元部がより大きな剛性
を保持し、かつ合成樹脂材料による軽量化を得られる。
During compression, the force of the compressed gas is applied to the blade portion over its height, and the stress is greater at the root portion than at the tip portion. However, since the thickness of the root portion of the reinforcing member of the wing portion is made thicker than the thickness of the tip portion, the root portion can maintain greater rigidity, and the weight can be reduced by using the synthetic resin material.

第2の発明は、スクロール型圧縮機に備えられ、鏡板部
と、この鏡板部の一端部に立設された渦巻状の翼部とか
らなるスクロール翼において、上記鏡板部と翼部とに亘
って金属材料からなる補強部材を設け、この補強部材を
合成樹脂材料からなる母材で覆ってなり、上記翼部の補
強部材は、その中心部の補強強度を外周部の補強強度よ
りも強くしたことを特徴とするスクロール翼である。
A second invention provides a scroll blade that is included in a scroll compressor and includes an end plate portion and a spiral wing portion erected at one end of the end plate portion. A reinforcing member made of a metal material is provided, and this reinforcing member is covered with a base material made of a synthetic resin material. It is a scroll wing characterized by this.

スクロール型圧縮機では、圧縮作用時に翼部の中心部は
、その外周部よりも強い荷重を受ける。
In a scroll compressor, during compression, the center of the blade receives a stronger load than the outer periphery.

しかるに、上記翼部の補強部材は、その中心部の補強強
度を外周部の補強強度よりも強くしたので、中心部がよ
り大きな剛性を保持し、かつ合成樹脂材料による軽量化
を得られる。
However, since the reinforcing member of the wing part has a reinforcement strength stronger at the center than at the outer peripheral part, the center part maintains greater rigidity, and the weight can be reduced by using a synthetic resin material.

第3の発明は、スクロール型圧縮機に備えられ、鏡板部
と、この鏡板部の一端部に立設された渦巻状の翼部とか
らなるスクロール翼において、上記鏡板部と翼部とに亘
って金属材料からなる補強部材を設け、この補強部材を
合成樹脂材料からなる母材で覆ってなり、上記翼部の補
強部材は、その中心部の高さ寸法を外周部の高さ寸法よ
りも高<シたことを特徴とするスクロール翼である。
A third aspect of the present invention is a scroll blade that is included in a scroll compressor and that includes an end plate and a spiral wing that is erected at one end of the end plate. A reinforcing member made of a metal material is provided, and this reinforcing member is covered with a base material made of a synthetic resin material. It is a scroll wing characterized by high height.

圧縮作用時に、中心部の温度は外周部の温度よりも高く
なる。合成樹脂材料は熱膨張係数が大であるから、高温
部分がより熱膨張する。しかるに、翼部の補強部材の中
心部の高さ寸法を外周部の高さ寸法よりも高くしたから
、中心部先端における合成樹脂材の量は外周部先端にお
ける合成樹脂材の量よりも少なくなり、結局、同一量の
熱膨張となって、均一な高さを保持し、合成樹脂材料に
よる軽量化を得られる。
During compression, the temperature at the center becomes higher than the temperature at the outer periphery. Since the synthetic resin material has a large coefficient of thermal expansion, the high temperature portion expands more thermally. However, since the height of the center of the wing reinforcing member is made higher than the height of the outer circumference, the amount of synthetic resin material at the tip of the center is smaller than the amount of synthetic resin material at the tip of the outer circumference. As a result, the same amount of thermal expansion is achieved, a uniform height is maintained, and the weight is reduced due to the synthetic resin material.

第4の発明は、スクロール型圧縮機に備えられ、鏡板部
と、この鏡板部の一端部に立設された渦巻状の翼部とか
らなるスクロール翼において、上記鏡板部と翼部とに亘
って金属材料からなる補強部材を設け、この補強部材を
合成樹脂材料からなる母材で覆ってなり、上記鏡板部の
補強部材は、その中心部の肉厚を周端部の肉厚よりも厚
くしたことを特徴とするスクロール翼である。
A fourth aspect of the present invention is a scroll blade that is included in a scroll compressor and includes an end plate and a spiral wing section that is erected at one end of the end plate. A reinforcing member made of a metal material is provided, and this reinforcing member is covered with a base material made of a synthetic resin material. It is a scroll wing that is characterized by the following.

圧縮作用時に、鏡板部が低圧の背圧を受ける構造のスク
ロール型圧縮機では、圧縮室圧力と背圧との圧力差が、
鏡板部の中心部の方が周端部よりも大となる。しかるに
、上記鏡板部の補強部材は、その中心部の肉厚を周端部
の肉厚よりも厚くしたので、中心部がより大きな剛性を
保持し、かつ合成樹脂材料による軽量化を得られる。
In a scroll compressor in which the end plate receives low back pressure during compression, the pressure difference between the compression chamber pressure and the back pressure is
The center portion of the mirror plate portion is larger than the peripheral edge portion. However, since the reinforcing member of the end plate is made thicker at the center than at the peripheral end, the center maintains greater rigidity and can be made lighter due to the synthetic resin material.

第5の発明は、スクロール型圧縮機に備えられ、鏡板部
と、この鏡板部の一端部に立設された渦巻状の翼部とか
らなるスクロール翼において、上記鏡板部と翼部とに亘
って金属材料からなる補強部材を設け、この補強部材を
合成樹脂材料で覆ってなり、上記鏡板部の補強部材は、
その周端部の肉厚を中心部の肉厚よりも厚くしたことを
特徴とするスクロール翼である。
A fifth invention is a scroll blade that is included in a scroll compressor and includes an end plate portion and a spiral wing portion erected at one end of the end plate portion. A reinforcing member made of a metal material is provided, and this reinforcing member is covered with a synthetic resin material.
This scroll blade is characterized in that the wall thickness at the peripheral end portion is thicker than the wall thickness at the center portion.

圧縮作用時に、鏡板部が高圧あるいは中間圧の背圧を受
ける構造のスクロール型圧縮機では、圧縮室圧力と背圧
との圧力差か、鏡板部の周端部の方が中心部よりも大と
なる。しかるに、上記鏡板部の補強部材は、その周端部
の肉厚を中心部の肉厚よりも厚くしたので、外周部かよ
り大きな剛性を保持し、かつ合成樹脂材料による軽量化
を得られる。
In a scroll compressor in which the head plate receives high or intermediate back pressure during compression, the peripheral edge of the head plate is larger than the center, perhaps due to the pressure difference between the compression chamber pressure and the back pressure. becomes. However, since the reinforcing member of the end plate is made thicker at the peripheral end than at the center, the outer peripheral part maintains greater rigidity and is made lighter due to the synthetic resin material.

第6の発明は、スクロール型圧縮機に偏えられ、鏡板部
と、この鏡板部の一端部に立設された渦巻状の翼部とか
らなるスクロール翼の製造方法において、スクロール翼
と略同一形状であり、かつ翼部の外周形成部が中心形成
部よりも高く形成された空洞部を有する金型の上記空洞
部内に、金属材料からなる補強部材を配置し、母材であ
る合成樹脂材料を射出して成形することを特徴とするス
クロール翼の製造方法である。
A sixth invention provides a method for manufacturing a scroll blade which is biased toward a scroll compressor and is comprised of an end plate portion and a spiral wing portion erected at one end of the end plate portion, which is substantially the same as the scroll blade. A reinforcing member made of a metal material is placed in the cavity of a mold having a shape in which the outer periphery forming part of the wing part is formed higher than the center forming part, and a reinforcing member made of a metal material is placed, and a reinforcing member made of a synthetic resin material as a base material is This is a method for manufacturing a scroll blade, which is characterized by injecting and molding.

上記第3の発明である、補強部材の中心部の高さ寸法を
外周部の高さ寸法よりも高くした翼部を有するスクロー
ル翼を製造するための製造方法である。予め、翼部の外
周形成部が中心形成部よりも高くした空洞部を有する金
型であるから、外周形成部側に中心形成部よりも多量の
合成樹脂材料が射出されることとなる。射出後の冷却状
態は、この外周形成部の方が中心形成部よりも熱収縮量
が大であり、完成すれば、翼部の高さは全て均一になる
The third aspect of the present invention is a manufacturing method for manufacturing a scroll blade having a blade portion in which the height of the center portion of the reinforcing member is higher than the height of the outer peripheral portion. Since the mold has a cavity in which the outer periphery forming part of the wing part is made higher than the center forming part, a larger amount of synthetic resin material is injected into the outer periphery forming part than the center forming part. In the cooling state after injection, the outer periphery forming part has a larger amount of thermal contraction than the center forming part, and when completed, the height of the wing parts will be uniform.

(実施例) 以下、本発明の一実施例を図面にもとづいて説明するに
、スクロール型圧縮機自体は、先に第9図にもとづいて
説明したので、新たな説明は省略する。
(Embodiment) Hereinafter, an embodiment of the present invention will be described based on the drawings. Since the scroll type compressor itself was previously explained based on FIG. 9, a new explanation will be omitted.

第1図に、旋回スクロール翼4を示す。これは、略円板
状である鏡板部40と、この鏡板部40の一端部に立設
された渦巻状の翼部41とからなり、全体的な形状寸法
については変わりかない。ただしその構成は、上記鏡板
部40と翼部41とに亘って埋設される金属材料からな
る補強部材42aと、この補強部材42aを覆い全体的
な形状寸法を形成する合成樹脂材料からなる母材43と
で構成される。
FIG. 1 shows an orbiting scroll blade 4. As shown in FIG. This is composed of a substantially disc-shaped end plate 40 and a spiral wing portion 41 erected at one end of the end plate 40, and the overall shape and dimensions remain the same. However, its structure consists of a reinforcing member 42a made of a metal material that is buried between the mirror plate part 40 and the wing part 41, and a base material made of a synthetic resin material that covers this reinforcing member 42a and forms the overall shape and dimensions. It consists of 43.

上記補強部材42aは、たとえば鋳鉄、アルミ合金鋳物
、鋼材の鍛造品などの金属材料から選択される。上記母
材43は、たとえばポリイミド樹脂、液晶ポリマなどの
合成樹脂材料から選択される。
The reinforcing member 42a is selected from metal materials such as cast iron, aluminum alloy casting, and steel forging. The base material 43 is selected from synthetic resin materials such as polyimide resin and liquid crystal polymer.

上記補強部材42aの寸法は、以下に述べるように設定
される。すなわち、上記翼部41に埋設される部分とし
て、その渦巻状に沿う根元部44の肉厚t、を充分厚く
し、かつ図における上端部である先端部45の肉厚t2
を薄くする。なお説明すれば、翼部41の補強部材42
aの断面形状は、先端部45から根元部44になるにし
たがって厚肉となる略山形状である。
The dimensions of the reinforcing member 42a are set as described below. That is, as a portion buried in the wing portion 41, the wall thickness t of the root portion 44 along the spiral shape is made sufficiently thick, and the wall thickness t2 of the tip portion 45, which is the upper end portion in the figure, is made sufficiently thick.
Make it thinner. To explain, the reinforcing member 42 of the wing portion 41
The cross-sectional shape of a is approximately a mountain shape that becomes thicker from the tip 45 to the root 44.

一方、補強部材42aの上記鏡板部40に埋設される部
分は、その中心部46の肉厚t3を充分厚くし、周端部
47の肉厚t4を薄くした。なお説明すれば、鏡板部4
0の補強部材42aの断面形状は、中心部46から周端
部47になるにしたがって薄肉となる形状である。
On the other hand, in the portion of the reinforcing member 42a that is embedded in the end plate portion 40, the wall thickness t3 of the central portion 46 is made sufficiently thick, and the wall thickness t4 of the peripheral end portion 47 is made thin. To explain, the end plate part 4
The cross-sectional shape of the reinforcing member 42a of No. 0 is such that it becomes thinner from the center portion 46 to the peripheral end portion 47.

このように、翼部41に埋設される補強部材42aの根
元部44の肉厚を先端部43の肉厚よりも厚くしたので
、根元部44がより大きな剛性を保持する。残りの部分
を合成樹脂材料からなる母材43としたから、合成樹脂
材料による軽量化を得られる。
In this way, since the thickness of the root portion 44 of the reinforcing member 42a embedded in the wing portion 41 is made thicker than the thickness of the tip portion 43, the root portion 44 maintains greater rigidity. Since the remaining portion is made of the base material 43 made of a synthetic resin material, weight reduction can be achieved due to the synthetic resin material.

また、上記鏡板部40の補強部材42aは、その中心部
46の肉厚を周端部47の肉厚よりも厚くしたので、中
心部46がより大きな剛性を保持する。ここでも、残り
の部分を合成樹脂材料からなる母材43としたから、合
成樹脂材料による軽量化を得られる。
Further, since the reinforcing member 42a of the mirror plate portion 40 has a center portion 46 thicker than a peripheral end portion 47, the center portion 46 maintains greater rigidity. Also here, since the remaining portion is made of the base material 43 made of synthetic resin material, weight reduction can be achieved due to the synthetic resin material.

圧縮作用時には、第2図(A)に示すように、上記翼部
41に対して、その高さ方向の全長に亘って圧縮ガスの
圧力F1が加わる。そして、その応力は第2図(B)に
示すように、先端部から根元部に亘って漸次大になる。
During compression, as shown in FIG. 2(A), the pressure F1 of the compressed gas is applied to the wing section 41 over its entire length in the height direction. As shown in FIG. 2(B), the stress gradually increases from the tip to the root.

再び第1図に示すように、翼部41の補強部材42aは
先端部43から根元部44に亘って大きな剛性を保持す
るよう形成したから、応力に耐えて長期間に亘る損傷破
壊から確実に保護する。
As shown in FIG. 1 again, the reinforcing member 42a of the wing portion 41 is formed to maintain high rigidity from the tip portion 43 to the root portion 44, so that it can withstand stress and reliably prevent damage and breakage over a long period of time. Protect.

さらにまた、特に第9図で示したような、密閉ケース1
内に低圧の吸込ガスを充満させた、低圧型の圧縮機にお
いては、圧縮作用時に、鏡板部40の背面側である翼部
41が設けられていない側の面は一般に低圧(吸込圧力
)である。このため、鏡板部40の背面側圧力(以下、
背圧と省略する)と上記圧縮室Sとの圧力差をみると、
鏡板部40における中心側の圧力差が大であり、周端側
の圧力差は小である。しかるに、上記鏡板部40の補強
部材42aは、その中心部46の肉厚を周端部47の肉
厚よりも厚くしたので、中心部46側がより大きな剛性
を保持し、圧縮作用にともなう強度的な悪影響がない。
Furthermore, a sealed case 1, particularly as shown in FIG.
In a low-pressure type compressor that is filled with low-pressure suction gas, during compression, the back surface of the end plate 40, which is the side where the wing portion 41 is not provided, is generally at low pressure (suction pressure). be. For this reason, the pressure on the back side of the end plate 40 (hereinafter referred to as
Looking at the pressure difference between the back pressure (abbreviated as back pressure) and the compression chamber S,
The pressure difference on the center side of the mirror plate portion 40 is large, and the pressure difference on the peripheral end side is small. However, since the reinforcing member 42a of the end plate portion 40 has a central portion 46 thicker than a peripheral end portion 47, the central portion 46 side maintains greater rigidity, and the strength is reduced due to compression. There are no negative effects.

なお上記実施例においては、翼部41の補強部材42a
を、渦巻状に沿って連続して埋設するようにしたが、こ
れに限定されるものではなく、第3図に示すように、部
分的に不連続に設ける補強部材42b・・・であって、
これら補強部材42b・・・相互間を合成樹脂材料から
なる母材43で埋めるようにしてもよい。
Note that in the above embodiment, the reinforcing member 42a of the wing portion 41
Although the reinforcing members 42b are buried continuously along a spiral shape, the reinforcement members 42b are not limited to this, but as shown in FIG. ,
The spaces between these reinforcing members 42b may be filled with a base material 43 made of a synthetic resin material.

ただし、補強部材42b・・・は外周部ては疎に設け、
中心部にかけて漸次密に設けられる。すなわち、翼部4
1の補強部材42bは、中心部46が外周部48よりも
補強強度が強くなるよう形成される。
However, the reinforcing members 42b... are provided sparsely on the outer periphery,
They are arranged gradually closer to the center. That is, the wing section 4
The first reinforcing member 42b is formed such that the center portion 46 has stronger reinforcement strength than the outer peripheral portion 48.

圧縮作用にともない、吸込ガスが外周部48側から吸込
まれて中心部46側である圧縮室S中心に順次送られて
圧縮される。したがって、翼部41に加わるガス圧力は
、外周側よりも中心側の方が強くなる。これに対して翼
部41の補強部材42b・・・は補強強度を中心部46
が外周部48よりも強くなるよう形成したから、圧縮作
用にともなう強度的な悪影響がない。
With the compression action, suction gas is sucked in from the outer circumferential portion 48 side, and is sequentially sent to the center of the compression chamber S, which is the central portion 46 side, and is compressed. Therefore, the gas pressure applied to the wing portion 41 is stronger on the center side than on the outer peripheral side. On the other hand, the reinforcing members 42b of the wing portions 41...
Since it is formed to be stronger than the outer peripheral portion 48, there is no adverse effect on strength due to compression.

たとえば第4図(A)に示すように、上記補強部材42
cは、鏡板部40に埋設される部分が円板状補強部材5
0てあり、この円板状補強部材50の所定位置に複数の
L字型補強部材51・・・が固着されてなる。上記り字
型補強部材51・・・は翼部41に埋設されることは勿
論である。この場合、L字型補強部材51・・・の間隔
を均一にするとともに外周部48から中心部46にかけ
て漸次板厚を厚くして補強強度を大にするようにしても
よい。
For example, as shown in FIG. 4(A), the reinforcing member 42
c, the portion buried in the mirror plate portion 40 is the disk-shaped reinforcing member 5.
0, and a plurality of L-shaped reinforcing members 51 are fixed to predetermined positions of this disc-shaped reinforcing member 50. Of course, the above-mentioned cross-shaped reinforcing members 51 are embedded in the wing portion 41. In this case, the intervals between the L-shaped reinforcing members 51 may be made uniform, and the plate thickness may be gradually increased from the outer peripheral portion 48 to the center portion 46 to increase the reinforcing strength.

第4図(B)に示すように、この変形としての補強部材
42dは、鏡板部40に埋設される部分が円板状補強部
材50てあり、この円板状補強部材50の所定位置に複
数の切起し補強部材52・を設けてなる。上記切起し補
強部材52・・・は翼部41に埋設されることは勿論で
ある。
As shown in FIG. 4(B), in this modified reinforcing member 42d, the portion buried in the end plate 40 is a disc-shaped reinforcing member 50. A cut and raised reinforcing member 52 is provided. Of course, the cut and raised reinforcing members 52 are embedded in the wing portion 41.

この補強部材42dの場合は、板厚が全て均一であり、
何よりも加工が容易にすむ。
In the case of this reinforcing member 42d, all plate thicknesses are uniform,
Best of all, it is easy to process.

第4図(C)に示すように、さらに変形としての補強部
材42eは、鏡板部40に埋設される部分が円板状補強
部材53であり、この円板状補強部材53の所定位置に
折返し補強部54を一体こ設けてなる。上記折返し補強
部材54は翼部41に埋設されることは勿論である。
As shown in FIG. 4(C), in the reinforcing member 42e as a further modification, the portion buried in the end plate portion 40 is a disc-shaped reinforcing member 53, and the reinforcing member 42e is folded back at a predetermined position of this disc-shaped reinforcing member 53. A reinforcing portion 54 is integrally provided. Of course, the folded reinforcing member 54 is embedded in the wing portion 41.

この補強部材42eの場合は、絞り加工によって得られ
るので、第4図(B)に示したものと同様、大量生産に
都合がよい。
Since this reinforcing member 42e is obtained by drawing, it is convenient for mass production, similar to the reinforcing member 42e shown in FIG. 4(B).

第5図に示す補強部材42fは、翼部41に埋設される
部分における中心部46の高さ寸法h1か、外周部48
の高さ寸法h2よりも高く形成されてなる。
The reinforcing member 42f shown in FIG.
It is formed higher than the height dimension h2 of.

すなわち、上記圧縮室Sの中心部46に順次送られて圧
縮されるガスは、高圧化するにともなって高温化する。
That is, the gas that is sequentially sent to the center portion 46 of the compression chamber S and compressed becomes high in temperature as the pressure increases.

上記旋回スクロール翼4においては、当然、中心部46
が外周部48よりも温度が高(なる。ところが、母材4
3として用いられる合成樹脂材は、金属材料よりも熱膨
張係数が高いのが一般的である。このことから、第6図
に示すように、旋回スクロール翼を全て合成樹脂材料で
形成すると、圧縮作用にともなって、中心部46の高さ
寸法り、が外周部48の高さ寸法L2よりも高くなって
しまう。
Of course, in the orbiting scroll blade 4, the center portion 46
However, the temperature of the base material 4 is higher than that of the outer peripheral portion 48.
The synthetic resin material used as No. 3 generally has a higher coefficient of thermal expansion than metal materials. From this, as shown in FIG. 6, if the orbiting scroll blades are entirely made of synthetic resin material, the height of the center portion 46 will be larger than the height L2 of the outer peripheral portion 48 due to the compression action. It gets expensive.

そこで再び第5図に示すように、翼部41における補強
部材42fの中心部46の高さ寸法り。
Therefore, as shown in FIG. 5 again, the height of the center portion 46 of the reinforcing member 42f in the wing portion 41 is determined.

を、外周部48の高さ寸法h2よりも高く形成する。た
だし、翼部41の高さ寸法り、は全周に亘って同一であ
る。その結果、補強部材42fの中心部46先端から翼
部41先端に亘る母材43の厚み(量)が少なく、外周
部48先端から翼部41先端に亘る母材43の厚み(量
)か大となる。
is formed higher than the height dimension h2 of the outer peripheral portion 48. However, the height dimension of the wing portion 41 is the same over the entire circumference. As a result, the thickness (amount) of the base material 43 extending from the tip of the center portion 46 to the tip of the wing portion 41 of the reinforcing member 42f is small, and the thickness (amount) of the base material 43 extending from the tip of the outer peripheral portion 48 to the tip of the wing portion 41 is large. becomes.

上述したように、母材43としての合成樹脂材料は熱膨
張係数が大であり、かつ中心部46は外周部48よりも
裔温の熱影響を受ける。したがって、この翼部41の先
端においては、母材43の量の関係から外周部48の方
の熱膨脹変形が大であり、中心部46の熱膨張変形は小
さい。このような圧縮作用時における翼部41は、たと
え熱膨脹変形があってもその高さ寸法h3は、全周に亘
って均一を保持することとなる。
As described above, the synthetic resin material used as the base material 43 has a large coefficient of thermal expansion, and the center portion 46 is more affected by the heat of the base temperature than the outer peripheral portion 48. Therefore, at the tip of the wing portion 41, due to the amount of the base material 43, the outer peripheral portion 48 undergoes a large thermal expansion deformation, and the central portion 46 undergoes a small thermal expansion deformation. During such compression, the height h3 of the wing portion 41 remains uniform over the entire circumference even if it undergoes thermal expansion deformation.

第7図は、先に第5図に示した翼部41に補強部材42
fを有する旋回スクロール翼4を製造するための金型で
ある。すなわち、上型20と下型21とからなる金型に
の空洞部22に、先に説明した形状の補強部材42fを
仮保持し、ついて合成樹脂材を射出充填して冷却後に離
型することにより、上述した形状構造の旋回スクロール
翼4が得られる。
FIG. 7 shows a reinforcing member 42 attached to the wing section 41 shown in FIG.
This is a mold for manufacturing an orbiting scroll blade 4 having f. That is, the reinforcing member 42f having the shape described above is temporarily held in the cavity 22 of the mold consisting of the upper mold 20 and the lower mold 21, and the reinforcing member 42f is injected and filled with a synthetic resin material, and the mold is released after cooling. As a result, the orbiting scroll blade 4 having the above-described shape and structure is obtained.

ここで上型20の空洞部22は、その外周形成部48a
の高さ寸法り、を中心部の高さ寸法り。
Here, the cavity 22 of the upper mold 20 has an outer peripheral forming portion 48a.
The height dimension is the center height dimension.

よりも高く形成する。したがって、射出充填される樹脂
量は、外周部48が多く、中心部46がそれよりも少な
い。合成樹脂材料の特徴として熱膨張係数が大であるこ
とは先に説明した通りであり、そのため熱収縮量も大で
ある。より多くの合成樹脂材か充填される外周部48は
、それよりも少ない量か充填される中心部46よりも熱
収縮量が大である。その結果、完成した状態では第5図
に示すように翼部41の高さ寸法は全長に亘って均一に
なる。
Form higher than. Therefore, the amount of resin injected and filled is larger in the outer peripheral portion 48 and smaller in the center portion 46. As explained above, a characteristic of synthetic resin materials is that they have a large coefficient of thermal expansion, and therefore the amount of thermal contraction is also large. The outer peripheral portion 48, which is filled with a larger amount of synthetic resin material, has a greater amount of heat shrinkage than the central portion 46, which is filled with a smaller amount. As a result, in the completed state, the height dimension of the wing portion 41 becomes uniform over the entire length as shown in FIG.

なお、スクロール型圧縮機として、先に第9図で説明し
たような密閉ケース1内が低圧型のものと、密閉ケース
1内に圧縮した高圧ガスを一旦吐出し、ここから吐出管
13を介して外部に吐出する、密閉ケース内高圧型のも
のとに使い分けされる。このような高圧型のものにあっ
ては、旋回スクロール翼4の鏡板部40は吐出圧力その
ままの、高圧の背圧を受ける。あるいは、上記鏡板部4
0に吸込圧力と吐出圧力の中間の圧力を背圧として受け
る構造の圧縮機もある。
Note that the scroll type compressor may be of a low-pressure type in the closed case 1 as previously explained in FIG. There are two types of high-pressure type in a sealed case, which are discharged to the outside. In such a high-pressure type, the end plate portion 40 of the orbiting scroll blade 4 receives a high back pressure which is the same as the discharge pressure. Alternatively, the mirror plate portion 4
Some compressors have a structure that receives a pressure between the suction pressure and the discharge pressure at 0 as back pressure.

これらの圧縮機においては、圧縮室Sと鏡板部40の中
心部46とにおける背圧との圧力差が、その外周部48
における背圧との圧力差よりも小さくなる。すなわち、
外周部48の方がより大きな圧力を受けることとなる。
In these compressors, the pressure difference between the compression chamber S and the back pressure at the center 46 of the end plate 40 is caused by
The pressure difference between the back pressure and the back pressure at That is,
The outer peripheral portion 48 will receive greater pressure.

そこで第8図に示すように、鏡板部40における補強部
材42gは、周端部47の板ff’ t :lを中心部
46の板厚t4よりも卸<シて、周端部47の強度を大
にすることにより、鏡板部40が高圧の、あるいは中間
圧の背圧を受ける構造のものに適応できる。
Therefore, as shown in FIG. 8, the reinforcing member 42g in the mirror plate part 40 is designed so that the plate ff' t :l of the peripheral end part 47 is lower than the thickness t4 of the central part 46, thereby increasing the strength of the peripheral part 47. By increasing , it is possible to adapt to a structure in which the end plate portion 40 is subjected to high pressure or intermediate pressure back pressure.

[発明の効果コ 以上説明したように本発明によれば、翼部における補強
部材の根元部の肉厚を先端部の肉厚よりも厚くしたから
、翼部の先端部より根元部が大である応力に対応する最
適な剛性を保持でき、耐久性の向上化と、軽量化を得ら
れる効果を奏する。
[Effects of the Invention] As explained above, according to the present invention, since the thickness of the root portion of the reinforcing member in the wing portion is made thicker than the thickness of the tip portion, the root portion is larger than the tip portion of the wing portion. It can maintain the optimal rigidity corresponding to a certain stress, and has the effect of improving durability and reducing weight.

また本発明によれば、翼部における補強部材の中心部の
補強強度を外周部の補強強度よりも強くしたから、翼部
の中心部がその外周部よりも強い荷重を受けても、最適
な剛性を保持し、耐久性の向上化と、軽量化を得られる
効果を奏する。
Furthermore, according to the present invention, the reinforcement strength at the center of the reinforcing member in the wing section is made stronger than the reinforcement strength at the outer periphery, so even if the center section of the wing receives a stronger load than the outer periphery, the optimal It has the effect of maintaining rigidity, improving durability, and reducing weight.

また本発明によれば、翼部における補強部材の中心部の
高さ寸法を外周部の高さ寸法よりも高くしたから、中心
部の温度が外周部の温度よりも高くなるとともに合成樹
脂材料の特徴である熱膨張係数が大であることによる熱
影響を受けて、翼部全体に亘って均一な高さを保持し、
圧縮効率の向上化と、合成樹脂材料による軽量化を得ら
れる。
Further, according to the present invention, since the height of the center of the reinforcing member in the wing section is made higher than the height of the outer periphery, the temperature of the center becomes higher than the temperature of the outer periphery, and the synthetic resin material increases. Under the influence of heat due to its characteristic large coefficient of thermal expansion, it maintains a uniform height over the entire wing section,
Improved compression efficiency and reduced weight due to synthetic resin material.

また本発明によれば、鏡板部における補強部材の中心部
の肉厚を周端部の肉厚よりも厚くしたから、鏡板部の中
心部が高圧側となってその外周部より強く影響する荷重
に対して最適な剛性を保持でき、耐久性の向上化と、軽
量化を得られる効果を奏する。
Further, according to the present invention, since the wall thickness of the center part of the reinforcing member in the head plate part is made thicker than the wall thickness of the peripheral end part, the center part of the head plate part becomes the high pressure side, and the load exerts a stronger influence than the outer peripheral part. It is possible to maintain optimal rigidity against the elements, resulting in improved durability and weight reduction.

また本発明によれば、鏡板部における補強部ヰ」の周端
部の肉厚を中心部の肉厚よりも厚くしたから、特に鏡板
部か高圧あるいは中間圧の背圧を受ける構造のものの特
徴である、圧縮室圧力と背圧との圧力差が、鏡板部の外
周部の方が中心部よりも大となることに対して最適な剛
性を保持てき、耐久性の向上化と、軽量化を得られる効
果を奏する。
Further, according to the present invention, since the wall thickness of the peripheral end of the reinforcement part I in the head plate part is made thicker than the wall thickness of the center part, the head plate part is particularly characterized by a structure in which the back pressure of high pressure or intermediate pressure is applied. , the pressure difference between the compression chamber pressure and the back pressure is larger at the outer periphery of the end plate than at the center, so it maintains optimal rigidity, improving durability and reducing weight. It has the effect of obtaining.

また本発明によれば、スクロール翼と略同一形状であり
、かつ翼部の外周形成部が中心形成部よりも高く形成さ
れた金型の空洞部に金属材料からなる補強部材を配置し
、合成樹脂材料を射出成形して製造するようにしたから
、補強部材の中心部の高さ寸法を外周部の高さ寸法より
も高くした翼部を有するスクロール翼を製造するにあた
って、外周形成部側が中心形成部よりも多量の合成樹脂
材料を射出することとなり、射出後の冷却で外周形成部
の熱収縮が大になり、完成すれば、翼部の高さは全て均
一になる。したがって、寸法調整の手間が不要になって
製造性の向上化を得られるという効果を奏する。
Further, according to the present invention, a reinforcing member made of a metal material is placed in the cavity of the mold, which has approximately the same shape as the scroll blade, and in which the outer circumference forming part of the wing part is formed higher than the center forming part, and Since the resin material is manufactured by injection molding, when manufacturing a scroll blade having a wing portion in which the height of the center of the reinforcing member is higher than the height of the outer periphery, it is necessary to Since a larger amount of synthetic resin material is injected than the forming part, the cooling after injection causes a large thermal contraction of the outer peripheral forming part, and when completed, the height of the wing parts will all be uniform. Therefore, it is possible to eliminate the need for dimensional adjustment and improve manufacturability.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は本発明の一実施例を示すスクロール翼の縦断面
図、第2図(A)は圧縮作用時における翼部に対するガ
ス圧力の作用説明図、第2図(B)はその応力発生状態
の説明図、第3図ないし第5図は互いに異なる本発明の
他の実施例を示し、第3図はスクロール翼の翼部の横断
平面図、第4図(A)ないしくC)は互いに異なる補強
部材を備えたスクロール翼の一部縦断面図、第5図はス
クロール翼の縦断面図、第6図はスクロール翼の熱変形
状態を説明する図、第7図はスクロール翼の製造で用い
られる金型と補強部材の縦断面図、第8図はさらに異な
る本発明の他の実施例を示すスクロール翼の縦断面図、
第9図は一般的なスクロール型圧縮機の一部省略した縦
断面図である。 40・・・鏡板部、41・・・翼部、4・・・旋回スク
ロール翼、42a〜42g・・・補強部材、43・・・
母材、44・・根元部、43・・・先端部、46・・中
心部、48・・・外周部、47・・・周端部、K・・・
金型、48a・・・外周形成部、46a・・中心形成部
、22・空洞部。
Figure 1 is a longitudinal cross-sectional view of a scroll blade showing an embodiment of the present invention, Figure 2 (A) is an explanatory diagram of the action of gas pressure on the blade during compression, and Figure 2 (B) is the stress generation. Explanatory diagrams of the state, FIGS. 3 to 5 show other embodiments of the present invention that are different from each other, FIG. 3 is a cross-sectional plan view of the blade part of the scroll blade, and FIGS. A partial vertical cross-sectional view of a scroll blade equipped with different reinforcing members, FIG. 5 is a vertical cross-sectional view of the scroll blade, FIG. 6 is a diagram illustrating the state of thermal deformation of the scroll blade, and FIG. 7 is a diagram showing the manufacturing of the scroll blade. FIG. 8 is a vertical cross-sectional view of a scroll blade showing another embodiment of the present invention, which is a further different embodiment of the present invention.
FIG. 9 is a partially omitted vertical cross-sectional view of a general scroll compressor. 40... End plate portion, 41... Wing portion, 4... Orbiting scroll wing, 42a to 42g... Reinforcement member, 43...
Base material, 44... Root part, 43... Tip part, 46... Center part, 48... Outer periphery part, 47... Peripheral end part, K...
Mold, 48a: outer periphery forming part, 46a: center forming part, 22: cavity part.

Claims (6)

【特許請求の範囲】[Claims] (1)スクロール型圧縮機に備えられ、鏡板部と、この
鏡板部の一端部に立設された渦巻状の翼部とからなるス
クロール翼において、上記鏡板部と翼部とに亘って金属
材料からなる補強部材を設け、この補強部材を合成樹脂
材料からなる母材で覆ってなり、上記翼部の補強部材は
、その根元部の肉厚を先端部の肉厚よりも厚くしたこと
を特徴とするスクロール翼。
(1) In a scroll blade that is included in a scroll compressor and consists of an end plate and a spiral wing section that is erected at one end of the end plate, a metal material is used across the end plate and the wing. A reinforcing member is provided, and this reinforcing member is covered with a base material made of a synthetic resin material, and the reinforcing member of the wing portion is characterized in that the thickness of the root portion is thicker than the thickness of the tip portion. Scroll wings.
(2)スクロール型圧縮機に備えられ、鏡板部と、この
鏡板部の一端部に立設された渦巻状の翼部とからなるス
クロール翼において、上記鏡板部と翼部とに亘って金属
材料からなる補強部材を設け、この補強部材を合成樹脂
材料からなる母材で覆ってなり、上記翼部の補強部材は
、その中心部の補強強度を外周部の補強強度よりも強く
したことを特徴とするスクロール翼。
(2) In a scroll blade that is included in a scroll compressor and consists of an end plate and a spiral wing section that is erected at one end of the end plate, a metal material is used across the end plate and the wing. A reinforcing member is provided, and this reinforcing member is covered with a base material made of a synthetic resin material, and the reinforcing member for the wing portion is characterized in that the reinforcing strength at the center portion thereof is made stronger than the reinforcing strength at the outer peripheral portion. Scroll wings.
(3)スクロール型圧縮機に備えられ、鏡板部と、この
鏡板部の一端部に立設された渦巻状の翼部とからなるス
クロール翼において、上記鏡板部と翼部とに亘って金属
材料からなる補強部材を設け、この補強部材を合成樹脂
材料からなる母材で覆ってなり、上記翼部の補強部材は
、その中心部の高さ寸法を外周部の高さ寸法よりも高く
したことを特徴とするスクロール翼。
(3) In a scroll blade that is included in a scroll compressor and consists of an end plate and a spiral wing section that is erected at one end of the end plate, a metal material is used across the end plate and the wing. A reinforcing member is provided, and this reinforcing member is covered with a base material made of a synthetic resin material, and the height of the reinforcing member of the wing portion is set higher at the center than at the outer periphery. Scroll wings featuring.
(4)スクロール型圧縮機に備えられ、鏡板部と、この
鏡板部の一端部に立設された渦巻状の翼部とからなるス
クロール翼において、上記鏡板部と翼部とに亘って金属
材料からなる補強部材を設け、この補強部材を合成樹脂
材料からなる母材で覆ってなり、上記鏡板部の補強部材
は、その中心部の肉厚を周端部の肉厚よりも厚くしたこ
とを特徴とするスクロール翼。
(4) In a scroll blade that is included in a scroll compressor and consists of a head plate and a spiral wing that is erected at one end of the head plate, a metal material is used across the head plate and the blade. A reinforcing member is provided, and this reinforcing member is covered with a base material made of a synthetic resin material. Features scroll wings.
(5)スクロール型圧縮機に備えられ、鏡板部と、この
鏡板部の一端部に立設された渦巻状の翼部とからなるス
クロール翼において、上記鏡板部と翼部とに亘って金属
材料からなる補強部材を設け、この補強部材を合成樹脂
材料からなる母材で覆ってなり、上記鏡板部の補強部材
は、その周端部の肉厚を中心部の肉厚よりも厚くしたこ
とを特徴とするスクロール翼。
(5) In a scroll blade that is included in a scroll compressor and consists of an end plate and a spiral wing section that is erected at one end of the end plate, a metal material is used across the end plate and the wing. A reinforcing member is provided, and this reinforcing member is covered with a base material made of a synthetic resin material. Features scroll wings.
(6)スクロール型圧縮機に備えられ、鏡板部と、この
鏡板部の一端部に立設された渦巻状の翼部とからなるス
クロール翼の製造方法において、スクロール翼と略同一
形状であり、かつ翼部の外周形成部が中心形成部よりも
高く形成された空洞部を有する金型の上記空洞部内に、
金属材料からなる補強部材を配置し、母材である合成樹
脂材料を射出して成形することを特徴とするスクロール
翼の製造方法。
(6) In a method for manufacturing a scroll blade that is included in a scroll compressor and includes an end plate portion and a spiral wing portion erected at one end of the end plate portion, the scroll blade has substantially the same shape as the scroll blade; and in the cavity of the mold having a cavity in which the outer periphery forming part of the wing part is formed higher than the center forming part,
A method for manufacturing a scroll blade, which comprises arranging a reinforcing member made of a metal material and injecting and molding a synthetic resin material as a base material.
JP13258290A 1990-05-24 1990-05-24 Scroll blade and manufacture thereof Pending JPH0427787A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP13258290A JPH0427787A (en) 1990-05-24 1990-05-24 Scroll blade and manufacture thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP13258290A JPH0427787A (en) 1990-05-24 1990-05-24 Scroll blade and manufacture thereof

Publications (1)

Publication Number Publication Date
JPH0427787A true JPH0427787A (en) 1992-01-30

Family

ID=15084706

Family Applications (1)

Application Number Title Priority Date Filing Date
JP13258290A Pending JPH0427787A (en) 1990-05-24 1990-05-24 Scroll blade and manufacture thereof

Country Status (1)

Country Link
JP (1) JPH0427787A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH07224771A (en) * 1994-01-28 1995-08-22 Ind Technol Res Inst Manufacture of scroll member, scroll mode used for said manufacture and scroll member
US6565339B2 (en) * 2001-08-03 2003-05-20 Lg Electronics, Inc. Abrasion resistance structure of scroll compressor

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH07224771A (en) * 1994-01-28 1995-08-22 Ind Technol Res Inst Manufacture of scroll member, scroll mode used for said manufacture and scroll member
US6565339B2 (en) * 2001-08-03 2003-05-20 Lg Electronics, Inc. Abrasion resistance structure of scroll compressor

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