JPS642496B2 - - Google Patents
Info
- Publication number
- JPS642496B2 JPS642496B2 JP59208908A JP20890884A JPS642496B2 JP S642496 B2 JPS642496 B2 JP S642496B2 JP 59208908 A JP59208908 A JP 59208908A JP 20890884 A JP20890884 A JP 20890884A JP S642496 B2 JPS642496 B2 JP S642496B2
- Authority
- JP
- Japan
- Prior art keywords
- flight
- auxiliary
- zone
- main flight
- screw
- 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
Links
- 230000006835 compression Effects 0.000 claims description 9
- 238000007906 compression Methods 0.000 claims description 9
- 239000000463 material Substances 0.000 claims description 6
- 239000012071 phase Substances 0.000 claims description 6
- 230000010006 flight Effects 0.000 claims description 5
- 238000001746 injection moulding Methods 0.000 claims description 5
- 239000011295 pitch Substances 0.000 claims description 5
- 239000007790 solid phase Substances 0.000 claims description 4
- 238000010137 moulding (plastic) Methods 0.000 claims description 3
- 239000011347 resin Substances 0.000 description 13
- 229920005989 resin Polymers 0.000 description 13
- 238000004898 kneading Methods 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 2
- 239000000155 melt Substances 0.000 description 2
- 238000000465 moulding Methods 0.000 description 2
- 239000000049 pigment Substances 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 239000003086 colorant Substances 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 230000014759 maintenance of location Effects 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 239000012768 molten material Substances 0.000 description 1
- 238000010008 shearing Methods 0.000 description 1
- 239000011343 solid material Substances 0.000 description 1
- 230000032258 transport Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
- B29C48/25—Component parts, details or accessories; Auxiliary operations
- B29C48/36—Means for plasticising or homogenising the moulding material or forcing it through the nozzle or die
- B29C48/50—Details of extruders
- B29C48/505—Screws
- B29C48/64—Screws with two or more threads
- B29C48/65—Screws with two or more threads neighbouring threads or channels having different configurations, e.g. one thread being lower than its neighbouring thread
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
- B29C48/03—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor characterised by the shape of the extruded material at extrusion
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Processing And Handling Of Plastics And Other Materials For Molding In General (AREA)
- Injection Moulding Of Plastics Or The Like (AREA)
- Extrusion Moulding Of Plastics Or The Like (AREA)
Description
【発明の詳細な説明】
〔発明の技術分野〕
本発明は、射出成形機、押出し成形機等の成形
機に用いられるスクリユに関する。DETAILED DESCRIPTION OF THE INVENTION [Technical Field of the Invention] The present invention relates to a screw used in a molding machine such as an injection molding machine or an extrusion molding machine.
射出成形機等に用いられるスクリユは、一般に
その基部側から先端にかけて、素材の固体相を予
熱しながら移送するフイードゾーンと、素材の溶
融相を形成するコンプレツシヨンゾーンと、溶融
素材を計量するメータリングゾーンとされ、供給
される固体素材を予熱溶融して計量しつゝ先端か
ら型側に供給するようになつている。
Screws used in injection molding machines generally have a feed zone that transports the solid phase of the material while preheating it, a compression zone that forms the molten phase of the material, and a meter that measures the molten material, from the base side to the tip. It is a ring zone, and the supplied solid material is preheated, melted, measured, and then supplied from the tip to the mold side.
ところでプラスチツク射出成形用スクリユで
は、後退計量動作により有効スクリユ長が短くな
り、そのため一般的には計量された樹脂の中でノ
ズル側は比較的樹脂温度が高く、後部で計量され
たものは樹脂温度が低くなる傾向がある。 By the way, in screws for plastic injection molding, the effective length of the screw is shortened due to the backward metering operation, so generally the resin temperature is relatively high on the nozzle side of the resin being metered, and the resin temperature of the resin metered at the rear is relatively high. tends to be lower.
このように樹脂温度が低下すると、通常混練不
足が発生しやすいという問題をもたらす。 When the resin temperature decreases in this way, a problem arises in that insufficient kneading is likely to occur.
これらの問題は、固体相を予熱しながら移送す
るフイードゾーンから溶融相を形成するコンプレ
ツシヨンゾーン、メータリングゾーンに至る間に
メルトプールとソリツドベツドとが共存して吐出
されるためであり、このようなことからソリツド
ベツドをメルトプールから分離させて早期に加熱
溶融させることを意図して従来からスクリユに補
助フライトを設けることにより種々の改良を施し
たものが提案されている。 These problems arise because a melt pool and a solid bed coexist and are discharged from the feed zone, where the solid phase is preheated and transported, to the compression zone, where the molten phase is formed, and the metering zone. For this reason, various improvements have been proposed in which the screw is provided with auxiliary flights with the intention of separating the solid bed from the melt pool and heating and melting it at an early stage.
すなわち、(1)スクリユのコンプレツシヨンゾー
ン域の主フライトにそつてこれと平行に補助フラ
イトを設けたもの(実開昭53−96070号公報)、(2)
主フライトから分岐して交流側の主フライトに連
続する補助フライトを設けたもの(実公昭55−
18180号公報)、(3)主フライトとリード角が異なる
補助フライトを設けたもの(特開昭48−59159号
公報)などがある。 Namely, (1) one in which an auxiliary flight is provided along and parallel to the main flight in the compression zone area of the screw (Utility Model Application Publication No. 53-96070); (2)
An auxiliary flight that branches off from the main flight and continues to the main flight on the AC side (Jikko 55-
18180), and (3) one with an auxiliary flight having a lead angle different from the main flight (Japanese Unexamined Patent Publication No. 1983-59159).
しかしながら上記いずれのスクリユにおいて
も、おしなべて主フライトに対して補助フライト
が長く、リードを保つていくか、あるいはリード
角を変えて製作されるものであり、いずれも製造
コストが大幅に高くなるという欠点を有し、また
補助フライトのリード角を主フライトと異にした
前記(2),(3)では、補助フライトの始端部や終端部
付近で樹脂の滞留が生じ、滞留焼けを起すという
問題がある。 However, in all of the screws mentioned above, the auxiliary flight is generally longer than the main flight, and they are manufactured either by maintaining the lead or by changing the lead angle, which both have the disadvantage of significantly increasing manufacturing costs. In (2) and (3) above, in which the lead angle of the auxiliary flight is different from that of the main flight, there is a problem that resin accumulates near the start and end of the auxiliary flight, causing retention burn. be.
本発明は上記従来技術の欠点を除去することを
目的としてなされたもので、素材の均一可塑化性
能および均一混練性能を一層向上させることので
きるプラスチツク成形用スクリユを提供するにあ
る。
The present invention has been made to eliminate the above-mentioned drawbacks of the prior art, and its object is to provide a screw for plastic molding that can further improve uniform plasticizing performance and uniform kneading performance of materials.
上記目的を達成するため、本発明は、基部側か
ら先端にかけて素材固体相を予熱しつゝ移送する
フイードゾーン、溶融相を形成するコンプレツシ
ヨンゾーン、および溶融相を計量するメータリン
グゾーンを有する射出成形機等に用いられるスク
リユにおいて、上記ゾーンの少なくとも1つに当
該ゾーンの主フライトよりもリード角が小さくか
つ始端が主フライトの背面を起点とし終端が主フ
ライトの前面に近接乃至は接触する周方向の長さ
が1ピツチ〜2ピツチの補助フライトを設けたこ
とを特徴とするものである。
To achieve the above object, the present invention provides an injection molding system having a feed zone for preheating and transferring the solid phase of the material from the base side to the tip, a compression zone for forming the molten phase, and a metering zone for metering the molten phase. In a screw used in a molding machine, etc., at least one of the zones has a circumference that has a smaller lead angle than the main flight of the zone and whose starting end is from the back of the main flight and whose end is close to or in contact with the front of the main flight. It is characterized by providing an auxiliary flight whose length in the direction is 1 pitch to 2 pitches.
以下、本発明を図面に示す実施例を参照して説
明する。
The present invention will be described below with reference to embodiments shown in the drawings.
本発明によるスクリユ1の補助フライト2は、
周方向の長さが1ピツチ〜2ピツチ程度の短いも
ので、この補助フライト2の始端2Aは主フライ
ト3の背面を起点とし、終端2Bは主フライト3
の前面で終るように形成され、このリード角は主
フライト3のリード角よりも小さくされている。 The auxiliary flight 2 of the screw 1 according to the invention comprises:
The length in the circumferential direction is short, about 1 to 2 pitches, and the starting end 2A of this auxiliary flight 2 starts from the back of the main flight 3, and the terminal end 2B starts from the back of the main flight 3.
The lead angle is smaller than that of the main flight 3.
上記補助フライト2の設け方の具体例について
説明すると、第1図はスクリユ1のフイードゾー
ンに前記補助フライト2を設けた場合を示すもの
で、補助フライト2の始端2Aはフイードゾーン
の始端部の主フライト3の背面に対し狭い間隙L
2をいて始まり、終端2Bは主フライト3の前面
に対し狭い間隙1をおいて終つており、この終
端2Bと主フライト3の背面とは広い間隔L1を
おいている。 To explain a specific example of how to provide the auxiliary flight 2, FIG. 1 shows a case where the auxiliary flight 2 is provided in the feed zone of the screw 1, and the starting end 2A of the auxiliary flight 2 is connected to the main flight at the starting end of the feed zone. Narrow gap L to the back of 3
2, the terminal end 2B ends with a narrow gap 1 to the front surface of the main flight 3, and the terminal end 2B and the rear surface of the main flight 3 are separated by a wide distance L1.
また補助フライト2の高さは、主フライト3よ
りHだけ低く形成されている。 Further, the height of the auxiliary flight 2 is formed to be lower than the main flight 3 by an amount H.
第2図は上記補助フライト2のスクリユ1のコ
ンプレツシヨンゾーンに設けた場合であり、第3
図はメータリングゾーンに設けた場合である。そ
して第4図はフイードゾーン、コンプレツシヨン
ゾーン、メータリングゾーンのそれぞれに設けた
場合である。上記各図例とも補助フライト2の構
成は前記第1図の場合と同様である。第5図は上
記補助フライト2と主フライト3の関係を展開し
て溶融樹脂6の流れの状況を示している。 Figure 2 shows the case where the screw 1 of the auxiliary flight 2 is installed in the compression zone.
The figure shows the case where it is installed in a metering zone. FIG. 4 shows the case where the feed zone, compression zone, and metering zone are provided. In each of the examples shown above, the configuration of the auxiliary flight 2 is the same as that shown in FIG. 1 above. FIG. 5 shows the flow of the molten resin 6 by developing the relationship between the auxiliary flight 2 and the main flight 3.
したがつて本発明によるスクリユによれば、第
5図示のように溶融樹脂6の大半は主フライト3
よりも高さHだけ低い補助フライト2の山を越え
て前方へ送られ、ダム的機能による剪断作用によ
つて溶融樹脂6の均一可塑化や混練性能、顔料等
の分散性能の向上を図ることができる。この場
合、樹脂素材の性状等により寸法L1,1,L
2(リード角)を適切に選択することにより一層
上記性能を高めることができる。 Therefore, according to the screw according to the present invention, as shown in FIG.
The auxiliary flight 2 is sent forward over the mountain of the auxiliary flight 2 which is lower by a height H than that of the molten resin 6, and aims to uniformly plasticize the molten resin 6, improve the kneading performance, and the dispersion performance of pigments etc. by the shearing action by the dam function. I can do it. In this case, depending on the properties of the resin material, the dimensions L1, 1, L
2 (lead angle), the above performance can be further improved.
なお他の変形実施例として、前記補助フライト
2をフイードゾーンとコンプレツシヨンゾーン、
またはコンプレツシヨンゾーンとメータリングゾ
ーン、あるいはフイードゾーンとメータリングゾ
ーンに設けるようにしてもよく、また補助フライ
ト2の始端2Aおよび終端2Bの双方またはいず
れか一方を主フライト3に接合してもよく、さら
にはスクリユ1の1つのゾーンに対し複数の補助
フライト2を設けるようにしてもよい。 In addition, as another modified embodiment, the auxiliary flight 2 may be a feed zone, a compression zone,
Alternatively, it may be provided in the compression zone and the metering zone, or in the feed zone and the metering zone, or both or either of the starting end 2A and the terminal end 2B of the auxiliary flight 2 may be joined to the main flight 3. Furthermore, a plurality of auxiliary flights 2 may be provided for one zone of the screw 1.
以上のように本発明は、補助フライトは始端が
主フライトの背面を起点とし、終端が主フライト
の前面で終るよう主フライトよりもリード角が小
さく、かつ主フライトより低く形成したので、流
れる樹脂は補助フライトによるダム作用によつて
剪断され、樹脂の均一可塑化、混練性、顔料等の
分散性の向上を図ることができ、また補助フライ
トは周方向の長さが1ピツチ〜2ピツチ程度と短
いので樹脂の滞留が生じず、色替えや樹脂替えに
も支障をきたすことがなく、スクリユの製作も容
易であり、安価に性能のよいスクリユを得ること
ができる。
As described above, in the present invention, the auxiliary flight has a smaller lead angle than the main flight and is formed lower than the main flight so that the starting end starts at the back of the main flight and the end ends at the front of the main flight. is sheared by the dam action of the auxiliary flights, which can improve uniform plasticization of the resin, kneading properties, and dispersibility of pigments, etc. The auxiliary flights have a circumferential length of about 1 to 2 pitches. Since the length is short, resin does not stagnate, there is no problem in changing colors or resins, the screws are easy to manufacture, and screws with good performance can be obtained at low cost.
第1図乃至第4図は本発明の実施例を示す正面
図、第5図は1つの補助フライトと主フライトと
の関係を示す展開図である。
1……スクリユ、2……補助フライト、3……
主フライト。
1 to 4 are front views showing an embodiment of the present invention, and FIG. 5 is a developed view showing the relationship between one auxiliary flight and the main flight. 1... Skrill, 2... Auxiliary flight, 3...
Main flight.
Claims (1)
つゝ移送するフイードゾーン、溶融相を形成する
コンプレツシヨンゾーン、および溶融相を計量す
るメータリングゾーンを有する射出成形機等に用
いられるスクリユにおいて、上記ゾーンの少なく
とも1つに当該ゾーンの主フライトよりもリード
角が小さくかつ始端が主フライトの背面を起点と
し終端が主フライトの前面に近接乃至は接触する
周方向の長さが1ピツチ〜2ピツチの補助フライ
トを設けたことを特徴とするプラスチツク成形用
スクリユ。 2 前記補助フライトの高さを主フライトより低
く形成した特許請求の範囲第1項記載のプラスチ
ツク成形用スクリユ。[Claims] 1. An injection molding machine or the like having a feed zone for preheating and transferring the solid phase of the material from the base side to the tip, a compression zone for forming the molten phase, and a metering zone for measuring the molten phase. In the screw to be used, at least one of the zones has a lead angle smaller than the main flight of the zone, and a length in the circumferential direction where the starting end is from the back of the main flight and the end is close to or in contact with the front of the main flight. A plastic molding screw characterized by having one to two pitches of auxiliary flights. 2. The plastic molding screw according to claim 1, wherein the height of the auxiliary flight is lower than that of the main flight.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP59208908A JPS6186232A (en) | 1984-10-04 | 1984-10-04 | Plastics molding screw |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP59208908A JPS6186232A (en) | 1984-10-04 | 1984-10-04 | Plastics molding screw |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS6186232A JPS6186232A (en) | 1986-05-01 |
| JPS642496B2 true JPS642496B2 (en) | 1989-01-17 |
Family
ID=16564112
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP59208908A Granted JPS6186232A (en) | 1984-10-04 | 1984-10-04 | Plastics molding screw |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6186232A (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH077136Y2 (en) * | 1989-07-21 | 1995-02-22 | 住友重機械工業株式会社 | Injection molding screw |
-
1984
- 1984-10-04 JP JP59208908A patent/JPS6186232A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS6186232A (en) | 1986-05-01 |
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