JPH0471818A - Screw for injection molder - Google Patents

Screw for injection molder

Info

Publication number
JPH0471818A
JPH0471818A JP18410690A JP18410690A JPH0471818A JP H0471818 A JPH0471818 A JP H0471818A JP 18410690 A JP18410690 A JP 18410690A JP 18410690 A JP18410690 A JP 18410690A JP H0471818 A JPH0471818 A JP H0471818A
Authority
JP
Japan
Prior art keywords
flight
sub
resin
screw
molten
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
JP18410690A
Other languages
Japanese (ja)
Inventor
Yotaro Fujiwara
洋太郎 藤原
Kazunari Kirimoto
桐元 一成
Hideo Ishida
英雄 石田
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.)
Ube Corp
Original Assignee
Ube Industries 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 Ube Industries Ltd filed Critical Ube Industries Ltd
Priority to JP18410690A priority Critical patent/JPH0471818A/en
Publication of JPH0471818A publication Critical patent/JPH0471818A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C45/00Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
    • B29C45/17Component parts, details or accessories; Auxiliary operations
    • B29C45/46Means for plasticising or homogenising the moulding material or forcing it into the mould
    • B29C45/58Details
    • B29C45/60Screws

Abstract

PURPOSE:To remarkably improve kneading properties by a method wherein two or more sub-flights are provided in compression zone. CONSTITUTION:At compression zone CZ, solid resin transferred from feeding zone FZ is dammed up with a first sub-flight beta1 and molten film is formed between a cylinder 5 and the solid resin in accompany with the rotation of a screw 1 by its strong shearing action. The melting of the surface of the solid resin is rapidly accelerated by the shearing force of the molten film. Further, when the molten resin, which is transferred by getting over the first sub-flight beta1, gets over a second sub-flight beta2, the molten resin receives much more shearing energy developed by the rotation of the screw 1, since the clearance Z2 between a cylinder barrel 5 and the second sub-flight beta2 is smaller than the clearance Z1 between the cylinder 5 and the first sub-flight beta1 and both semi- molten plasticized resin flight channel 3 and molten plasticized resin discharge side flight 4 are shallow, resulting in realizing the complete melting of the resin and consequently the improvement of kneading properties.

Description

【発明の詳細な説明】 〔産業上の利用分野] 本発明は射出成形機、押出成形機に応用することができ
る射出成形機用スクリュに関するものである。
DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a screw for an injection molding machine that can be applied to an injection molding machine or an extrusion molding machine.

〔従来の技術〕[Conventional technology]

第4図および第5図に従来の射出成形機用スクリュを示
す、第4図は射出成形機用スクリュの一部切断縦断面図
、第5図は第4図のスクリュ展開図を示す。
4 and 5 show a conventional screw for an injection molding machine, FIG. 4 is a partially cutaway longitudinal sectional view of the screw for an injection molding machine, and FIG. 5 is a developed view of the screw in FIG. 4.

第4図において、スクリュlは供給部FZ、圧縮部CZ
、計量部MZに分けられており、供給部FZと圧縮部C
Zの境界部の主フライトαから分岐して、圧縮部CZと
計量部MZの境界部で再度、対面の主フライトαと合体
する第1副フライトβ、と、圧縮部CZと計量部MZの
境界部の主フライトαから分岐して、スクリュ先端部方
向で再度、主フライトαと合体する第2副フライトβ2
を有する構成となっている。
In Fig. 4, the screw l is connected to the supply section FZ and the compression section CZ.
, a metering section MZ, a supply section FZ and a compression section C.
A first sub-flight β branches off from the main flight α at the boundary between the compression section CZ and the metering section MZ and joins the opposing main flight α again at the boundary between the compression section CZ and the metering section MZ; A second sub-flight β2 branches off from the main flight α at the boundary and merges with the main flight α again in the direction of the screw tip.
The structure has the following.

そして、第1副フライトβ1と第2副フライトβ2で樹
脂材料供給ねし溝2と半溶融可塑化樹脂ねし溝3および
溶融可塑化樹脂吐出側ねし溝4にそれぞれ区分しである
The first sub-flight β1 and the second sub-flight β2 are divided into a resin material supply threaded groove 2, a semi-molten plasticized resin threaded groove 3, and a molten plasticized resin discharge side threaded groove 4, respectively.

また、圧縮部CZにおけるシリンダバレル5と第1副フ
ライトβ、との隙間は、供給部FZ側から計量部MZ側
に向ってたえず一定であり、さらに、計量部MZにおい
ても同様に、シリンダバレル5と第2副フライトβ2と
の隙間も一定となっており、シリンダバレル5と第1副
フライトβ1間の隙間の方が、シリンダバレル5と第2
副フライトβ2間の隙間より大きくなるように構成され
ている。
Further, the gap between the cylinder barrel 5 and the first sub-flight β in the compression section CZ is always constant from the supply section FZ side to the metering section MZ side, and furthermore, similarly in the metering section MZ, the gap between the cylinder barrel 5 and the first sub flight β is constant. The gap between the cylinder barrel 5 and the second sub-flight β2 is also constant, and the gap between the cylinder barrel 5 and the first sub-flight β1 is larger than that between the cylinder barrel 5 and the second sub-flight β1.
The gap is configured to be larger than the gap between the sub-flights β2.

さて第4図においてホッパ6から供給部FZに供給され
た樹脂は、図示しないヒータからの熱エネルギと、スク
リュ1の回転による剪断エネルギを受け、漸次溶融しな
がら前方へ移送される。
Now, in FIG. 4, the resin supplied from the hopper 6 to the supply section FZ receives thermal energy from a heater (not shown) and shear energy due to the rotation of the screw 1, and is gradually melted and transferred forward.

また圧縮部CZでは固体樹脂は第1副フライトβ1で堰
き止められ、スクリュ1の回転に伴い、その強力な剪断
作用によりシリンダバレル5と固体樹脂の間に溶融フィ
ルムが形成され、溶融フィルムの剪断力により固体樹脂
の表面の溶融が急激に促進される。こうして、溶融樹脂
は第1副フライトβ1を乗り越えて半溶融可塑化樹脂ね
し溝3に移送される。溶融樹脂は、さらに半溶融可塑化
樹脂ねじ溝3から第2副フライトβ2を乗り越えて溶融
可塑化樹脂吐出側ねじ溝4に移送されるものの、シリン
ダバレル5と第1副フライトβ1との隙間および第2副
フライトβ2間との隙間とでは、前者のシリンダバレル
5と第1副フライトβオとの隙間の方が後者のものより
大きくなっており、第2副フライトβ2を乗り越える溶
融樹脂はさらに強力な剪断力を受け、完全に溶融される
In addition, in the compression section CZ, the solid resin is dammed up by the first sub-flight β1, and as the screw 1 rotates, a molten film is formed between the cylinder barrel 5 and the solid resin due to its strong shearing action, and the molten film is sheared. The force rapidly accelerates the melting of the surface of the solid resin. In this way, the molten resin passes over the first sub-flight β1 and is transferred to the semi-molten plasticized resin groove 3. Although the molten resin is further transferred from the semi-molten plasticized resin thread groove 3 to the molten plasticized resin discharge side thread groove 4 over the second sub-flight β2, the gap between the cylinder barrel 5 and the first sub-flight β1 and Regarding the gap between the second secondary flight β2, the gap between the former cylinder barrel 5 and the first secondary flight βO is larger than the latter, and the molten resin that crosses the second secondary flight β2 is further It is subjected to strong shearing forces and is completely melted.

〔発明が解決しようとする課題] このように従来における射出成形機用スクリュにおいて
は、圧縮部で主フライト間に第1副フライトを堰として
配し、さらに計量部MZで主フライト間に第2副フライ
トを堰として配した構成になっているために混練性が低
く、混線性を向上させようとしてシリンダバレルと第1
副フライトおよび第2副フライト間の隙間を小さくする
と処理能力が低下する欠点があった。
[Problems to be Solved by the Invention] As described above, in the conventional screw for an injection molding machine, the first sub-flight is arranged as a weir between the main flights in the compression section, and the second sub-flight is arranged between the main flights in the metering section MZ. Because the sub-flight is arranged as a weir, the kneading performance is low, and in order to improve the mixability, the cylinder barrel and the first
If the gap between the sub-flight and the second sub-flight is made smaller, there is a drawback that the throughput is reduced.

〔課題を解決するための手段〕[Means to solve the problem]

このような問題点を解決するために、本発明において、
シリンダバレル内に回転可能かつ前進・後退可能に取付
けられたスクリュであって、スクリュ本体の前端部から
後退部に向って計量部、圧縮部および供給部からなる射
出成形用スクリュにおいて、前記圧縮部に副フライト部
を2個以上設けた多重フライトとして構成にした。
In order to solve such problems, in the present invention,
A screw for injection molding that is rotatably installed in a cylinder barrel so as to be able to move forward and backward, the screw for injection molding comprising a metering section, a compression section, and a supply section from the front end of the screw body toward the retreating section. It is configured as a multiple flight with two or more sub-flight sections.

〔作 用〕[For production]

圧縮部における副フライト数を2個以上にしたため、混
練性が著しく向上する。
Since the number of sub-flights in the compression section is set to two or more, kneading performance is significantly improved.

〔実施例〕〔Example〕

第1図ないし第3図は本発明に係る射出成形機用スクリ
ュの1実施例を示し、第1図は射出成形機用スクリュの
一部切断縦断面図、第2図はスクリュ展開図、第3図は
第2図のA−D点の各断面における樹脂の流れ状態を示
す。
1 to 3 show one embodiment of a screw for an injection molding machine according to the present invention, FIG. 1 is a partially cut away longitudinal sectional view of the screw for an injection molding machine, FIG. FIG. 3 shows the flow state of the resin in each cross section taken along the line A-D in FIG.

本発明を、主フライトα間に第1副フライトβ1 と第
2副フライトβ2を有し、第1副フライトβ1と第2副
フライトβ2はともに計量部MZと圧縮部CZの境界域
の主フライトαがら分岐し、第1副フライトβ、は圧縮
部cZと供給部FZの境界域の主フライトαと合体し、
第2副フライトβ2は例えば圧縮部cZの略中央部域で
主フライトαと合体する場合について述べる。
The present invention has a first sub-flight β1 and a second sub-flight β2 between the main flights α, and the first sub-flight β1 and the second sub-flight β2 are both main flights in the boundary area between the measuring section MZ and the compression section CZ. The first sub-flight β branches off from α, and merges with the main flight α in the boundary area between the compression part cZ and the supply part FZ,
A case will be described in which the second sub-flight β2 is combined with the main flight α, for example, in a substantially central region of the compression portion cZ.

また、このときの樹脂材料供給側ねじ溝2の深さと溶融
可塑化樹脂吐出側ねじ溝4の深さを樹脂の射出方向に対
して深溝部から浅溝部へと連続的に漸減をなし、半溶融
可塑化樹脂側ねし溝3の深さを樹脂の射出方向に対して
不変とし、かつ、供給部FZと圧縮部02間からの第1
副フライトβ1形成開始点で前記樹脂材料供給側ねじ溝
2の深さを前記半溶融可塑化樹脂側ねじ溝3の深さより
深(するとともに、樹脂の射出方向の次なる第2副フラ
イトβ2形成開始点で、溶融可塑化樹脂吐出側ねじ溝4
の深さを半熔融可塑化樹脂側ねじ溝3より深くした場合
について述べる。
In addition, the depth of the resin material supply side screw groove 2 and the depth of the molten plasticized resin discharge side screw groove 4 at this time are continuously gradually decreased from the deep groove part to the shallow groove part in the resin injection direction, and the depth is halved. The depth of the molten plasticized resin side thread groove 3 is kept unchanged with respect to the injection direction of the resin, and the first
At the starting point of secondary flight β1 formation, the depth of the resin material supply side screw groove 2 is set to be deeper than the depth of the semi-molten plasticized resin side screw groove 3 (at the same time, the next second secondary flight β2 in the resin injection direction is formed). At the starting point, the molten plasticized resin discharge side thread groove 4
A case where the depth is made deeper than the thread groove 3 on the semi-molten plasticized resin side will be described.

第1図において、スクリュ1は供給部FZ、圧縮部CZ
、計量部MZに分けられている。また、圧縮部CZには
、第1副フライトβ1と第2副フライトβ2が配設され
ており、第1副フライトβ1と第2副フライトβ2で樹
脂材料供給ねじ溝2と半溶融可塑化樹脂ねじ溝3および
溶融可塑化吐出側ねじ溝4にそれぞれ区分しである。
In FIG. 1, the screw 1 has a supply section FZ and a compression section CZ.
, and a measuring section MZ. In addition, a first sub-flight β1 and a second sub-flight β2 are arranged in the compression section CZ, and the first sub-flight β1 and second sub-flight β2 connect the resin material supply screw groove 2 and the semi-molten plasticized resin. It is divided into a thread groove 3 and a thread groove 4 on the melt-plasticizing discharge side.

また、供給部FZと圧縮部CZの境界部の主フライトα
から分岐して、圧縮部CZと計量部MZの境界部で再度
、対面の主フライトαと合体する第1副フライトβ1と
、圧縮部C2の略中心近傍の主フライトαから分岐して
、圧縮部CZと計量部MZの境界部で再度対面の主フラ
イトαと合体する第2副フライトβ2を有する構成とな
っている。
In addition, the main flight α at the boundary between the supply section FZ and the compression section CZ
The first sub-flight β1 branches off from the main flight α near the center of the compression part C2 and merges with the opposing main flight α again at the boundary between the compression part CZ and the metering part MZ. The configuration includes a second sub-flight β2 that again joins the opposing main flight α at the boundary between the section CZ and the measuring section MZ.

第3図に示すように、圧縮部CZにおけるシリンダバレ
ル5と第1副フライトβ1間の隙間をZ8、また、シリ
ンダバレル5と第2副フライトβ2間の隙間を72とす
ると、シリンダバレル5と第1副フライトβ1との隙間
Z1は供給部FZ側から計量部MZ側に向ってたえず一
定であり、さらに、シリンダバレル5と第2副フライト
β2との隙間Z2も一定となっており、Z+>Zzとな
るように構成されている。
As shown in FIG. 3, if the gap between the cylinder barrel 5 and the first sub-flight β1 in the compression part CZ is Z8, and the gap between the cylinder barrel 5 and the second sub-flight β2 is 72, then the cylinder barrel 5 and The gap Z1 with the first sub-flight β1 is constantly constant from the supply section FZ side to the measuring section MZ side, and furthermore, the gap Z2 between the cylinder barrel 5 and the second sub-flight β2 is also constant, and Z+ >Zz.

さらに、圧縮部CZにおけるねし溝の深さについては、
まず、樹脂材料供給側ねじ溝2では、樹脂の射出方向に
深溝部から浅溝部へとH+ > Hz>Hs>Haとな
るように連続的に漸減をなした構成を有している。
Furthermore, regarding the depth of the threaded groove in the compression part CZ,
First, the resin material supply side screw groove 2 has a structure in which the threads gradually decrease in the resin injection direction from the deep groove part to the shallow groove part so that H+>Hz>Hs>Ha.

また、圧縮部CZにおける半溶融可塑化樹脂側ねし溝3
の深さH3は、樹脂の射出方向に不変となっている。さ
らに、主フライトαから分岐して半溶融可塑化樹脂ねじ
溝3と溶融可塑化樹脂吐出側ねじ溝4に分離する第2副
フライトβ2の形成開始点近傍では、半溶融可塑化樹脂
側ねじ溝3の溝の深さH3より、溶融可塑化樹脂吐出側
ねし溝4の溝の深さH6の方が深< (H,>Hs )
なっている。また、第2副フライトβ2が対面の主フラ
イトαと合体する第2副フライトβ2の形成終了点近傍
では、前記した樹脂材料供給側ねし溝2の深さH4、半
溶融可塑化樹脂側ねじ溝3の深さH3および溶融可塑化
樹脂吐出側ねし溝4の深さH6はほぼ同一(H= =H
s =Hb )になるように構成されている。
In addition, the semi-molten plasticized resin side thread groove 3 in the compression part CZ
The depth H3 remains unchanged in the resin injection direction. Furthermore, near the formation start point of the second sub-flight β2 which branches from the main flight α and separates into the semi-molten plasticized resin thread groove 3 and the molten plasticized resin discharge side thread groove 4, the semi-molten plasticized resin side thread groove The depth H6 of the groove on the molten plasticized resin discharge side threaded groove 4 is deeper than the depth H3 of the groove in No. 3 < (H, >Hs)
It has become. In addition, near the formation end point of the second secondary flight β2 where the second secondary flight β2 is combined with the opposing main flight α, the depth H4 of the resin material supply side thread groove 2 described above, the semi-molten plasticized resin side thread The depth H3 of the groove 3 and the depth H6 of the molten plasticized resin discharge side threaded groove 4 are almost the same (H= =H
s = Hb).

以上のように構成された高混練スクリュの動作を説明す
る。
The operation of the high kneading screw configured as above will be explained.

第1図においてホッパ6から供給部FZに供給された樹
脂は、図示しないヒータからの熱エネルギと、スクリュ
1の回転による剪断エネルギを受け、漸次溶融しながら
前方へ移送される。
In FIG. 1, the resin supplied from the hopper 6 to the supply section FZ receives thermal energy from a heater (not shown) and shear energy due to the rotation of the screw 1, and is gradually melted and transferred forward.

圧縮部CZでは、供給部FZから移動してきた固体樹脂
は第1副フライトβ1で堰き止められ、スクリュ1の回
転に伴い、その強力な剪断作用によりシリンダ5と固体
樹脂の間に溶融フィルムが形成され、溶融フィルムの剪
断力により固体樹脂の表面の溶融が急激に促進される。
In the compression section CZ, the solid resin that has moved from the supply section FZ is stopped by the first sub-flight β1, and as the screw 1 rotates, a molten film is formed between the cylinder 5 and the solid resin due to its strong shearing action. The melting of the surface of the solid resin is rapidly promoted by the shear force of the molten film.

さらに、第1副フライトβ1を乗り越えて移動してきた
溶融樹脂は、第2副フライトβ2を乗り越える際に、シ
リンダバレル5と第2副フライトβ2間の隙間Ztが、
前記したシリンダバレル5と第1副フライトβ1間の隙
間Z1より小さく、さらに、半溶融可塑化樹脂ねし溝3
ならびに溶融可塑化樹脂吐出側ねじ溝4が浅いために、
より一層スクリュ1の回転による剪断エネルギを受けて
、樹脂は完全に溶融され、混線性が向上する。また、特
に、本発明においては、圧縮部CZにおける樹脂材料供
給ねじ溝2と、半溶融可塑化樹脂ねし溝3および溶融可
塑化吐出側ねじ溝4に滞留する樹脂群は、スクリュ1の
軸方向へ供給部FZ側から計量部MZ側へとそれぞれス
ムースに移動を行なうことになり、供給群FZ側から送
られてきた一定量の樹脂が、この三重フライト部で閉塞
されて押出力が安定し計量化が一定に行われる。
Furthermore, when the molten resin that has moved over the first sub-flight β1 crosses the second sub-flight β2, the gap Zt between the cylinder barrel 5 and the second sub-flight β2 is
It is smaller than the gap Z1 between the cylinder barrel 5 and the first sub-flight β1 described above, and furthermore, the semi-molten plasticized resin threaded groove 3
Also, since the thread groove 4 on the molten plasticized resin discharge side is shallow,
As the resin receives more shear energy from the rotation of the screw 1, the resin is completely melted and the crosstalk property is improved. In particular, in the present invention, the resin group remaining in the resin material supply thread groove 2 in the compression part CZ, the semi-molten plasticized resin thread groove 3 and the molten plasticized discharge side thread groove 4 is located on the axis of the screw 1. The resin moves smoothly in the direction from the supply section FZ side to the metering section MZ side, and a certain amount of resin sent from the supply group FZ side is blocked by this triple flight section and the extrusion force is stabilized. The quantification is then constant.

なお、本発明の実施例においては、圧縮部CZにおける
シリンダバレル5と第1副フライトβ1間の隙間ZIを
、シリンダバレル5と第2副フライトβ2間の隙間Z2
より大きくした場合について述べたが、これに限定され
るものでなく、Z1=72としてもほぼ同様な効果が得
られる。
In addition, in the embodiment of the present invention, the gap ZI between the cylinder barrel 5 and the first sub-flight β1 in the compression part CZ is replaced by the gap Z2 between the cylinder barrel 5 and the second sub-flight β2.
Although the case where Z1 is made larger has been described, the invention is not limited to this, and almost the same effect can be obtained even if Z1=72.

また、本発明の実施例では、主フライトα間に第2.第
3のねし山を分岐させ、樹脂材料供給ねじ溝と半溶融可
塑化樹脂ねじ溝に分離する第2ねじ山の第1副フライト
と、前記半溶融可塑化樹脂ねじ溝と溶融可塑化樹脂吐出
側ねし溝に分離する第3ねし山の第2副フライトとから
なる三重フライトを有した高混練スクリュについて述べ
たが、これに限定されるものでなく、さらにねじ山を第
4以上に分岐させた多重フライトにしてもよい。
In addition, in the embodiment of the present invention, the second flight α is provided between the main flights α. A first subsidiary flight of the second thread that branches the third thread and separates it into a resin material supply thread groove and a semi-molten plasticized resin thread groove, and the semi-molten plasticized resin thread groove and the molten plasticized resin. Although we have described a high-kneading screw that has a triple flight consisting of a second sub-flight of a third thread that is separated into a thread groove on the discharge side, the invention is not limited to this. It is also possible to create multiple flights with branches.

また、本発明における実施例では、第2副フライトβ2
が主フライトαから分岐する位置を圧縮部CZの略中心
近傍の場合について述べたが、これに限定されずに圧縮
部CZの任意の位置から分岐させてもよい。
Further, in the embodiment of the present invention, the second secondary flight β2
Although the case where the position where the main flight α branches off from the main flight α is approximately near the center of the compression section CZ has been described, the branching position is not limited to this, and may be branched off from any arbitrary position of the compression section CZ.

さらに、本実施例では、第1副フライトβ1および第2
副フライトβ2が主フライトαと合体する最終合体点を
圧縮部CZと計量部MZとの境界部にしたが、これに限
定されるものでなく、前記最終合体点を計量部MZまで
延長してもよい。
Furthermore, in this embodiment, the first sub-flight β1 and the second
Although the final merging point where the secondary flight β2 joins the main flight α is set at the boundary between the compression section CZ and the measuring section MZ, the final merging point is not limited to this, and the final merging point can be extended to the measuring section MZ. Good too.

〔発明の効果〕〔Effect of the invention〕

以上説明したことからも明らかなように、本発明では、
シリンダバレル内に回転可能かつ前進・後退可能に取付
けられたスクリュであって、スクリュ本体の前端部から
後退部に向って計量部、圧縮部および供給部からなる射
出成形用スクリュにおいて、前記圧縮部に副フライト部
を2個以上設けた多重フライトにしたことにより、混線
性が著しく向上する。
As is clear from the above explanation, in the present invention,
A screw for injection molding that is rotatably installed in a cylinder barrel so as to be able to move forward and backward, the screw for injection molding comprising a metering section, a compression section, and a supply section from the front end of the screw body toward the retreating section. By providing multiple flights with two or more sub-flight sections, cross-talk is significantly improved.

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

第1図ないし第3図は本発明に係る高混練スクリュの1
実施例を示し、第1図は高混練スクリュの一部切断縦断
面図、第2図はスクリュ展開図、第3図は第2図のA−
D点の各断面における樹脂の流れ状態を示す。第4図お
よび第5図は従来の高混練スクリュを示し、第4図は高
混練スクリュの一部切断縦断面図、第5図は第4図のス
クリュ展開図を示す。 工・・・スクリュ、2・・・樹脂材料供給ねじ溝、3・
・・半溶融可塑化樹脂ねし溝、4・・・溶融可塑化樹脂
吐出側ねし溝、5・・・シリンダバレル、6・・・ホッ
パ、α・・・主フライト、β、・・・第1副フライト、
β2・・・第2副フライト、MZ・・・計量部、CZ・
・・圧縮部、FZ・・・供給部。
Figures 1 to 3 show one of the high kneading screws according to the present invention.
Examples are shown in which Fig. 1 is a partially cutaway vertical sectional view of a high-kneading screw, Fig. 2 is a developed view of the screw, and Fig. 3 is a cross-sectional view of the high kneading screw.
The flow state of the resin in each cross section at point D is shown. 4 and 5 show a conventional high-kneading screw, FIG. 4 is a partially cutaway vertical sectional view of the high-kneading screw, and FIG. 5 is a developed view of the screw in FIG. 4. Machining: Screw, 2: Resin material supply screw groove, 3:
... Semi-molten plasticized resin threaded groove, 4... Molten plasticized resin discharge side threaded groove, 5... Cylinder barrel, 6... Hopper, α... Main flight, β,... 1st sub flight,
β2...Second sub-flight, MZ...Weighing department, CZ.
... Compression section, FZ... Supply section.

Claims (1)

【特許請求の範囲】[Claims] シリンダバレル内に回転可能かつ前進・後退可能に取付
けられたスクリュであって、スクリュ本体の前端部から
後退部に向って計量部、圧縮部および供給部からなる射
出成形用スクリュにおいて、前記圧縮部に副フライト部
を2個以上設けた多重フライトにしたことを特徴とする
射出成形機用スクリュ。
A screw for injection molding that is rotatably installed in a cylinder barrel so as to be able to move forward and backward, the screw for injection molding comprising a metering section, a compression section, and a supply section from the front end of the screw body toward the retreating section. A screw for an injection molding machine, characterized in that the screw has multiple flights with two or more sub-flight sections.
JP18410690A 1990-07-13 1990-07-13 Screw for injection molder Pending JPH0471818A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP18410690A JPH0471818A (en) 1990-07-13 1990-07-13 Screw for injection molder

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP18410690A JPH0471818A (en) 1990-07-13 1990-07-13 Screw for injection molder

Publications (1)

Publication Number Publication Date
JPH0471818A true JPH0471818A (en) 1992-03-06

Family

ID=16147499

Family Applications (1)

Application Number Title Priority Date Filing Date
JP18410690A Pending JPH0471818A (en) 1990-07-13 1990-07-13 Screw for injection molder

Country Status (1)

Country Link
JP (1) JPH0471818A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH08282640A (en) * 1995-04-19 1996-10-29 Sitma Spa Device for rapidly supplying sheet-form insert to pusher conveyor of packaging device
KR100435028B1 (en) * 2001-03-21 2004-06-09 엘지전선 주식회사 An Injection Screw With A Double Flight Of The Injection Molding Machine
KR100620696B1 (en) * 2004-09-21 2006-09-19 주식회사 화승알앤에이 Manufacturing Process of Thermoplastic Elastomer by Using Two Axes Extruding Machine Having Low Shear Screw Flight

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH08282640A (en) * 1995-04-19 1996-10-29 Sitma Spa Device for rapidly supplying sheet-form insert to pusher conveyor of packaging device
KR100435028B1 (en) * 2001-03-21 2004-06-09 엘지전선 주식회사 An Injection Screw With A Double Flight Of The Injection Molding Machine
KR100620696B1 (en) * 2004-09-21 2006-09-19 주식회사 화승알앤에이 Manufacturing Process of Thermoplastic Elastomer by Using Two Axes Extruding Machine Having Low Shear Screw Flight

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