JPS5837629Y2 - Screw or rotor with carbide pin attached to the top of the flight - Google Patents

Screw or rotor with carbide pin attached to the top of the flight

Info

Publication number
JPS5837629Y2
JPS5837629Y2 JP1980105762U JP10576280U JPS5837629Y2 JP S5837629 Y2 JPS5837629 Y2 JP S5837629Y2 JP 1980105762 U JP1980105762 U JP 1980105762U JP 10576280 U JP10576280 U JP 10576280U JP S5837629 Y2 JPS5837629 Y2 JP S5837629Y2
Authority
JP
Japan
Prior art keywords
flight
screw
rotor
pin attached
carbide pin
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
Application number
JP1980105762U
Other languages
Japanese (ja)
Other versions
JPS5729313U (en
Inventor
淑樹 牧
Original Assignee
株式会社日本製鋼所
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 株式会社日本製鋼所 filed Critical 株式会社日本製鋼所
Priority to JP1980105762U priority Critical patent/JPS5837629Y2/en
Publication of JPS5729313U publication Critical patent/JPS5729313U/ja
Application granted granted Critical
Publication of JPS5837629Y2 publication Critical patent/JPS5837629Y2/en
Expired 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
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/25Component parts, details or accessories; Auxiliary operations
    • B29C48/36Means for plasticising or homogenising the moulding material or forcing it through the nozzle or die
    • B29C48/50Details of extruders
    • B29C48/505Screws
    • B29C48/53Screws having a varying channel depth, e.g. varying the diameter of the longitudinal screw trunk
    • 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
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/25Component parts, details or accessories; Auxiliary operations
    • B29C48/36Means for plasticising or homogenising the moulding material or forcing it through the nozzle or die
    • B29C48/395Means for plasticising or homogenising the moulding material or forcing it through the nozzle or die using screws surrounded by a cooperating barrel, e.g. single screw extruders
    • B29C48/40Means for plasticising or homogenising the moulding material or forcing it through the nozzle or die using screws surrounded by a cooperating barrel, e.g. single screw extruders using two or more parallel screws or at least two parallel non-intermeshing screws, e.g. twin screw extruders
    • 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
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/25Component parts, details or accessories; Auxiliary operations
    • B29C48/36Means for plasticising or homogenising the moulding material or forcing it through the nozzle or die
    • B29C48/50Details of extruders
    • B29C48/505Screws
    • B29C48/56Screws having grooves or cavities other than the thread or the channel
    • 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
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/25Component parts, details or accessories; Auxiliary operations
    • B29C48/36Means for plasticising or homogenising the moulding material or forcing it through the nozzle or die
    • B29C48/50Details of extruders
    • B29C48/505Screws
    • B29C48/64Screws with two or more threads

Description

【考案の詳細な説明】 本考案は、合成樹脂の、スクリューまたはローターのフ
ライトとシリンダとの間に、フライトの摩耗によって間
隙が生じ、合成樹脂の剪断能力とか混線処理能力が減少
するのを防止せんとする超硬ピンをフライト頂部に取付
けたスクリューまたはローターに関するものである。
[Detailed description of the invention] This invention prevents gaps from forming between the flights of the synthetic resin screw or rotor and the cylinder due to wear of the flights, which reduces the shearing capacity and crosstalk handling capacity of the synthetic resin. It concerns a screw or rotor with a carbide pin attached to the top of the flight.

合成樹脂に混入する添加材としては、顔料(カーボン、
チタンホワイトなど)、充填材(タンカル、タルク、ア
スベスト、水酸化アルミニウムなど)、補強材(ガラス
繊維、カーボン繊維など)、その他酸化鉄、フェライト
などがあるが、これらを混入して、単軸押出機、2軸連
続混練機、2軸連続押出機、あるいはバッチニーダなど
を用いて混練すると、何れもそのシリンダやスクリュー
側に摩耗が生じる。
Additives mixed into synthetic resins include pigments (carbon,
titanium white, etc.), fillers (tankal, talc, asbestos, aluminum hydroxide, etc.), reinforcing materials (glass fiber, carbon fiber, etc.), iron oxide, ferrite, etc., and these are mixed in and processed by uniaxial extrusion. When kneading is performed using a machine, a twin-screw continuous kneader, a twin-screw continuous extruder, a batch kneader, or the like, wear occurs on the cylinder or screw side of each machine.

とくに、スクリューおよびローターの圧縮部から溶融部
に到るフライト頂部の摩耗が激しい。
In particular, the top portion of the flight from the compression section of the screw and rotor to the melting section is severely worn.

このためシリンダとフライト頂部との間に間隙ができ、
混練されるべき合成樹脂材と添加材がこの間隙から逃げ
ることになる。
This creates a gap between the cylinder and the top of the flight.
The synthetic resin material and additives to be kneaded escape through this gap.

したがってスクリューまたはローターの回転による剪断
を、これら合成樹脂材および添加材にかけることができ
なくなる。
Therefore, it becomes impossible to apply shear due to the rotation of the screw or rotor to these synthetic resin materials and additives.

すなわち合成樹脂における添加材の分散が悪くなり、ま
た混線機としての処理能力が減少する。
In other words, the dispersion of additives in the synthetic resin deteriorates, and the throughput of the crosstalk device decreases.

そして、一般に、この対策としては、スクリューおよび
ローターのフライト頂部に、高周波焼入れとか、硬質ク
ロームメッキとか、ステライト肉盛を施すようにしてい
るが、それら自身が摩耗すると、その対策としては、ス
テライト肉盛を施す以外には手段がない。
Generally, as a countermeasure against this problem, induction hardening, hard chrome plating, or stellite overlay is applied to the flight tops of screws and rotors. There is no other way to do it other than to give it a veneer.

ところが、ステライト肉盛をすると、その高熱のため、
スクリューが曲がり、曲り直し処理とかその他色々補修
工程が必要となって多大の費用と多大な日数がかかる。
However, when overlaying Stellite, due to the high heat,
If the screw becomes bent, various repair processes such as re-bending are required, which costs a lot of money and takes a lot of time.

本考案はこのような事情に鑑みて開発したものであって
、その構成は極めて単純であって、しかもこれが摩耗し
た場合には現地でその取替えが容易に行うことができる
ようにしたものである。
The present invention was developed in view of these circumstances, and its structure is extremely simple, and moreover, when it wears out, it can be easily replaced on-site. .

これを図示のものについて説明する。This will be explained with reference to the diagram.

1はシリンダ、2はスクリューまたはローターであって
3はそのフライトである。
1 is the cylinder, 2 is the screw or rotor, and 3 is its flight.

フライト3のフライト頂部4には、そのフライト3母材
より硬い材質のピン5を0〜20mmの間隔で多数取付
ける。
A large number of pins 5 made of a material harder than the base material of the flight 3 are attached to the flight top 4 of the flight 3 at intervals of 0 to 20 mm.

6は供給部から圧縮部にかかる界、7は圧縮部から溶融
部にかかる界を示す。
6 indicates the field from the supply section to the compression section, and 7 indicates the field from the compression section to the melting section.

8はローターフライトである。8 is rotor flight.

ピン5の取付方は次のようにする。Install pin 5 as follows.

フライト頂部4とシリンダ1との間隔を予め0.5〜2
0mm程あけておき、この間隙の長さより多少短く、か
つフライト項中より稍径の小さいピン5を用い、そして
例えば、フライト頂部4にピン5径より少し太き目の穴
を明け、これにピン5を打込み、あるいはその穴に螺子
に切っておいてこれに螺合するなどし、その後で銀ロー
を流し込んで抜けないようにする。
The distance between the flight top 4 and the cylinder 1 is set in advance by 0.5 to 2.
Leave a gap of about 0 mm, use a pin 5 that is slightly shorter than the length of this gap and a diameter smaller than that of the flight section, and, for example, drill a hole slightly thicker than the diameter of the pin 5 in the flight top 4, and insert it into the hole. Drive the pin 5 into the hole, or cut a screw into the hole and screw it into place, and then pour in silver solder to prevent it from coming out.

なお単軸押出機または2軸押出機のスクリューおよびロ
ーターでは完全噛合の場合では、ピン5を単に打込んだ
りあるいは螺合しただけで充分である。
If the screws and rotors of a single-screw extruder or a twin-screw extruder are fully meshed, it is sufficient to simply drive or screw the pins 5 into each other.

またピン5は異形の棒をもって形成することもできる。Further, the pin 5 can also be formed by a rod of an irregular shape.

本考案はこのように構成しであるので、たとえピンが摩
耗しても直ぐこのピンを取替えることが可能であり、し
かもその取替え作業は簡単であるので、これをわざわざ
加工場に持っていって修理するような必要がなく、現場
で容易に取替えることができ、その費用および加工日数
が最小限ですむ。
Since the present invention is constructed in this way, even if the pin wears out, it is possible to immediately replace it, and since the replacement work is easy, it is not necessary to take it to the processing factory. There is no need for repair, and it can be easily replaced on site, minimizing costs and processing time.

そして添加材の分散が悪くなったり処理能力が少しでも
減少した場合には直ちにその対策がとれ、装置の効率が
よくなり、その能力を挙げることができる。
If the dispersion of additives deteriorates or the processing capacity decreases even slightly, countermeasures can be taken immediately, improving the efficiency of the equipment and increasing its capacity.

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

第1図はフライトの縦断側面図、第2図は単軸押出機ス
クリューの側面図、第3図はその横断側面図、第4図は
2軸連続混線機のローターの側面図、第5図はその横断
側面図である。 3・・・・・・フライト、4・・・・・・フライト頂部
、5・・・・・・ピン。
Figure 1 is a longitudinal side view of the flight, Figure 2 is a side view of the single-screw extruder screw, Figure 3 is its cross-sectional side view, Figure 4 is a side view of the rotor of the two-shaft continuous mixer, and Figure 5. is a cross-sectional side view thereof. 3...Flight, 4...Top of flight, 5...Pin.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] フライト頂部4にフライト3母材より硬くかつフライト
3巾よりも稍径の小さなピン5を多数近接して取付けた
超硬ピンをフライト頂部に取付けたスクリューまたはロ
ーター
A screw or rotor in which a large number of pins 5, which are harder than the flight 3 base material and smaller in diameter than the width of the flight 3, are attached closely to the flight top 4, and carbide pins are attached to the flight top.
JP1980105762U 1980-07-25 1980-07-25 Screw or rotor with carbide pin attached to the top of the flight Expired JPS5837629Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1980105762U JPS5837629Y2 (en) 1980-07-25 1980-07-25 Screw or rotor with carbide pin attached to the top of the flight

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1980105762U JPS5837629Y2 (en) 1980-07-25 1980-07-25 Screw or rotor with carbide pin attached to the top of the flight

Publications (2)

Publication Number Publication Date
JPS5729313U JPS5729313U (en) 1982-02-16
JPS5837629Y2 true JPS5837629Y2 (en) 1983-08-25

Family

ID=29467122

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1980105762U Expired JPS5837629Y2 (en) 1980-07-25 1980-07-25 Screw or rotor with carbide pin attached to the top of the flight

Country Status (1)

Country Link
JP (1) JPS5837629Y2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH11342499A (en) * 1998-05-27 1999-12-14 Fujisash Co Screw extruder

Also Published As

Publication number Publication date
JPS5729313U (en) 1982-02-16

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