JP4397120B2 - Crusher - Google Patents

Crusher Download PDF

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Publication number
JP4397120B2
JP4397120B2 JP2000400996A JP2000400996A JP4397120B2 JP 4397120 B2 JP4397120 B2 JP 4397120B2 JP 2000400996 A JP2000400996 A JP 2000400996A JP 2000400996 A JP2000400996 A JP 2000400996A JP 4397120 B2 JP4397120 B2 JP 4397120B2
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Japan
Prior art keywords
rotor blades
wear
crushed
opposed
resistant layer
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
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JP2000400996A
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Japanese (ja)
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JP2002200430A (en
Inventor
幸洋 小林
宜弘 金子
靖裕 西浦
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.)
KMEW Co Ltd
Original Assignee
Kubota Matsushitadenko Exterior Works Ltd
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Priority to JP2000400996A priority Critical patent/JP4397120B2/en
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Description

【0001】
【発明の属する技術分野】
本発明は、複数の回転翼体をそれらの翼面が回転軸芯方向に間隔を隔てて互いに対向するように設け、前記複数の回転翼体を一体に回転させながら、被破砕物をそれらの回転翼体に接触させて破砕するように構成してある破砕装置に関する。
【0002】
【従来の技術】
従来の破砕装置では、回転翼体の全体を、クロム鋼等の硬くて耐摩耗性が高いが比較的もろい材料で形成している。
【0003】
【発明が解決しようとする課題】
この為、回転翼体が被破砕物の破砕中に折損し易い欠点があり、その欠片が破砕物に混じると、被破砕物を次の加工工程で加工する場合に支障をきたすおそれがある。
本発明は上記実情に鑑みてなされたものであって、耐摩耗性を備えながら折損しにくい回転翼体で被破砕物を破砕できるようにすることを目的とする。
【0004】
【課題を解決するための手段】
請求項1記載の発明の特徴構成は、複数の回転翼体をそれらの翼面が回転軸芯方向に間隔を隔てて互いに対向するように設け、前記複数の回転翼体を一体に回転させながら、被破砕物をそれらの回転翼体に接触させて破砕するように構成してある破砕装置であって、前記複数の回転翼体を靱性材料で形成するとともに、それらの回転翼体のうちの前記回転軸芯方向で互いに対向しない部位の表面に耐摩耗性を備えた耐摩耗層を設け、前記耐摩耗層の縁部を、前記回転軸芯方向で互いに対向する対向翼面の周部に盛り上がるように延設して、前記対向翼面に前記耐摩耗層の縁部で囲まれた凹入部であって、当該対向翼面を覆う被破砕物が入り込む凹入部を形成してある点にある。
〔作用〕
複数の回転翼体を折損しにくい靱性材料で形成し、それらの回転翼体のうちの、翼面が回転軸芯方向に間隔を隔てて互いに対向するように設けたときに、回転軸芯方向で互いに対向しない部位の表面、つまり、被破砕物に接触しながらその被破砕物に対して相対回転して摩耗し易い部位の表面に耐摩耗性を備えた耐摩耗層を設けるとともに、その耐摩耗層の縁部を、回転軸芯方向で互いに対向する対向翼面の周部に盛り上がるように延設して、対向翼面に耐摩耗層の縁部で囲まれた凹入部を形成し、対向翼面に接触する被破砕物がその凹入部に入り込んで対向翼面とともに回転し易くなるようにして、対向翼面に対して相対回転しにくい被破砕物でその対向翼面を覆うようにすることができる。
〔効果〕
複数の回転翼体を靱性材料で形成して、被破砕物を破砕中に折損しにくくしながら、それらの回転翼体のうちの摩耗し易い部位の摩耗を、その部位の表面に設けた耐摩耗層で防止できるとともに、回転軸芯方向で互いに対向する対向翼面に凹入部を形成し、その凹入部に入り込んだ被破砕物で対向翼面を覆って、対向翼面の摩耗を防止できるので、耐摩耗性を備えながら折損しにくい回転翼体で被破砕物を破砕できる。
また、回転翼体の表面の一部に耐摩耗層を設ければ良いので、耐摩耗層の形成材料を少なくして、回転翼体の製作コストを安くすることができる。
【0005】
【発明の実施の形態】
以下に本発明の実施の形態を図面に基づいて説明する。
図1は、砂等の骨材と充填材とを所定比率でセメントに混ぜ合わせてあるセメント主材とパルプなどの繊維材とシリカなどの添加剤とからなる粉粒体Fを、所定量の水と共に攪拌混合して、セメント瓦の成形原料を調整する加水混合機Bを示し、この加水混合機Bに、本発明に係る破砕装置Aを設けてある。
【0006】
前記加水混合機Bは、粉粒体Fを収容する円筒状ケーシング1に、粉粒体Fを攪拌する攪拌装置Cと、粉粒体Fに水を噴霧する多数の噴霧装置Dとを設けて、ケーシング1に収容した粉粒体Fと噴霧装置Dで噴霧した水とを攪拌装置Cで攪拌混合して、セメント瓦の成形原料を調整するように構成してある。
【0007】
前記攪拌装置Cは、横向き回転軸2を円筒状ケーシング1の内側にケーシング軸芯Xと同芯状に支持して、その横向き回転軸2に固定してある多数のショベル状の攪拌羽根3を、モータM1による横向き回転軸2の駆動回転で、ケーシング1の内周面に沿って回動させて、粉粒体Fと水とを攪拌混合するミキサEと、図2にも示すように、ケーシング軸芯Xに直交する回転軸芯Y周りで回転自在な縦向き回転軸6に一体回転するように固定した破砕具4を、攪拌羽根3の移動に干渉しないように、ケーシング軸芯X方向で隣り合う攪拌羽根3の移動経路の間に支持して、モータM2の駆動による破砕具4の回転で、粉粒体F中に混じっている粉粒体Fの固まり(だま)を破砕する破砕装置(チョッパー)Aとを設けて構成してある。
【0008】
前記破砕具4は、図3.図4,図5に示すように、8枚の回転翼体(以下、基部に位置するものから順に、第1回転翼体G1,第2回転翼体G2,第3回転翼体G3,第4回転翼体G4,第5回転翼体G5,第6回転翼体G6,第7回転翼体G7,第8回転翼体G8という)Gをそれらの翼面5が回転軸芯Y方向に間隔を隔てて互いに対向するように、回転軸芯Y方向で隣り合う回転翼体Gどうしを回転軸芯Y周りで90°の角度差で重ね合わせて、縦向き回転軸6の異径軸部7に回り止め状態で挿通し、それらの回転翼体Gを一体に回転させながら、粉粒体(被破砕物の一例)Fに接触させて、粉粒体Fの固まりを破砕するように構成してある。
【0009】
前記回転翼体Gの各々は、例えばSS41(JIS規格)のような靱性を備えた鋼板(靱性材料の一例)で四隅を切除した略菱形(横長の八角形)の同一形状に形成して、その中心部に異径軸部7を挿通してあり、それらの回転翼体Gのうちの回転軸芯Y方向で互いに対向しない部位の表面に耐摩耗性を備えた耐摩耗層8を所定の厚さで設け、耐摩耗層8の縁部9を、回転軸芯Y方向で互いに対向する対向翼面10の周部に盛り上がるように延設して、対向翼面10に摩耗層8の縁部9で囲まれた凹入部11を形成してある。
【0010】
前記耐摩耗層8は、オープンアーク溶接法或いはサブマージアーク溶接法等により回転翼体(母材)Gの表面にタングステンカーバイトやクロームカーバイトなどを主な組成とする耐摩耗性金属を肉盛溶接したものや、プラズマ溶射法あるいはフレーム溶射法等により回転翼体(母材)Gの表面に自溶金属を溶射した上でその溶射表面を溶融(ヒュージング)処理したものである。
【0011】
つまり、回転軸芯Y方向の端部に隣り合わせに組み付ける第1,第2回転翼体G1,G2及び第7,第8回転翼体G7,G8は、第1回転翼体G1と第8回転翼体G8の各々が、第3回転翼体G3側或いは第6回転翼体G6側に対向しない非対向翼面12とその外周端面13とに亘って、異径軸部7の挿通孔周囲を残して、耐摩耗層8を設けるとともに、その耐摩耗層8を、第3回転翼体G3側或いは第6回転翼体G6側に対向する対向翼面10の周部に、隣り合う回転翼体Gとの重なり部分を残して、その対向翼面10よりも盛り上がるように延設して凹入部11を形成してあり、第2回転翼体G2及び第7回転翼体G7の各々が、第4回転翼体G4側或いは第5回転翼体G5側に対向しない非対向翼面12とその外周端面13とに亘って、隣り合う回転翼体Gとの重なり部分を残して、耐摩耗層8を設けるとともに、その耐摩耗層8を、第4回転翼体G4側或いは第5回転翼体G5側に対向する対向翼面10の周部に、隣り合う回転翼体Gとの重なり部分を残して、その対向翼面10よりも盛り上がるように延設して凹入部11を形成してある。
【0012】
また、第3〜第6回転翼体G3,G4,G5,G6の各々は、両面が回転軸芯Y方向で互いに対向する対向翼面10であって、その外周端面13が回転軸芯Y方向で互いに対向しない部位であるので、その外周端面13に耐摩耗層8を設けるとともに、その耐摩耗層8を、各対向翼面10の周部に、隣り合う回転翼体Gとの重なり部分を残して、その対向翼面10よりも盛り上がるように延設してある。
【0013】
〔その他の実施形態〕
1.本発明による破砕装置は、回転翼体をステンレス鋼などの靱性材料で形成してあっても良い。
2.本発明による破砕装置は、隣り合う回転翼体どうしの間にスペーサを挟んで、それらの回転翼体の翼面が回転軸芯方向に間隔を隔てて互いに対向するように設けてあっても良い。
3.本発明による破砕装置は、粉粒体以外に、岩石や鉱石、プラスチック、硬質の廃棄物などを破砕するものであっても良い。
【図面の簡単な説明】
【図1】 加水混合機の一部破断側面図
【図2】 加水混合機の横断面図
【図3】 要部の斜視図
【図4】 要部の一部断面側面図
【図5】 図4のV−V線矢視断面図
【符号の説明】
F 被破砕物
G 回転翼体
Y 回転軸芯
5 翼面
8 耐摩耗層
9 縁部
10 対向翼面
11 凹入部
[0001]
BACKGROUND OF THE INVENTION
The present invention provides a plurality of rotor blades so that their blade surfaces are opposed to each other with a gap in the direction of the rotation axis, and the objects to be crushed are rotated while the rotor blades are rotated integrally. The present invention relates to a crushing device configured to be brought into contact with a rotary blade and crush.
[0002]
[Prior art]
In the conventional crushing device, the entire rotor blade is formed of a hard and high wear-resistant but relatively brittle material such as chrome steel.
[0003]
[Problems to be solved by the invention]
For this reason, there exists a fault which a rotary blade body is easy to break during crushing of a to-be-crushed object, and when the fragment | piece fragment mixes with a crushing object, there exists a possibility of causing trouble when processing a to-be-crushed object in the next processing process.
This invention is made | formed in view of the said situation, Comprising: It aims at enabling it to crush a to-be-crushed object with the rotary blade body which is hard to break while providing abrasion resistance.
[0004]
[Means for Solving the Problems]
According to a first aspect of the present invention, a plurality of rotor blades are provided such that their blade surfaces are opposed to each other at intervals in the direction of the rotation axis, and the rotor blades are rotated integrally. A crushing apparatus configured to crush the object to be crushed by bringing them into contact with the rotor blades, wherein the plurality of rotor blades are formed of a tough material, and among the rotor blades, A wear-resistant layer having wear resistance is provided on the surfaces of the portions that do not face each other in the direction of the rotational axis, and the edges of the wear-resistant layer are arranged on the peripheral portions of the opposed blade surfaces that face each other in the direction of the rotational axis. Extending so as to rise up, a concave portion surrounded by an edge portion of the wear-resistant layer is formed on the opposing blade surface, and a concave portion into which an object to be crushed covering the opposing blade surface enters is formed. It is in.
[Action]
When a plurality of rotor blades are formed of a tough material that is not easily broken, and the blade surfaces of the rotor blades are provided so as to face each other at intervals in the axis of rotation axis, the axis of rotation axis direction In addition, a wear-resistant layer having wear resistance is provided on the surfaces of the parts that are not opposed to each other, that is, on the surface of the parts that are likely to be worn by rotating relative to the object to be crushed while contacting the object to be crushed. Extending the edge of the wear layer so as to rise to the periphery of the opposed blade surfaces facing each other in the direction of the rotation axis, forming a recessed portion surrounded by the edge of the wear-resistant layer on the opposed blade surface, The object to be crushed in contact with the opposite wing surface enters the recessed portion and easily rotates together with the opposite wing surface, and covers the opposite wing surface with the object to be crushed that is difficult to rotate relative to the opposite wing surface. can do.
〔effect〕
A plurality of rotor blades are formed of a tough material, and while the object to be crushed is not easily broken during crushing, the wear resistance of the rotor blades that are easily worn is provided on the surface of the part. It can be prevented by the wear layer, and a recessed portion is formed on the opposed blade surfaces facing each other in the direction of the rotation axis, and the opposed blade surface is covered with the crushed material that has entered the recessed portion, thereby preventing wear of the opposed blade surface. As a result, the object to be crushed can be crushed with a rotating wing body that is hard to break while having wear resistance.
In addition, since it is only necessary to provide a wear-resistant layer on a part of the surface of the rotary blade body, the material for forming the wear-resistant layer can be reduced, and the manufacturing cost of the rotary blade body can be reduced.
[0005]
DETAILED DESCRIPTION OF THE INVENTION
Embodiments of the present invention will be described below with reference to the drawings.
FIG. 1 shows a predetermined amount of a granular material F composed of a cement main material in which an aggregate such as sand and a filler are mixed with cement at a predetermined ratio, a fiber material such as pulp, and an additive such as silica. A hydration mixer B that adjusts a molding raw material of cement tile by stirring and mixing with water is shown, and the pulverizer A according to the present invention is provided in the hydration mixer B.
[0006]
The hydration mixer B is provided with a stirring device C that stirs the granular material F and a large number of spraying devices D that spray water on the granular material F in the cylindrical casing 1 that accommodates the granular material F. The granular material F accommodated in the casing 1 and the water sprayed by the spraying device D are stirred and mixed by the stirring device C to adjust the molding raw material of the cement tile.
[0007]
The stirring device C supports a plurality of shovel-shaped stirring blades 3 that are supported on the inner side of the cylindrical casing 1 in a concentric manner with the casing axis X and fixed to the sideways rotating shaft 2. In addition, as shown in FIG. 2, a mixer E that rotates and rotates along the inner peripheral surface of the casing 1 by the drive rotation of the horizontal rotation shaft 2 by the motor M1 and stirs and mixes the powder F and water. The crushing tool 4 fixed so as to rotate integrally with a vertical rotation shaft 6 that can rotate around a rotation axis Y that is orthogonal to the casing axis X does not interfere with the movement of the stirring blade 3 in the casing axis X direction. The crushing is performed by crushing the lump of the powder F mixed in the powder F by the rotation of the crushing tool 4 driven by the motor M2 while being supported between the movement paths of the adjacent stirring blades 3. An apparatus (chopper) A is provided.
[0008]
The crushing tool 4 is shown in FIG. As shown in FIGS. 4 and 5, eight rotary blade bodies (hereinafter, in order from the one located at the base, the first rotary blade body G1, the second rotary blade body G2, the third rotary blade body G3, the fourth rotary blade body, (Referred to as rotary blade body G4, fifth rotary blade body G5, sixth rotary blade body G6, seventh rotary blade body G7, and eighth rotary blade body G8) G have their blade surfaces 5 spaced apart in the direction of the rotation axis Y. The rotating blade bodies G adjacent in the direction of the rotation axis Y are overlapped with each other at an angle difference of 90 ° around the rotation axis Y so as to be opposed to each other. It is configured to be inserted in a non-rotating state and contact the powder body (an example of the object to be crushed) F while crushing the rotor blades G so as to crush the mass of the powder body F. is there.
[0009]
Each of the rotor blades G is formed in the same shape of a substantially rhombus (laterally long octagon) with four corners cut off by a steel plate (an example of a tough material) with toughness such as SS41 (JIS standard), for example. The different-diameter shaft portion 7 is inserted into the center portion, and a wear-resistant layer 8 having wear resistance is provided on a surface of a portion of the rotor blades G not facing each other in the direction of the rotation axis Y. The edge 9 of the wear-resistant layer 8 is provided in a thickness and extends so as to rise to the peripheral portion of the opposed blade surface 10 facing each other in the rotational axis Y direction. A recessed portion 11 surrounded by the portion 9 is formed.
[0010]
The wear-resistant layer 8 is formed by depositing a wear-resistant metal mainly composed of tungsten carbide or chrome carbide on the surface of the rotary blade body (base material) G by an open arc welding method or a submerged arc welding method. This is a welded one, a self-fluxing metal sprayed on the surface of the rotor blade (base material) G by a plasma spraying method or a flame spraying method, and then the sprayed surface is melted (fusing).
[0011]
That is, the first and second rotary wing bodies G1 and G2 and the seventh and eighth rotary wing bodies G7 and G8 assembled side by side at the end in the rotational axis Y direction are the first rotary wing body G1 and the eighth rotary wing. Each of the bodies G8 leaves the periphery of the insertion hole of the different diameter shaft portion 7 across the non-opposing blade surface 12 and the outer peripheral end surface 13 that do not face the third rotating blade body G3 or the sixth rotating blade body G6. In addition, the wear-resistant layer 8 is provided, and the wear-resistant layer 8 is disposed adjacent to the circumferential surface of the opposed blade surface 10 facing the third rotary blade body G3 or the sixth rotary blade body G6. And the recessed portion 11 is formed so as to rise above the opposed blade surface 10, and each of the second rotary blade body G 2 and the seventh rotary blade body G 7 has a fourth shape. Over the non-opposing blade surface 12 that does not face the rotary blade body G4 side or the fifth rotary blade body G5 side and the outer peripheral end surface 13 thereof. While providing an abrasion-resistant layer 8 while leaving an overlapping portion with the adjacent rotary blade body G, the opposite blade surface facing the wear-resistant layer 8 on the fourth rotary blade body G4 side or the fifth rotary blade body G5 side. The recessed portion 11 is formed by extending so as to rise above the opposing blade surface 10, leaving an overlapping portion with the adjacent rotary blade body G in the peripheral portion of 10.
[0012]
Further, each of the third to sixth rotating blade bodies G3, G4, G5, and G6 is an opposing blade surface 10 whose both surfaces are opposed to each other in the rotation axis Y direction, and an outer peripheral end surface 13 thereof is the rotation axis Y direction. Therefore, the wear resistant layer 8 is provided on the outer peripheral end face 13 and the wear resistant layer 8 is provided on the circumferential portion of each opposed blade surface 10 so as to overlap the adjacent rotary blade body G. It is left extending so as to rise above the opposed wing surface 10.
[0013]
[Other Embodiments]
1. In the crushing apparatus according to the present invention, the rotor blades may be formed of a tough material such as stainless steel.
2. The crushing device according to the present invention may be provided such that spacers are sandwiched between adjacent rotor blades so that the blade surfaces of the rotor blades face each other with a gap in the direction of the rotation axis. .
3. The crushing apparatus according to the present invention may crush rocks, ores, plastics, hard wastes, etc., in addition to the granular materials.
[Brief description of the drawings]
[Fig. 1] Partially cutaway side view of the hydration mixer [Fig.2] Cross sectional view of the hydration mixer [Fig.3] Perspective view of the essential part [Fig.4] Partial sectional side view of the essential part [Fig.5] 4 is a cross-sectional view taken along line VV [Explanation of symbols]
F object to be crushed G rotating blade body Y rotating shaft core 5 blade surface 8 wear-resistant layer 9 edge 10 opposed blade surface 11 recessed portion

Claims (1)

複数の回転翼体をそれらの翼面が回転軸芯方向に間隔を隔てて互いに対向するように設け、前記複数の回転翼体を一体に回転させながら、被破砕物をそれらの回転翼体に接触させて破砕するように構成してある破砕装置であって、
前記複数の回転翼体を靱性材料で形成するとともに、それらの回転翼体のうちの前記回転軸芯方向で互いに対向しない部位の表面に耐摩耗性を備えた耐摩耗層を設け、前記耐摩耗層の縁部を、前記回転軸芯方向で互いに対向する対向翼面の周部に盛り上がるように延設して、前記対向翼面に前記耐摩耗層の縁部で囲まれた凹入部であって、当該対向翼面を覆う被破砕物が入り込む凹入部を形成してある破砕装置。
A plurality of rotor blades are provided such that their blade surfaces are opposed to each other with an interval in the direction of the rotation axis, and the objects to be crushed are attached to the rotor blades while rotating the rotor blades integrally. A crushing device configured to crush by contact,
The plurality of rotor blades are formed of a tough material, and a wear-resistant layer having wear resistance is provided on the surfaces of the rotor blades that do not face each other in the direction of the rotation axis, and the wear resistance is provided. the edges of the layer, and extends to swell the peripheral part of the opposing blade surfaces facing each other in the rotational axis direction, to the opposing blade surface, in recesses surrounded by the edge of the wear-resistant layer A crushing apparatus in which a recessed portion into which an object to be crushed that covers the opposed blade surface enters is formed.
JP2000400996A 2000-12-28 2000-12-28 Crusher Expired - Lifetime JP4397120B2 (en)

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Publication number Priority date Publication date Assignee Title
CN103495467A (en) * 2013-10-16 2014-01-08 太仓市高泰机械有限公司 Wear-resistant impeller for crusher
CN106807504A (en) * 2015-12-01 2017-06-09 衡阳双雁运输机械有限公司 A kind of impeller assembly of pulverizer

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