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JPS6338256B2 - - Google Patents
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JPS6338256B2 - - Google Patents

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Publication number
JPS6338256B2
JPS6338256B2 JP5615586A JP5615586A JPS6338256B2 JP S6338256 B2 JPS6338256 B2 JP S6338256B2 JP 5615586 A JP5615586 A JP 5615586A JP 5615586 A JP5615586 A JP 5615586A JP S6338256 B2 JPS6338256 B2 JP S6338256B2
Authority
JP
Japan
Prior art keywords
mold
casting
deformation
sand
dry sand
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
JP5615586A
Other languages
Japanese (ja)
Other versions
JPS62214847A (en
Inventor
Reijiro Hirata
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.)
SHATAI KOGYO KK
Original Assignee
SHATAI KOGYO KK
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 SHATAI KOGYO KK filed Critical SHATAI KOGYO KK
Priority to JP5615586A priority Critical patent/JPS62214847A/en
Publication of JPS62214847A publication Critical patent/JPS62214847A/en
Publication of JPS6338256B2 publication Critical patent/JPS6338256B2/ja
Granted legal-status Critical Current

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  • Molds, Cores, And Manufacturing Methods Thereof (AREA)

Description

【発明の詳細な説明】[Detailed description of the invention]

産業上の利用分野 本発明は鋼板プレス用或いは合成樹脂射出成形
用の雄型と雌型を鋳造する分野で利用されるもの
で、大型金型の鋳造に於ける反り変型抑止工法に
関する。 従来の技術 従来、鋼板プレス成型用或いは合成樹脂射出成
形用の大型の金型を精密鋳造する場合には、雄型
と雌型の合せ精度は0.2mm以下が必要のため中子
鋳型の内底面にセラミツク層を敷設したセラミツ
ク鋳型を使用して細部まで精密に鋳造する方法が
採られていた。併し、鋳造物即ち金型の形状が複
雑であると、鋳物は凝固後冷却過程で、線収縮
し、中子状鋳型を圧縮するが、鋳型強度が大きい
時、鋳型を破壊しながら収縮することができない
ので、点線のように変形する。即ち、鋳物は鋳型
の拘束により形成され、且つ、自由収縮が阻害さ
れ反り変形が必ず発生するので、鋳造完了時の公
差が±0.2mm/m以内の鋳造は困難であつた。例
えば、高精度鋳造が可能なセラミツクモールド法
により鋳型を作り、亜鉛合金で精密鋳造した場
合、2メートルで10乃至13ミリメートルの相対反
り変形が発生して使用不能となり、雌型の再鋳
造、雄型の伽い加工、ダイスポツテイングで擦り
合せの対策を行わなければ使用出来る型を得られ
なかつた。 発明が解決しようとする問題点 従来の方法による最終完成品である鋳造物即ち
金型の変形の原因は (1) 鋳物肉厚の不均一により各部の冷却速度に差
が生ずること、 (2) 中子鋳型に溶湯を鋳造し、凝固時に収縮しよ
うとするが、中子鋳型の抵抗で自由収縮が阻害
される 以上(1)及び(2)によつて反り変型を生ずるという
問題があつた。 本発明は従来の問題点を除去するため、溶湯を
鋳型に注湯する場合、鋳型が十分な強度を持ち、
素材である鋳造金属の凝固が完了し鋳造物の形状
が凍結した時点で、鋳造品の各部分が自由に収縮
出来るように鋳型強度を解除して鋳造品を自然に
収縮させ、異常変形を抑止して高精度の鋳造品を
鋳造することを目的とした発明である。 問題点を解決するための手段 本発明は中子鋳型1の側壁1a或いはセラミツ
ク鋳型(以下、単に鋳型と言う)内に於いて鋳造
素材イの凝固時に生ずる収縮力を受ける部分に沿
つて巾10mm乃至20mmの間隙孔2を形成し、該間凝
孔2に乾燥砂3を充填し、鋳造素材イの凝固温度
に達した直後に乾燥砂3を除去し、中子鋳型1或
いは鋳型の側圧強度を低下させて金型を鋳造す
る。 作 用 本発明の方法によれば鋳造素材イの凝固温度到
達直後に中子鋳型1或いは鋳型内に形成してある
巾が10mm乃至20mmの間隙孔2の乾燥砂3を抜き取
ることによつて中子鋳型1或いは鋳型の強度は解
消され、鋳造素材イが凝固時に生ずる収縮力は厚
さ10mm乃至20mmの乾燥砂3が抜き取られた間隙孔
2がつぶされて吸収される。 実施例 本方法の実施例を亜鉛合金を素材とし第2図に
示したU字形状の鋳造物について説明すると、4
は上型、1は上型4を気密に重合した中子鋳型、
5はセラミツク層である。前記上型4の側部には
湯口4aを穿設する。前記中子鋳型1に内部には
側壁1a,1aから少許の間隔lを介して側壁1
a,1aに沿つて、即ち、鋳造素材イが凝固する
際に生ずる収縮力を受ける側に沿つて巾10mm乃至
20mmの間隙孔2,2を穿設しこれらの間隙孔2,
2には乾燥砂3,3を充填する。そして鋳造素材
イの内部には凝固温度を検知する温度センサー
(CA線)6を埋設し、底部1bに間隙孔2,2に
連通した排出管7,7を穿設し、該排出管7,7
は外部のバキユーム装置8に接続する。 実施例により鋳造する場合は、中子鋳型1に上
型4を重合し、間隙孔2,2に乾燥砂3,3を
夫々充填する。更に、湯口4aから溶湯を注湯し
て中子鋳型1に鋳造素材イを充填すると共に該鋳
造素材イの内部に、コンピユーター9と接続され
ている温度センサー6を埋設する。鋳造素材イの
上方に位置する上型4内には押し湯ハを注入す
る。そして鋳造素材イの凝固が始まり凝固完了温
度を温度センサー6が検知して、その電気信号を
温度センサー6に接続したコンピユーター9に入
力し、コンピユーター9からの指令によりバキユ
ーム装置8が作動し、乾燥砂3,3を排出管7,
7を通して吸出すると間隙孔2,2は空隙とな
る。一方、冷却が進む鋳造素材イに於ける中心に
向つての収縮力は中子鋳型1の側壁1aの側壁1
a,1aを押圧し間隙孔2,2を押し潰すことに
よつて吸収される。 本実施例の実験内容は次の通りである。試作鋳
造物としての亜鉛合金の化学成分は、
INDUSTRIAL APPLICATION FIELD The present invention is used in the field of casting male and female molds for steel sheet presses or synthetic resin injection molding, and relates to a method for suppressing warping and deformation in casting large molds. Conventional technology Conventionally, when precision casting a large mold for steel plate press molding or synthetic resin injection molding, the alignment accuracy of the male and female molds must be 0.2 mm or less, so the inner bottom surface of the core mold is The method used was to use a ceramic mold with a ceramic layer laid over it to precisely cast every detail. However, if the shape of the casting, that is, the mold, is complex, the casting will linearly contract during the cooling process after solidification, compressing the core-shaped mold, but when the mold strength is high, the mold will shrink while destroying the mold. Since this is not possible, it is transformed as shown by the dotted line. That is, since the casting is formed by the restraint of the mold, free shrinkage is inhibited, and warping deformation inevitably occurs, it has been difficult to perform casting with a tolerance within ±0.2 mm/m upon completion of casting. For example, if a mold is made using the ceramic molding method, which allows for high-precision casting, and precision cast with zinc alloy, a relative warpage of 10 to 13 mm will occur at 2 meters, making it unusable. It was not possible to obtain a usable mold unless we took measures against friction through excellent machining and die spotting. Problems to be Solved by the Invention The causes of deformation of the final finished product, that is, the mold, by the conventional method are (1) the unevenness of the thickness of the casting, which causes differences in the cooling rate of each part; (2) Molten metal is cast into a core mold and attempts to contract during solidification, but free contraction is inhibited by the resistance of the core mold.The problems described in (1) and (2) above result in warping and deformation. In order to eliminate the conventional problems, the present invention aims to ensure that when pouring molten metal into a mold, the mold has sufficient strength.
Once the solidification of the cast metal material is completed and the shape of the cast is frozen, the strength of the mold is released to allow each part of the cast to contract freely, allowing the cast to contract naturally and preventing abnormal deformation. This invention aims to cast high-precision cast products. Means for Solving the Problems The present invention provides a width of 10 mm along the side wall 1a of the core mold 1 or the part of the ceramic mold (hereinafter simply referred to as the mold) that receives the shrinkage force generated when the casting material I solidifies. Form a gap hole 2 of 20 mm to 20 mm, fill the coagulation hole 2 with dry sand 3, remove the dry sand 3 immediately after reaching the solidification temperature of the casting material A, and reduce the lateral pressure strength of the core mold 1 or mold. The mold is cast by lowering the temperature. Operation According to the method of the present invention, immediately after the casting material A reaches the solidification temperature, the core mold 1 or the dry sand 3 formed in the mold is removed from the gap hole 2 with a width of 10 mm to 20 mm. The strength of the child mold 1 or mold is eliminated, and the shrinkage force generated when the casting material A solidifies is absorbed by the gap hole 2 from which the dry sand 3 with a thickness of 10 mm to 20 mm has been extracted. Example An example of the present method will be described with respect to a U-shaped casting made of zinc alloy and shown in Fig. 2.
1 is an upper mold, 1 is a core mold made by airtightly polymerizing the upper mold 4,
5 is a ceramic layer. A sprue 4a is bored in the side of the upper mold 4. Inside the core mold 1, a side wall 1 is provided with a small distance 1 from the side walls 1a, 1a.
a, 1a, that is, along the side that receives the shrinkage force generated when the casting material A solidifies, with a width of 10 mm to
20mm gap holes 2, 2 are drilled and these gap holes 2,
2 is filled with dry sand 3,3. A temperature sensor (CA wire) 6 for detecting the solidification temperature is buried inside the casting material A, and exhaust pipes 7, 7 communicating with the gap holes 2, 2 are bored in the bottom part 1b, and the exhaust pipes 7, 7
is connected to an external vacuum device 8. When casting according to the embodiment, the upper mold 4 is superposed on the core mold 1, and the interstitial holes 2, 2 are filled with dry sands 3, 3, respectively. Further, the core mold 1 is filled with the casting material I by pouring molten metal from the sprue 4a, and a temperature sensor 6 connected to a computer 9 is embedded inside the casting material I. A riser water is injected into the upper mold 4 located above the casting material A. Then, the temperature sensor 6 detects the solidification completion temperature of the casting material A, and inputs the electric signal to the computer 9 connected to the temperature sensor 6. The vacuum device 8 is activated by the command from the computer 9, and the drying process is performed. Sand 3, 3 is discharged from pipe 7,
When the liquid is sucked out through the hole 7, the gap holes 2, 2 become voids. On the other hand, the shrinkage force toward the center of the casting material A that is being cooled is
It is absorbed by pressing a, 1a and crushing the gap holes 2, 2. The experimental details of this example are as follows. The chemical composition of the zinc alloy as a prototype casting is:

【表】 である。そして形状はU字形状とし、その各部の
寸法は第2図に示した通りである。断面をU字形
状とした理由は、変形の因子を少なくして、反り
変型原因を確実につかむために単純形状とした。
長さを比較的長く600mmにした理由は、収縮量が
長さの関数で表されるので、その変形量を顕著に
し、mm単位のスケールで計測しても目読できるこ
とを意とした。下面の厚さを厚くした理由は、鋳
物を充分厚くすることにより、下面の温度斑をな
くし、熱応力の発生を防止し、変形を起こさせな
い配慮である。立ち上り長さを150mmとした理由
は、変形角度を構成する辺の長さを大きくし、収
縮時の鋳型抵抗変形が表われるようにした。更
に、鋳型を精度よく作るために、鋳型用モデルを
0.05mm以内の精度で作り、次の工程のセラミツク
用鋳型モデルも離形時の変形を皆無にするため、
シリコンゴムにより忠実に反転し作成した。鋳型
の表面にセラミツク・スラリーを注形し、高精度
な鋳型とした。第4図に試作の鋳型抵抗による変
形を抑止するため開発した中空鋳型の断面を示し
た。鋳造重量を数トンに考えているので、鋳型の
耐圧強度は30〜50Kg/cm2必要である。 したがつて、中空層のままの鋳型に注湯すれ
ば、鋳型陥没を起し危険である。その対策とし
て、鋳型の中空層に乾燥砂を詰め、上述の耐圧強
度を確保することにし、その強度を保証するた
め、第6図に示す簡易試験装置を用いた。この簡
易試験装置は台板A上の左右に、間隔を介して支
え枠B,Cを固定し、一方の支え枠Bに向つて出
没する100KgロードセルDを備えた油圧ジヤツキ
Eを他方の支え枠Cに取り付け、前記支え枠Bと
ロードセルDとの間に乾燥砂3を挾み耐圧試験を
行うように構成してある。土質力学の理論式と乾
燥砂の耐圧試験の結果でkの定数補正を行い、第
5図の耐圧理論曲線を得た(点は実験値を表わ
す)。これを砂の力学的考察による理論式で表わ
すと下記の通りである。 W′=eh′−h′−1 h′=4k/dh W=3bρgd2/16k2W′ kが0.7の時の曲線 b=100 h=90 W:耐圧荷重 b:幅 ρ:砂の比重 g:重力加速度 d:砂の厚さ h:砂の高さ k:砂個有の摩擦を表わす定数 第5図の曲線より乾燥砂の耐圧保証を確保する
ための砂の厚さは10〜20mmで、実用値として採用
できると認められる。 中空鋳型工法が変形抑止に有効であるかどうか
検証するために、 (1) 開放鋳造(上枠鋳型がなく、直接上方より注
湯する構造。) (2) 一般鋳造(鋳物の全周を鋳型で囲み、放熱条
件を一定にする構造。) (3) 中空鋳型工法(上記(2)の内側壁に間隙孔を設
け、該間隙孔に乾燥砂を充填し、中子鋳型に注
湯し、鋳造素材の凝固後、形状が安定してから
砂を抜きとる方法。) の上記3種類の鋳造工法で鋳造実験し、その試作
鋳造物イの内側を計測し、比較することにより変
形抑止効果を判定した。 鋳造後48時間自然放置冷却し、鋳物温度が70℃
以下に降下したことを確認し、鋳型を解体した。
U字形状試作鋳造物の内側壁間の距離を計測し、
物性値との差を変形量として表わしたのが、第7
図である。試作鋳造素材イの中心から根元ロまで
の距離は300mmで、その収縮量は物性値より計算
すれば、2.73mmとなる。各鋳造法により、収縮量
がそれぞれ異なる結果となり、第7図の中空鋳型
工法での収縮量が物性計算値に最も近く、0.8mm
で狙い寸法に精鋳できたと考えられる。 中空鋳型工法の場合、一般鋳造法より収縮がよ
り自由となり、物性値に近づいていることが第7
図の値よりわかる。又、根元ロにおいては物性値
にほぼ近い値に収縮している。 効 果 依つて本考案によれば、間隙孔に充填した乾燥
砂の厚さを10ミリメートル乃至20ミリメートルと
したので耐圧強度に富み、而も鋳造素材が凝固を
完了する時点に、鋳造素材に生ずる収縮力が働く
鋳型の側壁に沿つた内部に間隙を生ずるので、鋳
型の強度は解除され鋳造素材の収縮力が中心に向
つて作用して鋳型の側壁を間隙へ向つて押し潰
し、収縮力が吸収されることとなり、鋳造素材は
素直に収縮し、反り変形が抑止されて反り変形が
極めて少ない高精度の金型を鋳造することが出来
る。
[Table] The shape is U-shaped, and the dimensions of each part are as shown in FIG. The reason for the U-shaped cross section is that the shape is simple in order to reduce the factors that cause deformation and to reliably identify the cause of warp deformation.
The reason why the length was made relatively long at 600 mm was because the amount of shrinkage is expressed as a function of length, so the amount of deformation is noticeable and can be read visually even when measured on a scale of mm. The reason for increasing the thickness of the lower surface is to make the casting sufficiently thick to eliminate temperature unevenness on the lower surface, prevent thermal stress from occurring, and prevent deformation. The reason why the rising length was set to 150 mm was to increase the length of the sides that make up the deformation angle, so that the mold resistance deformation during shrinkage would appear. Furthermore, in order to make molds with high precision, we created a mold model.
In order to make the ceramic mold model in the next process with an accuracy of within 0.05mm, there will be no deformation during mold release.
It was created by faithfully inverting it using silicone rubber. Ceramic slurry was poured onto the surface of the mold to create a highly accurate mold. Figure 4 shows a cross section of a hollow mold developed to suppress deformation due to prototype mold resistance. Since the casting weight is considered to be several tons, the pressure strength of the mold is required to be 30 to 50 kg/cm 2 . Therefore, if the metal is poured into a mold with the hollow layer still in place, the mold will collapse, which is dangerous. As a countermeasure, it was decided to fill the hollow layer of the mold with dry sand to ensure the above-mentioned pressure resistance, and in order to guarantee the strength, a simple test device shown in FIG. 6 was used. This simple test device fixes support frames B and C on the left and right sides of a base plate A with a gap between them, and a hydraulic jack E equipped with a 100 kg load cell D that retracts toward one support frame B is attached to the other support frame. C, and the dry sand 3 is sandwiched between the support frame B and the load cell D to conduct a pressure test. The constant correction of k was performed using the theoretical formula of soil mechanics and the results of the dry sand pressure test, and the pressure resistance theoretical curve shown in Figure 5 was obtained (the points represent experimental values). This can be expressed as a theoretical formula based on sand mechanical considerations as follows. W′=e h′ −h′−1 h′=4k/dh W=3bρgd 2 /16k 2 W′ Curve when k is 0.7 b=100 h=90 W: Pressure resistance b: Width ρ: Sand Specific gravity g: Gravitational acceleration d: Thickness of sand h: Height of sand k: Constant representing friction unique to sand From the curve in Figure 5, the thickness of sand to ensure pressure resistance of dry sand is 10~ At 20mm, it is recognized that it can be adopted as a practical value. In order to verify whether the hollow mold method is effective in suppressing deformation, we investigated (1) open casting (a structure in which there is no upper mold, and the metal is poured directly from above), and (2) general casting (a structure in which the entire circumference of the casting is poured into the mold). (3) Hollow mold construction method (a gap hole is provided in the inner wall of (2) above, the gap hole is filled with dry sand, and the metal is poured into the core mold. After solidifying the casting material, the sand is removed after the shape has stabilized.) We conducted casting experiments using the three types of casting methods mentioned above, measured the inside of the prototype castings, and compared them to determine the deformation prevention effect. I judged it. After casting, let it cool naturally for 48 hours until the casting temperature reaches 70℃.
After confirming that it had descended below, the mold was dismantled.
Measure the distance between the inner walls of the U-shaped prototype casting,
The seventh figure expresses the difference with the physical property value as the amount of deformation.
It is a diagram. The distance from the center of the prototype casting material A to the root R is 300 mm, and the amount of shrinkage is calculated from physical property values to be 2.73 mm. Each casting method results in a different amount of shrinkage, and the shrinkage amount for the hollow mold method in Figure 7 is closest to the physical property calculation value, 0.8 mm.
It is thought that precision casting was possible to the target dimensions. In the case of the hollow mold method, shrinkage is more free than in the general casting method, and the seventh point is that it approaches the physical property value.
This can be seen from the values in the figure. In addition, at the root region, the material is shrunk to a value that is almost close to the physical property value. Effects According to the present invention, the thickness of the dry sand filled in the interstitial holes is set to 10 mm to 20 mm, so it has high pressure resistance, and when the cast material completes solidification, the dry sand that is formed in the cast material is Since a gap is created inside along the side wall of the mold where the contraction force acts, the strength of the mold is released, and the contraction force of the casting material acts toward the center, crushing the side wall of the mold toward the gap, and the contraction force is released. As a result, the casting material contracts obediently and warping is suppressed, making it possible to cast a high-precision mold with extremely little warping.

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

図は本発明の実施例を示すもので、第1図はプ
レス用金型を鋳造する鋳型の断面図、第2図は試
験鋳造物の斜視図、第3図は鋳型抵抗変形の状態
の断面図、第4図は中空鋳型断面図、第5図は乾
燥砂の耐圧曲線で、点は実験値を表わしている。
第6図は乾燥砂の耐圧強度試験装置の側面図、第
7図はU字形状実験鋳造物の側壁収縮変形図であ
る。 符号;1……中子鋳型、1a……側壁、1b…
…底部、2……間隙孔、3……乾燥砂、4……上
型、4a……湯口、5……セラミツク層、6……
温度センサー、7……排出管、8……バキユーム
装置、9……コンピユーター、l……間隔、イ…
…鋳造素材、ロ……根元、ハ……押し湯、W……
耐圧荷重、b……幅、ρ……砂の比重、g……重
力加速度、d……砂の厚さ、h……砂の高さ、k
……砂個有の摩擦を表わす定数、A……台板、
B,C……支え枠、D……ロードセル。
The figures show examples of the present invention, in which Fig. 1 is a cross-sectional view of a mold for casting a press mold, Fig. 2 is a perspective view of a test casting, and Fig. 3 is a cross-section of the mold in a state of resistance deformation. Figure 4 is a sectional view of a hollow mold, Figure 5 is a pressure resistance curve of dry sand, and the dots represent experimental values.
FIG. 6 is a side view of the dry sand compressive strength testing apparatus, and FIG. 7 is a side wall shrinkage deformation diagram of the U-shaped experimental casting. Code; 1... Core mold, 1a... Side wall, 1b...
... Bottom, 2 ... Interstitial hole, 3 ... Dry sand, 4 ... Upper mold, 4a ... Sprue, 5 ... Ceramic layer, 6 ...
Temperature sensor, 7... Discharge pipe, 8... Vacuum device, 9... Computer, l... Interval, i...
...Casting material, B...root, C...boiling water, W...
Pressure load, b...width, ρ...specific gravity of sand, g...gravitational acceleration, d...thickness of sand, h...height of sand, k
...Constant representing the friction unique to sand, A...Bedplate,
B, C...Support frame, D...Load cell.

Claims (1)

【特許請求の範囲】[Claims] 1 中子鋳型1の内部に側壁1aから少許の間隔
lを介して側壁1aに沿つて巾10mm乃至20mmの間
隙孔2を形成し、これらの間隙孔2に乾燥砂3を
充填し、前記中子鋳型1に注湯した鋳造素材イが
凝固温度に達した直後に乾燥砂3を除去すること
を特徴とする大型金型鋳造に於ける反り変型抑止
工法。
1. Gap holes 2 with a width of 10 mm to 20 mm are formed inside the core mold 1 along the side wall 1a with a small distance 1 from the side wall 1a, and these gap holes 2 are filled with dry sand 3. A method for suppressing warping and deformation in large mold casting, characterized by removing dry sand 3 immediately after a casting material A poured into a child mold 1 reaches a solidification temperature.
JP5615586A 1986-03-14 1986-03-14 Warp deformation restraint method for large metallic mold casting Granted JPS62214847A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP5615586A JPS62214847A (en) 1986-03-14 1986-03-14 Warp deformation restraint method for large metallic mold casting

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP5615586A JPS62214847A (en) 1986-03-14 1986-03-14 Warp deformation restraint method for large metallic mold casting

Publications (2)

Publication Number Publication Date
JPS62214847A JPS62214847A (en) 1987-09-21
JPS6338256B2 true JPS6338256B2 (en) 1988-07-29

Family

ID=13019201

Family Applications (1)

Application Number Title Priority Date Filing Date
JP5615586A Granted JPS62214847A (en) 1986-03-14 1986-03-14 Warp deformation restraint method for large metallic mold casting

Country Status (1)

Country Link
JP (1) JPS62214847A (en)

Also Published As

Publication number Publication date
JPS62214847A (en) 1987-09-21

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