TW201738389A - Unit cell titanium casting - Google Patents
Unit cell titanium casting Download PDFInfo
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- TW201738389A TW201738389A TW106111607A TW106111607A TW201738389A TW 201738389 A TW201738389 A TW 201738389A TW 106111607 A TW106111607 A TW 106111607A TW 106111607 A TW106111607 A TW 106111607A TW 201738389 A TW201738389 A TW 201738389A
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- Prior art keywords
- mold
- crucible
- chamber
- evacuated
- outer chamber
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- 238000005266 casting Methods 0.000 title claims abstract description 43
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 title claims abstract description 28
- 239000010936 titanium Substances 0.000 title claims abstract description 28
- 229910052719 titanium Inorganic materials 0.000 title claims abstract description 28
- 230000006698 induction Effects 0.000 claims abstract description 53
- 238000000034 method Methods 0.000 claims abstract description 42
- 229910001069 Ti alloy Inorganic materials 0.000 claims abstract description 33
- 238000010438 heat treatment Methods 0.000 claims abstract description 13
- 239000000956 alloy Substances 0.000 claims abstract description 8
- 239000000919 ceramic Substances 0.000 claims description 28
- 238000002844 melting Methods 0.000 claims description 15
- 230000008018 melting Effects 0.000 claims description 15
- 239000007789 gas Substances 0.000 claims description 8
- 229910000420 cerium oxide Inorganic materials 0.000 claims description 7
- BMMGVYCKOGBVEV-UHFFFAOYSA-N oxo(oxoceriooxy)cerium Chemical compound [Ce]=O.O=[Ce]=O BMMGVYCKOGBVEV-UHFFFAOYSA-N 0.000 claims description 7
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical group [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 claims description 6
- 239000005995 Aluminium silicate Substances 0.000 claims description 4
- 235000012211 aluminium silicate Nutrition 0.000 claims description 4
- 238000001816 cooling Methods 0.000 claims description 4
- 239000012774 insulation material Substances 0.000 claims description 4
- NLYAJNPCOHFWQQ-UHFFFAOYSA-N kaolin Chemical compound O.O.O=[Al]O[Si](=O)O[Si](=O)O[Al]=O NLYAJNPCOHFWQQ-UHFFFAOYSA-N 0.000 claims description 4
- 229910052786 argon Inorganic materials 0.000 claims description 3
- 230000003014 reinforcing effect Effects 0.000 claims description 2
- 229910001925 ruthenium oxide Inorganic materials 0.000 claims description 2
- WOCIAKWEIIZHES-UHFFFAOYSA-N ruthenium(iv) oxide Chemical compound O=[Ru]=O WOCIAKWEIIZHES-UHFFFAOYSA-N 0.000 claims description 2
- 230000001939 inductive effect Effects 0.000 claims 2
- 229910052715 tantalum Inorganic materials 0.000 claims 2
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 claims 2
- 239000000463 material Substances 0.000 description 14
- 229910052751 metal Inorganic materials 0.000 description 10
- 239000002184 metal Substances 0.000 description 10
- 238000010309 melting process Methods 0.000 description 5
- 239000012768 molten material Substances 0.000 description 5
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 4
- 229910010293 ceramic material Inorganic materials 0.000 description 4
- 229910052802 copper Inorganic materials 0.000 description 4
- 239000010949 copper Substances 0.000 description 4
- KJTLSVCANCCWHF-UHFFFAOYSA-N Ruthenium Chemical compound [Ru] KJTLSVCANCCWHF-UHFFFAOYSA-N 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 239000011810 insulating material Substances 0.000 description 3
- 239000000155 melt Substances 0.000 description 3
- 229910052707 ruthenium Inorganic materials 0.000 description 3
- 239000007787 solid Substances 0.000 description 3
- CETPSERCERDGAM-UHFFFAOYSA-N ceric oxide Chemical compound O=[Ce]=O CETPSERCERDGAM-UHFFFAOYSA-N 0.000 description 2
- 229910000422 cerium(IV) oxide Inorganic materials 0.000 description 2
- 238000011068 loading method Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000002360 preparation method Methods 0.000 description 2
- 238000007711 solidification Methods 0.000 description 2
- 230000008023 solidification Effects 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 238000004140 cleaning Methods 0.000 description 1
- 238000004512 die casting Methods 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000005674 electromagnetic induction Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 230000005669 field effect Effects 0.000 description 1
- 238000011049 filling Methods 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 229910001338 liquidmetal Inorganic materials 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 238000003756 stirring Methods 0.000 description 1
- 230000035882 stress Effects 0.000 description 1
- 239000013077 target material Substances 0.000 description 1
- 230000008646 thermal stress Effects 0.000 description 1
- RUDFQVOCFDJEEF-UHFFFAOYSA-N yttrium(III) oxide Inorganic materials [O-2].[O-2].[O-2].[Y+3].[Y+3] RUDFQVOCFDJEEF-UHFFFAOYSA-N 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D18/00—Pressure casting; Vacuum casting
- B22D18/06—Vacuum casting, i.e. making use of vacuum to fill the mould
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63B—APPARATUS FOR PHYSICAL TRAINING, GYMNASTICS, SWIMMING, CLIMBING, OR FENCING; BALL GAMES; TRAINING EQUIPMENT
- A63B53/00—Golf clubs
- A63B53/04—Heads
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/22—Moulds for peculiarly-shaped castings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D18/00—Pressure casting; Vacuum casting
- B22D18/04—Low pressure casting, i.e. making use of pressures up to a few bars to fill the mould
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D18/00—Pressure casting; Vacuum casting
- B22D18/08—Controlling, supervising, e.g. for safety reasons
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D21/00—Casting non-ferrous metals or metallic compounds so far as their metallurgical properties are of importance for the casting procedure; Selection of compositions therefor
- B22D21/002—Castings of light metals
- B22D21/005—Castings of light metals with high melting point, e.g. Be 1280 degrees C, Ti 1725 degrees C
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Health & Medical Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Physical Education & Sports Medicine (AREA)
- Manufacture And Refinement Of Metals (AREA)
- Crucibles And Fluidized-Bed Furnaces (AREA)
- Dental Prosthetics (AREA)
Abstract
Description
本發明係關於精密鈦鑄造。更具體而言,本發明係關於一種用於利用感應加熱來進行精密鈦鑄造之設備及方法。The present invention relates to precision titanium casting. More specifically, the present invention relates to an apparatus and method for precision titanium casting using induction heating.
鈦鑄造之各種方法係眾所周知的。一種此類方法係涉及一脫蠟程序之包模鑄造法。 真空電弧熔煉係另一方法,在該方法中,一鈦鑄錠藉由互放電所產生之實質熱量而熔化,藉此在坩堝中形成一經熔化液態金屬且完成由鈦進行之鑄造,該互放電係藉由分別使用一鈦鑄錠坩堝及一水冷式銅坩堝作為一正電極及一負電極而以一高電流狀態進行。 另一方法係其中在一拼合型水冷式銅坩堝外側纏繞一感應線圈之真空感應熔煉。由感應線圈產生之電磁力通過銅坩堝之拼塊之間的一非金屬隔離部分且然後對放置於坩堝內之一鈦鑄錠起作用。然後,經熔化金屬在坩堝內形成一經熔化金屬液態且完成由鈦進行之鑄造。 真空感應熔煉及真空電弧熔煉需要使用產生實質熱量損失之一水冷式銅坩堝。所消耗之實際電力係極少的(僅實際上對鈦起作用之電力之20%至30%)。此外,鑄模殼體之製備係極複雜且耗時的,此會增添成本。在傳統鑄造技術中,一單個熔爐之操作時間通常為60分鐘至80分鐘,且裝載及放電製程需要許多人協作進行。在傳統鑄造技術中,從製備蠟模型至清理鑄模殼體之製程可花費十天時間。 鈦係一極端反應性金屬。在經由傳統鑄造製程進行熔化期間,需要一水冷卻環境。若坩堝破裂,則經熔化鈦液體將與水直接接觸,從而產生一強烈反應或甚至爆炸,此會對生產安全造成一極大威脅。 為解決上述問題,迫切需要一種新型鈦合金感應熔化真空抽吸鑄造裝置,以解決關於現有鈦合金鑄造法之問題,諸如低效率、高成本、複雜技術、繁重之工作量、難以製備高品質鑄模殼體、長循環及潛在危險。Various methods of titanium casting are well known. One such method involves a die casting process of a dewaxing procedure. Vacuum arc melting is another method in which a titanium ingot is melted by substantial heat generated by mutual discharge, thereby forming a molten liquid metal in the crucible and completing casting by titanium, the mutual discharge The process is carried out in a high current state by using a titanium ingot and a water-cooled copper crucible as a positive electrode and a negative electrode, respectively. Another method is vacuum induction melting in which an induction coil is wound on the outside of a split type water-cooled copper crucible. The electromagnetic force generated by the induction coil passes through a non-metallic isolation portion between the blocks of the copper crucible and then acts on a titanium ingot placed in the crucible. Then, a molten metal is formed in the crucible by the molten metal and the casting by titanium is completed. Vacuum induction melting and vacuum arc melting require the use of a water-cooled copper crucible that produces substantial heat loss. The actual power consumed is minimal (only 20% to 30% of the electricity actually acting on titanium). In addition, the preparation of the mold shell is extremely complicated and time consuming, which adds cost. In conventional casting techniques, the operating time of a single furnace typically ranges from 60 minutes to 80 minutes, and the loading and discharging processes require many people to collaborate. In the conventional casting technique, it takes ten days from the preparation of the wax model to the process of cleaning the mold casing. Titanium is an extremely reactive metal. A water cooling environment is required during melting through a conventional casting process. If the crucible breaks, the molten titanium liquid will come into direct contact with the water, causing a strong reaction or even an explosion, which poses a great threat to production safety. In order to solve the above problems, there is an urgent need for a new titanium alloy induction melting vacuum suction casting device to solve the problems associated with the existing titanium alloy casting method, such as low efficiency, high cost, complicated technology, heavy workload, and difficulty in preparing high quality molds. Housing, long cycle and potential hazard.
當前,經預加熱模型鑄模之裝載發生於預加熱熔爐與鑄造熔爐之間。模型鑄模本身當前利用一叉狀楔形物貼附至內室之頂板之底側。頂板(其與鑄模附接)然後被倒置且被放置至內室主體上。為減小裝載模型鑄模所需之時間(因此使熱量損失最小化)且減小模型鑄模破損之機會(由因楔形物及/或運輸期間之損壞導致之應力所致),應利用一支架來支撐鑄模。支架將形成於內室內且經特別設計以固持且定向模型鑄模。模型鑄模本身將經修改以在主閘之頂部處形成一漏斗以允許材料流動至鑄模中且填充該鑄模。使用此特徵將允許更快/更多可重複循環時間,此將使零件間變化最小化。 本發明之一項態樣係一種用於由鈦或鈦合金進行單位晶格鑄造之方法。該方法包含:將一外部室抽空以形成一經抽空外部室,其中含有一鈦合金鑄錠之一陶瓷坩堝定位於該外部室中。該方法亦包含:將一經加壓氣體注入至該經抽空外部室中以形成一經加壓外部室。該方法亦包含:利用由圍繞該陶瓷坩堝定位之一感應線圈產生之感應加熱使該陶瓷坩堝內之該鈦合金鑄錠熔化。該方法亦包含:將該內部室抽空以形成一經抽空內部室,其中一鑄模定位於該內部室內之該模型鑄模支架內。該方法亦包含:使用該外部室與該內部室之間所形成之一壓差將該經完全熔化鈦合金材料自該坩堝轉移至該鑄模中。該感應線圈中所產生之一頻率介於自1千赫至50千赫之範圍內,且一功率介於自15千瓦至50千瓦之範圍內。該經抽空內部室之一大氣壓力介於自3×10-2 大氣壓至9.87×10-7 大氣壓之範圍內。該經抽空內部室之一大氣壓力介於自9.87×10-7 大氣壓至9.87×10-13 大氣壓之範圍內。 該方法進一步包括:使用定位於該內部室內之一紅外線加熱單元來加熱該鑄模以形成一經加熱鑄模。該方法進一步包括:使該鈦合金在該鑄模內冷卻。 本發明之另一態樣係一種用於由鈦或鈦合金進行單位晶格鑄造之系統,該系統包括:一外部室;一陶瓷坩堝,其定位於該外部室內;一感應線圈,其圍繞該陶瓷坩堝之一底部區段而定位;一內部室,其定位於該外部室內;一模型鑄模支架,其位於該內部室內;及一鑄模,其定位於該內部室內之該模型鑄模支架內。該外部室經抽空以形成一經抽空外部室,其中該陶瓷坩堝含有定位於其中之一鈦合金鑄錠。一經加壓氣體被注入至該經抽空外部室中以形成一經加壓外部室。該鈦合金鑄錠利用由圍繞該陶瓷坩堝定位之該感應線圈產生之感應加熱而在該陶瓷坩堝內被熔化。該內部室經抽空以形成一經抽空內部室。該鈦合金材料使用該外部室與該內部室之間所形成之一壓差自該坩堝完全轉移至該鑄模中。 該經加壓氣體較佳地為氬氣。該鑄模較佳地用一高嶺棉絕緣材料覆蓋。該鑄模較佳地係用於一薄壁式高爾夫球桿頭。該鑄模替代地係用於具有小於0.250英吋之一壁厚度之一物品。感應熔化時間較佳地介於自30秒至90秒之範圍內。該陶瓷坩堝較佳地由兩個基於氧化釔之主要坩堝層構成,其中一第一主要坩堝層具有介於自0.010英吋至0.060英吋之範圍內之一厚度,且一第二主要坩堝層具有介於自0.001英吋至0.020英吋之範圍內之一厚度。該陶瓷坩堝進一步包括一個基於二氧化矽之加固層。該感應線圈較佳地圍繞該陶瓷坩堝之一底部區段而定位。該感應線圈替代地圍繞該陶瓷坩堝之一上部區段而定位。 已簡明地闡述了本發明,當連同附圖一起時,熟習此項技術者自本發明之以下詳細說明將認識到本發明之以上及其他目標、特徵及優點。Currently, the loading of the preheated mold mold occurs between the preheating furnace and the foundry furnace. The model mold itself is currently attached to the underside of the top panel of the inner chamber using a forked wedge. The top plate, which is attached to the mold, is then inverted and placed onto the inner chamber body. In order to reduce the time required to load the model mold (thus minimizing heat loss) and to reduce the chance of damage to the model mold (caused by stress caused by damage during wedges and/or transport), a bracket should be used Support the mold. The stent will be formed in the inner chamber and specially designed to hold and orient the model. The model mold itself will be modified to form a funnel at the top of the main gate to allow material to flow into the mold and fill the mold. Using this feature will allow faster/more repeatable cycle times, which will minimize variations between parts. One aspect of the invention is a method for unit cell casting from titanium or a titanium alloy. The method includes evacuating an outer chamber to form an evacuated outer chamber, wherein a ceramic crucible containing one of the titanium alloy ingots is positioned in the outer chamber. The method also includes injecting a pressurized gas into the evacuated outer chamber to form a pressurized outer chamber. The method also includes melting the titanium alloy ingot in the ceramic crucible by induction heating generated by an induction coil positioned around the ceramic crucible. The method also includes evacuating the interior chamber to form an evacuated interior chamber, wherein a mold is positioned within the mold holder of the interior chamber. The method also includes transferring the fully melted titanium alloy material from the crucible into the mold using a pressure differential formed between the outer chamber and the inner chamber. One of the frequencies generated in the induction coil is in the range from 1 kHz to 50 kHz, and a power is in the range from 15 kW to 50 kW. The atmospheric pressure of one of the evacuated internal chambers ranges from 3 x 10 -2 atmospheres to 9.87 x 10 -7 atmospheres. The atmospheric pressure of one of the evacuated internal chambers ranges from 9.87 x 10 -7 atmospheres to 9.87 x 10 -13 atmospheres. The method further includes heating the mold using an infrared heating unit positioned within the interior chamber to form a heated mold. The method further includes cooling the titanium alloy within the mold. Another aspect of the invention is a system for unit lattice casting from titanium or a titanium alloy, the system comprising: an outer chamber; a ceramic crucible positioned in the outer chamber; an induction coil surrounding the The ceramic crucible is positioned in a bottom section; an interior chamber positioned in the outer chamber; a model mold holder positioned within the interior chamber; and a mold positioned within the model mold holder in the interior chamber. The outer chamber is evacuated to form an evacuated outer chamber, wherein the ceramic crucible contains a titanium alloy ingot positioned therein. A pressurized gas is injected into the evacuated outer chamber to form a pressurized outer chamber. The titanium alloy ingot is melted in the ceramic crucible by induction heating generated by the induction coil positioned around the ceramic crucible. The interior chamber is evacuated to form an evacuated interior chamber. The titanium alloy material is completely transferred from the crucible into the mold using a pressure difference formed between the outer chamber and the inner chamber. The pressurized gas is preferably argon. The mold is preferably covered with a kaolin insulation material. The mold is preferably used in a thin walled golf club head. The mold is instead used for an article having a wall thickness of less than 0.250 inches. The induction melting time is preferably in the range of from 30 seconds to 90 seconds. The ceramic crucible preferably consists of two main ruthenium layers based on ruthenium oxide, wherein a first major ruthenium layer has a thickness ranging from 0.010 ft to 0.060 ft, and a second major ruthenium layer It has a thickness ranging from 0.001 inches to 0.020 inches. The ceramic crucible further includes a reinforcing layer based on cerium oxide. The induction coil is preferably positioned around a bottom section of the ceramic crucible. The induction coil is instead positioned around an upper section of the ceramic crucible. The above and other objects, features and advantages of the present invention will become apparent from the <RTIgt;
如圖1中所展示,一單位晶格之鈦鑄造系統5包括一外部容器44、一內部容器39、一真空機構60、一坩堝10、一感應線圈15、一線圈電產生機構25及一鑄模30。外部容器44界定一外部室45。內部容器39界定一內部室40。真空機構60包含一真空管線71、一真空連接器70以及壓力計75a及75b。真空機構60用於抽空並加壓外部室45及內部室40以便在內部室40與外部室45之間形成一壓差。 坩堝10較佳地由一陶瓷材料構成。在一最佳實施例中,坩堝10由一第一層11a、一第二層11b及一基於二氧化矽之第三層11c構成,如圖7中所展示。一金屬鑄錠20放置於坩堝10之內部內。金屬鑄錠20較佳地係一鈦合金材料。坩堝10之體積較佳地對應於形成物品所需之金屬量。該坩堝10之內部較佳地具有介於自15公分(「cm」)至90 cm之範圍內、更佳地介於自35 cm至60 cm之範圍內之一直徑。坩堝10之一高度較佳地介於自30 cm至200 cm之範圍內且更佳地介於自60 cm至100 cm之範圍內。 一連接噴嘴27連接於坩堝10之一底部開口(未展示)與鑄模30之一開口之間。連接噴嘴27允許經熔化金屬材料自鑄錠20流動至鑄模30中以用於鑄造物品。特定而言,連接噴嘴27之大小係基於鑄模30之腔之大小及形狀而判定,且較佳地介於自5 cm至100 cm之範圍內,且更佳地介於自15 cm至50 cm之範圍內。 感應線圈15圍繞坩堝10而纏繞。感應線圈15經激勵以產生一電磁力以使坩堝10內之金屬鑄錠20 (例如,鈦合金鑄錠)熔化。線圈電產生機構25給感應線圈15提供電力。如圖2中所展示,感應線圈15圍繞坩堝10之一底部區段10b而纏繞。此首先使鑄錠20之底部熔化。如圖2A中所展示,感應線圈15圍繞坩堝10之一上部區段10a而纏繞。此首先使鑄錠20之頂部熔化。 為使目標材料圍繞一陶瓷坩堝10之端口進行密封之能力最佳化,感應線圈15較佳地以鑄錠20之上部三分之一為中心。此定位允許感應線圈15首先對鑄錠20之上部部分起作用(使材料自上至下地熔化),從而致使經熔化材料圍繞仍固態之鑄錠20而落下且在感應線圈15之電磁力影響其餘材料之前形成一密封。 替代地,為充分利用感應線圈15之電磁力(包含對熔體之電磁攪拌),感應線圈15被朝向陶瓷坩堝10之底部10b而定位。此定位允許一均勻熔體作為經熔化材料落在其自身上並且增加傾倒之均質性,此乃因在經熔化材料被自坩堝10抽空之前,電磁力可較佳地對經熔化材料起作用。 鈦合金之鑄錠20之熔化係在用於感應熔化之一真空條件下實施。感應線圈15連接至線圈電產生機構25。 陶瓷坩堝10用於鈦合金之真空感應熔化。陶瓷材料不干擾電磁力之場效應,且由感應線圈15產生之電磁感應能量被充分集中用於使鈦合金鑄錠熔化。 在圖2B中所展示之一實施例中,一絕緣材料31圍繞鑄模30而纏繞,在鑄造期間,模型鑄模在使用之前先被預加熱以便改良材料至鑄模本身中之流動且更好地允許鑄模30完全地填充。由於鈦材料之本質及熔化製程本身,因此愈使熱量損失最小化,材料在凝固之前必須流動及填充鑄模30之時間愈長。為此,模型鑄模熱量透過使用一絕緣材料31 (例如:高嶺棉)而得以保存,藉此延長鑄模30在傾倒之前的使用週期且允許更好地進行填充,包含填充較困難之鑄模(例如,薄壁式鑄件)。 如圖3A、圖3B、圖3C、圖3D及圖3E中所展示,鑄模30在一爐80中被預加熱。在單位晶格鑄造期間,模型鑄模30在使用之前先被預加熱以便改良改良材料至鑄模30本身中之流動且更好地允許鑄模30完全地填充。由於鈦材料之本質及熔化製程本身,因此在鑄模30之溫度與填充複雜及/或薄壁式模型鑄模30之能力之間存在一可能相關性。溫度測試包含1050℃、1060℃、1100℃、1150℃、1200℃、1250℃及1260℃。經預加熱鑄模被自80移除且被附接至內部容器39之一蓋35。 在圖3F中所展示之一替代實施例中,在內部室40內使用紅外線加熱器50a及50b來維持鑄模30之熱量。由於鈦材料之本質及熔化製程本身,因此愈使熱量損失最小化,材料在凝固之前可流動及填充鑄模30之時間愈長。為此,模型鑄模熱量透過使用放置於內部容器39之內部室40之內部壁內之紅外線加熱器50a及50b而得以保存,以便使模型鑄模之冷卻最小化且改良鑄造複雜及/或薄壁式零件之能力。 圖4、圖4A及圖4B圖解說明在外部室45與內部室40之間使用一壓差來幫助使經熔化鈦合金材料流動至一鑄模30中之鑄造製程。 圖5圖解說明與單位晶格鑄造系統5一起利用之一可程式化邏輯電腦(「PLC」)及操作者電腦91。 圖6係一單位晶格鑄造方法600之一方塊圖。在步驟601處,一鑄錠20經製備以用於鑄造。單個鑄錠20用於製造一單個物品,諸如一高爾夫球桿頭29。不同於在一單個製程中製造多個物品(此產生材料損失),本發明在每一製程中僅製造一單個物品。在步驟602處,在一爐中預加熱鑄模30。在步驟603處,將外部室45抽空。在步驟604處,利用一氬氣氣體對外部室45進行加壓。在步驟605處,將內部室40抽空。在步驟606處,激勵感應線圈15,且在步驟607處,在坩堝10內使鑄錠20熔化。在步驟608處,經熔化材料流動至鑄模30中。在步驟609處,發生脫模製程。在步驟610處,完成物品(高爾夫球桿頭) 29。該感應線圈中所產生之一頻率介於自1千赫至50千赫之範圍內,且一功率介於自15千瓦至50千瓦之範圍內。該經抽空內部室之一大氣壓力介於自3×10-2 大氣壓至9.87×10-7 大氣壓之範圍內。該經抽空內部室之一大氣壓力介於自9.87×10-7 大氣壓至9.87×10-13 大氣壓之範圍內。 如圖7中所展示,第一層11a及第二層11b較佳地由氧化釔及其他材料構成。氧化釔在一高溫環境中對鈦係高度惰性的,因而在兩種材料之間不發生化學反應。氧化釔在熔化製程期間亦隔離陶瓷材料與鈦以防止陶瓷材料與鈦之間發生反應以確保鈦合金之平穩熔化。坩堝10之第三層11c較佳地由二氧化矽及其他材料構成。二氧化矽在熔化製程期間抵製金屬膨脹及熱應力以確保坩堝之強度。 第一層11a之一較佳厚度係自0.5 mm至1.5 mm且坩堝10之較佳厚度範圍係自5 mm至15 mm。 圖8中展示用於由鈦或鈦合金進行單位晶格鑄造之一方法800。在方塊801處,將一外部室抽空以形成一經抽空外部室,其中含有一鈦合金鑄錠之一陶瓷坩堝定位於該外部室中。在方塊802處,將一經加壓氣體注入至經抽空外部室中以形成一經加壓外部室。在方塊803處,利用由圍繞陶瓷坩堝定位之一感應線圈產生之感應加熱使陶瓷坩堝內之鈦合金鑄錠熔化。在方塊804處,將內部室抽空以形成一經抽空內部室,其中一鑄模定位於內部室內。在方塊805處,使用外部室與內部室之間所形成之一壓差將經完全熔化鈦合金材料自坩堝轉移至鑄模中。As shown in FIG. 1, a unit cell titanium casting system 5 includes an outer container 44, an inner container 39, a vacuum mechanism 60, a crucible 10, an induction coil 15, a coil electric generating mechanism 25, and a mold. 30. The outer container 44 defines an outer chamber 45. The inner container 39 defines an interior chamber 40. The vacuum mechanism 60 includes a vacuum line 71, a vacuum connector 70, and pressure gauges 75a and 75b. The vacuum mechanism 60 is for evacuating and pressurizing the outer chamber 45 and the inner chamber 40 to form a pressure difference between the inner chamber 40 and the outer chamber 45. The crucible 10 is preferably constructed of a ceramic material. In a preferred embodiment, the crucible 10 is comprised of a first layer 11a, a second layer 11b, and a third layer 11c based on ceria, as shown in FIG. A metal ingot 20 is placed inside the crucible 10. The metal ingot 20 is preferably a titanium alloy material. The volume of the crucible 10 preferably corresponds to the amount of metal required to form the article. The interior of the crucible 10 preferably has a diameter ranging from 15 cm ("cm") to 90 cm, more preferably from 35 cm to 60 cm. One of the heights of the crucible 10 is preferably in the range of from 30 cm to 200 cm and more preferably in the range of from 60 cm to 100 cm. A connecting nozzle 27 is coupled between one of the bottom openings (not shown) of the crucible 10 and one of the openings of the mold 30. The connecting nozzles 27 allow molten metal material to flow from the ingot 20 into the mold 30 for casting the article. In particular, the size of the attachment nozzle 27 is determined based on the size and shape of the cavity of the mold 30, and preferably ranges from 5 cm to 100 cm, and more preferably from 15 cm to 50 cm. Within the scope. The induction coil 15 is wound around the crucible 10. The induction coil 15 is energized to generate an electromagnetic force to melt the metal ingot 20 (e.g., titanium alloy ingot) in the crucible 10. The coil electric generating mechanism 25 supplies electric power to the induction coil 15. As shown in FIG. 2, the induction coil 15 is wound around one of the bottom sections 10b of the crucible 10. This first melts the bottom of the ingot 20. As shown in FIG. 2A, the induction coil 15 is wound around one of the upper sections 10a of the crucible 10. This first melts the top of the ingot 20. In order to optimize the ability of the target material to seal around the port of a ceramic crucible 10, the induction coil 15 is preferably centered about one third of the upper portion of the ingot 20. This positioning allows the induction coil 15 to first act on the upper portion of the ingot 20 (melting the material from top to bottom), causing the molten material to fall around the still solid ingot 20 and the electromagnetic force on the induction coil 15 affecting the rest. A seal is formed before the material. Alternatively, to fully utilize the electromagnetic force of the induction coil 15 (including electromagnetic stirring of the melt), the induction coil 15 is positioned toward the bottom 10b of the ceramic crucible 10. This positioning allows a uniform melt to fall on itself as a molten material and increase the homogeneity of the pour, since the electromagnetic force preferably acts on the molten material before the molten material is evacuated from the crucible 10. The melting of the titanium alloy ingot 20 is carried out under vacuum conditions for induction melting. The induction coil 15 is connected to the coil electric generating mechanism 25. The ceramic crucible 10 is used for vacuum induction melting of titanium alloy. The ceramic material does not interfere with the field effect of the electromagnetic force, and the electromagnetic induction energy generated by the induction coil 15 is sufficiently concentrated to melt the titanium alloy ingot. In one embodiment shown in Figure 2B, an insulating material 31 is wrapped around the mold 30. During casting, the mold is preheated prior to use to improve the flow of material into the mold itself and to better allow the mold to be molded. 30 is completely filled. Due to the nature of the titanium material and the melting process itself, the resulting heat loss is minimized, and the longer the material must flow and fill the mold 30 prior to solidification. To this end, the mold mold heat is preserved by using an insulating material 31 (e.g., kaolin), thereby extending the life cycle of the mold 30 prior to pouring and allowing for better filling, including castings that are more difficult to fill (e.g., Thin-walled castings). As shown in Figures 3A, 3B, 3C, 3D and 3E, the mold 30 is preheated in a furnace 80. During unit cell casting, the mold mold 30 is preheated prior to use to improve the flow of the modified material into the mold 30 itself and better allow the mold 30 to be completely filled. Due to the nature of the titanium material and the melting process itself, there is a possible correlation between the temperature of the mold 30 and the ability to fill the complex and/or thin-walled model mold 30. The temperature test includes 1050 ° C, 1060 ° C, 1100 ° C, 1150 ° C, 1200 ° C, 1250 ° C and 1260 ° C. The preheated mold is removed from 80 and attached to one of the lids 35 of the inner container 39. In an alternate embodiment shown in FIG. 3F, infrared heaters 50a and 50b are used within internal chamber 40 to maintain the heat of mold 30. Due to the nature of the titanium material and the melting process itself, the resulting heat loss is minimized, and the longer the material can flow and fill the mold 30 prior to solidification. To this end, the mold mold heat is preserved by using the infrared heaters 50a and 50b placed in the inner wall of the inner chamber 40 of the inner container 39 to minimize the cooling of the mold and improve the casting complexity and/or thin wall. The ability of the part. 4, 4A, and 4B illustrate a casting process that uses a pressure differential between the outer chamber 45 and the inner chamber 40 to help flow the molten titanium alloy material into a mold 30. FIG. 5 illustrates the use of a programmable logic computer ("PLC") and an operator computer 91 in conjunction with a unit cell casting system 5. Figure 6 is a block diagram of a unit cell casting method 600. At step 601, an ingot 20 is prepared for casting. A single ingot 20 is used to make a single item, such as a golf club head 29. Unlike the manufacture of multiple articles in a single process (which results in material loss), the present invention produces only a single article in each process. At step 602, the mold 30 is preheated in a furnace. At step 603, the outer chamber 45 is evacuated. At step 604, the outer chamber 45 is pressurized with an argon gas. At step 605, the interior chamber 40 is evacuated. At step 606, the induction coil 15 is energized, and at step 607, the ingot 20 is melted within the crucible 10. At step 608, the molten material flows into the mold 30. At step 609, a demolding process occurs. At step 610, the item (golf club head) 29 is completed. One of the frequencies generated in the induction coil is in the range from 1 kHz to 50 kHz, and a power is in the range from 15 kW to 50 kW. The atmospheric pressure of one of the evacuated internal chambers ranges from 3 x 10 -2 atmospheres to 9.87 x 10 -7 atmospheres. The atmospheric pressure of one of the evacuated internal chambers ranges from 9.87 x 10 -7 atmospheres to 9.87 x 10 -13 atmospheres. As shown in Figure 7, the first layer 11a and the second layer 11b are preferably constructed of yttria and other materials. Cerium oxide is highly inert to titanium in a high temperature environment and thus does not chemically react between the two materials. Cerium oxide also isolates the ceramic material from the titanium during the melting process to prevent reaction between the ceramic material and the titanium to ensure smooth melting of the titanium alloy. The third layer 11c of the crucible 10 is preferably composed of ceria and other materials. Cerium oxide resists metal expansion and thermal stress during the melting process to ensure the strength of the crucible. One of the first layers 11a preferably has a thickness of from 0.5 mm to 1.5 mm and a preferred thickness of the crucible 10 ranges from 5 mm to 15 mm. One method 800 for unit cell casting from titanium or a titanium alloy is shown in FIG. At block 801, an outer chamber is evacuated to form an evacuated outer chamber in which a ceramic crucible containing one of the titanium alloy ingots is positioned. At block 802, a pressurized gas is injected into the evacuated outer chamber to form a pressurized outer chamber. At block 803, the titanium alloy ingot in the ceramic crucible is melted using induction heating generated by an induction coil positioned around the ceramic crucible. At block 804, the interior chamber is evacuated to form an evacuated interior chamber, with a mold positioned within the interior chamber. At block 805, a fully melted titanium alloy material is transferred from the crucible to the mold using a pressure differential formed between the outer chamber and the inner chamber.
5‧‧‧單位晶格之鈦鑄造系統/單位晶格鑄造系統/系統
10‧‧‧坩堝/陶瓷坩堝
10a‧‧‧上部區段
10b‧‧‧底部區段/底部
11a‧‧‧第一層
11b‧‧‧第二層
11c‧‧‧基於二氧化矽之第三層/第三層
15‧‧‧感應線圈
20‧‧‧金屬鑄錠/鑄錠/仍固態之鑄錠
25‧‧‧線圈電產生機構
27‧‧‧連接噴嘴
29‧‧‧高爾夫球桿頭/物品
30‧‧‧鑄模/模型鑄模/複雜及/或薄壁式模型鑄模
31‧‧‧絕緣材料
35‧‧‧蓋
39‧‧‧內部容器
40‧‧‧內部室/經抽空內部室
44‧‧‧外部容器
45‧‧‧外部室/經抽空外部室/經加壓外部室
50a‧‧‧紅外線加熱器
50b‧‧‧紅外線加熱器
60‧‧‧真空機構
70‧‧‧真空連接器
71‧‧‧真空管線
75a‧‧‧壓力計
75b‧‧‧壓力計
80‧‧‧爐
91‧‧‧操作者電腦
5‧‧‧Unit Titanium Casting System / Unit Lattice Casting System / System
10‧‧‧坩埚/ceramics
10a‧‧‧ upper section
10b‧‧‧Bottom section/bottom
11a‧‧‧ first floor
11b‧‧‧ second floor
11c‧‧‧3rd/third layer based on cerium oxide
15‧‧‧Induction coil
20‧‧‧Metal ingots/ingots/still solid ingots
25‧‧‧ coil electric generating mechanism
27‧‧‧Connecting nozzle
29‧‧‧Golf club head/items
30‧‧‧Mold/Model Mold/Complex and/or Thin Wall Model Mold
31‧‧‧Insulation materials
35‧‧‧ Cover
39‧‧‧Internal containers
40‧‧‧Internal room/evacuated interior room
44‧‧‧External containers
45‧‧‧External room/extracted external room/pressurized external room
50a‧‧‧Infrared heater
50b‧‧‧Infrared heater
60‧‧‧vacuum mechanism
70‧‧‧vacuum connector
71‧‧‧vacuum pipeline
75a‧‧‧ pressure gauge
75b‧‧‧ pressure gauge
80‧‧‧ furnace
91‧‧‧Operator computer
圖1係一單位晶格鑄造系統之一圖解。 圖2係單位晶格鑄造系統之一內部室、坩堝、感應線圈及鑄模之一單獨視圖,其展示感應線圈放置於坩堝之一下部區段處。 圖2A係單位晶格鑄造系統之一內部室、坩堝、感應線圈及鑄模之一單獨視圖,其展示感應線圈放置於坩堝之一上部區段處。 圖2B係單位晶格鑄造系統之一內部室、坩堝、感應線圈及鑄模之一單獨視圖,其展示圍繞鑄模而纏繞一絕緣材料。 圖3A係一技術人員在一爐中預加熱一鑄模之一圖解。 圖3B係一技術人員將經預加熱鑄模附接至內部容器之一蓋之一圖解。 圖3C係一技術人員將蓋附接至內部容器之一圖解。 圖3D係內部容器之一單獨視圖。 圖3E係內部容器之蓋之一單獨視圖。 圖3F係內部容器之內部室之一單獨視圖,其展示紅外線加熱器。 圖4係一外部室抽空步驟期間之一單位晶格鑄造系統之一圖解。 圖4A係一外部室加壓步驟期間之一單位晶格鑄造系統之一圖解。 圖4B係一鑄錠熔化步驟期間之一單位晶格鑄造系統之一圖解。 圖5係用於一單位晶格鑄造系統之一PLC單元及電腦之一圖解。 圖6係一單位晶格鑄造方法之一方塊圖。 圖7係用於一單位晶格鑄造系統之一坩堝之一單獨視圖。 圖8係用於單位晶格之鈦鑄造之一方法之一流程圖。Figure 1 is an illustration of one unit of a lattice casting system. 2 is a separate view of one of the interior chambers, turns, induction coils, and molds of a unitary lattice casting system showing the induction coils placed at a lower section of the crucible. 2A is a separate view of one of the interior chambers, turns, induction coils, and molds of a unitary lattice casting system showing the induction coil placed at an upper section of the crucible. 2B is a separate view of one of the interior chambers, crucibles, induction coils, and molds of one of the unit cell casting systems, showing an insulating material wrapped around the mold. Figure 3A is a diagram of one of the technicians preheating a mold in a furnace. Figure 3B is an illustration of one of the technicians attaching a preheated mold to one of the inner containers. Figure 3C is an illustration of one of the technicians attaching a lid to an inner container. Figure 3D is a separate view of one of the internal containers. Figure 3E is a separate view of one of the covers of the inner container. Figure 3F is a separate view of one of the interior compartments of the inner container showing an infrared heater. Figure 4 is an illustration of one of the unit cell casting systems during an external chamber evacuation step. Figure 4A is an illustration of one of the unit cell casting systems during an external chamber pressurization step. Figure 4B is an illustration of one of the unitary lattice casting systems during an ingot melting step. Figure 5 is an illustration of one of the PLC units and computers used in a unit cell casting system. Figure 6 is a block diagram of a unit cell casting method. Figure 7 is a separate view of one of the unitary lattice casting systems. Figure 8 is a flow chart of one of the methods for titanium casting in a unit cell.
5‧‧‧單位晶格之鈦鑄造系統/單位晶格鑄造系統/系統 5‧‧‧Unit Titanium Casting System / Unit Lattice Casting System / System
10‧‧‧坩堝/陶瓷坩堝 10‧‧‧坩埚/ceramics
15‧‧‧感應線圈 15‧‧‧Induction coil
20‧‧‧金屬鑄錠/鑄錠/仍固態之鑄錠 20‧‧‧Metal ingots/ingots/still solid ingots
25‧‧‧線圈電產生機構 25‧‧‧ coil electric generating mechanism
30‧‧‧鑄模/模型鑄模/複雜及/或薄壁式模型鑄模 30‧‧‧Mold/Model Mold/Complex and/or Thin Wall Model Mold
39‧‧‧內部容器 39‧‧‧Internal containers
40‧‧‧內部室/經抽空內部室 40‧‧‧Internal room/evacuated interior room
44‧‧‧外部容器 44‧‧‧External containers
45‧‧‧外部室/經抽空外部室/經加壓外部室 45‧‧‧External room/extracted external room/pressurized external room
60‧‧‧真空機構 60‧‧‧vacuum mechanism
70‧‧‧真空連接器 70‧‧‧vacuum connector
71‧‧‧真空管線 71‧‧‧vacuum pipeline
75a‧‧‧壓力計 75a‧‧‧ pressure gauge
75b‧‧‧壓力計 75b‧‧‧ pressure gauge
Claims (20)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US201662319215P | 2016-04-06 | 2016-04-06 | |
| US201662318854P | 2016-04-06 | 2016-04-06 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| TW201738389A true TW201738389A (en) | 2017-11-01 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| TW106111607A TW201738389A (en) | 2016-04-06 | 2017-04-06 | Unit cell titanium casting |
Country Status (3)
| Country | Link |
|---|---|
| EP (1) | EP3439814B1 (en) |
| CN (1) | CN108883463A (en) |
| TW (1) | TW201738389A (en) |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116274895B (en) * | 2023-03-23 | 2023-11-07 | 陕西天成航空材料有限公司 | Preparation method of titanium alloy cast ingot with uniform components |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4478270A (en) * | 1981-04-01 | 1984-10-23 | Interlake, Inc. | Apparatus for casting low-density alloys |
| US5193607A (en) * | 1990-05-15 | 1993-03-16 | Daido Tokushuko K.K. | Method for precision casting of titanium or titanium alloy |
| RU2036049C1 (en) * | 1991-03-19 | 1995-05-27 | Всероссийский научно-исследовательский институт авиационных материалов | Plant for making oriented-crystallization castings |
| JP2842417B2 (en) * | 1996-11-28 | 1999-01-06 | 三菱マテリアル株式会社 | Golf club head |
| RU2300443C1 (en) * | 2005-09-15 | 2007-06-10 | Федеральное государственное унитарное предприятие "Московское машиностроительное производственное предприятие "Салют" | Apparatus for casting in vacuum |
| CN104646647B (en) * | 2015-01-16 | 2017-03-15 | 北京嘉毅万思科技发展有限公司 | Titanium-base alloy induction melting leakage type suction pouring equipment and control method |
| CN204584231U (en) * | 2015-01-16 | 2015-08-26 | 马旭东 | Titanium-base alloy induction melting leakage type suction pouring equipment |
-
2017
- 2017-04-04 CN CN201780021450.0A patent/CN108883463A/en active Pending
- 2017-04-04 EP EP17779664.6A patent/EP3439814B1/en active Active
- 2017-04-06 TW TW106111607A patent/TW201738389A/en unknown
Also Published As
| Publication number | Publication date |
|---|---|
| EP3439814A1 (en) | 2019-02-13 |
| CN108883463A (en) | 2018-11-23 |
| EP3439814B1 (en) | 2020-12-09 |
| EP3439814A4 (en) | 2019-09-18 |
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