TWI648410B - Method for fabricating aluminum-fly ash composite material - Google Patents

Method for fabricating aluminum-fly ash composite material Download PDF

Info

Publication number
TWI648410B
TWI648410B TW107119010A TW107119010A TWI648410B TW I648410 B TWI648410 B TW I648410B TW 107119010 A TW107119010 A TW 107119010A TW 107119010 A TW107119010 A TW 107119010A TW I648410 B TWI648410 B TW I648410B
Authority
TW
Taiwan
Prior art keywords
fly ash
aluminum
manufacturing
composite material
screen
Prior art date
Application number
TW107119010A
Other languages
Chinese (zh)
Other versions
TW202003872A (en
Inventor
莊水旺
Original Assignee
國立臺灣海洋大學
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 國立臺灣海洋大學 filed Critical 國立臺灣海洋大學
Priority to TW107119010A priority Critical patent/TWI648410B/en
Application granted granted Critical
Publication of TWI648410B publication Critical patent/TWI648410B/en
Publication of TW202003872A publication Critical patent/TW202003872A/en

Links

Landscapes

  • Processing Of Solid Wastes (AREA)

Abstract

利用習知技術所揭示的製造方法製得的鋁基飛灰鑄件,其通常具有過多的孔隙或氣孔,造成其機械性質下降或不佳。有鑑於此,本發明提出一種鋁基飛灰複合材料之製造方法。本發明之製造方法係特別地以浮篩與磁篩的方式完成對飛灰粗篩與精篩處理,接著再將完成預熱的飛灰批次性地添加入熔融狀態的鋁基材內,最後再利用模浸速固法將混有飛灰的鋁熔湯加工成鋁基飛灰鑄件。並且,實驗數據顯示,本發明所提出的鋁基飛灰複合材料之製造方法的確有助於降低鋁基飛灰鑄件的孔隙率並維持或增強其機械性質。Aluminum-based fly ash castings produced by the manufacturing methods disclosed by the prior art generally have excessive pores or pores, resulting in a decrease or poor mechanical properties. In view of this, the present invention provides a method of manufacturing an aluminum-based fly ash composite. The manufacturing method of the present invention specifically completes the coarse ash screening and the fine screening treatment of the fly ash by means of a floating sieve and a magnetic sieve, and then batch-adds the preheated fly ash into the molten aluminum substrate. Finally, the aluminum melt mixed with fly ash is processed into an aluminum-based fly ash casting by a die immersion quick-solid method. Moreover, experimental data shows that the method of manufacturing the aluminum-based fly ash composite proposed by the present invention does contribute to reducing the porosity of the aluminum-based fly ash casting and maintaining or enhancing its mechanical properties.

Description

鋁基飛灰複合材料之製造方法Aluminum-based fly ash composite material manufacturing method

本發明係關於鋁基-飛灰(Aluminum-Fly Ash, ALFA)複合材料的技術領域,尤指能夠降低內部孔隙並增強機械性質的一種鋁基飛灰複合材料之製造方法。The present invention relates to the technical field of aluminum-fly ash (ALFA) composite materials, and more particularly to a method for manufacturing an aluminum-based fly ash composite material capable of reducing internal pores and enhancing mechanical properties.

金屬基複合材料(Metal Matrix Composite, MMC)係藉由將至少一種強化相材料固溶至一基相金屬或其合金之中而製得。其中,所述強化相材料多為無機非金屬材料,例如:陶瓷(即,金屬氧化物)、碳、矽、石墨、與硼。1993年,Pradeep K. Rohatgi 透過令燃煤廢棄物飛灰所包含的SiO 2與Fe 2O 3等氧化物成分與鋁基材產生化學反應,藉此生成氧化鋁(Al 2O 3)以作為鋁基材之強化相,而後製得鋁基飛灰複合材料(Fly-Ash-Containing Aluminum Matrix Composites)。 A metal matrix composite (MMC) is produced by solid-solving at least one reinforcing phase material into a base phase metal or an alloy thereof. Wherein, the reinforcing phase material is mostly an inorganic non-metal material, such as ceramic (ie, metal oxide), carbon, germanium, graphite, and boron. In 1993, Pradeep K. Rohatgi chemically reacted with an aluminum substrate such as SiO 2 and Fe 2 O 3 contained in fly ash from coal-fired waste, thereby producing alumina (Al 2 O 3 ) as The strengthening phase of the aluminum substrate, and then the Fly-Ash-Containing Aluminum Matrix Composites.

隨著材料製造技術的持續進步,目前鋁基飛灰複合材料的製程技術主要有壓力滲透法(Pressure infiltration)、粉末冶金法(Powder metallurgy)與複合鑄造法(Compocasting)。其中,因具有低製程成本的優點,複合鑄造法目前被廣泛地應用於鋁基飛灰複合材料的製造。文獻一即揭示應用複合鑄造法製造鋁基飛灰複合材料的有關技術。於此,文獻一指的是:莊水旺等人 ,“製程參數對飛灰在鋁基飛灰複合材料中均勻性之影響”,鑄造工程學刊,39卷1期 (2013 / 03 / 01),P22 - P28。吾人可根據文獻一得知現有的鋁基飛灰複合材料的製造流程包括以下步驟: 步驟(1):選用美國材料標準試驗協會(ASTM)之C618-12a標準規範所規定的F級飛灰,其中,透過X射線繞射分析(X-Ray Diffraction, XRD)可知所述飛灰包含:52.73%的SiO 2、26.87%的Al 2O 3及5.11%的Fe 2O 3; 步驟(2):對所述飛灰進行過篩,以篩選出顆粒大小介於53µm至106µm之間的飛灰; 步驟(3):酸洗飛灰以去除其雜質; 步驟(4):日本工業規格(Japanese Industrial Standards, JIS)所規範的ADC6鋁合金,其中,所述ADC6鋁合金的化學元素組成包括:0.45%的Si、3.15%的Mg、0.31%的Fe、0.17%的Mn、以及89.39%的Al; 步驟(5):將飛灰置於一高溫爐內並預熱至800 oC; 步驟(6):將ADC6鋁合金置於高週波熔解爐內,加熱至700 oC以熔解所述ADC6鋁合金成為一鋁熔湯; 步驟(7):使用攪拌設備以500 rpm的轉速攪拌該鋁熔湯,並於攪拌過程中以0.2 克/秒的流量將完成預熱的飛灰添加至所述鋁熔湯之中; 步驟(8):利用模浸速固法(Mold Immersed Rapid Solidification Process, MIRSP)將混有飛灰的鋁熔湯加工成一鋁基飛灰鑄件。 With the continuous advancement of material manufacturing technology, the current process technology of aluminum-based fly ash composites mainly includes Pressure infiltration, Powder metallurgy and Composing. Among them, the composite casting method is currently widely used in the manufacture of aluminum-based fly ash composite materials because of its low process cost. The literature first reveals the related technology of manufacturing aluminum-based fly ash composite materials by composite casting method. Here, the literature refers to: Zhuang Shuiwang et al., “The influence of process 參數 on the uniformity of fly ash in aluminum-based fly ash composites”, Journal of Foundry Engineering, Vol. 39, No. 1 (2013 / 03 / 01), P22 - P28. According to the literature 1, we can know that the existing aluminum-based fly ash composite manufacturing process includes the following steps: Step (1): Select the F-class fly ash specified in the American Standards Testing Association (ASTM) C618-12a standard specification. The X-ray Diffraction (XRD) shows that the fly ash comprises: 52.73% SiO 2 , 26.87% Al 2 O 3 and 5.11% Fe 2 O 3 ; Step (2): The fly ash is sieved to screen fly ash having a particle size between 53 μm and 106 μm; step (3): pickling fly ash to remove impurities thereof; step (4): Japanese Industrial Specification (Japanese Industrial) Standards, JIS) is an ADC6 aluminum alloy, wherein the chemical composition of the ADC6 aluminum alloy comprises: 0.45% Si, 3.15% Mg, 0.31% Fe, 0.17% Mn, and 89.39% Al; Step (5): placing the fly ash in a high temperature furnace and preheating to 800 o C; Step (6): placing the ADC6 aluminum alloy in a high frequency melting furnace and heating to 700 o C to melt the ADC6 aluminum The alloy becomes an aluminum melt; step (7): the aluminum melt is stirred at 500 rpm using a stirring device, and during the stirring process The preheated fly ash is added to the aluminum melt at a flow rate of 0.2 g/sec; Step (8): Mold Immersed Rapid Solidification Process (MIRSP) is used to mix the fly ash The aluminum melt soup is processed into an aluminum-based fly ash casting.

本案的發明人基於多年的鋁基飛灰複合材料的研究經驗發現,上述步驟(1)至步驟(8)雖然可獲得硬度高達58.13勃式硬度(BHN)的鋁基飛灰鑄件,然而此製造流程仍顯示出以下實務缺點: (1)飛灰顆粒的密度、形狀及粒徑會影響飛灰顆粒於鋁熔湯中的分散性,一次性的大量添加會導致飛灰於鋁熔湯之中發生群聚現象,令飛灰所含有的SiO 2、Al 2O 3及Fe 2O 3及氧化物難以與鋁熔湯進行反應; (2)承上述第1點,氧化物與鋁熔湯之間的反應不足最終係導致所獲得的鋁基飛灰鑄件具有過多的孔隙或氣孔,造成鋁基飛灰鑄件之機械性質下降。 The inventor of the present invention found that based on the research experience of aluminum-based fly ash composite materials for many years, the above steps (1) to (8) can obtain aluminum-based fly ash castings having a hardness of up to 58.13 Burgundy hardness (BHN). The process still shows the following practical shortcomings: (1) The density, shape and particle size of the fly ash particles will affect the dispersibility of the fly ash particles in the aluminum melt soup. A large amount of one-time addition will cause the fly ash to be in the aluminum melt soup. The phenomenon of clustering causes the SiO 2 , Al 2 O 3 and Fe 2 O 3 and oxides contained in the fly ash to be difficult to react with the aluminum melt; (2) According to the above point 1, the oxide and the aluminum melt soup Insufficient reaction between the two ultimately results in the resulting aluminum-based fly ash casting having too many voids or pores, resulting in a decrease in the mechanical properties of the aluminum-based fly ash casting.

由上述說明可知,如何設計出能夠製造低孔隙的鋁基飛灰鑄件的製造流程進行有效改良於是成為相當重要的課題。有鑑於此,本案之發明人係極力加以研究創作,而終於研發完成本發明之一種鋁基複合材料之製造方法。As apparent from the above description, how to design and manufacture an aluminum-based fly ash casting capable of producing low porosity and to effectively improve it has become a very important issue. In view of this, the inventors of the present invention have vigorously studied and created, and finally developed a method for manufacturing the aluminum-based composite material of the present invention.

利用習知技術所揭示的製造方法製得的鋁基飛灰鑄件,其通常具有過多的孔隙或氣孔,造成其機械性質下降。因此,本發明之主要目的在於提供一種鋁基飛灰複合材料的製造方法。本發明之製造方法係特別以浮篩與磁篩對飛灰進行粗篩與精篩之後,再接著讓完成預熱的飛灰批次性地添加入熔融狀態的鋁基材內,最後再利用模浸速固法將混有飛灰的鋁熔湯加工成鋁基飛灰鑄件。並且,實驗數據顯示,本發明所提出的鋁基飛灰複合材料之製造方法的確有助於降低鋁基飛灰鑄件的孔隙率並維持或增強其機械性質。Aluminum-based fly ash castings produced by the manufacturing methods disclosed by the prior art generally have excessive pores or pores, resulting in a decrease in mechanical properties. Accordingly, it is a primary object of the present invention to provide a method of making an aluminum-based fly ash composite. In the manufacturing method of the present invention, the fly ash is roughly sieved and finely sieved by a floating sieve and a magnetic sieve, and then the preheated fly ash is batch-added into the molten aluminum substrate, and finally reused. The die immersion quick-solid method processes the aluminum melt mixed with fly ash into an aluminum-based fly ash casting. Moreover, experimental data shows that the method of manufacturing the aluminum-based fly ash composite proposed by the present invention does contribute to reducing the porosity of the aluminum-based fly ash casting and maintaining or enhancing its mechanical properties.

為了達成上述本發明之主要目的,本案發明人係提供所述鋁基飛灰複合材料之製造方法的一實施例,係包括以下步驟: (1)備好飛灰與一鋁基材; (2)對所述飛灰進行一初篩處理,以篩選出顆粒大小介於53µm至106µm之間的飛灰; (3)對所述飛灰進行一前處理以去除其雜質; (4)對所述飛灰進行一精篩處理,以篩去含鐵量較高的飛灰; (5)對所述飛灰進行一高溫烘烤處理,以燒除飛灰內的雜質與未燃碳; (6)將所述飛灰置入一預熱裝置內,預熱至600-800oC; (7)將所述鋁基材置入一金屬熔解裝置內,並加熱至700-800oC使得該鋁基材成為一鋁熔湯; (8)使用一攪拌裝置攪拌該鋁熔湯,並於攪拌過程中以0.05-0.15克/秒的流量將完成預熱的飛灰添加至該鋁熔湯之中;以及 (9)利用模浸速固法(Mold Immersed Rapid Solidification Process, MIRSP)將混有飛灰的鋁熔湯加工成一鋁基飛灰鑄件。In order to achieve the above-mentioned main object of the present invention, the inventor of the present invention provides an embodiment of the method for manufacturing the aluminum-based fly ash composite material, which comprises the following steps: (1) preparing fly ash and an aluminum substrate; Performing a preliminary screening treatment on the fly ash to select fly ash having a particle size between 53 μm and 106 μm; (3) performing a pretreatment on the fly ash to remove impurities; (4) The fly ash is subjected to a fine screening treatment to remove the fly ash having a higher iron content; (5) performing a high temperature baking treatment on the fly ash to burn off impurities and unburned carbon in the fly ash; 6) placing the fly ash into a preheating device and preheating to 600-800 ° C; (7) placing the aluminum substrate into a metal melting device and heating to 700-800 ° C to make the aluminum substrate (a) agitating the aluminum melt using a stirring device, and adding the preheated fly ash to the aluminum melt at a flow rate of 0.05-0.15 g/sec during the stirring; (9) The aluminum fused soup mixed with fly ash is processed into an aluminum base by Mold Immersed Rapid Solidification Process (MIRSP) Fly ash castings.

對於本發明之鋁基飛灰複合材料之製造方法的實施例而言,於該步驟(7)之中,可將一鎂材料與所述鋁基材一起置入該金屬熔解裝置內,並加熱至700-800 oC使得所述鎂材料與該鋁基材熔融成為所述鋁熔湯。 In the embodiment of the method for manufacturing the aluminum-based fly ash composite material of the present invention, in the step (7), a magnesium material may be placed in the metal melting device together with the aluminum substrate, and heated. Up to 700-800 o C melts the magnesium material and the aluminum substrate into the aluminum melt.

對於本發明之鋁基飛灰複合材料之製造方法的實施例而言,於該步驟(8)之中,係基於一特定批次數將完成預熱的飛灰添加至該鋁熔湯之中,且該特定批次數係至少二次。並且,執行步驟(8)的過程中,係必須等待前一批次的飛灰與該鋁熔湯完成反應之後,再接著將下一批次的飛灰加入鋁熔湯之中。In the embodiment of the method for manufacturing the aluminum-based fly ash composite material of the present invention, in the step (8), the preheated fly ash is added to the aluminum melt soup based on a specific batch number. And the specific number of batches is at least two times. Moreover, during the execution of the step (8), it is necessary to wait for the previous batch of fly ash to complete the reaction with the aluminum melt, and then add the next batch of fly ash to the aluminum melt soup.

為了能夠更清楚地描述本發明所提出之一種鋁基飛灰複合材料之製造方法,以下將配合圖式,詳盡說明本發明之較佳實施例。In order to more clearly describe a method of manufacturing an aluminum-based fly ash composite material proposed by the present invention, a preferred embodiment of the present invention will be described in detail below with reference to the drawings.

請參閱圖1A與圖1B,係顯示本發明之一種鋁基飛灰複合材料之製造方法的流程圖。根據圖1A與圖1B可知,欲藉由所述鋁基飛灰複合材料之製造方法製作具有低孔隙率與優秀機械性質的鋁基飛灰複合材料,係須於流程上首先執行步驟(S1):備好飛灰與一鋁基材。繼續地,本發明之製造方法係接著執行步驟(S2):對所述飛灰進行一初篩處理,以篩選出顆粒大小介於53µm至106µm之間的飛灰。請同時參閱圖2所示的初篩裝置的立體圖以及圖3所示的步驟(S2)的細部流程圖。特別說明的是,本發明係以浮篩的方式完成步驟(S2),其包括以下細部步驟: 步驟(S21):備好一初篩裝置2,其中該初篩裝置2包括一容器20以及設置於該容器20內的一第一篩網21與一第二篩網22;並且,該第一篩網21的設置位置係高於該第二篩網22,且該第一篩網21的篩網孔徑大小係大於該第二篩網22的篩網孔徑大小; 步驟(S22):將所述飛灰倒入該容器20內,並將流動水注入該容器20內,利用流動水沖刷飛灰;以及 步驟(S23):透過該容器20的一排水埠23將流動水自該容器20排出,顆粒大小介於53µm至106µm之間的飛灰即被篩出於該第一篩網21與該第二篩網22之間。1A and 1B are flow charts showing a method of manufacturing an aluminum-based fly ash composite material of the present invention. 1A and FIG. 1B, it is known that an aluminum-based fly ash composite material having low porosity and excellent mechanical properties is to be produced by the method for manufacturing the aluminum-based fly ash composite material, and the first step (S1) is performed on the flow. : Prepare fly ash and an aluminum substrate. Continuing, the manufacturing method of the present invention is followed by the step (S2) of performing a preliminary screening treatment on the fly ash to screen fly ash having a particle size between 53 μm and 106 μm. Please also refer to the perspective view of the primary screening device shown in FIG. 2 and the detailed flow chart of the step (S2) shown in FIG. Specifically, the present invention completes the step (S2) in a floating screen manner, which includes the following detailed steps: Step (S21): Preparing a preliminary screening device 2, wherein the primary screening device 2 includes a container 20 and a setting a first screen 21 and a second screen 22 in the container 20; and the first screen 21 is disposed higher than the second screen 22, and the screen of the first screen 21 The mesh aperture size is larger than the mesh aperture size of the second screen 22; Step (S22): the fly ash is poured into the container 20, and flowing water is injected into the container 20, and the fly ash is washed with flowing water. And step (S23): the flowing water is discharged from the container 20 through a drain raft 23 of the container 20, and the fly ash having a particle size of between 53 μm and 106 μm is sieved out of the first screen 21 and Between the second screens 22.

必須強調的是,習知技術通常以篩選機對飛灰進行初篩處理,然而篩選機通常必須花費一定的時間(例如:45分鐘)才能夠自飛灰原料中篩選出顆粒大小介於53µm至106µm之間的飛灰。不同地,本發明自行設計初篩裝置2並搭配流動水沖刷飛灰,這樣的初篩處理可以在5分鐘內便自飛灰原料中篩選出顆粒大小介於53µm至106µm之間的飛灰。另外,必須特別強調本發明並不特別限制鋁基材的種類,其可以是含有鎂成分壓鑄鋁合金(Die-casting aluminum alloy),例如:日本工業規格(Japanese Industrial Standards, JIS)所規範的ADC6鋁合金、ADC10鋁合金與ADC12鋁合金。此外,熟悉鋁合金設計與製造的材料工程師應該知道,ZL系鋁合金也是含有鎂成分的鑄造鋁合金,例如:ZL101、ZL103、ZL105、ZL108、ZL109、ZL301、ZL305等。另一方面,本發明所使用的飛灰為美國材料標準試驗協會(ASTM)之C618-12a標準規範所規定的F級飛灰,經測定後可知其包含以下表(1)所列多種成分: 表(1) <TABLE border="1" borderColor="#000000" width="85%"><TBODY><tr><td> SiO<sub>2</sub></td><td> Al<sub>2</sub>O<sub>3</sub></td><td> Fe<sub>2</sub>O<sub>3</sub></td><td> 燒失量 (Loss on ignition, LOI) </td></tr><tr><td> 58.9% </td><td> 25.5% </td><td> 4.93% </td><td> 4.1% </td></tr></TBODY></TABLE>It must be emphasized that conventional techniques usually use a screening machine to screen the fly ash. However, it usually takes a certain time (for example, 45 minutes) to screen the fly ash material from 53 μm. Fly ash between 106 μm. Differently, the present invention designs the primary screening device 2 and flushes the fly ash with flowing water. Such a preliminary screening process can select fly ash having a particle size between 53 μm and 106 μm from the fly ash raw material within 5 minutes. In addition, it is necessary to particularly emphasize that the present invention does not particularly limit the kind of the aluminum substrate, and may be a Die-casting aluminum alloy containing a magnesium component, for example, an ADC6 specified by Japanese Industrial Standards (JIS). Aluminum alloy, ADC10 aluminum alloy and ADC12 aluminum alloy. In addition, material engineers familiar with the design and manufacture of aluminum alloys should know that ZL-based aluminum alloys are also cast aluminum alloys containing magnesium components, such as ZL101, ZL103, ZL105, ZL108, ZL109, ZL301, ZL305, and the like. On the other hand, the fly ash used in the present invention is a Class F fly ash specified by the American Society for Testing and Materials (ASTM) C618-12a standard specification, and it is determined that it contains various components listed in the following Table (1): Table 1)  <TABLE border="1" borderColor="#000000" width="85%"><TBODY><tr><td> SiO<sub>2</sub></td><td> Al<sub>2 </sub>O<sub>3</sub></td><td> Fe<sub>2</sub>O<sub>3</sub></td><td> Loss on ignition (Loss On ignition, LOI) </td></tr><tr><td> 58.9% </td><td> 25.5% </td><td> 4.93% </td><td> 4.1% </ Td></tr></TBODY></TABLE>

繼續地,製造方法的流程係接著執行步驟(S3):對所述飛灰進行一前處理以去除其雜質。飛灰前處理是指將對飛灰進行表面處理以增加其潔淨度,同時也改善飛灰顆粒與液相基材間的潤濕性。於本發明的步驟(S3)之中,係先以酸性溶液清洗所述飛灰,再接著使用純水對酸洗過後的飛灰進行沖洗。完成步驟(S3)之後,係接著執行步驟(S4):對所述飛灰進行一精篩處理以篩去含鐵量較高的飛灰。值得注意的是,步驟(S3)係分別以酸性溶液與純水清洗飛灰,因此完成步驟(S3)後所獲得的飛灰是呈現如泥巴的濕潤狀態,無法直接對其進行精篩處理。基於這個理由,執行步驟(S4)之前,必須先對所述飛灰執行一低溫烘烤處理,以除去其水分。Continuing, the flow of the manufacturing method is followed by step (S3): a pre-treatment of the fly ash to remove impurities thereof. Fly ash pretreatment refers to the surface treatment of fly ash to increase its cleanliness while also improving the wettability between the fly ash particles and the liquid phase substrate. In the step (S3) of the present invention, the fly ash is first washed with an acidic solution, and then the acid washed fly ash is washed with pure water. After the completion of the step (S3), the step (S4) is subsequently performed: a fine screening treatment is performed on the fly ash to remove the fly ash having a higher iron content. It is worth noting that the step (S3) is to wash the fly ash with an acidic solution and pure water, respectively. Therefore, the fly ash obtained after the completion of the step (S3) is in a wet state like a mud, and cannot be directly subjected to fine screening treatment. For this reason, before the step (S4) is performed, a low-temperature baking treatment must be performed on the fly ash to remove moisture.

於步驟(S4)之中,係首先使用高頻震盪式篩選機搭配具有53µm篩網孔徑大小的篩網對所述飛灰進行篩選,並同時使用強力磁鐵對飛灰進行一磁吸處理,藉此方式吸除含鐵量較高的飛灰。完成步驟(S4)之後,本發明之製造方法便接著執行步驟(S5):對所述飛灰進行一高溫烘烤處理,以燒除飛灰內的雜質與未燃碳。完成步驟(S5)之後,經測定後可知飛灰包含以下表(2)所列多種成分: 表(2) <TABLE border="1" borderColor="#000000" width="85%"><TBODY><tr><td> SiO<sub>2</sub></td><td> Al<sub>2</sub>O<sub>3</sub></td><td> Fe<sub>2</sub>O<sub>3</sub></td><td> 燒失量 (Loss on ignition, LOI) </td></tr><tr><td> 68% </td><td> 26.9% </td><td> 2.9% </td><td> 0.2% </td></tr></TBODY></TABLE>In the step (S4), the fly ash is first screened by using a high frequency oscillating screening machine with a screen having a mesh size of 53 μm, and a magnetic magnet is used to magnetically treat the fly ash. This method absorbs fly ash with a high iron content. After the completion of the step (S4), the manufacturing method of the present invention then performs the step (S5): performing a high-temperature baking treatment on the fly ash to burn off impurities and unburned carbon in the fly ash. After the completion of the step (S5), it is determined that the fly ash contains various components listed in the following Table (2): Table (2)  <TABLE border="1" borderColor="#000000" width="85%"><TBODY><tr><td> SiO<sub>2</sub></td><td> Al<sub>2 </sub>O<sub>3</sub></td><td> Fe<sub>2</sub>O<sub>3</sub></td><td> Loss on ignition (Loss On ignition, LOI) </td></tr><tr><td> 68% </td><td> 26.9% </td><td> 2.9% </td><td> 0.2% </ Td></tr></TBODY></TABLE>

比較表(1)與表(2)可以輕易地發現,與未執行任何處理製程的飛灰相比,完成初篩處理、前處理、精篩處理、與高溫烘烤處理後所獲得的飛灰所含有的燒失量(LOI)與氧化鐵成分係大量減少;相反地,飛灰所含有的氧化鋁與二氧化矽成分卻提升了。完成高溫烘烤步驟之後,本發明之製造方法係接著執行步驟(S6)以將所述飛灰置入一預熱裝置內,預熱至600-800 oC,並接著執行步驟(S7)至步驟(S8)。圖4A與圖4B係顯示步驟(S7)至步驟(S8)的製程示意圖。如圖4A所示,所述鋁基材被置入一金屬熔解裝置3內,並加熱至700-800 oC使得該鋁基材成為一鋁熔湯31。進一步地,如圖4A所示,一攪拌裝置5被用來攪拌該鋁熔湯31,並於攪拌過程中利用飛灰送入裝置4以0.05-0.15克/秒的流量將完成預熱的飛灰添加至該鋁熔湯31之中。最終,如圖4B所示,本發明係利用模浸速固法(Mold Immersed Rapid Solidification Process, MIRSP)將混有飛灰的鋁熔湯31加工成為一鋁基飛灰鑄件。 The comparison table (1) and the table (2) can be easily found that the fly ash obtained after the preliminary screening treatment, the pretreatment, the fine screening treatment, and the high temperature baking treatment is completed as compared with the fly ash which has not been subjected to any treatment process. The loss on ignition (LOI) and the iron oxide component are greatly reduced; on the contrary, the alumina and cerium oxide components contained in the fly ash are improved. After completion of high temperature baking step of the manufacturing method of the present invention is then performed based step (S6) to said ash preheating means placed in a preheated to 600-800 o C, and then performing step (S7) to Step (S8). 4A and 4B are schematic diagrams showing processes of steps (S7) to (S8). 4A, the aluminum substrate is placed in a metal melting apparatus 3, and heated to 700-800 o C so that the aluminum substrate into a molten metal 31 of aluminum. Further, as shown in FIG. 4A, a stirring device 5 is used to stir the aluminum melt 31, and the fly ash feeding device 4 is used to complete the preheating fly at a flow rate of 0.05-0.15 g/sec during the stirring process. Ash is added to the aluminum melt 31. Finally, as shown in FIG. 4B, the present invention processes the aluminum melt soup 31 mixed with fly ash into an aluminum-based fly ash casting by a Mold Immersed Rapid Solidification Process (MIRSP).

必須補充說明的是,本發明係以含有鎂成分的鋁合金作為所述鋁基材;即使如此,為了增加改善飛灰與鋁基材之間的潤濕性,於該步驟(S7)之中,吾人也可將一鎂材料與所述鋁基材一起置入該金屬熔解裝置3之中,並加熱至700-800 oC使得所述鎂材料與該鋁基材一同熔融成為所謂的鋁熔湯31。值得特別強調的是,本案的發明人基於多年的鋁基飛灰複合材料的研究經驗發現,一次性添加大量的飛灰進入鋁熔湯31之中,會令飛灰於鋁熔湯31之中發生群聚現象,導致飛灰所含有的SiO 2、Al 2O 3及Fe 2O 3及氧化物難以與鋁熔湯31進行反應。因此,於該步驟(S8)之中,係基於一特定批次數將完成預熱的飛灰添加至該鋁熔湯31之中,且該批次數係至少二次。並且,批次性地添加飛灰時,必須等待前一批次的飛灰與鋁熔湯31完成反應之後,再接著將下一批次的飛灰加入鋁熔湯31之中。 It must be additionally noted that the present invention uses an aluminum alloy containing a magnesium component as the aluminum substrate; even so, in order to increase the wettability between the fly ash and the aluminum substrate, in the step (S7) , I may be a magnesium aluminum substrate with the material placed in the metal melting apparatus 3, and heated to 700-800 o C so that the magnesium and the aluminum base material with a so-called molten aluminum melt Soup 31. It is worth emphasizing that the inventor of this case based on years of research experience in aluminum-based fly ash composites found that adding a large amount of fly ash into the aluminum melting soup 31 at one time would cause fly ash to be in the aluminum melting soup 31. The phenomenon of clustering occurs, and it is difficult for SiO 2 , Al 2 O 3 , and Fe 2 O 3 and oxide contained in the fly ash to react with the aluminum melt 31. Therefore, in this step (S8), the preheated fly ash is added to the aluminum melt 31 based on a specific batch number, and the number of batches is at least twice. Further, when the fly ash is batch-added, it is necessary to wait for the previous batch of fly ash to complete the reaction with the aluminum melt 31, and then add the next batch of fly ash to the aluminum melt 31.

必須再行補充說明的是,於步驟(S9)之中,混有鎂材料與飛灰的鋁熔湯31被倒入模具6之後(如圖4B所示),係先以灑水器做鋁基飛灰鑄件表面冷卻約30秒;接著,令鋁基飛灰鑄件定型後將其取出,並立即以流動冷卻水將鋁基飛灰鑄件完全冷卻1分鐘。It must be additionally explained that, in the step (S9), the aluminum melt 31 mixed with the magnesium material and the fly ash is poured into the mold 6 (as shown in FIG. 4B), and the aluminum is first sprinkled. The surface of the base fly ash casting was cooled for about 30 seconds; then, the aluminum-based fly ash casting was shaped and removed, and the aluminum-based fly ash casting was immediately cooled with running cooling water for 1 minute.

實驗例Experimental example

就現有的鋁基-飛灰複合材料而言,其通常含有1-5 wt%的鎂成分、3-15 wt%的飛灰與96-83 wt%的鋁基材。因此,本發明的實驗例之中係以ADC10鋁合金作為所述鋁基材,並預定飛灰與鎂材料的添加量分為15wt%與2wt%,同時將飛灰的批次數設為三次。簡單地說,完成預熱的飛灰會分成三批次被加入鋁熔湯之中,且每批次的添加量各為6wt%、6wt%及3wt%。In the case of the existing aluminum-based fly ash composite, it usually contains 1-5 wt% of magnesium component, 3-15 wt% of fly ash and 96-83 wt% of aluminum substrate. Therefore, in the experimental example of the present invention, an aluminum alloy of ADC10 was used as the aluminum substrate, and the addition amount of the fly ash and the magnesium material was predetermined to be 15 wt% and 2 wt%, and the number of batches of fly ash was set to three times. Briefly, the preheated fly ash is added to the aluminum melt soup in three batches, and the amount added per batch is 6 wt%, 6 wt%, and 3 wt%.

圖5係顯示飛灰添加量相對於密度的資料圖,且圖6係顯示飛灰添加量相對於孔隙率的資料圖。由圖5與圖6的實驗數據可知,相較於具有一次性添加6wt%的飛灰之鋁基飛灰鑄件,具有二批次添加(6wt%+6wt%)的飛灰之鋁基飛灰鑄件係顯示出較低的孔隙率。請繼續參閱圖7,其係顯示飛灰添加量相對於硬度的資料圖。由圖7的實驗數據可知,具有一次性添加6wt%的飛灰之鋁基飛灰鑄件、具有二批次添加(6wt%+6wt%)的飛灰之鋁基飛灰鑄件、以及具有三批次添加(6wt%+6wt%+3wt%)的飛灰之鋁基飛灰鑄件,這三者的硬度質皆高於85勃式硬度(BHN)。Fig. 5 is a graph showing the amount of fly ash added relative to the density, and Fig. 6 is a graph showing the amount of fly ash added relative to the porosity. From the experimental data of FIG. 5 and FIG. 6, it can be seen that the aluminum-based fly ash with two batches of added (6 wt% + 6 wt%) fly ash is compared with the aluminum-based fly ash casting with fly ash added at a time of 6 wt%. The casting system shows a lower porosity. Please continue to refer to Figure 7, which shows a data plot of the amount of fly ash added versus hardness. It can be seen from the experimental data of FIG. 7 that the aluminum-based fly ash casting having a fly ash added at a time of 6 wt%, the aluminum-based fly ash casting having two batches of added (6 wt% + 6 wt%) fly ash, and having three batches A secondary (6 wt% + 6 wt% + 3 wt%) fly ash-based aluminum fly ash casting, all of which have a hardness higher than 85 Boar hardness (BHN).

如此,上述係已完整且清楚地說明本發明之一種鋁基飛灰複合材料之製造方法的步驟流程;並且,經由上述可知本發明係具有下列之優點:Thus, the above-described system has completely and clearly explained the flow of steps of a method for producing an aluminum-based fly ash composite material of the present invention; and, as apparent from the above, the present invention has the following advantages:

(1)習知技術(如文獻一)所揭示的製造方法所製得的鋁基飛灰鑄件具有過多的孔隙或氣孔,造成鋁基飛灰鑄件之機械性質下降。相較於習知的製造方法,本發明所提出鋁基飛灰複合材料之製造方法之中係特別以浮篩與磁篩對飛灰進行粗篩與精篩之後,再接著讓完成預熱的飛灰批次性地添加入熔融狀態的鋁基材內,最終利用模浸速固法將混有飛灰的鋁熔湯加工成一鋁基飛灰鑄件。並且,實驗數據顯示,本發明所提出的鋁基飛灰複合材料之製造方法有助於降低鋁基飛灰鑄件的孔隙率並維持或增強其機械性質。(1) Aluminum-based fly ash castings produced by the manufacturing method disclosed in the prior art (such as Document 1) have excessive pores or pores, resulting in a decrease in mechanical properties of the aluminum-based fly ash casting. Compared with the conventional manufacturing method, the method for manufacturing the aluminum-based fly ash composite material proposed by the present invention is particularly characterized in that the fly ash is coarsely sieved and finely sieved by a floating sieve and a magnetic sieve, and then the preheating is completed. The fly ash is batch-added into the aluminum substrate in a molten state, and finally the aluminum melt mixed with fly ash is processed into an aluminum-based fly ash casting by a die-dipping method. Moreover, experimental data shows that the method of manufacturing the aluminum-based fly ash composite proposed by the present invention contributes to reducing the porosity of the aluminum-based fly ash casting and maintaining or enhancing its mechanical properties.

必須加以強調的是,上述之詳細說明係針對本發明可行實施例之具體說明,惟該實施例並非用以限制本發明之專利範圍,凡未脫離本發明技藝精神所為之等效實施或變更,均應包含於本案之專利範圍中。It is to be understood that the foregoing detailed description of the embodiments of the present invention is not intended to Both should be included in the scope of the patent in this case.

<本發明><present invention>

S1-S9‧‧‧步驟 S1-S9‧‧ steps

2‧‧‧初篩裝置 2‧‧‧Primary screening device

20‧‧‧容器 20‧‧‧ container

21‧‧‧第一篩網 21‧‧‧First screen

22‧‧‧第二篩網 22‧‧‧Second screen

23‧‧‧排水埠 23‧‧‧Drainage

S21-S23‧‧‧步驟 S21-S23‧‧‧Steps

3‧‧‧金屬熔解裝置 3‧‧‧Metal melting device

31‧‧‧鋁熔湯 31‧‧‧Aluminium melt soup

5‧‧‧攪拌裝置 5‧‧‧Agitator

6‧‧‧模具 6‧‧‧Mold

4‧‧‧飛灰送入裝置 4‧‧‧ fly ash feeding device

<習知><知知>

no

圖1A與圖1B係顯示本發明之一種鋁基飛灰複合材料之製造方法的流程圖; 圖2係顯示初篩裝置的立體圖; 圖3係顯示步驟(S2)的細部流程圖; 圖4A與圖4B係顯示步驟(S7)至步驟(S8)的製程示意圖; 圖5係顯示飛灰添加量相對於密度的資料圖; 圖6係顯示飛灰添加量相對於孔隙率的資料圖;以及 圖7係顯示飛灰添加量相對於硬度的資料圖。1A and 1B are flow charts showing a method of manufacturing an aluminum-based fly ash composite material of the present invention; Fig. 2 is a perspective view showing a preliminary screening device; Fig. 3 is a detailed flow chart showing the step (S2); 4B is a schematic view showing a process of the steps (S7) to (S8); FIG. 5 is a data chart showing the amount of fly ash added relative to the density; and FIG. 6 is a data chart showing the amount of fly ash added relative to the porosity; The 7 series shows a data plot of the amount of fly ash added relative to the hardness.

Claims (10)

一種鋁基飛灰複合材料之製造方法,係包括以下步驟:(1)備好飛灰與一鋁基材;(2)對所述飛灰進行一初篩處理,將顆粒大小介於53μm至106μm之間的飛灰篩出;(3)對所述飛灰進行一前處理以去除其雜質;(4)使用高頻震盪式篩選機搭配具有53μm篩網孔徑大小的篩網對所述飛灰進行一精篩處理;(5)對所述飛灰進行一高溫烘烤處理,以燒除飛灰內的雜質與未燃碳;(6)將所述飛灰置入一預熱裝置內,預熱至600-800℃;(7)將所述鋁基材置入一金屬熔解裝置內,並加熱至700-800℃使得該鋁基材成為一鋁熔湯;(8)使用一攪拌裝置攪拌該鋁熔湯,並於攪拌過程中以0.05-0.15克/秒的流量將完成預熱的飛灰添加至該鋁熔湯之中;以及(9)利用模浸速固法(Mold Immersed Rapid Solidification Process,MIRSP)將混有飛灰的鋁熔湯加工成一鋁基飛灰鑄件。 The invention relates to a method for manufacturing an aluminum-based fly ash composite material, comprising the steps of: (1) preparing fly ash and an aluminum substrate; (2) performing a preliminary screening treatment on the fly ash, and the particle size is between 53 μm to Fly ash between 106 μm; (3) pre-treatment of the fly ash to remove impurities; (4) using a high-frequency oscillating screening machine with a screen having a pore size of 53 μm mesh The ash is subjected to a fine screening treatment; (5) the high temperature baking treatment is performed on the fly ash to burn off impurities and unburned carbon in the fly ash; (6) placing the fly ash into a preheating device Preheating to 600-800 ° C; (7) placing the aluminum substrate into a metal melting device and heating to 700-800 ° C to make the aluminum substrate an aluminum melt; (8) using a stirring The apparatus stirs the aluminum melt, and adds the preheated fly ash to the aluminum melt at a flow rate of 0.05-0.15 g/sec during the stirring; and (9) using the mold dip-solid method (Mold Immersed) Rapid Solidification Process (MIRSP) processes aluminum fused soup mixed with fly ash into an aluminum-based fly ash casting. 如申請專利範圍第1項所述之鋁基飛灰複合材料之製造方法,其中,該鋁基材為含有鎂成分的壓鑄鋁合金(Die-casting aluminum alloy)。 The method for producing an aluminum-based fly ash composite material according to claim 1, wherein the aluminum base material is a Die-casting aluminum alloy containing a magnesium component. 如申請專利範圍第1項所述之鋁基飛灰複合材料之製造方法,其中,該步驟(2)包括以下細部步驟:(21)備好一容器,並於該容器內設置一第一篩網與一第二篩網;其中,該第一篩網的設置位置係高於該第二篩網,且該第一篩網的篩網孔徑大小係大於該第二篩網的篩網孔徑大小;(22)將所述飛灰倒入該容器內,並將流動水注入該容器內,利用流動水沖刷飛灰;以及(23)透過該容器的一排水埠將流動水自該容器排出,顆粒大小介於53μm至106μm之間的飛灰即被篩出於該第一篩網與該第二篩網之間。 The method for manufacturing an aluminum-based fly ash composite material according to claim 1, wherein the step (2) comprises the following detailed steps: (21) preparing a container and setting a first sieve in the container a mesh and a second screen; wherein the first screen is disposed higher than the second screen, and the screen size of the first screen is larger than the screen size of the second screen (22) pouring the fly ash into the container, injecting flowing water into the container, flushing the fly ash with flowing water; and (23) discharging the flowing water from the container through a drain of the container, Fly ash having a particle size between 53 μm and 106 μm is screened between the first screen and the second screen. 如申請專利範圍第1項所述之鋁基飛灰複合材料之製造方法,其中,該步驟(3)包括以下細部步驟:使用酸性溶液清洗所述飛灰;以及以純水沖洗所述飛灰。 The method for producing an aluminum-based fly ash composite material according to claim 1, wherein the step (3) comprises the following detailed steps of: washing the fly ash with an acidic solution; and rinsing the fly ash with pure water. . 如申請專利範圍第1項所述之鋁基飛灰複合材料之製造方法,其中,該步驟(4)與該步驟(5)之間係更包括以下步驟:使用強力磁鐵對所述飛灰進行一磁吸處理,吸除含鐵量較高的飛灰。 The method for manufacturing an aluminum-based fly ash composite material according to claim 1, wherein the step (4) and the step (5) further comprise the step of: using the strong magnet to perform the fly ash. A magnetic treatment removes fly ash with a high iron content. 如申請專利範圍第1項所述之鋁基飛灰複合材料之製造方法,其中,於該步驟(8)之中,係基於一特定批次數將完成預熱的飛灰添加至該鋁熔湯之中,且該特定批次數係至少二次。 The method for manufacturing an aluminum-based fly ash composite material according to claim 1, wherein in the step (8), the preheated fly ash is added to the aluminum melt soup based on a specific batch number. And the specific number of batches is at least two times. 如申請專利範圍第5項所述之鋁基飛灰複合材料之製造方法,其中,於該步驟(8)之中,係等待前一批次的飛灰與該鋁熔湯完成反應之後,再接著將下一批次的飛灰加入鋁熔湯之中。 The method for manufacturing an aluminum-based fly ash composite material according to claim 5, wherein in the step (8), after waiting for the reaction of the previous batch of fly ash and the aluminum melt, The next batch of fly ash is then added to the aluminum melt. 如申請專利範圍第1項所述之鋁基飛灰複合材料之製造方法,其中,於該步驟(7)之中,可將一鎂材料與所述鋁基材一起置入該金屬熔解裝置內,並加熱至700-800℃使得所述鎂材料與該鋁基材熔融成為所述鋁熔湯。 The method for manufacturing an aluminum-based fly ash composite material according to claim 1, wherein in the step (7), a magnesium material is placed in the metal melting device together with the aluminum substrate. And heating to 700-800 ° C causes the magnesium material to melt with the aluminum substrate into the aluminum melt. 如申請專利範圍第1項所述之鋁基飛灰複合材料之製造方法,其中,該步驟(3)與該步驟(4)之間係更包括以下步驟:對所述飛灰執行一低溫烘烤處理,以除去其水分。 The method for manufacturing an aluminum-based fly ash composite material according to claim 1, wherein the step (3) and the step (4) further comprise the step of: performing a low-temperature drying on the fly ash. Bake to remove moisture. 如申請專利範圍第8項所述之鋁基飛灰複合材料之製造方法,其中,該金屬鎂、該飛灰與該鋁基材佔所述鋁基飛灰鑄件的重量百分比分別為1-5wt%、3-15wt%與96-83wt%。 The method for manufacturing an aluminum-based fly ash composite material according to claim 8, wherein the metal magnesium, the fly ash, and the aluminum substrate account for 1-5 wt% of the aluminum-based fly ash castings, respectively. %, 3-15 wt% and 96-83 wt%.
TW107119010A 2018-06-01 2018-06-01 Method for fabricating aluminum-fly ash composite material TWI648410B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
TW107119010A TWI648410B (en) 2018-06-01 2018-06-01 Method for fabricating aluminum-fly ash composite material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
TW107119010A TWI648410B (en) 2018-06-01 2018-06-01 Method for fabricating aluminum-fly ash composite material

Publications (2)

Publication Number Publication Date
TWI648410B true TWI648410B (en) 2019-01-21
TW202003872A TW202003872A (en) 2020-01-16

Family

ID=65803951

Family Applications (1)

Application Number Title Priority Date Filing Date
TW107119010A TWI648410B (en) 2018-06-01 2018-06-01 Method for fabricating aluminum-fly ash composite material

Country Status (1)

Country Link
TW (1) TWI648410B (en)

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
TW200909376A (en) * 2007-08-28 2009-03-01 You-Jing Wang Method for reproducing lightweight aggregate using incinerated flying ash
CN105712733A (en) * 2014-12-01 2016-06-29 北京大学深圳研究生院 Porous biological ceramsite prepared from waste incineration fly ash and biomass pyrolysis gasification residue, and preparation method thereof

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
TW200909376A (en) * 2007-08-28 2009-03-01 You-Jing Wang Method for reproducing lightweight aggregate using incinerated flying ash
CN105712733A (en) * 2014-12-01 2016-06-29 北京大学深圳研究生院 Porous biological ceramsite prepared from waste incineration fly ash and biomass pyrolysis gasification residue, and preparation method thereof

Also Published As

Publication number Publication date
TW202003872A (en) 2020-01-16

Similar Documents

Publication Publication Date Title
CN103252597B (en) Hot-setting backing welding flux and preparation method thereof
CN107552720A (en) A kind of steel-casting precoated sand, its preparation method and anti-agglutinatting property detection method
CN108085546A (en) A kind of 2024 aluminium alloy smelting casting methods
CN104294068A (en) Process method capable of improving refinement and modification effects of A356 aluminum alloy
JP2007533850A (en) Improved recycling method for Al-B4C composites
US9038708B1 (en) Foundry mixture and related methods for casting and cleaning cast metal parts
CN109825727A (en) A kind of Al-Si-Fe intermediate alloy preparation method based on thermit reaction
CN104313411A (en) Process method capable of improving mechanical properties of A356 aluminum alloy
WO2021035774A1 (en) Preparation method for lithium-containing magnesium/aluminum-based composite material
JP2022512329A (en) Die-casting method for filter cavities
US10577715B2 (en) Foundry mixture and related methods for casting and cleaning cast metal parts
CN108707813A (en) As cast condition hi-strength nodular iron and its manufacturing process
WO2021169074A1 (en) Iron-aluminum alloy and preparation method therefor
TWI648410B (en) Method for fabricating aluminum-fly ash composite material
CN107052306A (en) A kind of hypereutectic and hypoeutectic al-si alloy solid-liquid bimetal composite casting method
JP2004114152A (en) Method for producing metallic material in solid-liquid coexisting state
CN106048302A (en) Casting material for nuclear power and wind power and manufacture method thereof
CN104084545B (en) The mixed liquid Modification Manners of a kind of casting Mg-Al alloy liquid melt/semi-solid melt
CN106555066A (en) A kind of method that micro compound additive prepares high-performance richness ferrum secondary aluminium
CN110551912A (en) Method for manufacturing aluminum-based fly ash composite material
KR20130053010A (en) Method and apparatus for preparing thin plate by rheoforming
JP3735318B2 (en) High silicon cast iron excellent in acid resistance and method for producing the same
KR101260336B1 (en) A method for controlling the casting defect of Al-Si-Mg alloy through grain refinement and improving the cooling speed by using hydropulse
CN112195358A (en) Aluminum-based alloy, aluminum-based composite material, and preparation method and application thereof
JP4701035B2 (en) Casting method