scholarly journals PENGEMBANGAN PROSES PEMBUATAN IMPELLER DENGAN CETAKAN KULIT

2018 ◽  
Vol 8 (3) ◽  
pp. 115-119
Author(s):  
Suharno ◽  
Amin Suhadi
Keyword(s):  

Impeller merupakan komponen pompa air yang cukup vital dan umumnya terbuat dari kuningan yangharganya relatif mahal, maka dilakukan pengembangan dan dibuat dengan material paduan aluminium yanglebih murah. pembuatannya dicor dengan metode cetakan kulit (shell mold casting) Alat peleburanmenggunakan tungku crucible sederhana. Untuk mendapatkan performa dan karakteristik pada materialdengan uji mekanis dan fisik yaitu uji tarik, uji kekerasan, uji impak, uji komposisi material serta strukturmikro. Cetakan cor terbuat dari pasir cor jenis silika (SiO2) dengan ukuran butiran 0.06–0.1 mm, dengancampuran resin fenol dan katalis sebagai pengikat dan pengering resin. Komposisi aluminium paduan dibuattiga variabel, 1% Cu, 3% Cu dan 5% Cu.Kekuatan tarik maksimum 9950 N/mm², kekerasan maksimum 376N/mm², tenaga pukul impak 45 Joule.

2021 ◽  
pp. e01052
Author(s):  
J.K. Hatsu ◽  
A.K. Sunnu ◽  
G.K. Ayetor ◽  
G. Takyi

1973 ◽  
Author(s):  
William J. Buehler ◽  
Richard E. Jones ◽  
Ernest F. Heintzelman ◽  
Richard H. Lundsten

Author(s):  
A. Garg ◽  
R. D. Noebe ◽  
R. Darolia

Small additions of Hf to NiAl produce a significant increase in the high-temperature strength of single crystals. Hf has a very limited solubility in NiAl and in the presence of Si, results in a high density of G-phase (Ni16Hf6Si7) cuboidal precipitates and some G-platelets in a NiAl matrix. These precipitates have a F.C.C structure and nucleate on {100}NiAl planes with almost perfect coherency and a cube-on-cube orientation-relationship (O.R.). However, G-phase is metastable and after prolonged aging at high temperature dissolves at the expense of a more stable Heusler (β'-Ni2AlHf) phase. In addition to these two phases, a third phase was shown to be present in a NiAl-0.3at. % Hf alloy, but was not previously identified (Fig. 4 of ref. 2 ). In this work, we report the morphology, crystal-structure, O.R., and stability of this unknown phase, which were determined using conventional and analytical transmission electron microscopy (TEM).Single crystals of NiAl containing 0.5at. % Hf were grown by a Bridgman technique. Chemical analysis indicated that these crystals also contained Si, which was not an intentional alloying addition but was picked up from the shell mold during directional solidification.


Author(s):  
Olga Komissarchuk ◽  
Hai Hao ◽  
Xing-lu Zhang ◽  
Vladimir Karpov

Alloy Digest ◽  
1987 ◽  
Vol 36 (12) ◽  

Abstract UNS No. A02060 is an aluminum-mold casting alloy that responds to an age-hardening heat treatment. It is recommended for applications that require a combination of high tensile properties and good machinability. Among its many uses are fuel pump bodies, aircraft fittings and seat frames for railway passenger cars. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well as fatigue. It also includes information on high temperature performance as well as casting, heat treating, machining, and joining. Filing Code: Al-285. Producer or source: Various aluminum companies.


Alloy Digest ◽  
1982 ◽  
Vol 31 (11) ◽  

Abstract ALUMINUM 296.0 is an aluminum permanent-mold casting alloy that responds to an age-hardening heat treatment. It is recommended for applications that require a combination of high tensile properties and good machinability. Among its many uses are fuel pump bodies, aircraft fittings and seat frames for railway passengers cars. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well as fatigue. It also includes information on high temperature performance as well as casting, heat treating, machining, and joining. Filing Code: Al-241. Producer or source: Various aluminum companies. See also Alloy Digest Al-261, October 1985.


Alloy Digest ◽  
1986 ◽  
Vol 35 (2) ◽  

Abstract ALUMINUM 513.0 is an aluminum-magnesium-zinc permanent-mold casting alloy. It cannot be hardened nor strengthened by any thermal treatment and is characterized by moderate strength and ductility. It is recommended for such applications as chemical-plant equipment, food handling and marine hardware. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well as fatigue. It also includes information on corrosion resistance as well as heat treating, machining, and joining. Filing Code: Al-265. Producer or source: Various aluminum companies.


Alloy Digest ◽  
1969 ◽  
Vol 18 (11) ◽  

Abstract Aluminum A356 is a sand and permanent mold casting alloy that responds to an age-hardening heat treatment. It is recommended for aircraft and missile components where high strength and corrosion resistance are required. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well as fatigue. It also includes information on heat treating, machining, and joining. Filing Code: Al-192. Producer or source: Aluminum Company of America.


Metals ◽  
2021 ◽  
Vol 11 (7) ◽  
pp. 1036
Author(s):  
Eduardo Colin García ◽  
Alejandro Cruz Ramírez ◽  
Guillermo Reyes Castellanos ◽  
José Federico Chávez Alcalá ◽  
Jaime Téllez Ramírez ◽  
...  

Ductile iron camshafts low alloyed with 0.2 and 0.3 wt % vanadium were produced by one of the largest manufacturers of the ductile iron camshafts in México “ARBOMEX S.A de C.V” by a phenolic urethane no-bake sand mold casting method. During functioning, camshafts are subject to bending and torsional stresses, and the lobe surfaces are highly loaded. Thus, high toughness and wear resistance are essential for this component. In this work, two austempering ductile iron heat treatments were evaluated to increase the mechanical properties of tensile strength, hardness, and toughness of the ductile iron camshaft low alloyed with vanadium. The austempering process was held at 265 and 305 °C and austempering times of 30, 60, 90, and 120 min. The volume fraction of high-carbon austenite was determined for the heat treatment conditions by XRD measurements. The ausferritic matrix was determined in 90 min for both austempering temperatures, having a good agreement with the microstructural and hardness evolution as the austempering time increased. The mechanical properties of tensile strength, hardness, and toughness were evaluated from samples obtained from the camshaft and the standard Keel block. The highest mechanical properties were obtained for the austempering heat treatment of 265 °C for 90 min for the ADI containing 0.3 wt % V. The tensile and yield strength were 1200 and 1051 MPa, respectively, while the hardness and the energy impact values were of 47 HRC and 26 J; these values are in the range expected for an ADI grade 3.


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