810 resultados para TIG welding
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This study compared the tensile strength and fracture mechanism of tungsten inert gas (TIG) welds in cylindrical rods of commercially pure titanium (cp Ti) with those of laser welds and intact samples. Thirty dumbbell-shaped samples were developed by using brass rods as patterns. The samples were invested in casings, subjected to thermal cycles, and positioned in a plasma arc welding machine under argon atmosphere and vacuum, and titanium was injected under vacuum/pressure. The samples were X-rayed to detect possible welding flaws and randomly assigned to three groups to test the tensile strength and the fracture mechanism: intact, laser welding, and TIG welding. The tensile test results were investigated using ANOVA, which indicated that the samples were statistically similar. The fracture analysis showed that the cpTi samples subjected to laser welding exhibited brittle fracture and those subjected to TIG welding exhibited mixed brittle/ductile fracture with a predominance of ductile fracture with the presence of microcavities and cleavage areas. Intact samples presented the characteristic straightening in the fracture areas, indicating the ductility of the material.
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Mode of access: Internet.
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Joining processes and techniques need to meet the trend of new applications and the development of new materials. The application in connection with thick and thin plates in industrial fields is wide and the joining technology is in very urgent need. The laser-TIG hybrid welding technology can play the respective advantages of both of them. One major advantage of the hybrid laser-TIG welding technology is its efficient use of laser energy. Additionally, it can develop into a high and new advanced welding technology and become a hot spot in both the application and research area. This thesis investigated laser –TIG hybrid welding with the aim of enlightening the reader on its advantages, disadvantages and future areas of improvement. The main objective is to investigate laser-TIG hybrid on the welding of various metals (steels, magnesium, aluminium etc.). In addition, it elaborates on various possible combinations on hybrid laser-TIG welding technology and their benefits. The possibility of using laser-TIG hybrid in welding of thick materials was investigated. The method applied in carrying out this research is by using literature review. The results showed that hybrid laser-TIG is applicable to almost all weldable metals. Also it proves to be effective in welding refractive metals. The possibility of welding with or without filler materials is of economic advantage especially in welding of materials with no filler material. Thick plate’s hybrid laser-TIG welding is showing great prospects although it normally finds its used in welding thin materials in the range of 0.4 to 0.8 mm. The findings show that laser-TIG hybrid welding can be a versatile welding process and therefore will be increasingly used industrially due to its numerous advantages and the development of new TIG arc that enhances its capabilities.
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Shape memory alloys are characterized by the ability of recovering their initial shape after being deformed and by superelasticity. Since the discovery of these alloys, a new field of interest emerged not only for the scientific community but also to many industries. However, these alloys present poor machinability which constitute a constrain in the design of complex components for new applications. Thus, the demand for joining techniques able to join these alloys without compromising their properties became of great importance to enlarge the complexity of existing applications. Literature shows that these alloys are joined mainly using laser welding. In the present study, similar NiTi butt joints, were produced using TIG welding. The welds were performed in 1.5 mm thick plates across the rolling direction. A special fixture and gas assist device was designed and manufactured. Also a robot arm was adapted to accommodate the welding torch to assure the repeatability of the welding parameters. Welds were successfully achieved without macroscopic defects, such as pores and distortions. Very superficial oxidation was seen on the top surface due to insufficient shielding gas flow on the weld face. The welded joints were mechanically tested and structurally characterized. Testing methods were used to evaluate macro and microstructure, as well as the phase transformation temperatures, the mechanical single and cyclic behaviour and the shape recovery ability. Differential Scanning Calorimetry (DSC), Scanning Electron Microscopy (SEM), Energy Dispersive Spectroscopy (EDS), microhardness measurements were techniques also used to evaluate the welded joints. A depletion in Ni in the fusion zone was seen, as well as a shift in Ms temperature. For strain values of 4% the accumulated irrecoverable strain was of about 30% and increased with the strain imposed during cycling. Nevertheless, a complete recovery of initial shape was observed when testing the shape memory effect on a dedicated device that introduces a deformation of 6.7%. That is, the welding procedure does not remove the ability of the specimens to recover their initial shape.
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Diplomityön tavoitteena oli ruostumattoman teräksen koneellisen TIG-hitsauksen hitsausnopeuden lisääminen. Työssä tutkittiin suojakaasun koostumuksen vaikutusta hitsausnopeuteen sekä kahta uudehkoa prosessivariaatiota. Tutkitut prosessit olivat TIG-suurtaajuuspulssihitsaus sekä kaksoiskaasu-TIG-hitsaus. Kirjallisessa osassa perehdyttiin TIG-hitsauksen prosessiparametreihin ja -variaatioihin. Kokeellisessa osassa suoritettiin koehitsauksia hitsausnopeuksien selvittämiseksi. Tavoitteena oli tunkeuman kasvattaminen, mikä mahdollistaa hitsausnopeuden noston läpihitsattaessa. Suojakaasuina käytettiin sekä argonpohjaisia että heliumpohjaisia kaasuja, joihin oli lisätty vetyä. Vedyn avulla hitsausnopeus lisääntyi nykykäytäntöä suuremmillakin pitoisuuksilla. Uutena ilmiönä TIG-hitsauksessa havaittiin keyholen eli lävistysreiän syntyminen korkeita vetypitoisuuksia heliumpohjaisessa suojakaasussa käytettäessä. Keyhole oli kuitenkin erittäin epävakaa, joten jatkotutkimuksien tehtäväksi jää selvittää tarkemmin tämän ilmiön vaikutus. Tutkittuihin prosessivariaatioihin todettiin liittyvän useita laiteteknisiä ongelmia. Hitsausnopeuden suhteen tulokset jäivät vaatimattomiksi. Lähinnä keyholen aukaisemisessa ja aukipitämisessä menetelmistä havaittu hyöty antaa selvän aiheen jatkotutkimuksille.
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Additive manufacturing is a fast growing manufacturing technology capable of producing complex objects without the need for conventional manufacturing process planning. During the process the work piece is built by adding material one layer at a time according to a digital 3D CAD model. At first additive manufacturing was mainly used to make prototypes but the development of the technology has made it possible to also make final products. Welding is the most common joining method for metallic materials. As the maximum part size of additive manufacturing is often limited, it may sometimes be required to join two or more additively manufactured parts together. However there has been almost no research on the welding of additively manufactured parts so far, which means that there has been very little information available on the possible differences compared to the welding of sheet metal parts. The aim of this study was to compare the weld joint properties of additively manufactured parts to those of sheet metal parts. The welding process that was used was TIG welding and the test material was 316L austenitic stainless steel. Weld joint properties were studied by making tensile, bend and hardness tests and by studying the weld microstructures with a microscope. Results show that there are certain characteristics in the welds of additively manufactured parts. The building direction of the test pieces has some impact on the mechanical properties of the weld. Nevertheless all the welds exhibited higher yield strength than the sheet metal welds but at the same time elongation at break was lower. It was concluded that TIG welding is a feasible process for welding additively manufactured parts.
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Tässä työssä tutkittiin orbitaali-TIG-hitsauksen hyödyntämistä paineenalaisten compoundputkien jatkohitsien hitsaamiseen. Tutkimus tehtiin Warkaus Works Oy:n omistamalle konepajalle. Tutkimuksen tavoitteena oli laatia standardin SFS-EN ISO 15613 mukaan hyväksytty hitsausmenetelmä. Työn kirjallisuuskatsauksessa esiteltiin orbitaalihitsauksessa käytettävät hitsausprosessit ja laitteistot eri liitosmuodoille. Työssä esiteltiin myös kuumavedettyjen compoundputkien valmistusprosessia ja rakennetta. Tämän lisäksi kerrottiin putkien hitsattavuudesta ja hitsauksen esivalmisteluista, sekä käyttökohteista voimalaitoskattilassa. Ennen menetelmäkokeen hitsausta suoritettiin suuri määrä koehitsauksia yrityksen orbitaali-TIG-laitteistolla. Onnistuneiden koehitsausten perusteella laadittiin hitsausohjelma, jolla hitsattiin testiputket menetelmäkokeeseen. Hitsausmenetelmää varten valittiin Sandvikin valmistama compoundputki. Testihitseille suoritettiin rikkomattomia ja rikkovia tarkastuksia. Hyväksyttyjen tarkastusten pohjalta laadittiin hitsausmenetelmän hyväksymispöytäkirjan. Lisäksi diplomityössä verrattiin mekanisoidun hitsauksen hitsausaikaa käsinhitsauksen hitsausaikaa. Orbitaali-TIG-hitsauksen käyttäminen edellyttää hitsattavalta railolta aina mahdollisimman samanlaisen lähtötilanteen, jotta sen suoritusvarmuus saadaan mahdollisimman korkeaksi. Railon valmistamisen tarkkuudella on mahdollista saada riittävän tarkkoja railoja hitsien laadukkaaseen hitsaukseen. Hitsaus edellyttää laitteiston langansyötön ja elektrodin tarkkoja asetuksia, jotta hitsaus on laadukasta. Lisäaineen jähmeä sula ja hitsin tunkeumavaatimus hankaloittavat orbitaalihitsausta.
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In this work, three welding programs for orbital TIG previously developed were used, using pulsed current and increasing speed (M), constant current (#B) and pulsed current and decreasing current (#C). One of those should be used for the propulsion system of the satellite CBERS (CHINA-BRAZIL EARTH RESOURCES SATELLITE). Welded joints using tubes of commercially pure titanium were obtained with these procedures, which were characterized by means of mechanical and metallographic tests. The obtained results show that the three welding procedures produce welded joints free of defects and with adequate shape. Although small differences on mechanical properties and microstructure have been observed, the three welding programs attained compatible results with international standards used in the aerospace segment. The welding program #B, due the reduced heat input used, was considered to obtain slightly advantage over the others.
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Structures critical to the flight-safety are commonly submitted to several maintenance repairs at the welded joints in order to prolong the in-service life of aircrafts. The aim of this study is to analyze the effects of Tungsten Inert Gas (TIG) welding repair on the structural integrity of the AISI 4130 aeronautical steel by means of experimental fatigue crack growth tests in base-material, heat-affected zone (HAZ) and weld metal. The tests were performed on hot-rolled steel plate specimens, 0.89 mm thick, with load ratio R = 0.1, constant amplitude, at 10 Hz frequency and room temperature. Increase of the fracture resistance was observed in the weld metal but decreasing in the HAZ after repair. The results were associated to microhardness and microstructural changes with the welding sequence. (C) 2010 Published by Elsevier Ltd.
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Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)
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Pós-graduação em Odontologia - FOA
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This work examines the possible effects of successive repair procedures on the microstructure of welded steel SAE 4130 by TIG welding process. Discussions and results were made about the metallographic analysis , non-metallic inclusions and microhardness tests , which were conducted on samples taken from the cradle engine component after the end of its life , a model airplane T-27 Tucano , made by EMBRAER and belonging were performed FAB . The choice of such component is due to the fact that this is critical to flight safety since it provides support for the aircraft engine . Thus regions of the weld metal , base metal and heat affected , with samples of the original weld bead , free of weld bead and also with four rework procedures for TIG welding zone were analyzed . It was found that after the fourth rework there is an increase in the amount of martensite , which may weaken the material with respect to resistance to fatigue. It was also found that the regions of the heat affected zone and weld metal have higher microhardness values when compared to those found in the base metal due to favoring the formation of ferritic and tempered martensite microstructures . Moreover, a welding process promotes a region with less non-metallic inclusions than metal base , which also explains the difference in the results obtained
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Conselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)