International Research Journal of Engineering and Technology (IRJET)
e-ISSN: 2395 -0056
Volume: 04 Issue: 05 | May -2017
p-ISSN: 2395-0072
www.irjet.net
Optimization of Titanium Welding used in Aircrafts Prof. Anand Lahane1, Shubham Devanpalli2, Ritesh Patil3 , Suraj Thube4 1 Assistant
Professor, Dept. of Mechanical Engineering, Shatabdi Institute of Engineering and Research, Nashik, India. 234Dept. of Mechanical Engineering, Shatabdi Institute of Engineering and Research, Nashik, India. ---------------------------------------------------------------------***---------------------------------------------------------------------
Abstract - At Present Titanium is most preferred metal for
Aircraft Industries including Fighter Aircrafts due to its useful properties like high Corrosion resistance and High strength to density ratio. These Aircraft Industries uses TIG (Tungsten Inert gas ) welding for joining Titanium components. These Welding are generally done on Automatic welding machines but, as these machines are Automatic then too we have to provide the Voltage as well as Current depending on thickness of component or sheet to be welded as Inputs to the welding machine Currently these inputs are used on basis of welders skill and predefined values. But using those values of current and voltage have developed crack formation and decrease the life of welded joint of component up to some extent. Therefore in this Project we Aim in finding the Optimized values of the following Inputs i.e. Current and Voltage so that we can minimize as well as prevent the Crack Formation in those Precise components. Key Words: Titanium, Welding, Current, Voltage, Optimize, Cracks, Components. 1. INTRODUCTION Welding has become one of the most common fabrication techniques, which is extensively used to obtained good quality weld joints. The present trend in the fabrication industries is to automate welding processes to obtained high production rate. Arc welding, which is also called as HeatType is one of the most important manufacturing operations for the joining of structural elements for various applications, which includes Aircrafts, trains, bridges, building structures, automobiles. It requires a continuous supply of either Direct current (DC) or Alternating electric current (AC), which create an electric arc to generate enough heat to melt the metal and form a weld. In this Project we have consider the Titanium Welding process which is used in our Fighter Aircrafts. The Component which we are considering here is the Central Panel of Aircraft which is also called as Lower Panel fitted to the bottom of the Aircraft. This panel is supporting the Fuel tak of that aircraft So this Central Panel has to be Leak proof i.e. Crack Proof So welding used here should be Precise. Here, In this Project we have firstly gone through all the parameters which are affecting the welding process which include the welding Speed, Gas Flow rate, Current, Voltage, Feed rate. We have taken the values from actual Automatic Welding Machine at Industry. Š 2017, IRJET
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Impact Factor value: 5.181
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As welding Titanium is not similar to normally used welding process. These Includes some Special procedure as Titanium can react with the oxygen to form Oxide layer which can reduce the Strength of Component therefore Welding of Titanium is to carried out in Vacuum Chamber under Shielding gas Influence. In Automatic welding machine the Welding Arc is Shielded with Shielding Gas which is generally Argon Gas. These gas is allowed to shield Arc and avoid Oxidation[1] . In below we will see the Special process needed for welding Titanium metal.
1.1 T.I.G welding process:Tungsten Inert gas Welding (TIG) or also called as Gas Tungsten Arc (GTA) welding is an arc welding process. In which for high thickness welding molten pool is produced by heating the work piece with an electrical arc struck between a tungsten electrode and the workpiece. The electrical discharge generates a plasma arc between the electrode tip and the work piece to be welded. The arc is normally generated by a power source with a high frequency producer.
Fig -1: TIG Welding Process arc generates high-temperature of approximately 6200°C and melts the surface of base metal i.e. work-piece to form a molten pool. A welding gas or shielding gas (argon or helium) is used to avoid atmospheric contamination of the molten weld puddle. The shielding gas displaces the air and avoids the contact of oxygen and the nitrogen with the molten metal or hot tungsten electrode. As the molten metal cools and the parts are joined. The resulting weld is smooth and thus requires minimum finishing. The
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