2011
DOI: 10.4028/www.scientific.net/amm.62.67
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An Experimental Investigation of Hot Machining with Induction to Improve Ti-5553 Machinability

Abstract: OATAO is an open access repository that collects the work of Toulouse researchers and makes it freely available over the web where possible. Abstract. The manufacturing of aeronautic parts with high mechanical properties requires the use of high performance materials. That's why; new materials are used for landing gears such as the titanium alloy Ti-5553. The machining of this material leads to high cutting forces and temperatures, and poor machinability which requires the use of low cutting conditions. In ord… Show more

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Cited by 53 publications
(28 citation statements)
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References 17 publications
(26 reference statements)
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“…Boyer and Briggs [15] have presented a review on the history of the applications of beta titanium alloys in the aerospace industry for the past half century and the recent development of beta alloys such as Ti-15V-3Cr-3Al-2Sn and Ti-1023 as possible substitutes for various aircraft parts providing both improved performance and economic advantages. It has been reported by Baili et al [2] that Messier-Dowty uses the Ti-5553 beta titanium alloy for landing gear applications. However, work carried out on the machining of Ti-1023 with cryogenic coolant using carbon dioxide snow has shown that the machinability of this alloy cannot be improved further beyond a cutting speed of 100 m/min, due to the development of rapid tool wear, causing catastrophic tool failure [16].…”
Section: Introductionmentioning
confidence: 96%
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“…Boyer and Briggs [15] have presented a review on the history of the applications of beta titanium alloys in the aerospace industry for the past half century and the recent development of beta alloys such as Ti-15V-3Cr-3Al-2Sn and Ti-1023 as possible substitutes for various aircraft parts providing both improved performance and economic advantages. It has been reported by Baili et al [2] that Messier-Dowty uses the Ti-5553 beta titanium alloy for landing gear applications. However, work carried out on the machining of Ti-1023 with cryogenic coolant using carbon dioxide snow has shown that the machinability of this alloy cannot be improved further beyond a cutting speed of 100 m/min, due to the development of rapid tool wear, causing catastrophic tool failure [16].…”
Section: Introductionmentioning
confidence: 96%
“…These properties lead to the accumulation of high amounts of heat and mechanical stress around the cutting tool edge at high cutting speeds, subsequently increasing the cutting temperature and cutting force which leads to rapid cutting tool failure [2]. Hence, low cutting speeds and long production cycle times are common when machining aerospace materials.…”
Section: Introductionmentioning
confidence: 99%
“…From this, the optimum values in conventional machining of SKD11 were obtained as A3B1C1 with a cutting speed of 280 m/min, feed rate of 230 mm/min, and cutting depth of 0.5 mm, as shown in Figure 6. The mathematical model of cutting force depends on technological parameters (Vc, f, t) in the milling of SKD11 steel at room temperature, and is described by Equation (2).…”
Section: Experimental Machining At Room Temperaturementioning
confidence: 99%
“…Thermal-assisted machining (TAM) is one of the new technology solutions for the continuous development of advanced materials that have high hardness, less resistance to wear and thermal conductivity. It supports the cutting process, improves the machinability of material, increases machining productivity, improves surface quality, and reduces product cost [1,2]. With TAM, metals are softened and hardness decreases [3].…”
Section: Introductionmentioning
confidence: 99%
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