2003
DOI: 10.1016/j.actamat.2003.08.023
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Progress in structural materials for aerospace systems11The Golden Jubilee Issue—Selected topics in Materials Science and Engineering: Past, Present and Future, edited by S. Suresh.

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Cited by 1,853 publications
(460 citation statements)
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“…Processing parameter combinations that lead to regions of high residual stress formation and high distortion have been determined, and the impact of processing parameters upon the predicted lamellar spacing has been presented. FUSION welding techniques have been utilized in the structural joining of safety-critical components across aerospace, [1] automotive, [2] and power generation [3,4] industries for many years, thanks to the considerable joint-integrity that they can offer, and their relatively low capital investment and production costs. [1] Whilst older welding methods such as tungsten inert gas (TIG) produce large weld pools and heat-affected zones [5] due to the size of the arc formed, the newer ''high power-density'' beam-type processes, such as laser welding, offer a much narrower fusion zone and heat-affected zone, [6] as the energy from the power source is much more focused.…”
mentioning
confidence: 99%
“…Processing parameter combinations that lead to regions of high residual stress formation and high distortion have been determined, and the impact of processing parameters upon the predicted lamellar spacing has been presented. FUSION welding techniques have been utilized in the structural joining of safety-critical components across aerospace, [1] automotive, [2] and power generation [3,4] industries for many years, thanks to the considerable joint-integrity that they can offer, and their relatively low capital investment and production costs. [1] Whilst older welding methods such as tungsten inert gas (TIG) produce large weld pools and heat-affected zones [5] due to the size of the arc formed, the newer ''high power-density'' beam-type processes, such as laser welding, offer a much narrower fusion zone and heat-affected zone, [6] as the energy from the power source is much more focused.…”
mentioning
confidence: 99%
“…In order to comply with such requirements, the improvement of surface properties of these materials is essential, as well as the understanding of the links among their composition, processing method, microstructure and properties (1) . In addition, high temperature resistant alloys must combine two major requirements when thermal cycles are applied: low scale growth rate and adequate scale adherence (2) .…”
Section: Introductionmentioning
confidence: 99%
“…Titanium and titanium alloys are widely used in the aircraft industry; however, their temperature capability of up to 600°C and relatively low wear resistance restrict their application for high-temperature parts of gas turbine engines [8,15]. Due to the strong demand for reducing aircraft engine weight, the temperature and wear performance of Ti alloys need to be improved.…”
Section: Introductionmentioning
confidence: 99%