Application of High Speed Machining Technology in Aviation

被引:3
|
作者
Balon, Pawel [1 ]
Szostak, Janusz [2 ]
Kielbasa, Bartlomiej [1 ]
Rejman, Edward [3 ]
Smusz, Robert [3 ]
机构
[1] SZEL TECH SZeliga Grzegorz, Wojska Polskiego St 3, PL-39300 Mielec, Poland
[2] AGH Univ Sci & Technol, Dept Mfg Syst, Mickiewicza Ave 30-B2, PL-30059 Krakow, Poland
[3] Rzeszow Univ Technol, Fac Mech Engn & Aeronaut, Powstancow Warszawy Ave 8, PL-35959 Rzeszow, Poland
关键词
D O I
10.1063/1.5034899
中图分类号
O59 [应用物理学];
学科分类号
摘要
Aircraft structures are exposed to many loads during their working lifespan. Every particular action made during a flight is composed of a series of air movements which generate various aircraft loads. The most rigorous requirement which modem aircraft structures must fulfill is to maintain their high durability and reliability. This requirement involves taking many restrictions into account during the aircraft design process. The most important factor is the structure's overall mass, which has a crucial impact on both utility properties and cost-effectiveness. This makes aircraft one of the most complex results of modern technology. Additionally, there is currently an increasing utilization of high strength aluminum alloys, which requires the implementation of new manufacturing processes. High Speed Machining technology (HSM) is currently one of the most important machining technologies used in the aviation industry, especially in the machining of aluminium alloys. The primary difference between HSM and other milling techniques is the ability to select cutting parameters - depth of the cut layer, feed rate, and cutting speed in order to simultaneously ensure high quality, precision of the machined surface, and high machining efficiency, all of which shorten the manufacturing process of the integral components. In this paper, the authors explain the implementation of the HSM method in integral aircraft constructions. It presents the method of the airframe manufacturing method, and the final results. The HSM method is compared to the previous method where all subcomponents were manufactured by bending and forming processes, and then, they were joined by riveting.
引用
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页数:6
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