用于冷喷涂增材制造的气刺喷嘴的概念——探讨防止堵塞问题的潜在解决方案

R. Raoelison, S. Msolli, S. Deng, A. Vashishtha, Ajay Sharma, D. Callaghan, Wassim Zaim-Mounajed, Teng Zhang, E. Padayodi, J. Sagot, Ramesh Raghavendra
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引用次数: 0

摘要

堵塞是由于粉末在喷嘴内壁积聚而导致的气体通道频繁变形现象,是长时间冷喷涂(CS)操作的主要问题,也是冷喷涂技术应用于增材制造的主要挑战。本研究旨在设计和整合用于冷喷涂作业的新型喷嘴设计,以解决传统圆形聚散(CD)喷嘴的堵塞问题。为此,本文提出了气喷喷管的概念,并用数值模拟方法对其进行了研究。气刺喷嘴允许气体在外部加速,一边受环境约束,另一边受轮廓刺壁约束。射流喷管沿射流壁面加速后,可产生较长的超声速气流。尖峰区域可以在尖端附近被截断,以提供一个用于粉末注射的平面。这种提出的策略将允许粉末颗粒加速通过一个更长的超音速核心区域,而不与喷嘴壁相互作用。通过适当的操作参数,气喷喷嘴可以完全减少或消除堵塞问题。在滞止压力为30 bar,温度为623K的条件下,以30 g/min的速度在两种喷嘴的中心线处喷射铝粉颗粒,并加速到相近的速度,通过数值模拟比较了两种相同马赫数的C-D喷嘴的效率和运行情况。粉末颗粒在射流喷嘴的超声速核心区域内加速而不与喷嘴壁发生相互作用,因此射流喷嘴是一种很有前途的无堵塞长时间射流喷嘴设计。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A Concept of Aerospike Nozzle for Cold Spray Additive Manufacturing—Towards a Potential Solution for Preventing the Issue of Clogging
The clogging, a frequent gas passage deformation phenomenon because of powder accumulation on inner nozzle wall, is a major issue in long duration Cold Spray (CS) operations and a major challenge for Cold spray technology to be adopted for additive manufacturing. This study aims to design and integrate new nozzle design in Cold Spray operations for addressing the clogging issues in traditional circular convergent-divergent (CD) nozzles. The concept of the Aerospike nozzle is proposed for that purpose and is investigated using numerical simulation methods in this paper. An aerospike nozzle allows gases to accelerate externally bounded by environment on one-side and contoured spike wall on other side. After accelerating along the spike wall, aerospike nozzle can generate a longer supersonic gas stream. The spike region can be truncated near the tip to provide a flat face for powder injection. This proposed strategy will allow powder particles to accelerate through a longer supersonic core region, without interacting with nozzle wall. With appropriate operating parameters, an aerospike nozzle can reduce or eliminate the clogging issue completely. The efficiency and operation of aerospike nozzle is compared with same Mach number C-D nozzle using numerical simulations at stagnation pressure of 30 bar and temperature of 623K, where the aluminium powder particles are injected at 30 g/min in the centerline of both nozzles and are accelerated to similar velocities. The powder particles are accelerated in supersonic core region of aerospike nozzle without interacting with nozzle wall, it is concluded that the aerospike nozzle can be a promising nozzle design to provide clogging free long duration CS operations.
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