Study on ultrasonic vibration precision machining technology of aircraft fastener holes

Deyuan Zhang; Jing Liu

doi:10.3969/j.issn.1004-132X.2012.04.009

Study on ultrasonic vibration precision machining technology of aircraft fastener holes

Deyuan Zhang^*
, Jing Liu

^*此作品的通讯作者

机械工程及自动化学院

Beihang University

科研成果: 期刊稿件 › 文章 › 同行评审

4 引用（Scopus）

摘要

A kind of ultrasonic drill-reaming-countersink machining method and rotary ultrasonic vibration drilling tool system were proposed and developed, in order to solve a series of problems, such as long machining process route, low machining quality and low tool life for traditional manual multi-step drilling fastener holes on CFRP and titanium alloy stacks of aircraft skin. Experiments show that ultrasonic machining tools and method can obviously improve the quality and the processing efficiency of fastener big holes on CFRP and titanium alloy stacks and lower the production cost to satisfy the aircraft assembly industry requirements.

源语言	英语
页（从-至）	421-424
页数	4
期刊	Zhongguo Jixie Gongcheng/China Mechanical Engineering
卷	23
期	4
DOI	https://doi.org/10.3969/j.issn.1004-132X.2012.04.009
出版状态	已出版 - 25 2月 2012

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title = "Study on ultrasonic vibration precision machining technology of aircraft fastener holes",

abstract = "A kind of ultrasonic drill-reaming-countersink machining method and rotary ultrasonic vibration drilling tool system were proposed and developed, in order to solve a series of problems, such as long machining process route, low machining quality and low tool life for traditional manual multi-step drilling fastener holes on CFRP and titanium alloy stacks of aircraft skin. Experiments show that ultrasonic machining tools and method can obviously improve the quality and the processing efficiency of fastener big holes on CFRP and titanium alloy stacks and lower the production cost to satisfy the aircraft assembly industry requirements.",

keywords = "CFRP(carbon fiber reinforced plastic) and titanium alloy stacks, Core drill, Drilling tool, Machining method, Reaming, Ultrasonic vibration",

author = "Deyuan Zhang and Jing Liu",

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doi = "10.3969/j.issn.1004-132X.2012.04.009",

language = "英语",

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AU - Zhang, Deyuan

AU - Liu, Jing

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N2 - A kind of ultrasonic drill-reaming-countersink machining method and rotary ultrasonic vibration drilling tool system were proposed and developed, in order to solve a series of problems, such as long machining process route, low machining quality and low tool life for traditional manual multi-step drilling fastener holes on CFRP and titanium alloy stacks of aircraft skin. Experiments show that ultrasonic machining tools and method can obviously improve the quality and the processing efficiency of fastener big holes on CFRP and titanium alloy stacks and lower the production cost to satisfy the aircraft assembly industry requirements.

AB - A kind of ultrasonic drill-reaming-countersink machining method and rotary ultrasonic vibration drilling tool system were proposed and developed, in order to solve a series of problems, such as long machining process route, low machining quality and low tool life for traditional manual multi-step drilling fastener holes on CFRP and titanium alloy stacks of aircraft skin. Experiments show that ultrasonic machining tools and method can obviously improve the quality and the processing efficiency of fastener big holes on CFRP and titanium alloy stacks and lower the production cost to satisfy the aircraft assembly industry requirements.

KW - CFRP(carbon fiber reinforced plastic) and titanium alloy stacks

KW - Core drill

KW - Drilling tool

KW - Machining method

KW - Reaming

KW - Ultrasonic vibration

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DO - 10.3969/j.issn.1004-132X.2012.04.009

M3 - 文章

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JO - Zhongguo Jixie Gongcheng/China Mechanical Engineering

JF - Zhongguo Jixie Gongcheng/China Mechanical Engineering

IS - 4

ER -

Study on ultrasonic vibration precision machining technology of aircraft fastener holes

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