Error Analysis of Special Compound Measure

WANG Qian; LI Hui

doi:10.16080/j.issn1671-833x.2017.23/24.083

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Error Analysis of Special Compound Measure

更新时间：2025-10-30

- Error Analysis of Special Compound Measure
- Aeronautical Manufacturing Technology Vol. 60, Issue 23/24, (2017)
- 作者机构：
  
  1. 航空工业成都飞机工业（集团）有限责任公司复合材料加工厂,成都,610092
  2. 沈阳航空航天大学航空制造工艺国防重点学科实验室,沈阳,110136
- 作者简介：
- 基金信息：
- DOI：10.16080/j.issn1671-833x.2017.23/24.083
  CLC：
- Published：2017
- 稿件说明：
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王倩1，李辉1，高岩2，陈国强1，李静2，姜婷1，屈力刚2. 复合专用量具的研制及误差分析[J]. 航空制造技术, 2017, 60(23/24): 83-87. WANG Qian1，LI Hui1，GAO Yan2，CHEN Guoqiang1，LI Jing2，JIANG Ting1，QU Ligang2. Error Analysis of Special Compound Measure. Aeronautical Manufacturing Technology, 2017, 60(23/24): 83-87.

WANG Qian, LI Hui. Error Analysis of Special Compound Measure[J]. Aeronautical Manufacturing Technology, 2017, 60(23/24).
王倩1，李辉1，高岩2，陈国强1，李静2，姜婷1，屈力刚2. 复合专用量具的研制及误差分析[J]. 航空制造技术, 2017, 60(23/24): 83-87. WANG Qian1，LI Hui1，GAO Yan2，CHEN Guoqiang1，LI Jing2，JIANG Ting1，QU Ligang2. Error Analysis of Special Compound Measure. Aeronautical Manufacturing Technology, 2017, 60(23/24): 83-87. DOI： 10.16080/j.issn1671-833x.2017.23/24.083.

WANG Qian, LI Hui. Error Analysis of Special Compound Measure[J]. Aeronautical Manufacturing Technology, 2017, 60(23/24). DOI： 10.16080/j.issn1671-833x.2017.23/24.083.

摘要

针对飞机翼面后缘楔形结构的特点，在装配铆接时，必须根据准确的楔形角度和钉孔夹层厚度测量，选择合适的铆钉长度来实现双面埋头铆接的要求。针对楔形角度和钉孔夹层厚度实现一次性完成测量的要求，设计了一种复合专用量具。通过对量具的结构设计和可能产生的误差进行分析，完全能满足飞机翼面后缘楔形结构的测量要求。

Abstract

Considering the features of wedge structure on the trailing edge of aircraft wing surface during the assembly riveting

the rivets must be selected in appropriate length according to the accurate measurement of edge angle and laminated thickness of pin hole

so as to realize the double face riveting. This paper designs a special compound measure based on the requirement that wedge angle and laminated thickness of pin hole must be measured accurately by one time only

Therefore

the measurement requirements to wedge structure on the trailing edge of aircraft wing surface could be satisfied completely through the design in measure structure and the analysis on potential error.

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Related Institution

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