Design and Application of Drilling Assembly Clamp for XX UAV Tail Bar Made of CFRP

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- Design and Application of Drilling Assembly Clamp for XX UAV Tail Bar Made of CFRP
- Aeronautical Manufacturing Technology Vol. 51, Issue 19, Pages: 87-88(2008)
- 作者机构：
  
  西北工业大学无人机研究所
- 作者简介：
- 基金信息：
- DOI：10.16080/j.issn1671-833x.2008.19.002
  CLC：
- Published：2008
- 稿件说明：
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蔡闻峰，周惠群，倪昌龄. 某型无人机碳纤维尾撑钻孔组合夹具设计与应用[J]. 航空制造技术, 2008, 51(19): 87-88.

Design and Application of Drilling Assembly Clamp for XX UAV Tail Bar Made of CFRP[J]. Aeronautical Manufacturing Technology, 2008, 51(19): 87-88.
蔡闻峰，周惠群，倪昌龄. 某型无人机碳纤维尾撑钻孔组合夹具设计与应用[J]. 航空制造技术, 2008, 51(19): 87-88. DOI： 10.16080/j.issn1671-833x.2008.19.002.

Design and Application of Drilling Assembly Clamp for XX UAV Tail Bar Made of CFRP[J]. Aeronautical Manufacturing Technology, 2008, 51(19): 87-88. DOI： 10.16080/j.issn1671-833x.2008.19.002.

结合设计图样及材料特性

研究了一种用于加工碳纤维尾撑的工艺及钻孔组合夹具

并阐述了其设计要点。

According to the property of material and design drawings

a kind of machining process for CFRP tail bar and drilling assembly clamp are studied

and the key design points of the drilling assembly clamp are introduced.

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