HB/Z 223.7-2003
Aircraft Assembly Technology Part 7: Riveting for Swaged Collar Type Rivet
飞机装配工艺 第7部分:环槽铆钉铆接
Catalogue
前言 → 1 范围 → 2 规范性引用文件 → 3 分类 → 4 紧固件和材料 → 5 工具 → 6 环槽铆钉的铆接 → 7 工具维护 → 8 质量控制 → 9 技术安全要求 → 附录A (规范性附录) 钛合金环槽铆钉的铆接 Foreword → 1 Scope → 2 Normative References → 3 Classification → 4 Fasteners and Materials → 5 Tools → 6 Riveting of Swaged Collar Type Rivet → 7 Tool Maintenance → 8 Quality Control → 9 Technical Safety Requirements → Appendix A (Normative) Riveting of Titanium Alloy Swaged Collar Type Rivet
Scope
This part specifies the process procedures, technical requirements, process parameters, process methods, tools used, and quality control for riveting of swaged collar type rivets. Appendix A specifies special requirements for riveting of titanium alloy swaged collar type rivets. This part is applicable to the riveting of swaged collar type rivets on metal structural parts.
本部分规定了环槽铆钉铆接的工艺程序、技术要求、工艺参数、工艺方法、所用工具和质量控制等。其中附录A规定了钛合金环槽铆钉铆接的特殊要求。本部分适用于金属结构件的环槽铆钉铆接。
Normative References
Keywords
Application Summary AI generated
Assembly workers and process engineers in aircraft manufacturing and maintenance use this standard to guide the riveting operations of swaged collar type rivets on metal structures. It ensures consistent and reliable riveting quality, which is critical for the safety and durability of aircraft structures.
飞机制造和维修企业的装配工人和工艺工程师使用本标准,用于指导金属结构件中环槽铆钉的铆接操作。该标准确保了铆接质量的一致性和可靠性,对飞机结构的安全性和耐久性至关重要。
AI Summary AI generated
This standard is Part 7 of the HB/Z 223 series, specifying the complete riveting process for swaged collar type rivets on aircraft metal structures, including two methods: pull riveting and upset riveting. It details each step from positioning and clamping, hole making, countersinking and chamfering, rivet insertion, to riveting and anti-corrosion treatment, along with tool requirements, quality control, and technical safety requirements. Appendix A adds special requirements for riveting titanium alloy swaged collar type rivets. This standard replaces the 1996 version and adds content such as riveting defect characteristics and elimination methods.
本标准为HB/Z 223系列的第7部分,规定了飞机金属结构件中环槽铆钉铆接的完整工艺,包括拉铆法和镦铆法两种分类。详细描述了从定位夹紧、制孔、制窝倒角、放钉到施铆及防腐蚀处理的每一步骤,并给出了工具要求、质量控制和技术安全要求。附录A专门针对钛合金环槽铆钉的铆接增加了特殊要求。该标准替代了1996年版本,新增了铆接缺陷特征及排除方法等内容。
Key Sentences extracted from text
本部分规定了环槽铆钉铆接的工艺程序、技术要求、工艺参数、工艺方法、所用工具和质量控制等。
环槽铆钉的孔位按产品图样上标注的环槽铆钉的位置确定。
孔径公差带为H10。
钉套成形后不得松动,表面应光滑,无裂纹,与结构表面不允许有间隙。
拉枪的拉力应不小于29kN,行程约为23mm。
This part specifies the process procedures, technical requirements, process parameters, process methods, tools used, and quality control for riveting of swaged collar type rivets.
The hole position of the swaged collar type rivet shall be determined according to the position of the swaged collar type rivet marked on the product drawing.
The hole diameter tolerance zone is H10.
After forming, the collar shall not be loose, the surface shall be smooth, free of cracks, and no gap with the structural surface is allowed.
The pulling force of the pull gun shall be not less than 29kN, and the stroke is approximately 23mm.
Standard Timeline
Changes from replaced version:
- 增加了环槽铆钉铆接的缺陷特征,原因及排除方法
- 增加了钛合金环槽铆钉铆接
- Added defect characteristics, causes, and elimination methods for swaged collar type rivet riveting
- Added riveting of titanium alloy swaged collar type rivets