HB/Z 223.3-2003
Aircraft assembling technology Part 3: Conventional riveting
飞机装配工艺 第3部分 普通铆接
Catalogue
前言 → 1 范围 → 2 规范性引用文件 → 3 紧固件和材料 → 4 工具 → 5 普通铆钉铆接 → 6 维护控制 → 7 质量控制 → 8 技术安全要求 → 附录A (规范性附录)高温合金铆钉铆接 → 附录B (规范性附录) 不锈钢、钛合金的铆接件铆接 Foreword → 1 Scope → 2 Normative References → 3 Fasteners and Materials → 4 Tools → 5 Conventional Rivet Riveting → 6 Maintenance Control → 7 Quality Control → 8 Technical Safety Requirements → Appendix A (Normative) Riveting of High-Temperature Alloy Rivets → Appendix B (Normative) Riveting of Stainless Steel and Titanium Alloy Riveted Parts
Scope
This part specifies the technical requirements, process parameters, process methods, materials and tools used, and inspection methods for conventional rivet riveting. Appendices A and B respectively specify special requirements for riveting of high-temperature alloy rivets and riveting of titanium alloy and stainless steel riveted parts. This part is applicable to the riveting of round head, flat cone head, countersunk head, 120° countersunk head, large flat round head conventional rivets and high-temperature alloy rivets.
本部分规定了普通铆钉铆接的技术要求、工艺参数、工艺方法、所用材料与工具，以及检验方法等。其中附录A和附录B分别规定了高温合金铆钉铆接、钛合金和不锈钢铆接件铆接的特殊要求。本部分适用于半圆头、平锥头、沉头、120°沉头、大扁圆头的普通铆钉和高温合金铆钉的铆接。
Normative References
Keywords
Application Summary AI generated
Aircraft assembly workers and process engineers use this standard to guide conventional rivet riveting operations in aircraft structural assembly. It provides complete process flows and technical parameters from positioning, hole making, countersinking to riveting, ensuring riveting quality and structural strength. This standard is critical for ensuring consistency and reliability in aircraft assembly.
飞机制造企业的装配工人和工艺工程师使用本标准来指导飞机结构件中普通铆钉的铆接操作。它提供了从定位、制孔、制窝到施铆的完整工艺流程和技术参数，确保铆接质量和结构强度。本标准对于保证飞机装配的一致性和可靠性至关重要。
AI Summary AI generated
This standard specifies the complete process for conventional rivet riveting in aircraft assembly, including technical requirements, process parameters, materials, tools, and inspection methods. It covers every operational detail from positioning and clamping, hole location determination, hole making and countersinking to riveting, and provides specific quality requirements for rivet heads, upset heads, and riveted parts. Appendices A and B propose special requirements for high-temperature alloy and titanium alloy/stainless steel riveting respectively. It is applicable to riveting operations for various types of conventional rivets.
本标准规定了飞机装配中普通铆钉铆接的完整工艺，包括技术要求、工艺参数、材料工具及检验方法。涵盖从定位压紧、确定孔位、制孔制窝到施铆的每一步操作细节，并给出了铆钉头、墩头及铆接件的具体质量要求。附录A和B分别针对高温合金及钛合金/不锈钢铆接提出了特殊要求。适用于多种类型普通铆钉的铆接操作。
Key Sentences extracted from text
铆钉孔轴线应垂直于零件表面，其偏差用孔量规凸边端面和零件表面之间的单向间隙量表示。
标准墩头应呈鼓形，不允许成“喇叭形”或“马蹄形”。
铆钉头应贴紧零件表面，允许不贴合的单向间隙不大于0.05mm，但这种铆钉数不大于铆钉排总钉数的10%。
蒙皮窝的深度应比铆钉头最小高度小0.02-0.05mm。
不允许铆钉孔有棱角、破边和裂纹。
The axis of the rivet hole shall be perpendicular to the part surface, and its deviation is indicated by the unilateral gap between the raised edge face of the hole gauge and the part surface.
The standard upset head shall be drum-shaped, and shall not be 'bell-mouthed' or 'horse-hoof-shaped'.
The rivet head shall fit tightly against the part surface, and the allowable unilateral gap for non-fit shall not exceed 0.05mm, but the number of such rivets shall not exceed 10% of the total number of rivets in the rivet row.
The depth of the skin countersink shall be 0.02-0.05mm less than the minimum height of the rivet head.
Rivet holes shall not have sharp edges, broken edges, or cracks.
Standard Timeline
Changes from replaced version:
- 增加了用铆钉孔量规检查孔轴线偏差方法
- 增加了《普通铆钉铆接所需的能量及顶把质量表》
- 增加了压铆所需压铆力
- 增加了高温合金铆钉铆接
- 增加了不锈钢和钛合金构件的铆接
- Added method for checking hole axis deviation using rivet hole gauge
- Added 'Energy required for conventional rivet riveting and bucking bar mass table'
- Added required riveting force for press riveting
- Added riveting of high-temperature alloy rivets
- Added riveting of stainless steel and titanium alloy components