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GB/T 44562-2024 PDF English

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GB/T 44562-2024: Titanium 100° flush head blind fastener for aerospace
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GB/T 44562-2024English599 Add to Cart 5 days [Need to translate] Titanium 100° flush head blind fastener for aerospace

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Basic data

Standard ID GB/T 44562-2024 (GB/T44562-2024)
Description (Translated English) Titanium 100�� flush head blind fastener for aerospace
Sector / Industry National Standard (Recommended)
Classification of Chinese Standard V20
Classification of International Standard 49.030.60
Word Count Estimation 30,360
Date of Issue 2024-09-29
Date of Implementation 2025-04-01
Issuing agency(ies) State Administration for Market Regulation, China National Standardization Administration

GB/T 44562-2024: Titanium 100° flush head blind fastener for aerospace


---This is a DRAFT version for illustration, not a final translation. Full copy of true-PDF in English version (including equations, symbols, images, flow-chart, tables, and figures etc.) will be manually/carefully translated upon your order.
ICS 49.030.60 CCSV20 National Standard of the People's Republic of China Titanium alloy 100° countersunk head large foot thread for aviation Blind rivets Released on 2024-09-29 2025-04-01 Implementation State Administration for Market Regulation The National Standardization Administration issued

Table of Contents

Preface III 1 Scope 1 2 Normative references 1 3 Terms and Definitions 1 4 Requirements 1 4.1 Component 1 4.2 Nail body 3 4.3 Core rod 5 4.4 Nail sleeve 7 4.5 Ring 8 4.6 Drive nut 9 Appendix A (Normative) Technical Requirements 11 Appendix B (Normative) Cross slot 24 Appendix C (Normative) MJ Modified Thread 25

Foreword

This document is in accordance with the provisions of GB/T 1.1-2020 "Guidelines for standardization work Part 1.Structure and drafting rules for standardization documents" Drafting. Please note that some of the contents of this document may involve patents. The issuing organization of this document does not assume the responsibility for identifying patents. This document is proposed and coordinated by the National Aircraft Standardization Technical Committee (SAC/TC435). This document was drafted by. China Aviation Technology Research Institute, Shenyang Aircraft Design and Research Institute of China Aviation Industry Corporation, Aerospace Manufacturing Technology Research Institute, Aerospace Precision Industry Co., Ltd. The main drafters of this document. Hou Kun, Zou Xiaohui, Li Weiqiang and Zhang Xiaobin. Titanium alloy 100° countersunk head large foot thread for aviation Blind rivets

1 Scope

This document specifies the structure, size and specifications of titanium alloy 100° countersunk head large foot threaded blind rivets (hereinafter referred to as "blind rivets") for aviation use. Technical requirements. This document applies to the design, manufacture and acceptance of titanium alloy 100° countersunk head large foot threaded blind rivets for aviation use.

2 Normative references

The contents of the following documents constitute essential clauses of this document through normative references in this document. For referenced documents without a date, only the version corresponding to that date applies to this document; for referenced documents without a date, the latest version (including all amendments) applies to This document. GB/T 90.2 Fastener marking and packaging GB/T 2965 Titanium and titanium alloy bars GB/T 3078 High-quality structural steel cold-drawn steel GB/T 4237 Stainless steel hot-rolled steel plates and strips GB/T 6403.3 Knurling GB/T 14994 High temperature alloy cold drawn bars GB/T 22271.3-2016 Plastics Polyoxymethylene (POM) molding and extrusion materials Part 3.General product requirements HB5800 General Tolerance

3 Terms and definitions

There are no terms or definitions that require definition in this document.

4 Requirements

4.1 Components 4.1.1 Structure The structure of the blind rivet is shown in Figure 1, the dimensions and mass are shown in Table 1, and the usage example is shown in Figure 2.The locking points on the rivet body are evenly arranged along the circumference. 3 places (120° apart). ...

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