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GB/T 44563-2024 English PDF

Standard IDContents [version]USDSTEP2[PDF] delivered inStandard Title (Description)StatusPDF
GB/T 44563-2024English359 Add to Cart 4 days [Need to translate] Titanium protruding head blind fastener for aerospace Valid GB/T 44563-2024

PDF similar to GB/T 44563-2024


Standard similar to GB/T 44563-2024

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Basic data

Standard ID GB/T 44563-2024 (GB/T44563-2024)
Description (Translated English) Titanium protruding 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 18,180
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 44563-2024: Titanium protruding 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 convex head large foot threaded blind rivets for aviation 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

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 are. Hou Kun, Li Haitao, Wang Shoucai, Liu Fenglei, Lü Ruilin and Zhang Xiaobin. Titanium alloy convex head large foot threaded blind rivets for aviation

1 Scope

This document specifies the structure, size and technology of titanium alloy convex head large foot threaded blind rivets (hereinafter referred to as "blind rivets") for aviation Require. This document applies to the design, manufacture and acceptance of titanium alloy protruding 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 44562-2024 Titanium alloy 100° countersunk head large foot threaded blind rivets for aviation 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 assembly 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 spaced along the circumference. Evenly arrange 3 places (120° apart).



Price & Delivery

US$359.00 · In stock
Delivery: <= 4 days. True-PDF full-copy in English will be manually translated and delivered via email.
GB/T 44563-2024: Titanium protruding head blind fastener for aerospace
Status: Valid

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