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| GB/T 44563-2024 | English | 359 |
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Titanium protruding head blind fastener for aerospace
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GB/T 44563-2024
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PDF similar to GB/T 44563-2024
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).
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