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GB/T 41027-2021 English PDF

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GB/T 41027-2021: Aluminum alloy MJ thread with small flange blind hole self locking insert for aviation
Status: Valid
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GB/T 41027-2021English134 Add to Cart 3 days [Need to translate] Aluminum alloy MJ thread with small flange blind hole self locking insert for aviation Valid GB/T 41027-2021

PDF similar to GB/T 41027-2021


Standard similar to GB/T 41027-2021

GB/T 28878.10   GB/T 28878.9   GB/T 45612   GB/T 45572   

Basic data

Standard ID GB/T 41027-2021 (GB/T41027-2021)
Description (Translated English) Aluminum alloy MJ thread with small flange blind hole self locking insert for aviation
Sector / Industry National Standard (Recommended)
Classification of Chinese Standard V20
Word Count Estimation 6,636
Issuing agency(ies) State Administration for Market Regulation, China National Standardization Administration

GB/T 41027-2021: Aluminum alloy MJ thread with small flange blind hole self locking insert for aviation


---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.
Aluminum alloy MJ thread with small flange blind hole self locking insert for aviation ICS 49:030:99 CCSV20 National Standards of People's Republic of China Aviation MJ thread aluminum alloy with small flange blind hole Self-locking inserts foraviation (ISO 13598:2000, Aerospace-Inserts, self-locking, withMJthreads, Published on 2021-12-31 2022-07-01 Implementation State Administration for Market Regulation Released by the National Standardization Administration directory Preface I 1 Scope 1 2 Normative references 1 3 Terms and Definitions 1 4 Structure and dimensions 1 5 Application example 3

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 of Standardization Documents" drafted: This document is equivalent to ISO 13598:2000 "Coated or uncoated, made of metallic materials, reduced flanges, with MJ threads for aerospace purposes: Dimensions of closed self-locking inserts: A chapter "Terms and Definitions" has been added to this document: The following minimal editorial changes have been made to this document: --- In order to coordinate with the existing standards, the standard name is changed to "MJ threaded aluminum alloy with small flange blind hole self-locking inserts for aviation": Please note that some content of this document may be patented: The issuing agency of this document assumes no responsibility for identifying patents: This document is proposed and managed by the National Aircraft Standardization Technical Committee (SAC/TC435): This document is drafted by: State-owned Wuhu Machinery Factory, China Aviation Comprehensive Technology Research Institute, Yixiang Intelligent Equipment (Shenzhen) Co:, Ltd:, China Luoyang Electro-optical Equipment Research Institute of Aviation Industry Group Corporation, AVIC Tongfei South China Aircraft Industry Co:, Ltd:, Hefei Jianghang Aircraft Equipment Co:, Ltd: Company, Shenyang Aerodynamics Research Institute of China Aviation Industry Corporation, China Standardization Association: The main drafters of this document: Kan Yan, Shao Wentao, Li Haicheng, Shan Yimeng, Fan Xin, Yuan Rong, Zhu Meng, Li Wei, Cheng Zonghui, Guanjiadong, Li Xiaofei, Li Junsheng, Yi Rong, Ren Haitao, Dan Dan, Liu Zhanping, Lu Yuan, Yang Bao, Kan Qi, Wang Yin, Tong Peisheng: Aviation MJ thread aluminum alloy with small flange blind hole Self-locking inserts

1 Scope

This document specifies the dimensions of coated or uncoated MJ thread with small flange metal blind hole self-locking inserts: This document applies to Aerospace MJ Threaded Metal Blind Hole Self-Locking Inserts with Small Flange: Note: The strength and temperature grade of MJ thread with small flange metal blind hole self-locking inserts are determined by the core material and sealant, which are not specified in this document:

2 Normative references

The contents of the following documents constitute essential provisions of this document through normative references in the text: Among them, dated citations documents, only the version corresponding to that date applies to this document; for undated references, the latest edition (including all amendments) applies to this document: ISO 5855-2:1999 Aerospace MJ threads - Part 2: Limiting dimensions of bolt and nut threads (Aerospace-MJ threads-Part 2:Limitdimensionsforboltsandnuts)

3 Terms and Definitions

There are no terms and definitions that need to be defined in this document:

4 Structure and dimensions

The structure and dimensions of the inserts are shown in Figure 1 and Table 1:

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