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Aluminium alloy MJ threads inserts of self-locking floating nut for aviation
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Basic data
| Standard ID | GB/T 36153-2018 (GB/T36153-2018) |
| Description (Translated English) | Aluminium alloy MJ threads inserts of self-locking floating nut for aviation |
| Sector / Industry | National Standard (Recommended) |
| Classification of Chinese Standard | V20 |
| Classification of International Standard | 49.030.99 |
| Word Count Estimation | 5,557 |
| Date of Issue | 2018-05-14 |
| Date of Implementation | 2018-12-01 |
| Regulation (derived from) | National Standards Announcement No. 6 of 2018 |
| Issuing agency(ies) | State Administration for Market Regulation, China National Standardization Administration |
GB/T 36153-2018: Aluminium alloy MJ threads inserts of self-locking floating nut 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.
(MJ thread aluminum alloy with floating self-locking nuts for aviation)
ICS 49.030.99
V20
National Standards of People's Republic of China
Aviation MJ threaded aluminum alloy belt
Insert piece for swimming self-locking nut
Published on.2018-05-14
2018-12-01 implementation
State market supervision and administration
China National Standardization Administration issued
Foreword
This standard was drafted in accordance with the rules given in GB/T 1.1-2009.
This standard was proposed by China Aviation Industry Corporation.
This standard is under the jurisdiction of the National Aircraft Standardization Technical Committee (SAC/TC435).
This standard was drafted. China Aviation Integrated Technology Research Institute, Shanghai Aircraft Design and Research Institute, Shenyang Aircraft Design Institute.
The main drafters of this standard. Wang Xu, Hou Kun, Zheng Jianfeng, Zou Xiaohui, Yin Zhenbo.
Aviation MJ threaded aluminum alloy belt
Insert piece for swimming self-locking nut
1 Scope
This standard specifies the structure, dimensions and requirements of the inserts for the MJ-threaded aluminum alloy with flying self-locking nuts for aviation.
This standard is applicable to the inserts of MJ threaded aluminum alloy with aeronautical self-locking nut for aviation.
2 Normative references
The following documents are indispensable for the application of this document. For dated references, only dated versions apply to this article.
Pieces. For undated references, the latest edition (including all amendments) applies to this document.
GB/T 5267.4 fastener surface treatment corrosion resistant stainless steel passivation treatment
GJB3.2AMJ Threads Part 2. Limits for bolt and nut threads
HB7595 General specification for MJ threaded self-locking nuts with a temperature not higher than 425 ° C
MIL-A-8625F Aluminum and Aluminum Alloy Anodizing (Anodiccoatingsforaluminumandaluminumaloys)
AMS5731 Corrosion and heat resistant steel bars, wires, forges, tubes and rings, annealed (SteelCorrosionandHeat
Resistance,Bars,Wire,Forgings,Tubing,Rings,15Cr25.5Ni1.2Mo2.1Ti0.006B0.30V.Consumable
ElectrodeMelted, 1800°F (982°C) SolutionHeatTreated)
EN2694 Aerospace series aluminium alloy 6061 sheet and strip (Aerospaceseries-Aluminiumaloy
AL-P6061-T6orT62SheetandStrip-0.4mm≤a≤6mm)
EN3347 Aerospace series aluminium alloy 2024 extruded bars and profiles (Aerospaceseries-Aluminiumaloy
AL-P2024-T8511-ExtrudedbarandsectionAorD)
3 Structure, size and requirements
3.1 Structure and size
The structure and dimensions of the insert are as shown in Figure 1 and Table 1.
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