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GB/T 36224-2018: Inserts for aviation, self-locking with MJ threads, open type, in aluminium alloy
Status: Valid
| Standard ID | Contents [version] | USD | STEP2 | [PDF] delivered in | Standard Title (Description) | Status | PDF |
| GB/T 36224-2018 | English | 89 |
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Inserts for aviation, self-locking with MJ threads, open type, in aluminium alloy
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GB/T 36224-2018
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PDF similar to GB/T 36224-2018
Basic data | Standard ID | GB/T 36224-2018 (GB/T36224-2018) | | Description (Translated English) | Inserts for aviation, self-locking with MJ threads, open type, in aluminium alloy | | Sector / Industry | National Standard (Recommended) | | Classification of Chinese Standard | V20 | | Classification of International Standard | 49.030.99 | | Word Count Estimation | 4,451 | | 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 36224-2018: Inserts for aviation, self-locking with MJ threads, open type, in aluminium alloy
---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.
(Aerospace MJ threaded aluminum alloy through hole self-locking insert)
ICS 49.030.99
V20
National Standards of People's Republic of China
Aviation MJ threaded aluminum alloy through hole self-locking insert
Insertsforaviation, self-lockingwithMJthreads,opentype,inaluminiumaloy
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, China Aviation Standard Parts Manufacturing Co., Ltd., Shanghai Aircraft Design and Research Institute,
Chengdu Aircraft Design Institute.
The main drafters of this standard. Yin Zhenbo, He Ying, Wang Xu, Hou Kun, Wang Shanling.
Aviation MJ threaded aluminum alloy through hole self-locking insert
1 Scope
This standard specifies the structure, dimensions and requirements of self-locking inserts for MJ-threaded aluminum alloy through-holes for aviation.
This standard applies to aviation MJ threaded aluminum alloy through-hole self-locking inserts.
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.
GJB3.2A MJ threading Part 2. Limiting dimensions for bolts and nut threads
HB7595 General specification for MJ threaded self-locking nuts with a temperature not higher than 425 ° C
ISO 8076 Aerospace process aluminium alloy anodizing without coloring chromic acid 40VDC treatment (Aerospaceprocess-Anodic
Treatmentofaluminiumaloys-Chromicacidprocess40VDC,undyedcoating)
EN3347 Aerospace series 2024 aluminum alloy extruded bar and profile A or D (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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