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GB/T 36150-2018: Aluminium alloy 100° countersunk head inserts for aviation
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Std ID	Version	USD	Buy	Deliver [PDF] in	Title (Description)
GB/T 36150-2018	English	109	Add to Cart	3 days [Need to translate]	Aluminium alloy 100° countersunk head inserts for aviation

GB/T 36150-2018: Aluminium alloy 100° countersunk head inserts for aviation

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(Aerospace Aluminum Alloy 100° Counterbored Hole Inserts) ICS 49.030.99 V20 National Standards of People's Republic of China Aluminum alloy 100° countersunk hole insert 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, Shenyang Aircraft Design Institute. The main drafters of this standard. Hou Kun, He Ying, Zheng Jianfeng, Yin Zhenbo, Zou Xiaohui. Aluminum alloy 100° countersunk hole insert

1 Scope

This standard specifies the structure, dimensions and requirements of 100° counterbored inserts for aerospace aluminum alloys. This standard applies to aerospace aluminum alloy 100 ° countersunk hole 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. MIL-A-8625F Aluminum and Aluminum Alloy Anodizing (Anodiccoatingsforaluminiumandaluminumaloys) 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. ...