49.035 航空航天制造用零部件 标准查询与下载

GB/T 28878.1-2012 空间科学实验转动部件规范.第1部分：设计总则

GB/T28878 的本部分规定了空间科学实验转动部件的设计原则、流程和内容。 本部分适用于在空间环境中使用、高可靠性的空间科学实验转动部件的设计。 真他有效载荷和空间飞行器平台转动部件的设计可参照使用e 注﹕本标准中在不发生歧义的倌况下.空间科学实验转动部件简称转动部件。

Specification of the rotating component in space sciene experiments.Part 1:General requirements of design

GB 2279-1989 邻甲酚

o-Cresol

GB 7160-1987 微米级羰基镍粉

Micron nickel carbonyl powder

T/CASME 1444-2024 飞机静气弹风洞试验模型制造规范

本文件规定了飞机静气弹风洞试验模型制造规范的术语和定义、基本要求、结构与尺寸、原材料与标准件的选择、模型加工、检测规则、装配与运输。

Manufacturing specification for aircraft static aeroelastic wind tunnel test models

ASTM E2580-24 航空航天应用中使用的平板复合材料和夹层芯材的超声波试验的标准实施规程

Standard Practice for Ultrasonic Testing of Flat Panel Composites and Sandwich Core Materials Used in Aerospace Applications

T/CI 222-2023 三通管液压成形技术规范

本文件规定了三通管液压成形工艺的材料、设备、工装、工艺过程控制、质量控制、人员、安全等要求。 本文件适用于管外径为(5~150)mm、管壁厚为(0.5~2.5)mm的三通管液压成形,其中薄壁管的材料可适用于铝合金、不锈钢、钛合金等。

Technical specification for T-shape tube forming

T/CI 204-2023 小弯曲半径管内胀推弯成形工艺规程

本文件规定了小弯曲半径管内胀推弯成形工艺的材料、设备、工装、工艺过程控制、质量控制、人员、安全等要求。 本文件适用于管外径为(15~100)mm、管壁厚为(0.5~2.5)mm、弯曲半径与公称外径的比值不小于0.9、弯曲线在一个平面内的管材的内胀推弯成形，其中管的材料可适用于铝合金、不锈钢、高温合金。

Inner expansion and push bending forming process for small bending radius tube

T/WHQASA 4-2023 LED光源滑行灯通用技术规范

本文件规定了LED光源滑行灯的术语和定义、技术要求、试验方法、检验规则、标志、包装、运输和贮存。 本文件适用于LED光源滑行灯。

General Technical Specifications for LED Light Source Taxiing Lights

T/CI 113-2023 航空发动机压气机高精密 静子叶片电化学制造通用技术要求

本文件规定了航空发动机压气机高精密静子叶片电化学制造用阴极、夹具、电解液、电源、工艺参数、质量控制、技术安全等通用技术要求。 本文件适用于航空发动机压气机静子叶片的电化学加工制造,其他发动机压气机静子叶片的电化学加工制造也可参照执行。

General Technical Requirements for Electrochemical ManufactureofHigh Precision Stator Blades of Aeroengine Compressor

23/30477043 DC BS EN 2588 航空航天系列 轴承 耐腐蚀钢球面滑动轴承 带有装配槽 尺寸和负载

BS EN 2588. Aerospace series. Bearing, spherical plain in corrosion resisting steel with assembly slots. Dimensions and loads

T/SHJMRH 0051.1-2023 航空应急撤离滑基本 要求 第 1 部分：术语

航空应急撤离滑梯相关术语、定义。

basic requirements for aviation emergency evacuation slides-Part 1: term

T/SHJMRH 0051.4-2023 航空应急撤离滑基本 要求 第 4 部分：试验

1 范围 2 规范性引用文件 3 术语和定义 4 气囊模拟抛放和展开时间测定试验 4.1 试验目的 4.2 试验方法 4.3 试验结果判定标准 5 气囊刚性试验 5.1 试验目的 5.2 试验方法 5.3 试验结果判断标准 6 使用高度测定试验 6.1 试验目的 6.2 试验方法 6.3 试验结果判断标准 7 撤离速率测定试验 7.1 试验目的 7.2 试验方法 7.3 试验结果判断标准

basic requirements for aviation emergency evacuation slides-Part 4: experiment

T/SHJMRH 0051.2-2023 航空应急撤离滑基本 要求 第 2 部分：设计

1 范围 2 规范性引用文件 3 术语和定义 4 基本要求 5 设计对象 5.1 滑梯 5.2 打包工装及工艺 5.3 维修工具及工艺 5.4 检测程序 6 设计阶段划分 6.1 初样阶段 6.2 试样阶段 6.3 定型阶段 7 设计输入输出 7.1 输入 7.2 输出

basic requirements for aviation emergency evacuation slides-Part 2: design

T/SHJMRH 0051.3-2023 航空应急撤离滑基本 要求 第 3 部分：制造

1 范围 2 规范性引用文件 3 术语和定义 4 生产工艺基本要求 5 折叠打包基本要求 6 高压气瓶充气基本要求

basic requirements for aviation emergency evacuation slides-Part 3: manufacturing

ASTM E2662-15(2022) 航空航天应用中平板复合材料和夹层芯材的射线照相检验

1.1 This practice is intended to be used as a supplement to Practices E1742, E1255, E2033, and E2698. 1.2 This practice describes procedures for radiographic examination of flat panel composites and sandwich core materials made entirely or in part from fiber-reinforced polymer matrix composites. Radiographic examination is: a) Film Radiography (RT), b) Computed Radiography (CR) with Imaging Plate, c) Digital Radiography (DR) with Digital Detector Array’s (DDA), and d) Radioscopic (RTR) Real Time Radiography with a detection system such as an Image Intensifier. The composite materials under consideration typically contain continuous high modulus fibers (> 20 GPa), such as those listed in 1.4. 1.3 This practice describes established radiographic examination methods that are currently used by industry that have demonstrated utility in quality assurance of flat panel composites and sandwich core materials during product process design and optimization, process control, after manufacture inspection, in service examination, and health monitoring. Additional guidance can be found in E2533, Guide for Nondestructive Testing of Polymer Matrix Composites Used in Aerospace. 1.4 This practice has utility for examination of flat panel composites and sandwich constructions containing, but not limited to, bismaleimide, epoxy, phenolic, poly(amide imide), polybenzimidazole, polyester (thermosetting and thermoplastic), poly(ether ether ketone), poly(ether imide), polyimide (thermosetting and thermoplastic), poly(phenylene sulfide), or polysulfone matrices; and alumina, aramid, boron, carbon, glass, quartz, or silicon carbide fibers. Typical asfabricated geometries include uniaxial, cross ply and angle ply laminates; as well as honeycomb core sandwich constructions. 1.5 This practice does not specify accept-reject criteria and is not intended to be used as a means for approving flat panel composites or sandwich core materials for service. 1.6 To ensure proper use of the referenced standards, there are recognized nondestructive testing (NDT) specialists that are certified according to industry and company NDT specifications. It is recommended that a NDT specialist be a part of any composite component design, quality assurance, in service maintenance or damage examination. 1.7 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use. 1.8 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.

Standard Practice for Radiographic Examination of Flat Panel Composites and Sandwich Core Materials Used in Aerospace Applications

BS EN 4841-1:2022 航空航天系列 带衬套的减震架 技术规格

1   Scope This document specifies the required characteristics, inspection and test methods, qualification and acceptance conditions for shock mounts with bushes, designed to withstand static and dynamic loads possible for aerospace interior applications in the temperature range from −55 °C to 85 °C.

Aerospace series. Shock mount with bushes - Technical specification

BS EN 4841-2:2022 航空航天系列 带衬套的减震架 技术概述

1   Scope This document specifies the dimensions, masses, the tolerances and the required characteristics of shock mounts with bushes for aerospace interior application and without contamination by phosphate-ester hydraulic fluids.

Aerospace series. Shock mount with bushes - Technical overview

ASTM F2156-17(2022) 用网格线斜率测量透明部件光学畸变的标准试验方法

1.1 When an observer looks through an aerospace transparency, relative optical distortion results, specifically in thick, highly angled, multilayered plastic parts. Distortion occurs in all transparencies but is especially critical to aerospace applications such as combat and commercial aircraft windscreens, canopies, or cabin windows. This is especially true during operations such as takeoff, landing, and aerial refueling. It is critical to be able to quantify optical distortion for procurement activities. 1.2 This test method covers the apparatus and procedures that are suitable for measuring the grid line slope (GLS) of transparent parts, including those that are small or large, thin or thick, flat or curved, or already installed. This test method is not recommended for raw material. 1.3 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard. 1.3.1 Exception—The values given in parentheses are for information only. 1.4 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use. 1.5 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.

Standard Test Method for Measuring Optical Distortion in Transparent Parts Using Grid Line Slope

BS EN 2755:2021 航空航天系列 球形滑动轴承 采用耐腐蚀钢制成 带自润滑衬里 环境温度下负载升高 技术规格

What is BS EN 2755 about?    BS EN 2755 specifies the required characteristics, inspection and test methods, qualification and acceptance conditions for a spherical plain bearing in corrosion resisting steel, with self-lubricating liner, for elevated loads at ambient temperature intended for use in fixed or moving parts of the aircraft structure and control mechanisms.   Who is BS EN 2755 for?   BS EN 2755 on characteristics, inspection and test methods, qualification and acceptance conditions for a spherical plain bearing in corrosion resisting steel is applicable to:   Aerospace parts manufacturers          Spherical plain bearing manufacturers

Aerospace series. Bearing, spherical, plain in corrosion resisting steel with self-lubricating liner. Elevated load at ambient temperature. Technical specification

DS/EN 4614:2021 航空航天系列“带自润滑衬套的耐腐蚀钢球面滑动轴承，宽系列”“尺寸和载荷”“英制系列”

Aerospace series – Spherical plain bearing in corrosion resisting steel with self-lubricating liner, wide series – Dimensions and loads – Inch series