V29 航天用液压元件与附件 标准查询与下载

GB/T 41033-2021 CMOS集成电路抗辐射加固设计要求

本文件规定了CMOS集成电路抗辐射(总剂量、单粒子)加固设计的流程、设计要求、建模仿真、验证试验要求。 本文件适用于基于体硅/SOICMOS工艺的数字集成电路、模拟集成电路和数模混合集成电路的抗辐射(总剂量、单粒子)加固设计。

Design requirements of radiation hardening for CMOS IC

GB/T 30213-2013 飞机 液压附件 识别附件所适用液压油的标志

本标准规定「飞机液压系统中附件(不包括导管、软管及宾接头)的标志方案,用于在车间的装配和试验操作中正确地显示介质种类”本标志不用于机上识别。 注﹕航空航大设备导管和软管卜用于识别其所适用介质种类的标志方法规定于ISOl2。

Aircraft.Hydraulic components.Marking to indicate fluid for which component is approved

BS ISO 18487-1:2017 航空航天系列 适用于35MPa工作压力的钛管 英制系列

Aerospace series. Titanium tube for 35 MPa operating pressure. Inch series

ISO 18487-1:2017 航空航天系列. 工作压力35 MPa的钛管. 第1部分: 英制系列

This document is applicable to seamless tubing of circular cross-section made from titanium alloy and intended for use primarily in systems with system operating pressure of 35 MPa (5080 psi) (Pressure Class J), but usage is not limited to such applications.

Aerospace series - Titanium tube for 35 MPa operating pressure - Part 1: Inch series

ISO 23748:2016 航空航天系列. O形环槽. 尺寸

Aerospace series - O-ring grooves - Dimensions

BS EN 6123:2016 航空航天系列. 24°内圆锥外螺纹非扩口型管件端. 超细螺距. 英制系列. 设计标准

Aerospace series. Fitting end, 24 internal cone, external thread, flareless type. Extra fine thread pitch. Inch series. Design standard

BS ISO 8177:2015 航空航天. 流体系统用Ω形卡箍 (鞍型卡箍). 尺寸

Aerospace. Omega clamps (saddle clamps) for fluid systems. Dimensions

DIN EN 4686:2014 航空航天系列. 钛合金管连接件 8°30'. 装备盲箍; 德文和英文版本EN 4686-2014

Aerospace series - Pipe coupling 8°30′ in titanium alloy - Equipped blind ferrules; German and English version EN 4686:2014

BS ISO 7169:2014 航空航天.液压系统用24°锥形的、压力范围截至3000psi或21000kPa的可拆卸管接头.采购规范(英制/米制)

Aerospace. Separable tube fittings for fluid systems, for 24 cones, for pressures up to 3 000 psi or 21 000 kPa Procurement specification, inch/metric

SAE AS5230B-2014 非扩口式组合及异径配件

Scope is unavailable.

FITTING, UNION AND REDUCER, FLARELESS

SAE AS5238B-2014 非扩口到扩口式适配器配件

Scope is unavailable.

FITTING, ADAPTER, FLARELESS TO FLARED

SAE ARP725B-2014 滤清器元件清洗方法的评估效益

This SAE Aerospace Recommended Practice (ARP) presents a procedure for evaluating cleaning methods with respect to contaminant removal and element degradation particularly for metallic filter elements. A procedure for checking durability of cleaning equipment and a referee cleaning method are also included. It is applicable only to the evaluation of cleaning methods proposed for removal of service dirt and not for built-in dirt, liquid oxygen (LOX) cleaning, etc. Supporting information for use with the ARP is also included.

Evaluating Effectiveness of Filter Element Cleaning Methods

SAE AS6047B-2014 精密型非扩口隔板标准和减径统一配件

Scope is unavailable.

FITTING, UNION, STANDARD AND REDUCER, BULKHEAD, FLARELESS, PRECISION TYPE

BS ISO 12584:2013 航空航天. 液压部件. 颗粒物污染水平的特征

Aerospace. Hydraulic fluid components. Expression of particulate contamination levels

ISO 12584:2013 航空航天.液压机液体成份.微粒子污染物等级的表示

This International Standard defines the method of reporting and communicating the contamination (or cleanliness) level of components used in aerospace fluid systems. It also presents a coding system which allows cleanliness data to be reported, both in a shortened manner and in a complete manner, when communicating for reporting contamination level measurement results and for specifying cleanliness requirements.

Aerospace.Hydraulic fluid components.Expression of particulate contamination levels

SAE ARP1383C-2013 航空航天.液压元件的脉冲测试

This SAE Aerospace Recommended Practice (ARP) defines impulse test procedures that are recommended for hydraulic components.

Aerospace - Impulse Testing of Hydraulic Components

SAE AS5008A-2013 外部锻造活接头的液压配件

Fitting, Union, External Swage, Hydraulic

SAE ARP4493A-2013 航空航天.直接驱动伺服器

This SAE Aerospace Recommended Practice (ARP) is intended as a guide to aid in the specification and testing of Direct Drive Servovalves, but does not include the associated electronic controller. The recommendations contained in this ARP are primarily confined to the input and output characteristics of Direct Drive Servovalves (DDV). The only exception to this approach involves the definition and specification of chip shear force, which is not typically measurable by nondestructive external testing. The information presented should be useful in standardizing the terminology, the specification of physical and performance parameters, and the test procedures

Aerospace - Direct Drive Servovalves

SAE AS6046A-2012 精确型非扩口标准和减径十字交叉配件

Fitting, Cross, Standard and Reducer, Flareless, Precision Type

SAE AS4688B-2012 减径管非扩口和短非扩口T型配件

Fitting, Tee, Reducer, Flareless and Short Flareless