GB/T 41033-2021 CMOS集成電路抗輻射加固設計要求

本文件規(guī)定了CMOS集成電路抗輻射(總劑量、單粒子)加固設計的流程、設計要求、建模仿真、驗證試驗要求。 本文件適用于基于體硅/SOICMOS工藝的數字集成電路、模擬集成電路和數?；旌霞呻娐返目馆椛?總劑量、單粒子)加固設計。

Design requirements of radiation hardening for CMOS IC

GB/T 30213-2013 飛機 液壓附件 識別附件所適用液壓油的標志

本標準規(guī)定「飛機液壓系統(tǒng)中附件(不包括導管、軟管及賓接頭)的標志方案,用于在車間的裝配和試驗操作中正確地顯示介質種類”本標志不用于機上識別。 注﹕航空航大設備導管和軟管卜用于識別其所適用介質種類的標志方法規(guī)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 適用于35MPa工作壓力的鈦管 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. 工作壓力35 MPa的鈦管. 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形環(huán)槽. 尺寸

Aerospace series - O-ring grooves - Dimensions

BS EN 6123:2016 航空航天系列. 24°內圓錐外螺紋非擴口型管件端. 超細螺距. 英制系列. 設計標準

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. 流體系統(tǒng)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. 鈦合金管連接件 8°30'. 裝備盲箍; 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.液壓系統(tǒng)用24°錐形的、壓力范圍截至3000psi或21000kPa的可拆卸管接頭.采購規(guī)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 非擴口式組合及異徑配件

FITTING, UNION AND REDUCER, FLARELESS

SAE AS5238B-2014 非擴口到擴口式適配器配件

FITTING, ADAPTER, FLARELESS TO FLARED

SAE ARP725B-2014 濾清器元件清洗方法的評估效益

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 精密型非擴口隔板標準和減徑統(tǒng)一配件

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

BS ISO 12584:2013 航空航天. 液壓部件. 顆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.液壓機液體成份.微粒子污染物等級的表示

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.液壓元件的脈沖測試

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 外部鍛造活接頭的液壓配件

Fitting, Union, External Swage, Hydraulic

SAE ARP4493A-2013 航空航天.直接驅動伺服器

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 精確型非擴口標準和減徑十字交叉配件

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

SAE AS4688B-2012 減徑管非擴口和短非擴口T型配件

Fitting, Tee, Reducer, Flareless and Short Flareless