49.045 结构和结构元件 标准查询与下载

20/30394594 DC BS IEC 62899-506-1 印刷电子产品 第 506-1 部分 质量评估-印刷加热元件的加速应力测试

BS IEC 62899-506-1. Printed electronics - Part 506-1. Quality assessment- Accelerated stress test of printed heating element

ASTM E3266-20 限制摩擦的飞机刹车测量和报告的标准指南

Standard Guide for Friction-Limited Aircraft Braking Measurements and Reporting

ASTM F3120/F3120M-20 通用航空器防冰标准规范

1.1 This specification covers international standards for ice protection aspects of airworthiness and design for “general aviation” aircraft. 1.2 The applicant for a design approval must seek the individual guidance of their respective civil aviation authority (CAA) body concerning the use of this specification as part of a certification plan. For information on which CAA regulatory bodies have accepted this specification (in whole or in part) as a means of compliance to their Small Aircraft Airworthiness regulations (hereinafter referred to as “the Rules”), refer to ASTM F44 webpage (www.ASTM.org/COMMITTEE/ F44.htm) which includes CAA website links. 1.3 Units—The values are stated in units common to the field of aircraft icing. Typically SI or inch-pound units are used, but in some cases this has resulted in the use of mixed units due to the historical development of these values. In cases where values are given in one system with the other system following in brackets, the values stated in each system are not necessarily exact equivalents; therefore, to ensure conformance with the standard, each system shall be used independently of the other, and values from the two systems shall not be combined. 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 Specification for Ice Protection for General Aviation Aircraft

ASTM F3114-19 结构标准规范

Standard Specification for Structures

ASTM F548-19 航空航天透明塑料划痕强度的标准试验方法

1.1 This test method covers the visual inspection of shallow or superficial scratches on the surface of aerospace transparent plastic materials. 1.2 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. 1.3 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 Intensity of Scratches on Aerospace Transparent Plastics

ASTM F3120/F3120M-19 通用航空器防冰标准规范

Standard Specification for Ice Protection for General Aviation Aircraft

ASTM F3409-19e1 简易飞机载荷测定的标准实施规程

1.1 This practice provides an acceptable, and simplified, means of determining certain design loads criteria and conditions for fixed wing aircraft. In particular, the practice provides overall aircraft flight loads and flight conditions as well as control surface loads, wing loads, gust load factors, and gust loads on stabilizing surfaces. 1.2 This practice is intended to be referenced by other standards that define requirements for comprehensive aircraft loads. This practice does not provide all aircraft loads required for structural compliance. In addition, each load or condition determined through this practice has limitations on its use within the relevant section to which it must adhere. 1.3 Units—The values given in this standard are in SI units and are to be regarded as standard. Any values given in parentheses are mathematical conversions to inch-pound (or other) units that are provided for information only and are not considered standard. The values stated in each system may not be exact equivalents. Where it may not be clear, some equations provide the units of the result directly following the equation. 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 Practice for Simplified Aircraft Loads Determination

ASTM F428-19 航空航天玻璃外壳划痕强度的标准试验方法

1.1 This test method covers the visual inspection of scratches on the glass surface of aerospace transparent enclosures. 1.2 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard. 1.3 This standard may involve hazardous materials, operations, and equipment. 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. 1.4 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 Intensity of Scratches on Aerospace Glass Enclosures

ASTM F3409-19 简易飞机载荷测定的标准实施规程

Standard Practice for Simplified Aircraft Loads Determination

BS EN 3001:2019 航空航天系列 用于飞机应用的钢化浮法玻璃层 技术规格

What is BS EN 3001- Tempered float glass plies for aircraft applications about?    BS EN 3001 specifies the requirements for tempered soda-lime float glass plies which are made from annealed glass either of the universally available type or of high light transmission type. The annealed glass is manufactured by a continuous process for general use.   Note 1: The plies are tempered by either a thermal or chemical process.   Note 2: The tempered glass is used mainly for cockpit glazing.  Who is BS EN 3001- Tempered float glass plies for aircraft applications for?   BS EN 3001 on tempered float glass plies for aircraft applications is useful for:

Aerospace series. Tempered float glass plies for aircraft applications. Technical specification

ASTM F1362-18 航空航天玻璃夹层材料剪切强度和剪切模量的标准试验方法

1.1 This test method covers the determination of the shear strength and shear modulus of interlayer materials that are restrained by relatively high modulus plies in laminated transparencies. This test method can be used with single or multiple plies of the same interlayer materials. 1.2 The values stated in SI units are to be regarded as the standard. The values in parentheses are for information only. 1.3 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. 1.4 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 Shear Strength and Shear Modulus of Aerospace Glazing Interlayer Materials

ASTM F790-18 航空塑料透明外壳材料测试标准指南

1.1 This guide is intended to summarize the standard test methods available on individual and composite materials utilized in fabrication of aerospace plastic transparent enclosures. As such, it is intended to specifically include transparent thermoplastics, transparent elastomers, and reinforced plastics, whether thermoplastic or thermosetting. 1.2 This guide is intended as an aid in the search for test methods pertinent to Aerospace Plastic Transparent Enclosures. It should be understood that all methods listed may not apply to all enclosures. 1.3 The standards included refer to the properties or aspects listed in Table 1. The properties or aspects are listed in alphabetical order and the descriptions used are intended to facilitate the search. 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 Guide for Testing Materials for Aerospace Plastic Transparent Enclosures

ASTM F3310-18 飞机非基本冰探测器的标准规范

1.1 This specification covers international standards for non-essential ice detection system aspects of airworthiness and design for aeroplanes. 1.2 The term “aeroplane” is utilized in this specification as it was originally conceived for normal category fixed wing aircraft with a certified maximum takeoff weight (MTOW) of 19 000 lb or less and a passenger seating configuration up to 19 as defined in the Rules. However, these standards may be more broadly applicable and their usage should not be unnecessarily limited. 1.3 The applicant for a design approval must seek the individual guidance of their respective CAA body concerning the use of this specification as part of a certification plan. For information on which CAA regulatory bodies have accepted this specification (in whole or in part) as a means of compliance to their Small Aircraft Airworthiness regulations (hereinafter referred to as “the Rules”), refer to ASTM F44 webpage (www.ASTM.org/COMMITTEE/F44.htm) which includes CAA website links. It is the responsibility of the Applicant to validate any applicability beyond that identified in this specification and request acceptance from the applicable CAA. 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 Specification for Non-Essential Ice Detectors for Aircraft

GSO ISO 5843-10:2016 航空航天 等效术语列表 第10部分：飞机结构

ISO 5843 establishes a list of equivalent terms used in the field of aerospace construction. This part of ISO 5843 gives those terms relating to aircraft structure. NOTE — In addition to the terms given in the three official ISO languages (English, French and Russian), this part of ISO 5843 gives the equivalent terms in German. These terms have been included at the request of ISO Technical Committee ISO/TC 20, and are published under the responsibility of the member body for Germany, F.R. (DIN). However, only the terms given in the official languages can be considered as ISO terms.

Aerospace -- List of equivalent terms -- Part 10: Aircraft structure

ASTM F520-16 航空透明件对人工诱导暴露环境的环境抗性的标准试验方法

4.1 This test method, when applied to aerospace transparencies of either monolithic glass/plastic or laminated combinations, is a measure of the ability of the transparency to withstand the effects of artificially induced environments. The test applies to on configurations employing electrically conductive coatings, and also to uncoated materials. 4.2 The resistance of the transparent enclosure to environmental effects may vary appreciably depending on the size, geometry, material of construction, coating integrity, coating density, and other factors. 1.1 This test method covers determination of the effects of exposure to thermal shock, condensing humidity, and simulated weather on aerospace transparent enclosures. 1.2 This test method is not recommended for quality control nor is it intended to provide a correlation to actual service life. 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 Exceptions—Certain inch-pound units are furnished in parentheses (not mandatory) and certain temperatures in Fahrenheit associated with other standards are also furnished. 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 and health practices and determine the applicability of regulatory limitations prior to use.

Standard Test Method for Environmental Resistance of Aerospace Transparencies to Artificially Induced Exposures

GSO ISO 10046:2015 飞机货舱容积计算方法

  Scope is not provided for this standard

Aircraft -- Methodology of calculating cargo compartment volumes

SAE AIR5320A-2015 结冰模拟试验设施概述

This SAE Aerospace Information Report (AIR) contains information on most of the major icing simulation ground facilities. An effort was made to obtain data from as many facilities as possible over a two year time period. The data in this document represents the state of the facilities in calendar year 1996. Facilities are constantly changing and upgrading and, therefore, some facility specifications may change during the life of this report. Of the 27 facilities described in this report, the primary use is split with approximately half for engine testing and half for wind tunnel testing. The facilities are limited to ground facilities and, therefore, icing tankers have not been included.

Summary of Icing Simulation Test Facilities

GOST R 56528-2015 在飞行条件中静电火箭和航天火箭技术产品防护的维护方法和手段. 创建要求和操作流程

Methods and means of maintenance of protection of products of rocket and space-rocket technics from a static electricity in the flight conditions. Requirements for creation and operation processes

SAE AS27647D-2014 轴承 BALL AIRFRAME ANTI-FRICTION EXTRA WIDE DOUBLE ROW Intermediate Duty

Scope is unavailable.

BEARING@ BALL@ AIRFRAME@ ANTI-FRICTION@ EXTRA WIDE@ DOUBLE ROW@ INTERMEDIATE DUTY

SAE AS28914C-2014 III型密封抗摩擦双排机架用自对准滚珠轴承

Scope is unavailable.

BEARING, ROLLER, SELF-ALIGNING, DOUBLE ROW, AIRFRAME, ANTI-FRICTION, SEALED, TYPE III