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Standard Test Method for Hail Impact Resistance of Aerospace Transparent Enclosures 航空航天透明外壳防雹抗冲击试验方法
发布日期: 2021-05-01
1.1 本试验方法包括在冰雹天气条件下,使用由严格控制的条件下模制的冰球组成的模拟冰雹,测定航空航天透明外壳(挡风玻璃、雨篷、窗户、透镜盖等)(以下简称挡风玻璃)的抗冲击性。该试验还应用于满足冰雹试验或设计或合同规定的性能要求。 1.2 单位- 以英寸-磅为单位的数值应视为标准值。括号中给出的值是到国际单位制的数学转换,仅供参考,不被视为标准值。 1.3 本标准并非旨在解决与其使用相关的所有安全问题(如有)。 本标准的用户有责任在使用前制定适当的安全、健康和环境实践,并确定监管限制的适用性。 有关具体的危险说明,请参阅第节 7. . 1.4 本国际标准是根据世界贸易组织技术性贸易壁垒(TBT)委员会发布的《关于制定国际标准、指南和建议的原则的决定》中确立的国际公认标准化原则制定的。 ====意义和用途====== 4.1 本试验方法应用于确定挡风玻璃的耐冰雹冲击性,以用于验收、设计、服务或研究目的。 通过对特定航空航天飞行器的安装挡风玻璃角度和速度使用该方法,可以为该飞行器的挡风玻璃建立设计允许值、标准和公差。
1.1 This test method covers the determination of the impact resistance of an aerospace transparent enclosure (windshield, canopy, window, lens cover, etc.), hereinafter called windshield, during hailstorm conditions using simulated hailstones consisting of ice balls molded under tightly controlled conditions. This test shall also be used to meet hail test or performance requirements that are specified by design or contract. 1.2 Units— The values stated in inch-pound units are to be regarded as standard. The values given in parentheses are mathematical conversions to SI units that are provided for information only and are not considered standard. 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. For specific hazard statements, see Section 7 . 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. ====== Significance And Use ====== 4.1 This test method shall be used to determine the hail impact resistance of windshields for acceptance, design, service, or research purposes. By using this method with the installed windshield angle and velocity of a specific aerospace vehicle, design allowables, criteria, and tolerances can be established for that vehicle's windshield.
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归口单位: F07.08
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