SAE AIR 6232-2013
与飞机除冰/防冻液相互作用的飞机表面涂层

Aircraft Surface Coating Interaction with Aircraft Deicing/Anti-Icing Fluids

SAE AIR 6232-2013 发布历史

This SAE Aerospace Information Report (AIR) provides descriptions of test methods for determining if an aircraft surface coating of any thickness has adverse effects on aircraft deicing/anti-icing fluids with respect to fluid holdover time performance and aerodynamic performance. Although not the primary mandate of the G-12 Aircraft Ground Deicing Committee, this document also provides descriptions of suggested test methods for evaluating aircraft surface coatings with respect to durability, hardness, weathering, aerodynamic drag, ice adhesion, ice accumulation, contact angle, and thermal conductivity. These additional tests can provide informational data f

SAE AIR 6232-2013由美国机动车工程师协会 US-SAE 发布于 2013-08-12。

SAE AIR 6232-2013 在中国标准分类中归属于: V13 航空与航天用非金属材料，在国际标准分类中归属于: 49.040 有关航空航天制造用镀涂和有关工艺。

SAE AIR 6232-2013 发布之时，引用了标准

• ISO 8301-1991 绝热 稳态热阻及有关特性的测定 热流计法
• ISO 11507-2007 色漆和清漆.暴露涂层到人工风化环境.暴露在荧光紫外线灯和水环境
• ISO 22007-2-2008 塑料.热传导率和热扩散率的测定.第2部分:瞬时平面热源(发热盘)法
• ISO 22007-3-2008 塑料.热传导率和热扩散率的测定.第3部分:温度波形分析方法
• ISO 22007-4-2008 塑料.热传导率和热扩散率的测定.第4部分:激光闪光法
• SAE AIR 6130-2011 镉板循环腐蚀试验

SAE AIR 6232-2013的历代版本如下：

• 2013年08月12日 SAE AIR 6232-2013 与飞机除冰/防冻液相互作用的飞机表面涂层

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标准号

SAE AIR 6232-2013

发布日期

2013年08月12日

实施日期

废止日期

无

中国标准分类号

V13

国际标准分类号

49.040

发布单位

US-SAE

引用标准

ASTM C 518-2010 ASTM D 5930-2009 ASTM E 1225-2009 ASTM F 483-2009 ASTM F 484-2008 ASTM F 502-2008 ASTM F 519-2012 ASTM F 1110-2009 ISO 8301-1991 ISO 11507-2007 ISO 22007-2-2008 ISO 22007-3-2008 ISO 22007-4-2008 SAE AIR 6130-2011 SAE AMS 1424 SAE AMS 1428

适用范围

This SAE Aerospace Information Report (AIR) provides descriptions of test methods for determining if an aircraft surface coating of any thickness has adverse effects on aircraft deicing/anti-icing fluids with respect to fluid holdover time performance and aerodynamic performance. Although not the primary mandate of the G-12 Aircraft Ground Deicing Committee, this document also provides descriptions of suggested test methods for evaluating aircraft surface coatings with respect to durability, hardness, weathering, aerodynamic drag, ice adhesion, ice accumulation, contact angle, and thermal conductivity. These additional tests can provide informational data f