SAE AS 707B-1988
真空胎飞机轮的热敏感膨胀压力释放装置

Thermal Sensitive Inflation Pressure Release Devices for Tubeless Aircraft Wheels

SAE AS 707B-1988 发布历史

This standard establishes minimum design, installation, qualification, and operational requirements for thermally actuated, pressure release devices for use only in tubeless tire type aircraft wheels. These devices are designed to completely release the contained inflation pressure from a tubeless tire and wheel assembly when brake generated heat causes the assembly to exceed a safe temperature operating level. The objective is to prevent tire or wheel rupture from brake generated heat which could cause serious personnel injuries or serious aircraft operational hazards.

SAE AS 707B-1988由美国机动车工程师协会 US-SAE 发布于 1988。

SAE AS 707B-1988 在中国标准分类中归属于: V42 起飞着陆装置。

SAE AS 707B-1988的历代版本如下：

• 1988年 SAE AS 707B-1988 真空胎飞机轮的热敏感膨胀压力释放装置

SAE AS 707B-1988 真空胎飞机轮的热敏感膨胀压力释放装置 于 2013-11-01 变更为 SAE AS 707C-2013 无内胎飞机轮的热敏感膨胀压力释放装置。

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标准号

SAE AS 707B-1988

发布日期

1988年

实施日期

废止日期

无

中国标准分类号

V42

国际标准分类号

83.160.20

发布单位

US-SAE

代替标准

SAE AS 707C-2013

适用范围

This standard establishes minimum design, installation, qualification, and operational requirements for thermally actuated, pressure release devices for use only in tubeless tire type aircraft wheels. These devices are designed to completely release the contained inflation pressure from a tubeless tire and wheel assembly when brake generated heat causes the assembly to exceed a safe temperature operating level. The objective is to prevent tire or wheel rupture from brake generated heat which could cause serious personnel injuries or serious aircraft operational hazards.