SAE ARP 1270A-2000
飞行器舱加压控制标准

Aircraft Cabin Pressurization Control Criteria

SAE ARP 1270A-2000 发布历史

These recommendations cover the basic criteria for the design of aircraft cabin pressurization control systems as follows: 1. To ensure aircraft safety 2. Physiology and limits which govern maximum permissible pressure time relations as related to aircraft passenger comfort. 3. General pressurization control system performance requirements design to satisfy (2). 4. Technical considerations relevant to satisfying (3). The purpose of the recommended practice is to provide the aerospace industry with guidelines as to the pertinent technology relating to the physiological consideration, the technical system requirements and design objectives for aircraft pressurization control systems. This recommended practice is applicable to pressurized aircraft regardless of the number of passengers or crew. The pressurization control system must provide maximum safety and passenger and crew comfort as a result of changes in cabin pressure altitude during the entire aircraft flight and during ground operation.

SAE ARP 1270A-2000由美国机动车工程师协会 US-SAE 发布于 2000-04-01。

SAE ARP 1270A-2000 在中国标准分类中归属于: V36 总体技术要求，在国际标准分类中归属于: 49.090 机上设备和仪器。

SAE ARP 1270A-2000的历代版本如下：

• 2000年04月01日 SAE ARP 1270A-2000 飞行器舱加压控制标准

SAE ARP 1270A-2000 飞行器舱加压控制标准 于 2010-05-11 变更为 SAE ARP 1270B-2010 飞机座舱增压控制标准。

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标准号

SAE ARP 1270A-2000

发布日期

2000年04月01日

实施日期

废止日期

无

中国标准分类号

V36

国际标准分类号

49.090

发布单位

美国机动车工程师协会

代替标准

SAE ARP 1270B-2010

适用范围

These recommendations cover the basic criteria for the design of aircraft cabin pressurization control systems as follows: 1. To ensure aircraft safety 2. Physiology and limits which govern maximum permissible pressure time relations as related to aircraft passenger comfort. 3. General pressurization control system performance requirements design to satisfy (2). 4. Technical considerations relevant to satisfying (3). The purpose of the recommended practice is to provide the aerospace industry with guidelines as to the pertinent technology relating to the physiological consideration, the technical system requirements and design objectives for aircraft pressurization control systems. This recommended practice is applicable to pressurized aircraft regardless of the number of passengers or crew. The pressurization control system must provide maximum safety and passenger and crew comfort as a result of changes in cabin pressure altitude during the entire aircraft flight and during ground operation.