此文档已被声明为“非当前”。因此，建议本文件不适用于新设计。“非现行”是指以前被广泛引用的文件，并且可能在某些现有设计中继续需要这些文件。本航空航天标准确立了主要用于往复式发动机动力运输机的电气式温度仪表的最低sage性能标准，其运行可能会使仪表受到第3节规定的环境条件的影响。 4.本航空航天标准涵盖两种基本类型的温度仪表，如下所示:I型辐射计，由感温电阻元件的电阻变化驱动；通过感温电阻元件的温度变化获得电阻变化。II型:毫伏表型，通过改变热电偶的电动势输出来操作和驱动；通过温度传感热电偶的温度变化获得仪器的不同E.M.F.输入。

This document has been declared "NONCURRENT". It is recommended, therefore, that this document not be specified for new designs. "NONCURRENT" refers to those documents which have previously been widely referenced and may continue to be required on some existing designs.This Aerospace Standard establishes the minimum sage performance standards for electrical type temperature instruments primarily for use with reciprocating engine powered transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.4. This Aerospace Standard covers two basic types of temperature instruments as follows: TYPE I Radiometer type, actuated by changes in electrical resistance of a temperature sensing electrical resistance element; the resistance changes being obtained by temperature changes of the temperature sensing resistance element. TYPE II: Millivoltmeter type, operated and actuated by varying E.M.F. output of a thermocouple; the varying E.M.F. input to the instrument being obtained by temperature changes of the temperature sensing thermocouple.