发动机辅助系统及其附件标准-分析测试百科网

SAE AIR4068A-1996 燃气涡轮发射探头参数

This report describes the concept and data analysis of the probe factor (pf) scheme. Conclusions are drawn and recommendations made for action to further the requirements for improved methods and procedures in emissions sampling technology.

Gas Turbine Emission Probe Factors

ICS: 49.050
CCS: V31
发布: 1996-09-01
实施

SAE AS20C-1996 飞机用往复式发动机性能的定义

This document lists definitions that are commonly used in describing aircraft reciprocating engine performance.

Definitions, Aircraft Reciprocating Engine Performance

ICS: 01.040.49;49.050
CCS: V31
发布: 1996-05-01
实施

SAE ARP1533-1996 飞机涡轮发动机气体排放的计算规程

This is a procedure for calculation of gaseous emissions data, specifically, emission index, fuel-air ratio, and combustion efficiency for aircraft turbine engines based on the measurement of carbon monoxide, carbon dioxide, total hydrocarbons, and the oxides of nitrogen, This document includes instructions for the adjustment of the measured concentrations of the constituents of the exhaust for: a. the humidity of the inlet air, b. the car dioxide content of the inlet air, c. the interference of carbon dioxide and water on the measured concentrations of carbon monoxide and the oxides of nitrogen, d. the interference of oxygen on the measured concentration of carbon dioxide, e. the efficiency of the converter for changing other oxides of nitrogen to nitric oxide, and f. the basis of measurement (semidry or wet).

Procedure for the Calculation of Gaseous Emissions from Aircraft Turbine Engines

ICS: 49.050
CCS: V31
发布: 1996-01-01
实施

SAE AIR46B-1996 航空燃气涡轮发动机镍铬.镍铝热电偶的制备和使用

This SAE Aerospace Information Report (AIR) reviews the precautions which must be taken and the corrections which must be evaluated and applied if the experimental error in measuring the temperature of a hot gas stream with a thermocouple is to be kept to a practicable minimum. Discussions will focus on Type K thermocouples. These are defined in NBS Monograph 125 as nickel-chromium alloy versus nickel-aluminum alloy thermocouples.

Preparation and Use of Chromel-Alumel Thermocouples for Aircraft Gas Turbine Engines

ICS: 49.050
CCS: V31
发布: 1996
实施

HB 7173-1995 飞机发电机反流断路器通用规范

本标准规定了额定电压为28.5V的飞机直流发电机反流断路器（以下简称反流断路器）的通用要求、试验方法和检验规则。　　本标准适用于额定电压为28.5V的飞机直流发电机反流断路器。

General specification for reverse flow circuit breakers of aircraft generators

ICS
CCS: V31
发布: 1995-12-13
实施: 1996-01-01

SAE AIR784C-1995 气轮机发动机的发动机设计和燃烧器配置与电气点火系统的选择和性能之间的相互关系

To describe typical ignition systems in general usage and their parameters that warrant considerations during the development of a gas turbine engine. To describe those parameters in gas turbine engine design and, in particular, burner configurations that influence the type selection and performance of the ignition system. To indicate the areas where future work may uncover important effects having a direct bearing on certain interrelated parameters, with resultant benefits to both the engine and ignition designers. To provide the designer of gas turbine engines with a working knowledge of the interrelation between engine performance objectives and the part played by ignition in meeting the objectives. To present a definitive collection of standard references, nomenclature, and descriptive terminology sufficient to provide a basis for design approach in specification of gas turbine ignition systems. To stimulate further work necessary in the development of knowledge of the unknown, interrelated parameters.

Interrelation of Engine Design and Burner Configuration with Selection and Performance of Electrical Ignition Systems for Gas Turbine Engines