V31 发动机辅助系统及其附件 标准查询与下载

ARINC 608A ITEM 4.0-1993 测试系统设计指南

Test System Design Guidelines

Test System Design Guidelines

ARINC 608A ITEM 3.0-1993 测试系统功能

Test System Functions

Test System Functions

ARINC 608A ITEM 2.0-1993 系统概念

System Concept

System Concept

SAE ARP588B-1993 燃气轮机转翼的垂直,单平面和软轴承型平衡机的描述和评价

This Aerospace Recommended Practice (ARP) delineates the technical specifications for rotating type of soft-bearing, single plane (i.e., static) balancing machine used for measuring the amount and angle of unbalance in gas turbine rotors.

Balancing Machines - Description and Evaluation Vertical, Single-Plane, Soft-Bearing Type for Gas Turbine Rotors

SAE ARP1755B-1993 清洗剂对飞机发动机物料损失的影响的测试方法

This SAE Aerospace Recommended Practice (ARP) covers the determination of the amount of stock loss caused by use of chemical cleaning agents on aircraft turbine engine materials. The evaluation is conducted on representative engine materials by determination of weight loss during total immersion in the cleaning solution with the weight-loss measurement converted to stock loss by calculation.

Effect of Cleaning Agents on Aircraft Engine Materials Stock Loss Test Method

HB 6630-1992 航空涡轮发动机起动系统设计要求

本标准规定了航空涡轮发动机起动系统设计所要求的发动机特性的标准表示方法。 　　本标准适用于发动机设计部门进行起动系统的设计。

Design requirements for aero turbine engine starting system

SAE MAP749B-1992 飞机涡轮发动机燃油系统部件耐久试验规程(室温污染燃料)

This recommended practice describes a method of conducting a room temperature endurance (contaminated fuel) test when the applicable specification requires non-recirculation of the contaminants. The objective of the test is to determine the resistance of the engine fuel system components to wear or damage caused by contaminated fuel. The method described herein calls for non-recirculation of the contaminants and is intended to provide a uniform distribution of the contaminant at the engine fuel system inlet.

AIRCRAFT TURBINE ENGINE FUEL SYSTEM COMPONENT ENDURANCE TEST PROCEDURE (ROOM TEMPERATURE CONTAMINATED FUEL)

SAE AS1875-1992 低压(500 psi)凸台的标准尺寸规格

This SAE Aerospace Standard (AS) presents all appropriate boss dimensions from .125 inch to 2.0 inch tube sizes. This AS has been developed for low pressure fuel systems and associated components operating up to 500 pounds per square inch (psi) as an alternate to MS33649 and MS16142(SH).

Boss, Low Pressure (500 psi) Standard Dimensions for

SAE AS1606-1992 燃气涡轮起动机(喷气式发动机燃料起动机)规范

This specification establishes the requirements for the (TBS) jet fuel starter for the (TBS) gas turbine engine used in the (TBS) aircraft. The jet fuel starter covered by this specification shall be designed to operate on jet fuel as a self-contained unit (subsequently called unit).

Gas Turbine Starter (Jet Fuel Starter) Specification

SAE AS1607A-1992 使用阀门,起动机控制和气动装置的飞机发动机通用规范(代替SAE ARP 1607)

This specification covers the general requirements for pneumatic control valve sfor use with the starters on aircraft gas turbine engines. This specification shall be used in conjunction with SAE AS 943, SAE ARP 949, and SAE AIR 1639.

Valve, Starter Control, Pneumatic, Aircraft Engine General Specification for (Replaced SAE ARP 1607)

ANSI B3.3-1992 飞行器发动机、发动机齿轮箱和辅助设备的滚动轴承.表面回火侵蚀剂

Applies to rolling element bearings used in aircraft engines, engine gearboxes and accessory applications.

Rolling Element Bearings - Aircraft Engine, Engine Gearbox, and Accessory Applications - Surface Temper Etch

AECMA PREN 3717-1991 航空航天系列.引擎防冻液管材选择.P1版

The present standard gives a selection of external diameters and thicknesses of tubes according to ISO 2964. These tubes shall be used for conveying fluids such as kerosen, oil, air, etc… for engine application.

Aerospace Series Tubes Selection for Engines Fluid Systems Issue P 1

SAE ARP1862A-1991 涡轮发动机气路清洁器的清洗效率的实验室测试方法

This SAE Aerospace Recommended Practice covers a laboratory procedure for determining the cleaning efficiency of aircraft turbine engine gas path cleaners. Results are indicative of cleaning compound performance in the compressor sections of installed aircraft turbine engines, when used in starter crank/soak/rinse application.

CLEANING EFFICIENCY OF TURBINE ENGINE GAS PATH CLEANERS Laboratory Test Method

BS G 243:1990 发动机用点火电缆规范(4kV直流)

Requirements and tests for a range of aircraft engine ignition cables suitable for use on high energy ignition circuits with working voltages not exceeding 4 kV DC. To be read in conjunction with BS G 230

Specification for igniter cables for engine use (4 kV d.c.)

ARINC 714-6 ITEM PT I-1990 选择调用系统规范

Selective Calling System Specification

Selective Calling System Specification

SAE AIR4090-1990 点火器陶瓷耐电弧试验

This report describes basic methods, typical results, limitations, and technical variables which may provide some relative performance expectations for different lots of the same material, or comparison characteristics for different materials. This testing alone does not assure satisfactory operation in the engine, i.e., there is not a direct relationship to actual engine performance. This report provides specific information on procedures for evaluating, on an accelerated comparison basis, the durability of ceramic materials under conditions of compressed electrical (capacitor) discharge.

Igniter Ceramic ARC Resistance Tests

SAE ARP594D-1990 燃气泵热能安全设计

These recommendations cover only those design factors which might cause the pump motor or pump housing to act as an autogenous or spark-ignition source for explosive fuel vapors within the airplane tank. This Aerospace Recommended Practice (ARP) recommends fuel booster pump design requirements commensurate with the presently known state-of-the-art, relating to the prevention of autogenous ignition of explosive fuel vapors and the confinement of autogenous or spark-initiated flames by means of flame-suppressing devices.

FUEL PUMP THERMAL SAFETY DESIGN

SAE ARP587B-1990 燃气涡轮转子用横向,双平面,软支撑型平衡机的描述和评估

This Aerospace Recommended Practice (ARP) specifies the requirements of balancing machines that make them suitable for the subject class of work. It was developed for soft-bearing balancing machines but may also be used for hard-bearing machines until ARP4048 is issued for that type of machine. Particular not should be taken that this ARP examines only the capability of a balancing machine to indicate the correct amount of dynamic or static/couple unbalance in specified proving rotors. Such rotors are commonly used for testing balancing machines to provide precisely controlled and comparable test results. Further tests of a particular machine may be necessary to assess the capability to balance rotors of different weights and configurations, rotors with outboard c.g. and/or correction planes, and those with disturbance causing features, such as rotors subject blade scatter, windage, etc.

Balancing Machines - Description and Evaluation Horizontal, Two-Plane, Soft-Bearing Type for Gas Turbine Rotors

NAVY MIL-S-22432 A-1990 伺服电动机的一般规格

This Fification mers the general requixements for servomotors. It is not cumplete in itself, ht should be used in ConjUnction witMhI L-S-81963 which will faonn nin herent part of this specification.

SERVOMOTORS, GENERAL SPECIFICATION FOR

AECMA PREN 2824-1990 航空和航天系列物质在热和火焰辐射下的燃烧行为的烟浓度和气体成分判断

This draft is now available for public comment and your views and technical comments on it would be appreciated. If you have no specific comments to make hut find it generally acceptable it would be helpful if you would notify US accordingly. Suggestions entailing revision of the text should indicate the preferred wording. Please quote the relevant clause number against any comment.

Aerospace Series Burning Behaviour, Determination of Smoke Density and Gas Components in the Smoke of Materials Under the Influence of Radiating Heat and Flames - Test Equipment, Apparatus and Media