V31 发动机辅助系统及其附件 标准查询与下载

ARINC 596-4 PART II 空气传播选择调用系统

Airborne Selective Calling Unit

Airborne Selective Calling Unit

ARINC 561-11 SEC 9.0 模选择器系统设计

Mode Selector Unit Design

Mode Selector Unit Design

ARINC 573-7 SEC 5.0 飞行数据获得系统设计

Flight Data Acquisition Unit Design

Flight Data Acquisition Unit Design

ARINC 596-4 PART IV 选择调用系统清单

List of Selective Calling Codes

List of Selective Calling Codes

ARINC 603-1 ITEM 4.0 系统设计

Unit Design

Unit Design

SAE AS961B-1974 方形5.000B.C.有钉齿附件传动装置的设计标准

Drive - Studded, Accessory, 5.000 B.C. Square, Design Standard for

Drive - Studded, Accessory, 5.000 B.C. Square, Design Standard for

BS 2C 4:1973 飞机发动机制冷剂压力灌注接头尺寸规范

This British Standard specifies the basic dimensional requirements for connections on aircraft to ensure coupling to ground equipment supplying engine refrigerant under pressure. Provision is made for two sizes of connection: 3/4 inch — suitable for rates of flow up to 25 gallons (114 litres) per minute. 3/2 inch — suitable for rates of flow up to 120 gallons (546 litres) per minute.

Specification for coupling dimensions for aero-engine refrigerant pressure replenishment connections

BS C 17:1973 发动机启动用低压气体连接的连接件尺寸规范

This British Standard specifies the basic dimensional and installational requirements for connections on aircraft to ensure coupling to ground equipment supplying low pressure air for engine starting.

Specification for coupling dimensions for low pressure air connections for engine starting

ARINC 591-1972 AIDS系统快速进入记录器(QAR)

Quick Access Recorder for AIDS System (QAR)

Quick Access Recorder for AIDS System (QAR)

ARINC 591 BOOK-1972 AIDS系统快速进入记录器(QAR)

Quick Access Recorder for AIDS System (QAR)

Quick Access Recorder for AIDS System (QAR)

SAE ARP721-1970 涡轮机传动轴连接件

this arp applies to turbine engines that are to be used in helicopters.It provides the engline designer guide lines in achieving a satisfactory turbine engine drive shaft connection.

Turbine Drive Shaft Connection

SAE AIR1076-1970 飞机往复式气轮机发动机的防火装置

This document was issued in 1963 by the Powerplant Installation Committee of the Aerospace Industries Association (A.I.A.) as a design manual for all types of aircraft. Since then the originating Committee was dissolved and the manual became unavailable. In this period, advancements in aircraft fire protection methods have been produced by both governmental and private agencies that are not reflected in the manual. Recognizing this, but nevertheless feeling that there is much of present-day value in the manual, the SAE S-12 Helicopter Powerplant Committee believes it is performing a useful service to the helicopter industry in again making it available. Hence, the Committee herewith reissues without change, as an AIR, the entire original manual except for deletion of Acknowledgements. A future revision to this AIR to bring it up to date and to emphasize helicopter powerplant fire protection is under consideration by the S-12 Committee.

Aircraft Fire Protection for Reciprocating and Gas Turbine Engine Installations

SAE ARP676-1970 连杆末端(渐开线锯齿)

Lever Ends (Involute Serrations)

Lever Ends (Involute Serrations)

SAE AS960A-1969 方形26.53B.C.有钉齿附件传动装置的设计标准

Drive - Studded, Accessory, 2.653 B.C. Square, Design Standard for

Drive - Studded, Accessory, 2.653 B.C. Square, Design Standard for

SAE AIR1090-1969 使用压力球隙测量点火励磁器输出电压脉冲

The purpose of this report is to provide reference information for equipment and procedure to be used in measurement of high tension ignition exciter output voltage pulses using a pressurized ball gap. This report includes a procedure for typical pulse voltage measurement using the pressurized ball gap, calibration procedure, and a description of the pressurized ball gap.

Ignition Exciter Output Voltage Pulse Measurement Using a Pressurized Ball Gap

SAE AIR713A-1967 确定,展示和证明涡轮发动机启动和电动回转特性的指南

This information report includes procedures for determining and presenting instandard form and terminology turbine engine starting and motoring characteristics. Itfurther includes the requirement for substantiating the accuracy of the information pre -sented

Guideline for Determining, Presenting, and Substantiating Turbine Engine Starting and Motoring Characteristics,

BS G 194:1965 飞行器用杠杆操作手动开关规范

This British Standard specifies the requirements for two classes of single-hole fixing, lever-operated manual switches for use in nominal 28 volt d.c. and 115/200 volt three-phase, 400 cycle a.c. systems in aircraft. Class 1 switches are sealed and are suitable for higher altitude and wider temperature conditions than Class 2, which are sealed only at the lever entry.

Specification for lever-operated manual switches for aircraft

SAE AS840-1964 SAE 17.6 立方英寸火花塞等级发动机手册，包括维护和大修

This manual was prepared under the auspices of the SAE Ignition Research Committee by the Spark Plug Rating Engine Standardization Panel of the Aircraft Piston Engine Ignition Subcommittee. It defines the standard engine to be used in determining spark plug preignition ratings. The engine is known as the SAE 17.6 Cubic Inch Spark Plug Rating Engine. The background of its design, development, and applications is contained in SAE publication SP-243.

Manual for the SAE 17.6 Cubic Inch Spark Plug Rating Engine Including Maintenance and Overhaul

SAE ARP373B-1963 传动轴力矩额定值

The following table shows the recommended allowable ratings for propeller shaft ends for low horsepower engines. Ratings are based on the formula: ALLOWABLE RATING = RATED TAKE-OFF PROPELLER SHAFT TORQUE IN FOOT POUNDS X CYLINDER BORE IN INCHES.

Propeller Shaft Torque Ratings

SAE AIR781-1962 确定发动机起动器传动力矩要求的指南

A general discussion is presented herein, to outline the starter functionswhich are necessary for a successful engine start.In addition, sample calculations are included to illustrate an accepted method of determiningthe engine starting time from known data. Further consideration is thengiven to the relationship between starter torque output and engine paüstrength and a generalized formula is presen-bed for calculating the theoreticaltransient torque peaks for a simplified starter-engine system. Samplecalculations for actual tests are included, and the results of these calculationsare compared with measured values.

Guide for Determining Engine Starter Drive Torque Requirements