V31 发动机辅助系统及其附件 标准查询与下载

ARINC 753-3-2001 高频数据链接系统

HF Data Link System

HF Data Link System 1994; Includes Supplements 1-3

ARINC 753-3 ITEM 3.0-2001 系统设计

System Design

System Design

ARINC 628P7 ITEM 5.0-2001 IFE系统安装

IFE System Installation

IFE System Installation

ARINC 628P1-3 ITEM 14.0-2001 系统设定初值或功率干扰

System Initialization/Power Interrupts

System Initialization/Power Interrupts

ARINC 562-2001 地形警报系统类似体

Terrain Awareness and Warning System (TAWS) - Analog

Terrain Awareness and Warning System (TAWS) - Analog

ARINC 562 BOOK-2001 地形警报系统类似体

Terrain Awareness and Warning System (TAWS) - Analog

Terrain Awareness and Warning System (TAWS) - Analog

ARINC 622-4 ITEM 2.0-2001 ACARS兼容系统

ACARS Compatible Systems

ACARS Compatible Systems

SAE AS177B-2001 飞机发动机操作说明书的编制

The operating instructions covered by this specification are published for the purpose of providing a background of engine operating information with which a pilot and his crew should be familiar when operating an aircraft powered by a particular engine model. Operating instructions also contain engine operational procedures which serve as a guide for: (1) the preparation of the right manual by the aircraft manufacturer, (2) operating an engine prior to the publication of the aircraft right manual, and (3) instructional purposes. This specification covers the requirements for format and outline of contents of operating instructions in published form or in manuscript from suitable for publication.

Operating Instructions for Aircraft Engines (Preparation of)

SAE ARP868C-2001 方法.燃气系统部件的压力释放测试

To describe useful methods for conducting pressure drop tests of fuel system components for MIL-F-8615 or similar requirements and to present general suggestions for improving accuracy of test results.

Method-Pressure Drop Tests for Fuel System Components

SAE ARP246C-2001 用于航空燃气涡轮发动机的发动机轴,坐标系和编号系统的定位

To establish an orientation standard for aircraft gas turbine engines and their component parts. Orientation of the engine, engine axis and coordinate system referred to herein shall be the conventional terminology used in all references to aircraft gas turbine engines. Numbering as provided herein is intended for convenience in locating a particular unit in a group of like or similar units.

Orientation of Engine Axis, Coordinate and Numbering Systems for Aircraft Gas Turbine Engines

HB 7667-2000 航空发动机燃油喷嘴性能试验

本标准规定了航空发动机燃油喷嘴性能试验的内容和方法，提出了对试验设备、测量方法与测量准确度的要求。 　　本标准适用于燃油喷嘴的常规试验、雾化试验及燃油总管试验。

Aeroengine fuel nozzle performance test

ARINC 762-1 ITEM 3.0-2000 系统设计需注意事项

System Design Considerations

System Design Considerations

ARINC 760-1 ITEM 3.0-2000 系统设计需注意事项

System Design Considerations

System Design Considerations

ARINC 760-1-2000 GNSS航海系统

GNSS Navigation Unit (GNU)

GNSS Navigation Unit (GNU)

ARINC 760-1 BOOK-2000 GNSS航海系统

GNSS Navigation Unit (GNU)

GNSS Navigation Unit (GNU)

SAE AS25109-1999 飞机往复式发动机的一般规范FSC 2810

This specification covers standard requirements for reciprocating aircraft engines.

Engines, Aircraft, Reciprocating, General Specification for FSC 2810

SAE AIR1087B-1999 发动机启动期间的飞机附件制动力矩

This SAE Aerospace Information Report (AIR) presents a discussion of drag torques of engine accessories operating at cold temperature. Various conditions of temperature, speed, and acceleration rates are reviewed showing the merits of each method and recommending a standard test method. The purpose of this Aerospace Information Report is to present a brief discussion of the drag torques caused by accessory units while starting under -65 conditions. The various parameters affecting the magnitude of the drag torque at various speeds and accelerations rates are reviewed. In conclusion, this report establishes the difference in accessory drag torque characteristics that are obtained by various test procedures, and thereby this difference warrants the need for the establishment of a standard test method.

Aircraft Accessory Drag Torque During Engine Starts

ARINC 704A-1999 惯性参考系统

Inertial Reference System

Inertial Reference System

SAE AIR1639A-1999 气动启动系统的安全标准

This SAE Aerospace Information Report (AIR) presents safety criteria for pneumatic type engine starting system design and component hardware. Included are safety criteria in design of both starter control valves and starters as well as in design of airframe control systems. Safety topics concern starter valve operation and material application, airframe controls and instrumentation installations and starter rotor integrity and containment.

Safety Criteria for Pneumatic Starting Sytems

SAE AIR1419A-1999 燃气涡轮发动机的进气口总压变形考虑

AIR1419 Inlet Total Pressure Distortion Considerations for Gas Turbine Engines documents engineering information for use as reference material and for guidance. Inlet total-pressure distortion and other forms of flow distortion that cna influence inlet/engine compatibility require examination to establish their effect on engine stability and performance. This report centers on inlet-generated total-pressure distortion measured at the aerodynamic interface plane (AIP), not because this is necessarily the sole concern, but b ecause it has been given sufficient attention in the aircraft and engine communities to produce generally accepted engineering practices for dealing with it. The report does not address procedures for dealing with performance destabilizing influences other than those due to total-pressure distortion, or with the effects of any distortion on aeroelastic stability. The propulsion system designer must be careful to assure that, throughout the development process, other forms of inlet flow distortion, which can have just as serious effects on system stability and performance, have been effectively addressed.

Inlet Total-Pressure-Distortion Considerations for Gas-Turbine Engines