V30 发动机总体 标准查询与下载

GJB 5963-2007 军用直升机涡轮轴发动机安装要求

Installation requirements for turboshaft engines for military helicopters

SAE ARP1587B-2007 航空燃气涡轮发动机监测系统指南

This SAE Aerospace Recommended Practice (ARP) examines the whole construct of an Engine Health Management (EHM) system. This keystone document gives a top-level view and addresses EHM description, benefits, and capabilities, and provides examples. This ARP purposely addresses a wide range of EHM architectures to demonstrate possible EHM design options. This ARP is not intended as a legal document and does not provide detailed implementation steps, but does address general implementation concerns and potential benefits. Other SAE documents (Aerospace Standards, Aerospace Recommended Practices, and Aerospace Information Reports) address specific component specifications, procedures and "lessons learned". The purpose of this ARP is to provide an Aircraft Gas Turbine Engine Health Management System Guide for commercial and government operators, aircraft manufacturers, engine producers and equipment suppliers. This guide is provided for program managers to obtain a sufficiently detailed understanding of EHM systems to make funding decisions. Similarly, it can be used by design personnel to obtain a systems perspective as well as references to guides on detail design of all aspects of an EHM system.

Aircraft Gas Turbine Engine Health Management System Guide

DLA A-A-1928 C VALID NOTICE 1-2007 挂锁(组合)

A-A-1928C, dated 15 March 2002, has been reviewed and determined to be valid for use in acquisition.

PADLOCK (COMBINATION)

SAE ARP1796A-2007 航天器发动机空气释放系统

The purpose of this document is to provide the guidelines and recommended practices for analysis, design, and installation of aircraft engine bleed air systems. This SAE Aerospace Recommended Practice (ARP) discusses design philosophy, system and equipment requirements, installation environment and design considerations for military and commercial aircraft systems within the Air Transport Association (ATA) ATA 100 specification, Chapter 36, Pneumatic. This ATA system/chapter covers equipment used to deliver compressed air from a power source to connecting points for other systems such as air conditioning, pressurization, ice protection, cross-engine starting, air turbine motors, air driven hydraulic pumps, on board oxygen generating systems (OBOGS), on board inert gas generating systems (OBIGGS), and other pneumatic demands.

(R) Engine Bleed Air Systems for Aircraft

SAE AS4273A-2007 航空器发动机和航空器发动机装置用流体处理部件的防火测试

This document establishes requirements, test procedures, and acceptance criteria for the fire testing of fluid handling components and materials used in aircraft fluid systems. It is applicable to fluid handling components other than those prescribed by AS1055 (e.g., hoses, tube assemblies, coils, fittings). It also is applicable to materials, wiring, and components such as reservoirs, valves, gearboxes, pumps, filter assemblies, accumulators, fluid-cooled electrical/electronic components, in-flight fluid system instrumentation, hydromechanical controls, actuators, heat exchangers, and manifolds. These components may be used in fuel, lubrication, hydraulic, or pneumatic systems.

(R) Fire Testing of Fluid Handling Components for Aircraft Engines and Aircraft Engine Installations

ASTM F2538-07a(2010) 设计和制造轻型娱乐飞机用往复压缩点火发动机的标准操作规程

This practice provides designers and manufacturers of engines for light sport aircraft design references and criteria to use in designing and manufacturing engines. Declaration of compliance is based on testing and documentation during the design and testing or flight-testing of the engine type by the manufacturer or under the manufacturer''s guidance.1.1 This practice covers minimum requirements for the design and manufacture of reciprocating compression ignition engines for light sport aircraft, Visual Flight Rules (VFR) use. 1.2 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.

Standard Practice for Design and Manufacture of Reciprocating Compression Ignition Engines for Light Sport Aircraft

ASTM F2538-07a 轻型运动飞机用往复式压缩点火发动机的设计和制造的标准实施规程

This practice provides designers and manufacturers of engines for light sport aircraft design references and criteria to use in designing and manufacturing engines. Declaration of compliance is based on testing and documentation during the design and testing or flight-testing of the engine type by the manufacturer or under the manufacturerrsquo;guidance.1.1 This practice covers minimum requirements for the design and manufacture of reciprocating compression ignition engines for light sport aircraft, Visual Flight Rules (VFR) use.This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.

Standard Practice for Design and Manufacture of Reciprocating Compression Ignition Engines for Light Sport Aircraft

ASTM F2667-07 无人航空器系统用往复式压缩点火发动机设计和制造的标准实施规程

1.1 This practice covers minimum requirements for the design and manufacture of reciprocating compression ignition engines for unmanned aircraft systems use.This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.

Standard Practice for Design and Manufacture of Reciprocating Compression Ignition Engines for Unmanned Aircraft Systems

ASTM F2538-07 轻型运动飞机用往复式压缩点火发动机的设计和制造的标准实施规程

1.1 This practice covers minimum requirements for the design and manufacture of reciprocating compression ignition engines for light sport aircraft, day Visual Flight Rules (VFR) use.This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.

Standard Practice for Design and Manufacture of Reciprocating Compression Ignition Engines for Light Sport Aircraft

ASTM F2612-07 无人驾驶飞机系统用涡轮发动机设计和制造的标准实施规程

1.1 This practice covers minimum requirements for the design and manufacture of turbine engines for unmanned aircraft systems.1.2 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.

Standard Practice for Design and Manufacture of Turbine Engines for Unmanned Aircraft System

HB 7806-2006 发动机数字样机通用要求

本标准规定了航空发动机数字样机的构建、应用和管理的通用要求。 本标准适用于航空发动机的研制，航空发动机附件的研制可参照使用。

General requirements for digital mock-up of areoengine

HB 7808-2006 圆弧端齿

本标准规定了圆弧端齿的基本齿廓、尺寸系列、画法与标注。 本标准适用于航空发动机圆弧端齿的设计。

Curvic Coupling

HB 7774.4-2006 基于UG航空发动机建模要求 第4部分:叶片

本部分规定了使用Unigraphics软件进行航空发动机叶片类零件三维建模、装配及二维制图的要求。 本部分适用于航空发动机叶片类零件的设计，其他叶片类零件可参照使用。

Requirements for aeroengine modeling in Unigraphics Part 4: Blade and vane parts

HB 7809-2006 飞机螺旋桨通用技术要求

本标准规定了飞机螺旋桨设计、试验与验证的通用技术要求。 本标准适用于各类飞机螺旋桨。

General technical requirements of propeller for aircraft

GJB 5855-2006 固体火箭发动机维护使用通用技术要求

本标准规定了固体火箭发动机起吊、运输、贮存与定期检查的通用要求。 本标准适用于导弹、运载火箭、航天器、火箭弹用的固体火箭发动机（以下简称发动机）的维护与使用。

General technical requirements for maintenance and application of solid rocket motor

HB 7774.2-2006 基于UG航空发动机建模要求 第2部分:机匣

本部分规定了应用Unigraphics软件实施航空发动机机匣类零件三维建模、装配和制图的要求。 本部分适用于航空发动机机匣类零件的设计。

Requirements for aeroengine modeling in Unigraphics Part 2: Casing

HB 7774.3-2006 基于UG航空发动机建模要求 第3部分:盘类零件

本部分规定了应用Unigraphics软件实施航空发动机盘类零件三维建模、装配及二维制图的要求。 本部分适用于航空发动机盘类零件的设计，轴类零件可参照使用。

Requirements for aeroengine modeling in Unigraphics Part 3: Disk parts

DLA A-A-51187 B VALID NOTICE 1-2006 (GTAW)钨电极惰性气体保护焊,焊接电极和组合零件

A-A-51187B, dated 27 July 2001, has been reviewed and determined to be valid for use in acquisition.

WELDING TORCHES AND COMPONENT PARTS, GAS TUNGSTEN ARC WELDING (GTAW)

DLA A-A-55014 A VALID NOTICE 1-2006 钨电极惰性气体保护焊和组合零件焊接条配备

A-A-55014A, dated 27 July 2001, has been reviewed and determined to be valid for use in acquisition.

TORCH OUTFITS, WELDING, GAS TUNGSTEN ARC WELDING (GTAW) AND COMPONENT PARTS

GJB 5581-2006 航空发动机安装手册编制要求

本标准规定了军用飞机发动机安装手册编写内容、编写格式和方法。 本标准适用于涡喷、涡扇、涡桨、涡轴发动机安装手册的编制。

Requirement for preparation of aircraft propulsion installation manual