V31 发动机辅助系统及其附件 标准查询与下载

GJB 5580-2006 航空发动机大修手册编制要求

本标准规定了航空发动机大修手册（以下简称“手册”）的编制、出版及交付要求。 本标准适用于军用航空发动机大修手册的编制。

Requirements for preparation of overhaul manual for aircraft engine

GJB 5556-2006 飞机燃油副油箱试验要求

本标准规定了军用飞机外挂燃油副油箱（以下简称油箱）的试验要求。 本标准适用于副油箱的设计、生产和验收。

Test requirements for auxiliary external fuel tank of aircraft

SAE AIR5317-2006 辅助动力系统(APU)安全管理指南

The SAE Guide to APU health management establishes the foundation for developing a successful APU health management program at any aircraft or APU operator, such as an airline, an OEM, an equipment supplier, or a military transport unit. This guide identifies the best practices for using an APU health management program to improve dispatch reliability and to satisfy Extended Operations (ETOPS) availability requirements. There have been many attempts to institute APU health management programs but most programs were modeled after the pre-existing main engine programs. These models often overlooked special considerations that are necessary to make an APU health management program successful. This report will identify the unique characteristics of a successful APU health management program and the best practices for establishing a system. The purpose of this report is to guide the development and use of a successful APU health management effort in a practical, cost effective method. This report will: Identify the costs and benefits associated with developing an effective APU health management program; Identify the best practices and technologies for developing and implementing an APU health management program; Identify the best practices for using APU health management to prevent failures and disruptions to operations; Identify a recommended collection of data, including recommended measurements and recommended events.

A Guide to APU Health Management

AECMA PREN 3661-001-2005 航空航天系列. 单杆温度补偿断路器 额定电流20A至50A.第001部分 ;技术规格

This standard is part of the series of EN metallic material standards for aerospace applications. The general organization of this series is described in EN 4258. This standard has been prepared in accordance with EN 4500-2.

Aerospace Series Circuit Breakers, Single-Pole, Temperature Compensated, Rated Current 20 A to 50 A Part 001: Technical Specification Edition P 3

ARINC 758-2-2005 通信管理系统Mark 2

Communications Management Unit (CMU) Mark 2

Communications Management Unit (CMU) Mark 2 1996; Includes Supplements 1-2

ARINC 429 SET-2004 Mark 33数字信息传递系统部分1, 2, 3包括429P1-17, 429P2-16,和429P3-18

Mark 33 Digital Information Transfer System Parts 1, 2, 3 Includes 429P1-17, 429P2-16, and 429P3-18

Mark 33 Digital Information Transfer System Parts 1, 2, 3 Includes 429P1-17, 429P2-16, and 429P3-18

HB 7735-2003 燃气轮机成套设备型号命名

本标准规定了燃气轮机成套设备型号命名的确定方法。 本标准适用于燃气轮机成套设备的型号命名。

Gas turbine turnkey installation nomination

SAE ARP4755A-2003 涡轴/涡桨气体涡轮发动机试验室的相互联系

This paper describes a recommended practice and procedure for the correlation of test cells that are used for the performance testing of turboprop and turboshaft engines. This Aerospace Recommended Practice (ARP) shall apply to both dynamometer and propeller based testing. Test cell correlation is performed to determine the effect of any given test cell enclosure and equipment on the performance of an engine relative to the baseline performance of that engine.

Turboshaft/Turboprop Gas Turbine Engine Test Cell Correlation

SAE ARP4191C-2003 使用FORTRAN 77数码电脑程序的燃气涡轮发动机性能演示

This Aerospace Recommended Practice (ARP) provides a method for digital computer programs for gas turbine engine, steady-state or transient, performance to be written using the FORTRAN 77 Language. When it is agreed between the program User and Supplier that a particular program will be supplied in FORTRAN 77, it is recommended that this ARP be used in conjunction with AS681 for steady-state and transient programs. This ARP has two purposes: 1. to remove the requirement for HOLLERITH stores by replacing them with FORTRAN 77 CHARACTER stores; and 2. to take advantage of the FORTRAN 77 CHARACTER storage to extend the information interface between the calling program and the engine subroutine. The ARP has the same major section numbers as AS 681 to facilitate its use with these documents. The information given in each section of this ARP is additional to that given in AS 681.

Gas Turbine Engine Performance Presentation for Digital Computer Programs Using FORTRAN 77

ARINC 765 BOOK-2003 以太网开关系统

ETHERNET SWITCH UNIT (ESU)

ETHERNET SWITCH UNIT (ESU)

ARINC 765-2003 以太网开关系统

ETHERNET SWITCH UNIT (ESU)

ETHERNET SWITCH UNIT (ESU)

HB 7712-2002 飞机燃气涡轮发动机空气起动机控制活门通用规范

本规范规定了飞机燃气涡轮发动机起动机控制活门的性能、设计、试验和鉴定验收 的一般要求。 本规范适用于飞机燃气涡轮发动机空气起动机控制活门的研制及其批生产。

Valve,starter control,pneumatic,aircraft engine general specification for

HB 7728-2002 航空用高温合金.涡轮工作叶片精铸件规范

Specification for superalloy turbine blade investment castings for aviation

HB 7727-2002 涡轴发动机用FGH95粉末高温合金盘形件规范

本规范规定了涡轴发动机用 FGH95 粉末高温合金盘形件的要求、质量保证规定和交货准备等内容。 本规范适用于采用直接热等静压成形工艺生产的 FGH95 涡轴发动机盘形件。

Specification for the disks of FGH95 powder metallurgy superalloy for turbine shaft enging

HB 7719-2002 航空发动机减速器通用规范

General specification for aircraft engine gearbox

SAE ARP1420B-2002 燃气涡轮发动机进气道气流畸变指南

The turbine-engine inlet flow distortion methodology addressed in this document applies only to the effects of inlet total-pressure distortion. Practices employed to quantify these effects are developing and therefore, periodic updates are anticipated. The effects of other forms of distortion on flow stability and performance and of any distortion on aeroelastic stability are not addressed. The guidelines can be used as necessary to create a development method to minimize the risk of inlet/engine compatibility problems. The degree to which guidelines for descriptor use, assessment techniques, and testing outlined in this document are applied to a specific program should be consistent with the expected severity of the compatibility problem. This Aerospace Recommended Practice (ARP) provides guidelines by which gas turbine engine aerodynamic stability and performance, as affected by the quality of the airflow delivered to the engine, can be evaluated consistently. The following subjects are addressed: distortion descriptors: distortion descriptors are presented that permit the representation and evaluation of inlet total-pressure distortion effects on propulsion system stability and performance. Stability assessment: guidelines are presented for developing an evaluation method that relates the distortion descriptor levels to engine stability in a form suitable for use in computer simulations. Testing: guidelines are provided for testing, instrumentation, data acquisition, and data processing.

Gas Turbine Engine Inlet Flow Distortion Guidelines

SAE ARP1210D-2002 燃气涡轮机发动机接口测试数据处理的计算机程序

This SAE Aerospace Recommended Practice (ARP) describes a class of digital computer programs for use by organizations other than the engine supplier for reduction of engine test data relating to the interface of the engine in the airframe or test facility. This ARP also is intended as a guide for the preparation of such computer programs.

Gas Turbine Engine Interface Test Data Reduction Computer Programs

ARINC 738-3 ITEM 4.0-2001 ADIRU空中数据参考部分系统设计

System Design for the Air Data Reference Segment of ADIRU

System Design for the Air Data Reference Segment of ADIRU

ARINC 738A-1 ITEM 4.0-2001 ADIRU空中数据参考部分系统设计

System Design for the Air Data Reference Segment of ADIRU

System Design for the Air Data Reference Segment of ADIRU

ARINC 738-3 ITEM 3.0-2001 ADIRU惯性参考部分系统设计

System Design for the Inertial Reference Segment of the ADIRU

System Design for the Inertial Reference Segment of the ADIRU