V30 发动机总体 标准查询与下载

HB/Z 355-2002 航空发动机材料采购原则、程序与要求

本指导性技术文件规定了航空发动机材料(含锻.铸件)采购的原则、程序与要求。 本指导性技术文件适用于航空发动机材料的采购。

Principles,procedures and requirements for aero-engines material purchase

HB/Z 354-2002 航空发动机材料研制原则、程序与要求

本指导性技术文件规定了航空发动机材料研制的原则、程序与要求。 本指导性技术文件适用于航空发动机所需的新材料研制、材料仿制及材料改进(以下统称为材料研 制)。

Principles,procedures and requirements for aero-engines material research and development

HB/Z 353-2002 航空发动机材料选用原则、程序与要求

Principles,procedures and requirements for aero-engines material selection

SAE ARP741B-2002 涡轮风扇喷气发动机和涡轮喷气飞机燃气涡轮发动机试验单元相关性

This paper describes a recommended practice and procedure for the correlation of test cells that are used for the performance testing of turbofan and turbojet engines. 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. When baseline testing is performed in an indoor test cell, the baseline performance data are adjusted to open air conditions.

Turbofan and Turbojet Gas Turbine Engine Test Cell Correlation

GSA A-A-3179 A-2002 机工组合角尺

This commercial item description covers machinists’ combination center and miter head squares.

SQUARES, MACHINISTS' COMBINATION

GSA QPL-FF-L-2740-8-2002 锁具组合

The activity responsible for this Qualified Products List is the General Services Administration, Federal Supply Service, Furniture Commodity Center (3FNE), Washington, DC 20406.

LOCKS, COMBINATION

DLA A-A-1928C-2002 挂锁(组合)

The General Services Administration has authorized the use of this commercial item description as a replacement for Military Specifications MIL-V-16720E and MIL-V-16721D which are cancelled.

PADLOCK (COMBINATION)

SAE AIR4174-2002 飞机传动系监控指南

The purpose of this SAE Aerospace Information Report(AIR) is to provide managment,designers,and operators with information to assist them to decide what type of power train monitoring they desire.This document is to provide assistance in optimizing system complexity,performance and cost effectiveness.This document covers all power train elements from the point at which the gas generator energy is transferred to mechanical energy for propulsion purposes. The document covers engine power train components,their interfaces,transmissions,gearboxes,hanger bearings,shafting and associated rotating accessories,propellers and rotor systems as shown in Figure 1.This document addresses application for rotorcraft,turboprop,and propfan drive trains for both commercial and military aircraft.Information is provided to assist in:a.Defining technology maturity and application riskb.Cost benefit analysis (Value analysis)C.Selection of system componentsd.Selection of technologye.Managing interface requirementsf.Defining information flow requirments

A Guide to Aircraft Power Train Monitoring

SAE AIR4174-2002(R2008) 飞机动力传动机构监测指南

The purpose of this SAE Aerospace Information Report (AIR) is to provide managment, designers, desire. This document is to provide assistance in optimizing system complexity, performance and cost effectiveness.This document covers all power train elements from the point at which the gas generator eneray is transferred to mechanical energy for propulsion purposes.The document covers engine power train components, their interfaces, transmissions, gearboxes, hanger bearing, shafting and associated rotating accessories, propellers and rotor systems as shown in Figure1.This document addresses application for rotorcraft, turboprop, and propfan drive trains for both commerical and military aircraft.Information is provided to assist in;a. Defining technology maturity and application riskb. Cost benefit analysis (Value analysis)c. Selection of system componentsd. Selection of technologye. Managing interface requirementsf. Defining information flow requirements

A Guide to Aircraft Power Train Monitoring

DLA A-A-51187 B-2001 (GTAW)钨电极惰性气体保护焊,焊接电极和组合零件

This commercial item description (CID) covers gas tungsten arc welding (GTAW) torches, also referred to as tungsten inert gas (TIG) welding torches.

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

DLA A-A-55014 A-2001 钨电极惰性气体保护焊和组合零件焊接条配备

This commercial item description (CID) covers complete welding torch outfits intended for use in gas tungsten arc welding (GTAW), also commonly referred to as tungsten inert gas (TIG) welding.

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

SAE AIR4548A-2001 燃气涡轮发动机性能的实时建模方法

This SAE Aerospace Information Report (AI) provides a review of real-time modeling methodologies for gas turbine engine performance. The application of real-time models and modeling methodologies are discussed. The modeling methodologies addressed in this AIR concentrate on the aerothermal portion of the gas turbine propulsion system. Characteristics of the models, the various algorithms used in them, and system integration issues are also reviewed. In addition, example cases of digital models in source code are provided for several methodologies. The purpose of this document is to provide a source of information on current practices and procedures for developing real-time turbine engine models, not models of controls or other installation subsystems. This document is intended to be a basis for communication between supplier and customer.

Real-Time Modeling Methods for Gas Turbine Engine Performance

SAE ARP906B-2001 飞机发动机起动和辅助动力系统的词汇表

The Aircraft Engine Starting and Auxiliary Power System Glossary presents definitions of terms commonly encountered and associated with aircraft engine starting and auxiliary power systems. Terms have been arranged alphabetically. The purpose of the Aircraft Engine Starting and Auxiliary Power System Glossary is to promote the consistent usage of terms commonly encountered and associated with aircraft engine starting and auxiliary power systems. The usage of terms presented herein will serve to promote clarity and avoid many misunderstandings throughout the aerospace industry.

Glossary, Aircraft Engine Starting and Auxiliary Power Systems

SAE AIR1174B-2001 启动系统规范和标准索引

This report lists military and industry specifications and standards which are used in aerospace engine starting and auxiliary power systems. Only those hardware standards which have been specifically designed for engine starting systems are listed. Revisions and amendments which are current for these specifications and standards are not listed.

Index of Starting System Specifications and Standards

SAE AIR5306-2000 气体涡轮机试验室的进口空气流斜面

This SAE Aerospace Information Report (AIR) has been written for individuals associated with the ground-level testing of gas turbine engines and particularly for those who might be interested in upgrading their existing engine test facility to meet the airflow requirements for higher thrust engine models. The intellectual property rights on the material contained in this document are protected by US Paten Number 5,293,775 dated March 15, 1994 assigned to United Technologies Corporation, Hartford, Connecticut, USA. Any individual, or organization, attempting to use the system described in this document should get a clearance from United Technologies Corporation, to avoid any potential liability arising from paten infringement. To provide guidelines for inlet airflow ramps for gas turbine engine test cells.

Inlet Airflow Ramps for Gas Turbine Engine Test Cells

SAE AS8581-2000 发动机.5秒固体推进剂4500英镑推力火箭

This specification established the requirements for a 5 second duration, 4500 pound thrust (when determined at 60 °F) solid propellant rocket engine hereinafter specified as 5 S-4500. The 5 S-4500 rocket engine is a moderate duration, low- thrust, self-contained power plant employing a solid propellant. The engine is designed specifically for jet assist take-off (JATO) of aircraft, and to deliver a nominal thrust of 4500 pounds for 5 seconds duration at 60°F and sea level. The engine contains aircraft attachment fittings and an ignition system.

Engine; Rocket, Solid Propellant 5 Second Duration, 4500 Pounds Thrust FSC 2845; Should Be Used Instead of MIL-E-8581A(AS), Which Was Cancelled on 26 May 2000

ISO 12333:2000 航空航天 连续置换液压马达 35000 kPa系统的一般规范

This International Standard establishes the general specifications for constant displacement hydraulic motors to be installed in aircraft, which transform hydraulic power into mechanical energy in the form of a rotational torque to 35 000 kPa systems. Primary and secondary function motors (see clause 3) are covered in this International Standard; actuators with internal rotation angle limits and low-speed motors are not covered in this International Standard. This International Standard shall be used in conjunction with the detail specification particular to each application.

Aerospace - Constant-displacement hydraulic motors - General specifications for 35000 kPa systems

DLA MS27249 REV E REINST NOTICE 2-2000 可组合的接线端子板

MS27249E, dated 5 March 1993, is hereby reinstated as inactive for new design.

TERMINAL BOARDS, SECTIONAL

NAVY MIL-I-8693 NOTICE 1-1999 CU-395/ARN-21A连接器指标

This notice should be filed in front of MIL-1-8693, dated 15 April 1955

INDICATOR COUPLER CU-395/ARN-21A

DLA MS51524 REV A NOTICE 1-1999 37度扩口式组合三通管接头

This notice should be filed in front of MS51524A, dated 17 January 1979.

TEE, TUBE TO SWIVEL, SWIVEL ON BRANCH, 37 DEGREE FLARED [Refer To: SAE J514, SAE J514, SAE J514, SAE J514, SAE J514]