V30 发动机总体 标准查询与下载

SAE AIR4979-1996 以北约阿加德统一引擎测试程序为基础的引擎测试中不确定度的测量的估算

The primary objective of this document is to describe the systematic and random measurement uncertainties which may be expected when testing gas turbine engines in a range of different test facilities. The documentation covers a traditional method for estimating pretest uncertainties and a new method for computing and comparing posttest uncertainties. To determine these posttest uncertainties, data generated during the AGARD Uniform Engine Test Program (UETP) were analyzed and compared to the pretest estimates. The proposed procedure provides a mechanism for determining the expected accuracy of test results obtained from facilities which were not previously cross calibrated. Furthermore, the method can be used to assist in making cost-effective management decisions on the level of validation/cross calibration necessary when bringing a test facility on line. This document is also intended to act as a guide for improving uncertainty analyses in a broad spectrum of related industries. Measurement uncertainty and measurement system approaches and practices for the UETP are presented in a systematic format. Readers can use these uncertainty approaches and practices for comparison to their own measurement systems. The approach chose was to analyze three of the UETP test conditions at eight test facilities along with the individual measurement system approaches and practices. The test program provided a wide range of performance measurements and corresponding pretest uncertainty estimates encompassing a variety of test and measurement approaches and practices. Included in the analysis are the basic gas turbine performance measurements of temperature, pressure, airflow, fuel flow, area, speed, thrust, and typical performance parameter functions and associated uncertainty estimates.

Estimation of Measurement Uncertainty in Engine Tests Based on NATO AGARD Uniform Engine Test Program

ARMY MIL-F-45060 D NOTICE 2-1996 M605组合式地雷引信零件

This notice should be filed in front of MIL-F-45060D(AR), dated 15 May 1975

FUZE, MINE, COMBINATION M605, PARTS FOR

SAE ARP169A-1996 飞机发动机气缸的编号

This SAE Aerospace Recommended Practice (ARP) defines a method of numbering aircraft engine

Numbering of Aircraft Engine Cylinders

JIS W 4601:1996 飞行器用涡轮喷气及涡轮风扇发动机通用规范

この規格は，航空ターボジェットユンジン及びターボファンエンジンに対する性能，作動特性，設計の特徴，詳細なインタフょース形態の定義及び装備範囲について規定する。

General specification of turbojet engines and turbofan engines for aircraft

ARMY MIL-F-60020 NOTICE 2-1996 组合式M10A2地雷引信零件

This notice should be filed in front of MIL-F-60020(AR) dated 31 January 1964

FUZE, MINE, COMBINATION M10A2, PARTS FOR

AECMA PREN 4301-1996 航空系列 发动机打印标号方法.P1版

This draft is now available for public comment and your views and technical comments on it would be appreciated. If you have no specific comments to make hut find it generally acceptable it would be helpful if you would notify US accordingly. Suggestions entailing revision of the text should indicate the preferred wording. Please quote the relevant clause number against any comment.

Aerospace Series Identification Marking Methods for Engine Items Edition P1

AECMA PREN 4300-1996 航空系列 发动机设计打印标号标准.P1版

This drafe is now available for public comment and your views and technical comments on it would be appreciated.

Aerospace Series Identification Marking of Engine Items Design Standard Edition P1

SAE AIR4989-1996 封闭的涡轴发动机测试单元的设计注意事项

This SAE Aerospace Information Report (AIR) developed by a broad cross section of personnel from the aviation industry and government agencies is offered to provide state-of-the-art information for the use of individuals and organizations designing new or upgraded turboshaft engine test facilities. The purpose of this document is: a. to provide guidelines for the design of state-of-the-art ground-level enclosed test facilities for turboshaft engine testing; b. to address the major test cell engine load absorption device physical, aerodynamic and acoustic characteristics which can influence operation, performance, accuracy and stability of an engine under test; and c. to consider acoustic and environmental effects and methods to control them.

DESIGN CONSIDERATIONS FOR ENCLOSED TURBOSHAFT ENGINE TEST CELLS

HB/Z 281-1995 航空发动机故障模式、影响及危害性分析指南

本标准规定了航空发动机进行故障模式、影响及危害性分析（ＦＭＥＣＡ）的基本程序和方法。 　　本标准适用于航空发动机本体构件及其系统的研制阶段，也可用于生产和使用阶段，但不适用于软件。

Guidelines for Failure Modes, Effects and Hazard Analysis of Aeroengines

HB 7175-1995 飞机变流机通用规范

本规范规定了将额定电压为28.5V直流电变换成额定频率为400Hz交流电的变流机通用要求。 　　本标准适用于飞机变流机的设计、制造及其专用规范的编制。

General specification for aircraft converters

HB 7259-1995 航空发动机测绘设计工作细则

本标准规定了自测绘设计准备工作开始，至发出测绘设计工作图样为止的整个测绘设计过程中的一般工作内容和有关要求。 　　本标准适用于航空燃气涡轮型发动机的生产性测绘设计。对于研究性测绘分析，可参照执行。也可供其它产品测绘设计参考。

Detailed Rules for Surveying and Designing of Aeroengines

HB 7113-1994 发动机重量控制与平衡要求

Engine Weight Control and Balance Requirements

SAE AIR4416-1995 直升机涡轮发动机清洗

Engines subject to dust, industrial pollution, saltwater contamination or other chemically laden atmosphere (including pesticies and herbicides) lose performance due to deposits of contaminants on surfaces in the air/gas flow path. Engine wash and engine rinse procedures are utilized to restore turbine engine performance. These procedures are generated by the engine manufacturer and are included in the Engine Maintenance/Service Manuals. For most turbine engines these procedures are similar in concept and practice; however, application details choice of solvents and many other service features can vary from engine manufacturer to engine manufacturer and may even vary within the range of engine models produced by any manufacturer. The intent of this SAE Aerospace Information Report (AIR) is to outline the general nature, considerations, and background of engine wash and engine rinse and is directed towards the needs of the entry level engineer, service engineer, and those involved in the general maintenance of installed turbine engines.

Helicopter Turbine Engine Wash

NAVY MIL-C-28779 B NOTICE 1-1995 CU-2007( )/SRR扩展频带组合器

MIL-C-28779B(EC) is inactive for new design and is no longer used by the Navy except for replacement purposes.

COMBINER, EXTENDED FREQUENCY RANGE CU-2007( )/SRR

BS M 79:1995 航空发动机运输装置规范

This International Standard specifies functional, di-mensional, structural and environmental requirements for the design of aircraft engine transport devices, used to transport aircraft engines in wide-body air-craft. These devices are intended to be used in con-junction with pallets compatible with ISO 8097 Class II restraint requirements. The restraint system parameters and requirements are also to be met for those devices where the pallet structural capability is an integral part of the design. Design parameters specified for air transport of engine transport devices should enable interline capability where feasible with respect to dimensions and loads. This International Standard specifies minimum air and ground handling features and is intended to ensure interchangeability and compatibility with present and future air transport and ground handling system. The devices specified herein should be designed primarily for air transport and alternatively for surface transport, stowage and maintenance purposes.

Specification for aircraft engine transport devices

HB 7086-1994 民用飞机气动外缘公差

本标准规定了民用飞机气动外缘公差。 　　本标准适用于民用飞机；直升机的固定部件亦可参照使用。

Aerodynamic outer edge tolerance of civil aircraft

HB 7081-1994 轴流涡轮气动性能试验

本标准规定了轴流涡轮的气动性能模拟试验方法和试验要求。 　　本标准适用于试验工质为空气或混有少量燃气的空气的轴流式单级、多级涡轮与单转子及双转子涡轮的气动性能模拟试验。

Axial flow turbine aerodynamic performance test

HB 7079-1994 飞机动力装置冷却要求

本标准规定了飞机动力装置冷却要求。包括发动机安装温度和有关其他工作参数规定值。 　　本标准适用于军用飞机（包括直升机）动力装置。

Aircraft Powerplant Cooling Requirements

ISO 11241:1994 航空器 航空发动机运输装置

Specifies functional, dimensional, structural and environmental requirements for the design of aircraft engine transport devices, used to transport aircraft engines in wide-body aircraft. These devices are intended to be used in conjunction with pallets compatible with ISO 8097 Class II restraint requirements. Specifies minimum air and ground handling features and is intended to ensure interchangeability and compatibility with present and future air transport and ground handling system.

Aircraft - Aircraft engine transport devices

JIS W 1842:1994 航空航天.恒定置换液压马达.一般规范

この規格は，航空機に装備し，作動油の圧力を同転トルクの形の機械的エネルギーに変換する定容量形油圧モータに対する一般要求事項について規定する。

Aerospace -- Constant displacement hydraulic motors -- General specifications