V30 发动机总体 标准查询与下载

HB 20059-2011 航空发动机离心压气机设计要求

本标准规定了航空发动机离心压气机的设计依据、设计准则、设计流程、设计内容和设计方法、验证试验项目。 本标准适用于航空发动机离心压气机设计。航空燃气涡轮辅助动力装置和航空派生型燃气轮机的离心压气机设计也可参照使用。

Centrifugal compressor design requirement of aero engine

QJ 20019-2011 复合固体推进剂安全性能试验方法

本部分规定了复合固体推进剂爆轰感度试验的试验原理、试验要求、试验程序、数据处理、试验记录和试验报告。 本部分适用于复合固体推进剂的爆轰感度测试。其它固体推进剂可参照执行。

Test method for safety performance of composite solid propellants

SAE AIR4951-2011 测试单元推理测量

Thrust measurement systems come in many sizes and shapes, with varying degrees of complexity, accuracy and cost. For the purposes of this information report, the discussions of thrust measurement will be limited to axial thrust in single-axis test systems. These are several purposes served by this information report: a. To provide guidelines for the specification of thrust measurement systems; b. To address the major factors which can influence thrust measurement uncertainty; c. To consider the operational characteristics and the effects on system performance.

Test Cell Thrust Measurement

SAE AMS2647D-2011 荧光渗透剂检查法进行航空器和发动机组件维修

This specification details requirements and procedures for the detection of defects in aircraft and engine components during maintenance and overhaul operations.

Fluorescent Penetrant Inspection Aircraft and Engine Component Maintenance

ASTM F2840-11 设计和制造轻型运动飞机用电力推进装置的标准操作规程

This specification provides designers and manufacturers of electric propulsion for light sport aircraft design references and criteria to use in designing and manufacturing EPUs. Declaration of compliance is based on testing and documentation during the design, ground testing and flight testing of the EPU by the manufacturer or under the manufacturers’ guidance. Manufacturers of the EPUs are encouraged to review and incorporate appropriate standards and lessons learned from ground based systems as documented in SAE J2344 and EASA CRI F-58 (see Appendix X2). Electric aircraft may contain potentially hazardous level of electrical voltage or current. It is important to protect persons from exposure to this hazard. Under normal operating conditions, adequate electrical isolation is achieved through physical separation means such as the use of insulated wire, enclosures, or other barriers to direct contact. There are conditions or events that can occur outside normal operation that can cause this protection to be degraded. Some means should be provided to detect degraded isolation or ground fault. In addition, processes or hardware, or both, should be provided to allow for controlled access to the high voltage system for maintenance or repair. A number of alternative means may be used to achieve these electrical safety goals including automatic hazardous voltage disconnects, manual disconnects, interlock systems, special tools and grounding. The intention of all these means is either to prevent inadvertent contact with hazardous voltages or to prevent damage or injury from the uncontrolled release of electric energy. Lightning strikes are not addressed in this Standard Practice because LSA aircraft are limited to VMC flight only.1.1 This specification covers minimum requirements for the design and manufacture of Electric Propulsion Units (EPU) for light sport aircraft, VFR use. The EPU shall as a minimum consist of the electric motor, associated controllers, disconnects and wiring, an Energy Storage Device (ESD) such as a battery or capacitor, or both, and EPU monitoring gauges and meters. Optional onboard charging devices, in-flight charging devices or other technology may be included. 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 Electric Propulsion Units for Light Sport Aircraft

SAE AIR5686-2010 进气道涡流变形评定方法

This Aerospace Information Report (AIR) addresses the subject of aircraft inlet-swirl distortion. A structured methodology for characterizing steady-state swirl distortion in terms of swirl descriptors and for correlating the swirl descriptors with loss in stability pressure ratio is presented. The methodology is to be considered in conjunction with other SAE inlet distortion methodologies. In particular, the combined effects of swirl and total-pressure distortion on stability margin are considered. However, dynamic swirl, i.e., time-variant swirl, is not considered. The implementation of the swirl assessment methodology is shown through both computational and experimental examples. Different types of swirl distortion encountered in various engine installations and operations are described, and case studies which highlight the impact of swirl on engine stability are provided. Supplemental material is included in the appendices. This AIR is issued to bring together information and ideas required to address the inlet-swirl problem for which common industry practice has yet to be established. This document should foster the tests and analyses necessary to mature the ideas proposed by the committee to a recommended practice. These tests and analyses must include information that justifies three main features of the proposed swirl methodology: (1) swirl descriptors for correlating inlet swirl and stability pressure ratio loss, (2) computational techniques for analyzing compression systems (inlets, fans, compressors), and (3) test protocols (instrumentation and test techniques). The committee anticipates serving the industry by using such information to establish the consensus necessary for issuance of an SAE recommended practice.

A Methodology for Assessing Inlet Swirl Distortion

GJB 241A-2010 航空涡轮喷气和涡轮风扇发动机通用规范

本规范规定了航空涡轮喷气和涡轮风扇发动机的通用要求。 本规范适用于有人驾驶固定翼飞机用涡轮喷气和涡轮风扇发动机的研制、生产和交付。

Engine,aircraft,turbojet and turbofan,general specification for

GJB 7079-2010 航空发动机外场质量监控通用要求

本标准规定了航空发动机外场质量监控实施、质量等级评定、质量信息管理的通用要求。 本标准适用于航空发动机外场质量监控。

General requirements for field quality supervision and control of aeroengine

GJB 624.8A-2010 军用飞机科研试飞训练要求 第8部分：发动机强度和振动

本部分规定了有人驾驶固定翼飞机进行发动机强度和振动科研试飞训练的通用要求。 本部分适用于有人驾驶固定翼飞机发动机强度和振动科研试飞训练的技术准备、组织实施与评价。特种用途固定翼军用飞机可参照执行。

Training requirements of flight test research for military aircraft.Part 8:Engine strength and vibration

GJB 6887-2009 军用直升机涡轮轴发动机整机低循环疲劳试验规程

本规范规定了军用直升机涡轮轴发动机整机低循环疲劳试验的技术要求和试验方法。 本规范适用于军用直升机涡轮轴发动机整机低循环疲劳试验。

Procedure for low cycle fatigue test of military helicopter turboshaft engine

GJB 6850.219-2009 水面舰船系泊和航行试验规程 第219部分：舰载直升机喷气燃料系统试验

Mooring and sailing test procedures for surface ships part 219: Jet fuel system tests for shipboard helicopters

SAE AIR4986A-2009 发动机静电气体通道监控

This document has been declared "CANCELLED" as of October 2009. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index. Turbine engine malfunctions account for a substantial portion of the maintenance actions required to keep both fixed and rotary wing aircraft operational. Undetected incipient component failures can result in secondary engine damage and expensive unscheduled maintenance actions. Recent developments of electrostatic methods now provide the potential for the detection of foreign object ingestion and early detection of distress in gas path components. This SAE Aerospace Information Report (AIR) seeks to outline the history of the electrostatic technique and provides examples of state-of- the-art systems for both inlet and exhaust gas debris monitoring systems along with examples of most recent testing.

Engine Electrostatic Gas Path Monitoring

DIN EN 4301:2009 航空航天系列.发动机的打印标号.工程要求.德文和英文版本EN 4301-2009

This standard describes the coding system for marks, the processes used to produce these marks, as well as the general marking requirements for the identification of aerospace engine items. This document is applicable to items whose engineering drawing or design folder refers to EN 4301 for all issues that are not in contradiction with specific indications appearing on the engineering drawing or in the design folder. This document is not applicable to items requiring an identification plate.

Aerospace series - Identification marking methods for engine items - Engineering requirements; German and English version EN 4301:2009

SAE AMS2647C-2009 飞行器与发动机部件维护中的荧光穿透探伤

This specification details requirements and procedures for the detection of defects in aircraft and engine components during maintenance and overhaul operations. This processes has been used typically by maintenance and overhaul facilities to inspect aircraft and engine components and associated accessories when fluorescent penetrant inspection is specified, but usage is not limited to such applications.

Fluorescent Penetrant Inspection Aircraft and Engine Component Maintenance

SAE AIR4827A-2009 喷气发动机试验室空气动力学建模技术

Research studies focusing on jet engine test cell aerodynamics, acoustics, and cell flow characteristics as affecting engine performance can be conducted with scale models for a variety of test cells. Such studies require the simulation of a number of jet engines in rather accurate detail, both as to geometry and as to flow characteristics. It has been demonstrated that simulators of low-bypass afterburning turbojets, high-bypass turbofans, turboshaft engines (without propellers), and unducted fan engines can be designed, fabricated, and successfully operated using either high-pressure air ejector systems or turbine driven systems for the motive power. Specific components of a test cell such as inlets or exhaust sections alone may be tested independently by employing a vacuum source and bellmouth to simulate engine inlet flow or compressed air and scaled nozzle to simulate engine exhaust flow. The peculiar problems associated with scale model testing and engine simulators and the methods which can be used to attack these problems are described. This SAE Aerospace Information Report (AIR) has been written for individuals associated with ground level testing of turbofan and turbojet engines and particularly for those who might be interested in investigating the performance characteristics of a new test cell design or of proposed modifications to an existing test cell by means of a scale model test.

Modeling Techniques for Jet Engine Test Cell Aerodynamics

GJB 6753-2009 啤旋桨飞机带动力模型低速风洞试验方法

本标准规定了在螺旋桨飞机带动力模型试验的基本方法。 本标准适用于在低速风洞中测量拉进式螺旋桨模型滑流对飞机全模气动特性影响的测力试验。实物螺旋浆滑流影响试验、螺旋浆气动特性试验、螺旋浆滑流对飞机部件气动特性影响试验、推进式螺旋浆滑流影响试验、其他螺旋浆滑流影响试验及与螺旋浆滑流相关的测压试验亦可参照使用。

Test method for powered model of propeller driven aircraft in low speed wind tunnel

SAE AIR4869A-2009 封闭式涡轮风扇/涡轮喷射发动机测试腔的设计研究

This SAE Aerospace Information Report (AIR) has been written for individuals associated with the ground-level testing of large and small gas turbine engines and particularly for those who might be interested in upgrading their existing or acquiring new test cell facilities. There are several purposes served by this document: a. to provide guidelines for the design of state-of-the-art ground-level enclosed test facilities for turbofan and turbojet engine testing applications; b. to address the major test cell/engine aerodynamic and acoustic characteristics which can influence the operation of a gas turbine engine and its performance stability in a test cell; and c. to consider acoustic environmental impact and methods to control it.

Design Considerations for Enclosed Turbofan/Turbojet Engine Test Cells

BS EN 4301:2009 航空航天系列.引擎部件的识别标记法.工程要求

This standard describes the coding system for marks, the processes used to produce these marks, as well as the general marking requirements for the identification of aerospace engine items. This document is applicable to items whose engineering drawing or design folder refers to EN 4301 for all issues that are not in contradiction with specific indications appearing on the engineering drawing or in the design folder. This document is not applicable to items requiring an identification plate.

Aerospace series - Identification marking methods for engine items - Engineering requirements

DIN EN 4300:2009 航空航天系列.发动机项目的识别标识.设计标准

This standard: describes the location and the layout of the marks of the item; describes the marking processes to be used according to the environment and the function of the items; determines the selection conditions of the marks; determines the compatibility conditions of the marking processes with the constitution, the production and the use of the items. This document applies to aerospace engine items and shall be used in conjunction with EN 4301.

Aerospace series - Identification marking of engine items - Design standard; German and English version EN 4300:2008

GOST R 53374-2009 液体.火箭发动机.公共使用期间产品和质量检查的一般技术要求

Liquid - propellant rocket engines.General technical requirements for production and quality inspection during supply for use