V30 发动机总体 标准查询与下载

HB 20119-2012 高空舱台架系统发动机试验安全技术要求

本标准规定了航空发动机高空舱台架系统发动机试验的一般安全、过程安全、设备维护和维修过程安全以及应急预案与演练等安全技术的要求。本标准适用于航空发动机高空舱台架系统发动机试验。

Demand for the safety technology of aero engine simulation test in the altitude test facility

HB 20115-2012 航空发动机叶片热障涂层厚度测量方法涡流法

本标准规定了航空发动机叶片热障涂层厚度涡流法测厚的一般要求、测量准确度控制、有涂层的标准试件选择和制作要求、测量程序等。本标准适用于采用电子束物理气相沉积(EB-PVD)工艺制备的热障涂层。采用大气等离子喷涂(APS)工艺制备的热障涂层可参照使用。

Eddy current measurement method for thermal barrier coating thickness of aero-engine blades

HB 20116-2012 航空发动机叶片表面残余应力的测定X射线衍射法

本标准规定了用X射线衍射法测定航空发动机叶片表面残余应力的一般要求、测试程序、结果评定、测试报告、安全与防护等内容。本标准适用于多晶材料叶片表面残余应力的X射线衍射测定,不适用于具有强烈择优取向生长的多晶叶片和单晶叶片表面残余应力的X射线衍射测定。

Test method for residual stress analysis on aero-engine blade by x-ray diffraction

HB 20085-2012 航空燃气涡轮发动机弹性支承器及挤压油膜阻尼器试验方法

本标准规定了航空燃气涡轮发动机弹性支承器(以下简称弹支)静态刚度测试、带弹支的挤压油膜阻尼器频响特性试验及采用动态应变测试法对弹支振动位移监测的一般要求、试验内容、试验程序、试验数据处理及其结果评定等。本标准适用于航空燃气涡轮发动机弹支和带弹支的挤压油膜阻尼器,采用弹支和带弹支的挤压油膜阻尼器的地面燃气轮机可参照使用。与弹支静态刚度测试相关的内容适用于其他类型弹性支承器,与挤压油膜阻尼器频响特性试验有关的内容可供不带弹支的挤压油膜阻尼器参照使用。

Test methods of elastic support with squeeze oil film damper of aircraft gas turbine engine

HB 20113-2012 航空发动机叶片渗层金相检验

本标准规定了航空发动机涡轮叶片(以下简称叶片)渗层(渗铝层、铝铬渗层、铝硅渗层、铝钛渗层、铝钴渗层、铝铬-铝硅渗层及镍铬-铬铝渗层等)金相检验的一般要求、检验方法、质量要求以及相应的渗层金相图片。本标准适用于航空发动机涡轮叶片表面渗层的金相检验。

Metallographic examination for coatings of aero-engine blade

SAE ARP1533B-2013 航空器发动机气体发射物的分析和评价规程

Aerospace Recommended Practice (ARP) 1533 is a procedure for the analysis and evaluation of the measured composition of the exhasut gas from aircraft engines. Measurements of carbon monoxide, carbon dioxide, total hydrocarbon, and the oxides of nitrogen are used to deduce emission indices, fuel-air ratio, combustion efficiency, and exhaust gas thermodynamic properties. The emission indices (EI) are the parameters of critical interest to the engine developers and the atmospheric emissions regulatory agencies because they relate engine performance to environmental impact.

Procedure for the Analysis and Evaluation of Gaseous Emissions from Aircraft Engines

ANSI/ASME PTC55-2013 燃气涡轮航空发动机

Gas Turbine Aircraft Engines

SAE AIR5128A-2012 飞机燃油系统的电气连接

This SAE Aerospace Information Report (AIR) is limited to the subject of aircraft fuel systems and the questions concerning the requirements for electrical bonding of the various components of the system as related to Static Electric Charges, Fault Current, Electromagnectic Interference (EMI) and Lightning Strikes (Direct and Indirect Effects). this AIR contains engineering guidelines for the design, installation, testing (measurement) and inspection of electrical bonds. The purpose of this document is to provide some guidelines for electrical bonding of structure, fluid lines and components of an aircraft fuel system. These guidelines are related to the va

Electrical Bonding of Aircraft Fuel Systems

KS W 4512-2012 航空器活塞发动机的火花塞端子

Spark plug terminals for aircraft piston engines

KS W 4511-2012 航空器活塞发动机的火花塞

Spark plugs for aircraft piston engines

SAE AIR5774-2012 复合燃料罐、燃油系统设计考虑

This SAE Aerospace Information Report (AIR) is a compilation of engineering references and data useful to the technical community that can be used to ensure fuel system compatibility with composite structure. This AIR is not a complete detailed design guide and is not intended to satisfy all potential fuel system applications. Extensive research, design, and development are required for each individual application.

Composite Fuel Tanks, Fuel System Design Considerations

SAE AIR1703A-2012 飞行推力的测定

In-Flight Thrust Determination, SAE AIR1703 reviews the major aspects of processes that may be used for the determination of in-flight thrust (IFT). It includes discussions of basic definitions, analytical and ground test methods to predict installed thrust of a given propulsion system, and methods to gather data and calculate thrust of the propulsion system during the flight development program of the aircraft. In-Flight Thrust Determination, SAE AIR1703 reviews the major aspects of processes that may be used for the determination of in-flight thrust (IFT). It includes discussions of basic definitions, analytical and ground test methods to predict installe

In-Flight Thrust Determination

SAE AIR5436-2012 测试储存单元分析推力修正

This document describes a method to correct engine thrust, measured in an indoor test cell, for the aerodynamic effects caused by the secondary airflow induces in the test cell by the engine operating in an enclosed environment in close proximity to an exhaust duct. While it is not recommended to be used to replace test cell correlation, it does provide a means to verify an existing thrust correlation factor.

Test Cell Analytical Thrust Correction

SAE ARP1401B-2012 飞机燃料系统和组件结冰试验

This Aerospace Recommended Practice (ARP) covers a brief discussion of the icing problem in aircraft fuel systems and different means that have been used for icing. Fuel preparation procedures and icing tests for aircraft fuel system and components are proposed herein as a recommended practice to be used in the aircraft industry for fixed wing aircraft and their operational environment only. In the context of this ARP, the engine (and APU) is not considered to be a component of the aircraft fuel system, for the engine fuel system is subjected to icing tests by the engine/APU manufacturer for commercial and specific military applications. This ARP is written mostly to address fuel system level testing. It also provides a means to address the requirements of 14 CFT 23.951(c) and 25.951(c). Some of the methods described in this document can be applied to engine and APU level testing or components of those application domains. This revision does not completely address new developments in ice accretion resulting from internal flow in tubing. This will be addressed ina future revision when more experimental data is available. Some background information on the topic is planned to be available in AIR 790.

Aircraft Fuel System and Component Icing Test

SAE AIR4979A-2012 基于北大西洋公约组织(NATO)航天研发顾问团(AGARD)一致性引擎检测规程的引擎检测中不确定性测量的评估

This document has been declared "Stabilized" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. 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

SAE AIR4246D-2012 航空器涡轮发动机燃料系统组件试验的污染物

This Aerospace Information Report (AIR) is intended as a guide toward standardization in fluid contamination descriptions and specifications. This document discusses descriptions of fluid contamination products. These contaminants are used for design evaluation and formal component qualification/certification testing. Such tests are routinely performed on candidate aircraft engine fuel and pneumatic system components. Typical of these components are fuel pumps, fuel filters, fuel controls, pressurizing valves, flow dividers, selector valves and combustor nozzles. The purpose of this document is to recommend standard descriptions to be used by specification writers.

Contaminants for Aircraft Turbine Engine Fuel System Component Testing

SAE AIR5892B-2012 排放的不挥发性颗粒的测量技术

This document has been declared "Stabilized" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. This SAE Aerospace Information Report (AIR) addresses procedures applicable to quantifying the emission of nonvolatile particulate matter at the exit plane of aircraft gas turbine engines. While both volatile and nonvolatile particulate matter (PM) are present in aircraft gas turbine exhaust, the methods used to measure nonvolatile particles are farther advanced and are addressed here. Existing PM measurement regulations employ the SAE Smoke Number measurement (Reference 2.1.1), a stained filter technique used in evaluating visible emissions. The environmental and human health issues associated with submicronic PM emissions require more detailed measurement of the mass, size, and quantity of these particle emissions. Responding to regulatory agency requests, this AIR describes measurement techniques that are well developed and could be applied to the measurement of aircraft engine particulate matter. The techniques discussed here are considered relevant for measuring particle parameters identified with environmental and health concerns. The discussion that follows is based on research made while developing measurement techniques and in scientific and engineering experiments regarding PM emissions. The techniques are not yet used in routine aircraft engine certification. Future use in regulatory testing is likely to involve further refinements in methodology and application. It is planned that these refinements will be included in the subsequent publication of an Aerospace Recommended Practice. The distinction between nonvolatile and volatile particle types is a critical task in the measurement of particles in aircraft engine exhaust. Appendix A, SAE E-31 Position Paper on Particle Matter Measurements, provides additional technical bases for the scope of this AIR. The measurement methods for volatile condensed particles in turbine exhaust will be covered in a subsequent report. Observations to date show that volatile particles occur mainly at diameters less than 10 nanometers (

Nonvolatile Exhaust Particle Measurement Techniques

SAE AIR6197-2011 重新装载新燃气涡轮发动机试验设施的现场选择考虑因素

This document discusses, in broad and general terms, the effects of various natural and man-made influences on the design, construction, equipping, operation and long term supportability of gas turbine engine test facilities. It will assist existing or future operators of gas turbine engine test facilities in making informed decisions regarding the siting, design, construction or long term support of their facilities. This document is intended to aid operators in understanding the basic terms and concerns regarding gas turbine engine test facility site selection. It is not intended that this document be an exhaustive design guide such that any operator or contractor could accomplish the task of gas turbine test facility site selection independently and without further specialist advice or assistance. To this end it is suggested that this document be read in in conjunction with other SAE International specialist ARP and AIR documents and in association with other industry experts from the OEM's, test facility specialist design houses, architects with specialized knowledge or independent consultants (SME's) within the field.

Site Selection Considerations for New Re-Loaded Gas Turbine Engine Test Facilities

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

SAE ARP1179D-2011 航空器燃气涡轮发动机排气烟度的测量

This SAE Aerospace Recommended Practice (ARP) standardizes test equipment and procedures for the measurement of smoke emission from aircraft gas turbine engines. The procedures included are for determining and reporting the amount of smoke emission. Tests have indicated that the practically achievable precision of the smoke number is within +3 when the system is properly used as outlined herein. This procedure is not intended for in-flight testing, nor does it apply to afterburning mode.

Aircraft Gas Turbine Engine Exhaust Smoke Measurement