49.050 航空航天发动机和推进系统 标准查询与下载

ASTM F3063/F3063M-16a 燃油/能源储存和运输系统设备的设计和整合标准规范

1.1 This specification covers minimum requirements for the design and integration of Fuel/Energy Storage and Delivery system installations for aeroplanes. 1.2 This specification is applicable to aeroplanes as defined in the F44 terminology standard. 1.3 The applicant for a design approval must seek the individual guidance to their respective CAA body concerning the use of this standard as part of a certification plan. For information on which CAA regulatory bodies have accepted this standard (in whole or in part) as a means of compliance to their Aeroplane Airworthiness regulations (Hereinafter referred to as “the Rules”), refer to ASTM F44 webpage (www.ASTM.org/COMITTEE/F44.htm) which includes CAA website links. 1.4 Units—The values stated are SI units followed by imperial units in brackets. The values stated in each system may not be exact equivalents; therefore, each system shall be used independently of the other. Combining values from the two systems may result in non-conformance with the standard. 1.5 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 Specification for Design and Integration of Fuel/Energy Storage and Delivery System Installations for Aeroplanes

ASTM D7685-11(2016) 用于铁磁和非铁磁性磨损碎片的在线全流量感应传感器的标准实践航空衍生和飞机燃气轮机发动机轴承的测定和诊断

1.1 This practice covers the minimum requirements for an in-line, non-intrusive, through-flow oil debris monitoring system that monitors ferromagnetic and non-ferromagnetic metallic wear debris from both industrial aero-derivative and aircraft gas turbine engine bearings. Gas turbine engines are rotating machines fitted with high-speed ball and roller bearings that can be the cause of failure modes with high secondary damage potential. (1)2 1.2 Metallic wear debris considered in this practice range in size from 120 µm (micron) and greater. Metallic wear debris over 1000 µm are sized as over 1000 µm. 1.3 This practice is suitable for use with the following lubricants: polyol esters, phosphate esters, petroleum industrial gear oils and petroleum crankcase oils. 1.4 This practice is for metallic wear debris detection, not cleanliness. 1.5 The values stated in SI units are to be regarded as standard. The values given in parentheses are provided for information only. 1.6 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 In-Line, Full Flow, Inductive Sensor for Ferromagnetic and Non-ferromagnetic Wear Debris Determination and Diagnostics for Aero-Derivative and Aircraft Gas Turbine Engine Bearing

GSO ISO 482:2015 飞机 推进装置和部件 确定和描述旋转方向的方法

  Scope is not provided for this standard

Aircraft -- Propulsion units and components -- Methods of numbering and describing direction of rotation

GSO ISO 45:2015 飞机 压力加油连接

  Scope is not provided for this standard

Aircraft -- Pressure refuelling connections

ASTM F3065/F3065M-15 螺旋桨系统的安装和集成标准规范

1.1 This specification addresses the airworthiness requirements for the installation and integration of propeller systems. 1.2 This specification is applicable to aeroplanes as defined in F44 terminology standard. 1.3 The applicant for a design approval must seek the individual guidance to their respective CAA body concerning the use of this standard as part of a certification plan. For information on which CAA regulatory bodies have accepted this standard (in whole or in part) as a means of compliance to their Small Aircraft Airworthiness regulations (Hereinafter referred to as “the Rules”), refer to ASTM F44 webpage (www.ASTM.org/COMITTEE/F44.htm) which includes CAA website links. 1.4 Units—The values stated are SI units followed by Imperial units in square brackets. The values stated in each system may not be exact equivalents; therefore, each system shall be used independently of the other. Combining values from the two systems may result in non-conformance with the standard. 1.5 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 Specification for Installation and Integration of Propeller Systems

ASTM F3066/F3066M-15 动力装置系统特定危害减轻标准规范

1.1 This specification covers minimum requirements for hazard mitigation in propulsion systems installed on small aeroplanes. 1.2 The applicant for a design approval must seek the individual guidance to their respective CAA body concerning the use of this standard as part of a certification plan. For information on which CAA regulatory bodies have accepted this standard (in whole or in part) as a means of compliance to their Small Aircraft Airworthiness regulations (Hereinafter referred to as “the Rules”), refer to ASTM F44 webpage (www.ASTM.org/COMITTEE/F44.htm) which includes CAA website links. 1.3 Units—The values stated are SI units followed by imperial units in brackets. The values stated in each system may not be exact equivalents; therefore, each system shall be used independently of the other. Combining values from the two systems may result in non-conformance with the standard. 1.4 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 Specification for Powerplant Systems Specific Hazard Mitigation

GOST R 56517-2015 液体火箭发动机. 在考虑测量误差的情况下根据输入参数最大允许值进行的生产质量控制规则

Liquid rocket engines. Production quality control rules according to maximum permissible value of output parameters, considering measurement error

GOST R 56463-2015 小推力液体火箭发动机. 服务中交付条件下生产, 试验以及指令保证的通用要求

Liquid-propellant rocket engines of small thrust. Production, tests and quality assurance general requirements under in-service delivery

SAE AS3075E-2014 垫片 37° 喇叭管接头，镍，AMS5553

SCOPE IS UNAVAILABLE.

GASKET - 37° FLARED TUBE FITTING, NICKEL, AMS5553

SAE AS17107B-2014 BEARING BALL ANNULAR 主要用于飞机发电机和电动发电机 STANDARD LIGHT TYPE I

No abstract available.

BEARING@ BALL@ ANNULAR@ PRIMARILY FOR AIRCRAFT GENERATORS AND MOTOR-GENERATORS@ STANDARD LIGHT@ TYPE I

SAE AS3074D-2014 衬垫.AMS 5553镍37°扩口管接头

Scope is unavailable.

GASKET - 37° FLARED TUBE FITTING, NICKEL, AMS5553

SAE AS3073D-2014 垫圈.AMS 4500型37°铜扩口管配件

Scope is unavailable.

GASKET - 37° FLARED TUBE FITTING, COPPER, AMS4500

SAE AS3484C-2014 垫片 37° 喇叭管接头，镍，AMS5553

Scope is unavailable.

GASKET - 37° FLARED TUBE FITTING, NICKEL, AMS5553

SAE AS131B-2014 飞机发动机所用的I型,II& III型飞机连接进油口和出油口衬垫

Scope is unavailable.

PADS, OIL INLET AND OUTLET, TYPES I, II & III - FOR AIRPLANE CONNECTIONS AIRCRAFT ENGINES

MH/T 9007-2014 民用航空发动机系统部件环境试验指南

本标准规定了民用航空发动机系统部件的26项环境试验的指导性方法。本标准适用于民用航空发动机控制系统、润滑系统、液压系统、电气系统以及反推系统的部件环境试验。飞机液压系统、电气系统以及环控等系统的部件环境试验可参照本标准执行。

Guides for environmental tests of civil aero-engine components

MH/T 9006-2014 航空燃气涡轮发动机气态排出物计算方法

本标准规定了航空燃气涡轮发动机气态排出物的计算条件和计算方法。本标准适用于航空涡轮喷气发动机、涡轮风扇发动机和涡轮螺旋桨发动机产生的气态排出物的计算。

Calculating methods of gaseous emissions for aircraft gas turbine engines

SAE ARP4940-2014 航空液压马达的应用指南

This SAE Aerospace Recommended Practice (ARP) is an application guide for fixed and variable displacement hydraulic motors. It provides details of the characteristics of fixed and variable displacement hydraulic motors, architectures, circuit designs, controls, and typical applications. The applications include airborne and defense vehicles with emphasis on high performance applications.

Application Guide for Aerospace Hydraulic Motors

SAE AS5625A-2014 静态电力变频器的最低性能标准

This SAE Aerospace Standard (AS) establishes the minimum performance standards for equipment used as secondary alternating current (AC) electrical power sources in aerospace electric power systems.

Minimum Performance Standards for Static Electric Power Frequency Converters

ASTM F3005-14a 用于小型无人机系统的电池的标准规范

1.1 This standard defines the requirements for batteries used in small Unmanned Aircraft Systems (sUAS). 1.2 This standard does not define requirements for the systems in which sUAS battery packs may be utilized. 1.3 This standard is subordinate to Specification F2910. 1.4 If allowed by a nation’s GAA, certain sUAS may be exempt from this standard and may use commercial off-theshelf (COTS) batteries in non-safety-critical payloads (lithium chemistries may not be exempted). Air transport regulations still shall be adhered to when air transport is used for COTS cells or batteries in bulk. 1.5 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 Specification for Batteries for Use in Small Unmanned Aircraft Systems (sUAS)

SAE AIR1666B-2014 飞机动力和推进润滑系统中采用的润滑剂滤芯性能试验

This SAE Aerospace Information Report (AIR) reviews performance testing parameters for non-cleanable, often referred to as disposable, filter elements utilized in aircraft power and propulsion lubrication systems, including gas turbine engines and auxiliary power units (APUs), propulsion and transmission gear boxes, and constant speed drives and integrated drive generators (IDGs). This document is confined to laboratory testing of filter element performance to qualify the filtration medium and filter element construction as opposed to qualification of the complete filter assembly. The testing discussed here is usually followed by laboratory and on-engine te

Performance Testing of Lubricant Filter Elements Utilized in Aircraft Power and Propulsion Lubrication Systems