V31 发动机辅助系统及其附件 标准查询与下载
共找到 252 条与 发动机辅助系统及其附件 相关的标准，共 17 页
本标准规定了编写以可靠性为中心的维修大纲的方法和决断逻辑。 本标准适用于军用和民用飞机（含直升机）、发动机和设备的寿命周期各阶段。本标准中的以可靠性为中心的维修分析方法适用于确定预研、在研和现役的军用和民用飞机、发动机设备的预防维修要求，也适用于修改初始的维修大纲。
Establishment of Reliability-centered Maintenance Program for Aircraft, Engines and Equipment
- ICS
- CCS
- V31
- 发布
- 1989-05-13
- 实施
- 1989-12-01
System Characteristics
System Characteristics
- ICS
- 49.050
- CCS
- V31
- 发布
- 1989-01-01
- 实施
Turbine engines installed in rotorcraft have an exhaust system that is designed and produced by the aircraft manufacturer. The primary function of the exhaust system is to direct hot exhaust gases away from the airframe. The exhaust system may consist of a tailpipe, which is attached to the engine, and an exhaust fairing, which is part of the rotorcraft. The engine manufacturer specifies a baseline referee tailpipe design, and guaranteed engine performance is based upon the use of the referee tailpipe and tailpipe exit diameter. The configuration used on the rotorcraft may differ from the referee tailpipe, but it is intended to minimize additional losses attributed to the installation. This Aerospace Recommended Practice (ARP) describes the physical, functional, and performance interfaces to be considered in the design of the aircraft exhaust system.
Engine Exhaust System Design Considerations for Rotorcraft
- ICS
- 49.050
- CCS
- V31
- 发布
- 1989
- 实施
This AIR describes a Limited Engine Monitoring System that can be used by the flight crew or the maintenance staff, or both, to monitor the health of gas turbine engines in aircraft. This AIR considers monitoring of gas path performance and mechanical properties, and systems such as low cycle fatigue counters and engine history recorders. It also considers typical measurement system accuracies and their impact. This AIR is intended as a technical guide. It is not intended to be used as a legal document or standard. AIR 1873 supplements ARP 1587, Aircraft Gas Turbine Engine Monitoring System Guide.
Guide to Limited Engine Monitoring Systems for Aircraft Gas Turbine Engines
- ICS
- 49.050
- CCS
- V31
- 发布
- 1988-05-05
- 实施
General specifications for isolated fuel tanks of aircraft hydraulic systems
- ICS
- CCS
- V31
- 发布
- 1988-02-03
- 实施
- 1988-08-01
System Design Considerations
System Design Considerations
- ICS
- 49.050
- CCS
- V31
- 发布
- 1988-01-11
- 实施
本标准规定了ＦＹＸ－１４００型分解式飞机副油箱的设计、制造和试验要求。 ＦＹＸ－１４００型分解式飞机副油箱是一种通用副油箱，适用于采用符合ＧＪＢ１Ａ－８５《机载悬挂物和悬挂装置接合部位的通用设计准则》规定的７６２ｍｍ吊耳间距吊挂系统的各种军用飞机的机身和机翼下挂用，以增加飞机的航程。副油箱在飞行中可弹射投放。
Specifications for FYX-1400 Decomposed Aircraft Auxiliary Fuel Tank
- ICS
- CCS
- V31
- 发布
- 1987-03-11
- 实施
- 1987-07-01
This SAE Aerospace Information Report includes procedures for the analysis of a gas turbine engine start. It utilizes a standard form for the essential starting characteristics of the gas turbine engine and for the starting power capability of the aircraft battery. This report illustrates the format of the characteristic which is provided by the electric starter to transform the battery electric power (voltage and current) to the mechanical power (torque and speed) required to successfully start the engine. An aircraft engine start battery typically also serves as a backup source for emergency electrical energy. Guidelines are therefore provided for the determination of battery capacity to fulfill the emergency energy requirements of the aircraft. The purpose of this information report is to provide a general analysis guide for the optimization of the design of a battery/electric-starter starting system for turbine-engines, including determination of appropriate minimum ratings for both Power (Imp) and one hour energy (C1 capacity).
Starter System Optimization Start Analysis, Turbine Engine - Electric, Battery Power
- ICS
- 49.050
- CCS
- V31
- 发布
- 1987-01-01
- 实施
Design Guidance for Aircraft Electrical Power Systems
Design Guidance for Aircraft Electrical Power Systems
- ICS
- 49.050
- CCS
- V31
- 发布
- 1987-01-01
- 实施
本标准规定了绝对过滤度为5～80微米、波纹式滤层结构的航空滑油过滤器和滤芯的一般技术要求。 本标准适用于航空滑油过滤器及滤芯新品的研制及其批生产和老产品的改进、改型。
General technical specification for aviation lubricating oil filter
- ICS
- CCS
- V31
- 发布
- 1986-12-30
- 实施
- 1987-05-01
The starters covered by this specification shall be designed to operate on compressed air from ground support equipment, engine interbleed or on board air supply, for the purpose of starting aircraft jet engines.
Starter, Pneumatic, Aircraft Engine, General Specification for
- ICS
- 49.050
- CCS
- V31
- 发布
- 1986-01-01
- 实施
本标准适用于航空产品的铜合金熔模铸件。
Standard for Copper Alloy Investment Castings for Aerospace
- ICS
- CCS
- V31
- 发布
- 1985-06-07
- 实施
- 1985-10-01
PtIr25 Alloy Plates for Contacts of Aeroengine Ignition Devices
- ICS
- CCS
- V31
- 发布
- 1985-03-26
- 实施
- 1985-10-01
Generally it is desirable during static engine noise testing to simulate the noise-generating processes that occur during takeoff or landing. One factor that may have significant influence on fan noise from turbofan engines during static testing is the airflow distortion encountered by the low-pressure fan stage. This report presents technical details on devices that "condition" the airflow entering the engine to more nearly simulate flight operations without introducing a detrimental impact on sound propagating from the engine.
Methods of Controlling Distortion of Inlet Airflow During Static Acoustical Tests of Turbofan Engines and Fan Rigs
- ICS
- 17.140.30;49.050
- CCS
- V31
- 发布
- 1985-02-01
- 实施
本标准适用于航空涡轮发动机技术文件、设计资料和有关手册中关于重复构件和要素的编号。
Numbering of repetitive components and elements of aero-turbine engines
- ICS
- CCS
- V31
- 发布
- 1984-08-23
- 实施
- 1985-01-01
Digital System Element Classification
Digital System Element Classification
- ICS
- 49.050
- CCS
- V31
- 发布
- 1984
- 实施
