49.045 结构和结构元件 标准查询与下载

SAE AIR5914-2014 第25部分飞机用起落架疲劳谱发展

This SAE Aerospace Information Report (AIR) provides guidelines for the development of landing gear fatigue spectra for the purpose of designing and certification testing of Part 25 landing gear. Many of the recommendations herein are generalizations based on data obtained from a wide range of landing gears. The aircraft manufacturer or the landing gear supplier is encouraged to use data more specific to their particular undercarriage whenever possible.

Landing Gear Fatigue Spectrum Development For Part 25 Aircraft

SAE AIR1106B-2014 影响飞机导航和防撞灯可视性的几个因素

The scope of this SAE Aerospace Information Report (AIR) is to discuss factors affecting visibility of aircraft navigation and anticollision lights, enabling those concerned with their use to have a better technical understanding of such factors, and to aid in exercising appropriate judgment in the many possible flight eventualities.

Some Factors Affecting Visibility of Aircraft Navigation and Anticollision Lights

HB 8438-2014 民用飞机复合材料结构设计通用要求

本标准规定了民用飞机复合材料结构的设计原则、选材、强度/刚度、损伤容限、耐久性及典型结构的设计要求和相关的验证要求。 本标准适用于民用运输类飞机，其他飞机可参照使用。

General requirements of composite structure design for civil airplane

HB 8447-2014 民用飞机结构防腐蚀设计要求

本标准规定了民用飞机结构腐蚀防护、腐蚀控制等通用设计要求。 本标准适用于民用运输类飞机，其他飞机可参照使用。

General requirements of structure anticorrosion design for civil airplane

HB 8455-2014 民用飞机损伤容限要求

本标准规定了民用飞机影响飞行安全的主要结构和其他选定结构的损伤容限要求，包括设计、评定、验证和适航要求。 本标准适用于民用运输类飞机。其他飞机可参照执行。

Requirements of damage tolerance for civil airplane

HB 8449-2014 民用飞机起落架结构设计通用要求

本标准规定了民用飞机起落架结构设计与验证应遵循的要求。 本标准适用于民用飞机起落架结构设计与验证。

General design requirement for landing gear structures of civil aircraft

SAE AS27648D-2014 抗摩外部自动对准超轻负载滚珠轴承

Scope is unavailable.

BEARING, BALL, AIRFRAME, ANTI-FRICTION, EXTERNAL SELF ALIGNING, EXTRA LIGHT DUTY

SAE AIR1168/4A-2014 冰,雨,雾,以及防霜冻的SAE航空应用热力学手册

This section presents the basic equations for computing ice protection requirements for nontransparent and transparent surfaces and for fog and frost protection of windshields. Simplified graphical presentations suitable for preliminary design and a description of various types of ice, fog, frost, and rain protection systems are also presented.

SAE Aerospace Applied Thermodynamics Manual Ice, Rain, Fog, and Frost Protection

SAE AIR4777B-2013 在飞机轮胎和制动器的生产和操作过程中使用的无损检测 (NDI) 方法

This SAE Aerospace Information Report (AIR) identifies current nondestructive inspection (NDI) methods used to ensure product integrity and maximize ""in service"" life of the major structural components of aircraft wheel and brake assemblies.

Nondestructive Inspection (NDI) Methods Used During Production and Operation of Aircraft Wheels and Brakes

KS W 3223-2013 飞机发动机空中启动连接

Aircraft－Connections for starting engines by air

SAE ARP1493C-2013 军事航空器用轮子和液压制动器的设计和试验要求

This document covers military aircraft wheel and hydraulically actuated brake equipment.

Wheel and Hydraulically Actuated Brake Design and Test Requirements for Military Aircraft

SAE ARP5448B-2013 滑动轴承试验方法

This SAE Aerospace Recommended Practice (ARP) establishes methods for testing airframe plain bearings. The purpose of ARP5448 and its associated slash sheets is to document test methods commonly used to evaluate airframe bearings. These test methods may be referenced in specifications, part standards, purchase orders, etc., when the test is deemed appropriate to the intended use of the bearing by the end user of the bearing. These test methods are not intended to encompass every conceivable requirement for an airframe bearing. The end user of the bearing must exercise engineering judgment to determine the most appropriate standard and/or nonstandard tests f

Plain Bearing Test Methods

SAE AS27649D-2013 机身抗摩擦中型滚珠轴承

Scope is unavailable.

BEARING, BALL, AIRFRAME, ANTIFRICTION, INTERMEDIATE DUTY

SAE AS8037C-2013 飞机定位航灯用最低性能标准

This Aerospace Standard (AS) establishes minimum performance standards for new equipment position lights. This Aerospace Standard defines minimum light intensity in terms of candelas in vertical and horizontal directions about the longitudinal, vertical, and lateral axes of the aircraft. It also defines color tolerances in terms of limiting chromaticities for the light emitted from the position lights. It is not intended that this standard require the use of any particular light source such as quartz-halogen, incandescent, or any other specific design of lamp.

Minimum Performance Standard for Aircraft Position Lights

SAE AS26805B-2013 空气/气体压缩机组通用要求

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 specification has been declared ""NONCURRENT"" as of April 2008. It is recommended, therefore, that this document not be specified for new designs. This specification covers the general requirements for the design and construction of air/gas compressor units (see 6.4.1). The detail requirements for a particular air compressor unit shall be as specified in the individual equipment specification for that particular air

Compressor Units, Air/Gas, General Requirements For

SAE ARP5644-2013 民用飞机起落架减震测试

The intent of this document is to provide recommended practices for conducting shock absorption testing of civil aircraft landing gear equipped with oleo-pneumatic shock absorbers. The primary focus is for Part 25 aircraft, but differences for Part 23, 27, and 29 aircraft are provided where appropriate.

Landing Gear Shock Absorption Testing of Civil Aircraft

SAE ARP1598B-2013 起落装置系统开发计划

This Aerospace Recommended Practice (ARP) is intended to document the process of landing gear system development. This document includes landing gear system development plans for commercial, military, fixed wing and rotary wing air vehicles.

Landing Gear System Development Plan

SAE ARP4902B-2013 飞机除冰设施的设计和操作

This document provides information and guidance material to assist in assessing the need for and feasibility of developing deicing facilities, the planning (size and location) and design of deicing facilities, and assessing environmental considerations and operational considerations associated with deicing facilities. The document presents relevant information necessary to define the need for a deicing facility and factors influencing its size, location, and operation. The determination of the need for deicing facilities rest with Airports. Although this document intends to provide information to airport operator and deicing facility planner/designer, all s

Design and Operation of Aircraft Deicing Facilities

SAE ARP1595B-2013 飞机前机轮转弯系统的设计和检验

This document provides recommended practices for the design, development, and verification testing of aircraft nosewheel steering of NWS systems.

Design and Verification of Aircraft Nose Wheel Steering Systems

SAE ARP5412B-2013 飞行器雷电环境和相关检测波形

The environment and test waveforms defined in this SAE Aerospace Recommended Practice (ARP) account for the best lightning data and analysis currently available. The quantified environment and levels herein represent the minimum currently required by certifying authorities, consistent with the approach applied in related lightning documents. Lightning, like other weather phenomenon, is probabilistic in nature. Levels and waveforms vary considerably from one flash to the next. Within this document, standardized voltage and current waveforms have been derived to represent the lightning environment external to an aircraft. These standardized waveforms are used

Aircraft Lightning Environment and Related Test Waveforms