HB 8680-2021 飛機(jī)起落架應(yīng)急斷離試驗(yàn)通用要求

General requirements for emergency break-away test of aircraft landing gear

HB 8681-2021 飛機(jī)起落架擺振試驗(yàn)通用要求

General requirements for landing gear shimmy test of aircraft

DIN EN 16603-70-41:2017 航空工程 遙測(cè)技術(shù)和遙控指令數(shù)據(jù)包應(yīng)用 英文版本EN 16603-70-41-2017

This Standard addresses the utilization of telecommand packets and telemetry packets for the purposes of remote monitoring and control of spacecraft subsystems and payloads. This Standard does not address mission-specific payload data packets, but the rules contained herein can be extended to suit the requirements of any mission. This Standard does not address audio and video data as they are not contained within either telecommand or telemetry packets. This Standard defines a set of services that satisfy all the fundamental operational requirements for spacecraft monitoring and control during spacecraft integration, testing and flight operations, refer to ECSS-E-ST-70-11. It also specifies the structure and contents of the telecommand packets used to transport the requests and the telemetry packets used to transport the reports.

Space engineering - Telemetry and telecommand packet utilization; English version EN 16603-70-41:2017, only on CD-ROM

ISO 7295:1988/Amd 1:2014 航空器用輪胎汽門(mén)嘴. 互換性尺寸; 修改件1

Tyre valves for aircraft - Interchangeability dimensions; Amendment 1

SAE AIR4994A-2013 航空航天應(yīng)用高壓氣胎壓縮機(jī)用戶指南

Gas compressors (air and other compressible fluids) have been used sporadically since the 1940's for various utility functions in aerospace applications. They have been used to provide power to gun purge and drive systems, engine or APU starters (recharge accumulators), reservoir pressurization, cockpit pressurization, braking systems, canopy seals, engine control divides, landing gear activation, and boosted flight controls (see Table 1). In current state-of-the-art aircraft, most pneumatic system power is extracted from a stage of compression in the turbo-jet engine. As more and more demands are put on new generation engines for fuel economy and performan

High Pressure Pneumatic Compressors Users Guide For Aerospace Applications

SAE AS8584B-2013 軍用飛機(jī)輪制動(dòng)系統(tǒng)

This SAE Aerospace Standard (AS) defines the requirements for brake systems used on military aircraft equipped with wheel-type landing gears.

Brake Systems, Wheel, Military Aircraft

SAE ARP5644-2013 民用飛機(jī)起落架減震測(cè)試

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 起落裝置系統(tǒng)開(kāi)發(fā)計(jì)劃

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 AS7431A-2013 支撐夾托架

Bracket, Support Clamp

SAE ARP1595B-2013 飛機(jī)前機(jī)輪轉(zhuǎn)彎系統(tǒng)的設(shè)計(jì)和檢驗(yàn)

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 AIR5697A-2012 航空航天起落裝置FAA管理歷史飛機(jī)機(jī)輪、輪胎和制動(dòng)器

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) contains regulatory and guidance information related to airplane wheels, tires, and brakes. It contains certain Civil Air Regulations (CAR) and Federal Aviation Regulations (formerly referred to as FARs) from Title 14 Code of Federal Regulations (CFR) in their current version as well as the historical versions. This gives the reader an ability to assemble certain CAR/CFR parts as t

Aerospace Landing Gear FAA Regulatory History Airplane Wheels, Tires, and Brakes

SAE AS6053A-2012 航空器減震器起落架的沖擊試驗(yàn)

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 covers definition of landing impact tests which are to be conducted on landing gear assemblies including shock absorbers, suggested instrumentation for the tests and required data of the resulting test report. It is intended to standardize impact test procedures on landing gear shock absorbers and to provide sufficient data to allow evaluation of the design with respect to requirements of MIL-L-8552 and MI

Tests, Impact, Shock Absorber Landing Gear, Aircraft

SAE ARP4102/2A-2012 自動(dòng)剎車(chē)系統(tǒng)(ABS)

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 document recommends design criteria for an Automatic Braking System. The ABS shall enhance braking performance under most aircraft configurations and all runway conditions.

Automatic Braking System (ABS) (Stabilized Type)

SAE AIR4012C-2012 美國(guó)空軍(USAF)飛機(jī)車(chē)輪

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 is intended to provide comprehensive reference and background information pertaining to military aircraft wheel service experience. The document contains extensive technical performance information for a variety of active military aircraft as well as field and depot service experience and lessons learned. This SAE Aerospace Information Report (AIR) documents general technical data associated with many of the wheels used in the Air Force. This document is intended to be used as a general reference for the aerospace community.

USAF Aircraft Wheels (Stabilized Type)

SAE AIR1489C-2012 航空器起落裝置系統(tǒng)術(shù)語(yǔ)

This report has been compiled by the Landing Gear Systems Terminology Panel of SAE Committee A-5 (Aerospace Landing Gear Systems). It represents an effort to gather together those terms commonly used within the discipline. Some terms are of course common to other disciplines as well. Others, however, are unique in form and/or meaning to the landing gear discipline. The need has been noted to set these terms down and provide a standard definition in order that communication within the discipline may be conducted with a common understanding. Full use has been made of available published information, and a list of references is provided.

Aerospace Landing Gear Systems Terminology

SAE ARP813C-2012 飛行器輪子和液壓制動(dòng)器的可維修性推薦規(guī)程

This Aerospace Recommended Practice (ARP) recommends the maintainability features which should be considered in the design of aircraft wheels and brakes. The effect on other factors, such as, cost, weight, reliability, and compatibility with other systems should be weighed before the incorporation of any of these maintainability features into the design.

Maintainability Recommendations for Aircraft Wheel and Hydraulically Actuated Brake Design

SAE AIR5938-2011 硬著陸信息

This document provides information on the current practices used by commercial and military operators in regards to hard landings (or overload events designated as hard landings). Since detailed information on inspections would be aircraft specific, this AIR provides only a general framework. Detailed information and procedures are available in the maintenance manuals for specific aircraft. Because hard landings potentially affect the entire aircraft, guidelines are listed here for non-landing gear areas. But, the primary focus of the document is the landing gear and related systems. The document may be considered to be applicable to all types of aircraft. This document does NOT provide recommended practices for hard landing inspections, nor does it provide recommendations on the disposition of damaged equipment. Refer to ARP 4915 and ARP 5600. Also, this document does not necessarily address overloads from circumstances other than landings, such as from tow vehicles, runway bumps, traversing cables, etc.

Information on Hard Landings

GJB 1184A-2010 航空機(jī)輪和剎車(chē)裝置通用規(guī)范

本規(guī)范規(guī)定了航空機(jī)輪和剎車(chē)裝置的研制、制造、交付及質(zhì)量保證要求。 本規(guī)范適用于軍用飛機(jī)的航空機(jī)輪和剎車(chē)裝置。直升機(jī)可參照使用。

General specification for aircraft wheel and brake assemblies

SAE AIR5567A-2010 剎車(chē)盤(pán)催化氧化測(cè)試方法

The scope of the test method is to provide stakeholders including fluid manufacturers, airport operators, brake manufacturers, aircraft constructors, aircraft operators and airworthiness authorities with a relative assessment of the effect of deicing chemicals on carbon oxidation. This simple test is only designed to assess the relative effects of runway deicing chemicals by measuring mass change of contaminated and bare carbon samples tested under the same conditions. It is not possible to set a general acceptance threshold oxidation limit based on this test method because carbon brake stack oxidation is a function of heat sink design and the operating environment.

Test Method for Catalytic Carbon Brake Disk Oxidation

SAE AIR4566A-2010 防撞起落架設(shè)計(jì)

The intent of this SAE Aerospace Information Report (AIR) is to document the design requirements and approaches for the crashworthy design of aircraft landing gear. This document covers the field of commercial and military airplanes and helicopters. This summary of crashworthy landing gear design requirements and approaches may be used as a reference for future aircraft.

Crashworthy Landing Gear Design