V42 起飞着陆装置 标准查询与下载

HB/Z 223.19-2002 飞机装配工艺.起落架的装配与试验

Aircraft assembling technology assembling ang test for landing gear

SAE ARP5507-2002 航空器轮胎到轮子的工作特性

The performance of an aircraft tire/wheel assembly in service is dependent on the geometrical fit, load distribution, and performance at the tire/wheel interface while rolling. This document focuses on the tire-to-wheel circumferential movement for a new tubeless tire.

Aircraft Tire-to-Wheel Performance Characteristics

IEC TS 62143:2002 机场照明和信标用电气装置.航空地面照明系统.安全生命周期方法制定指南

This technical specification: - outlines a methodology to address the safety at all lifecycle phases of an AGL system, including the evaluation, design, procurement, manufacture, installation, commissioning, operational use, maintenance, modification, an

Electrical installations for lighting and beaconing of aerodromes - Aeronautical ground lighting systems - Guidelines for the development of a safety lifecycle methodology

ASTM D6812-02 评价涡轮增压器/增加负荷量的火花点燃飞行器发动电机的地面站辛烷的实施规程

1.1 This practice covers ground-based octane rating procedures for turbocharged/supercharged spark ignition aircraft engines. This practice has been developed to allow the widest range of applicability possible but may not be appropriate for all engine types. This practice is specifically directed to ground-based testing and actual in-flight octane ratings may produce significantly different results.1.2 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 Ground-Based Octane Rating Procedures for Turbocharged/Supercharged Spark Ignition Aircraft Engines

KS W 1554-2001 轮胎气门嘴.芯腔No.1

이 규격은 주로 농기계, 도로 차량, 민간 항공기용 타이어에서 사용되는 밸브의 No.1 코

Tyre valves-Core chamber No. 1

KS W 1555-2001 轮胎气门嘴.芯腔No.2

이 규격은 농기계, 도로 차량, 민간 항공기용 타이어에서 사용되는 밸브의 No.2 코어 챔

Tyre valves-Core chamber No. 2

SAE ARP5429-2001 使用等效损伤谱的降落装置疲劳试验

This SAE Aerospace Recommended Practice (ARP) applies to fatigue testing of landing gear and landing gear components. Advancements in fatigue analysis methodology, combined with larger and faster computers, have led to more thorough and accurate fatigue life predictions. Traditional methodology involved the analysis of block loading spectra using S-N curves excluding the effect of plastic strain, residual stresses and the effect of the loading sequence. Todays methodology employs strain-life analysis combined with the application of Neubers equation and the effects of the loading sequence to determine the true state of stress of every load set in a flight-by-flight spectrum. While providing the ability to analyze the real world our advancements in analytical methodology have surpassed the practicality of physical testing. While it is relatively simple to analyze a flight-by-flight spectrum, the cost and time required to test a flight-by-flight spectrum is prohibitive. The purpose of this document is to provide a method and rationale for creating a physical test spectrum which is significantly reduced from the analytical spectrum and yet provides an accurate accumulation of the analytical damage for all critical areas of the article under test. While the focus of this document is the fatigue testing of landing gear, the approach is applicable to most mechanical structures subject to safe life fatigue analyses.

Landing Gear Fatigue Tests with Equivalent Damage Spectra

SAE AIR5388-2001 独特的机轮和制动器设计

This SAE Aerospace Information Report (AIR) has been prepared by a panel of the SAE A-5A Committee and is presented to document unique design approaches used for aircraft wheels and brakes. The purpose of this AIR is to describe wheel and brake designs possessing unique features or approaches to allow them the meet the requirements of the particular airplane for which they were intended. Wherever possible, the requirements driving these design and the lessons learned are documented. This AIR is intended to document the ingenuous solutions that have lead eventually to the wheel and brake designs in use today and pointing to the brakes for tomorrow.

Unique Wheel and Brake Designs

SAE AS6053-2001 飞机起落架减震器撞击测试

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 MIL-S- 8959 as applicable.

Tests, Impact, Shock Absorber Landing Gear, Aircraft

KS W 1926-2000 自锁系紧连杆端滚珠轴承

This standard defines self-aligning rod end ball bearing that used in the control system device of aircraft. Note 1. This specification covers rod end roller bearings with application in temperature ranges -55 ~ 149°c and intermittent maximum allowable temperature is 177°C. 2. Unit and dimension in parenthesis in this standard are that use through consultation as things by unit hitherto.

Self-aligning rod end roller bearing for aircraft

KS W 1925-2000 航空器双列连杆端滚珠轴承

This standard defines double-row rod end ball bearing that used in the control system device of aircraft. Note 1. This specification covers rod end ball bearings with application in temperature ranges -54~121 °C and -54°C to 149°C with 20% reduction of the predicted performance. 2. Unit and dimension in parenthesis in this standard are that use through consultation as things by unit hitherto.

Double-row rod end ball bearing for aircraft

HB 7666-2000 飞机起落架系统性能试验验证要求

本标准规定了飞机起落架系统性能试验验证要求。 　　本标准适用于飞机起落架系统各主要性能的试验验证。对于具体型号的飞机起落架系统，可用合同方式对本试验验证要求进行修改和补充。

Aircraft landing gear system performance test verification requirements

AIAA S-017A-2000 气动减速器和降落伞图

This drawing standard refers to federal and military specifications which, as of the time of this revision, are either equivalent to existing commercial specifications or are in the process of being converted to commercial specifications. The federal or military specification should be considered a reference only.

Aerodynamic Decelerator and Parachute Drawings

SAE ARP5381-2000 第23,27,29部分飞行器轮子,制动器及轮子和制动器组件的最低性能推荐规程

This minimum performance document defines the testing required for wheels, brakes, and wheel and brake assemblies to be used on civil aircraft certified under 14 Code of Federal Regulations (CFR) Part 23, 27, and 29.

Minimum Performance Recommendations for Part 23, 27, and 29 Aircraft Wheels, Brakes, and Wheel and Brake Assemblies

KS W 1537-1999 航空器轮胎和轮辋.第1部分:规范

이 규격은 ISO 3324에 의해 항공기의 재생 및 새 타이어와 림에 관하여 규정한다.

Aircraft tyres and rims-Part 1:Specification

KS W 1538-1999 航空器轮胎和轮辋.第2部分:轮胎的试验方法

이 규격은 민간 항공기의 새 타이어 및 재생 타이어의 시험 방법을 아래와 같이 규정한다.

Aircraft tyres and rims-Part 2:Test methods for tyres

SAE AIR5024-1999 起落架开关选择标准

The scope of this document is to discuss the differences between electromechanical and proximity position sensing devices when used on landing gears. It also contains information, which may be helpful, when applying either type of technology after the selection has been made. The purpose is to help the designer make better choices when selecting a position-sensing device. Once that choice has been made, this document includes information to improve the reliability of new or current designs. It is not intended to replace recommendations from sensor manufacturers or actual experience, but to provide a set of general guidelines.

Landing Gear Switch Selection Criteria

SAE AMS1431B-1998 硬跑道和滑行道除冰/防冰用化合物

This specification covers a deicing and anti-icing compound in the form of a solid. This compound are intended for use at airports on aircraft maneuvering areas, such as aprons, runways, and taxiways, for the prevention and removal of frozen deposits of snow, frost, and ice..

Compound, Solid Runaway and Taxiway Deicing/Anti-Icing

HB 7584-1998 飞机起落装置系统 术语

标准规定了有关飞机起落装置系统的常用术语。 　　本标准适用于飞机起落装置系统。包括：起落架结构，刹车防滑系统，滚动部件，方向控制系统，起落架的和舱门收放系统，辅助减速和弹射起飞装置，地面操作和专用辅助系统，地面漂浮性等方面的专业术语。

Terminology for aircraft landing gear systems

HB 7598-1998 飞机操纵滑轮通用规范

General specification for aircraft control pulleys