V42 起飞着陆装置 标准查询与下载

GJB 5586-2006 微波着陆系统机载接收机地面测试设备通用规范

本规范规定了微波着陆系统机载接收地面测试设备的通用要求、质量保证规定、交货准备及说明事项。本规范适用于微波着陆系统机载接收机的地面测试设备（以下简称测试设备），是制定该类产品规范的依据。

General specification of ground measuring equipment for microwave landing system(MLS)airborne equipment

SAE AIR5883-2006 起落架装置振动Struts框架轴承选择

This document defines the criteria used for the selection of landing gear shock strut supper and lower bearings. Common problems associated with shock strut bearings are presented.

Landing Gears Shock Struts Bearing Selection

SAE AIR4846-2006 特别专用的起落架装置

A landing gear system comprises the most compelling assembly of engineering skills. Its importance to the successful design of an aircraft can be favorably compared with that of the aircrafts wings and engines. A landing gear system consists of several different engineering disciplines, and is continually in the public eye especially with regard to safety. The primary objective of AIR4846 is to present a record of a variety of interesting gears, gear/aircraft systems and patents, and to discuss wherever possible the lessons learned, and the reasons for the design. Thus, the document is not only a historical account, but a means of recording technical knowledge for the practical benefit of future landing gear designers.

Extraordinary and Special Purpose Landing Gear Systems

GJB 5448-2005 直升机滑橇起落架通用规范

本规范规定了直升机滑撬起落架的技术要求、质量保证规定和交货准备。 本规范适用于直升机梁式滑橇起落架，其它类型的滑橇起落架可参照使用。

General specification for helicopter skid-type landing gear

DIN EN 14776:2005 航空工程.地面设备和操作.遥测技术和遥控指令数据包应用

This packet utilization standard complements these standards by defining the application-level interface between ground and space, in order to satisfy the requirements of electrical integration and testing and flight operations.#,,#

Space engineering - Ground systems and operations - Telemetry and telecommand packet utilization; English version EN 14776:2004

DIN EN 14777:2005 航天工程.Multipaction设计和试验

Space engineering - Multipaction design and test; English version EN 14777:2004

DIN EN 14737-2:2005 航天工程.地面系统和操作.第2部分:文件要求定义(DRDs)

Space engineering - Ground systems and operations - Part 2: Documents requirements definitions (DRDs); English version EN 14737-2:2004

SAE ARP5146-2005 飞行器轮子密封系统的评定

This SAE Aerospace Recommended Practice (ARP) is intended to provide guidance on verifying the integrity of inflation pressure sealing systems of aircraft wheel/tire assemblies. Aircraft wheel/tire assemblies can maintain inflation integrity only if the entire sealing system, consisting of the tire, wheel, inflation valve, over pressure relief devices, pressure monitoring systems , valve caps, gauges, fuse plugs, O-rings, seal glands and interfaces/boundaries between these components, successfully contains the tire inflation gas. This document is to be used as a guide for sealing system validation when new design concepts not proven in service are being employed. It may also be used for evaluating alternate design approaches, material changes and trouble shooting service problems. The design of the sealing system and the need for verification testing are left to the discretion of the wheel manufacturer, and the cognizant wheel design and configuration controller. This document is not intended to be a new qualification/certification standard.

Assessment of Aircraft Wheel Sealing Systems

NF L91-102-2:2005 飞行器地面设备.带前起落架的无牵引杆的牵引车辆(TLTV)的设计、试验和维护.第2部分:区域性飞行器

Aircraft ground equipment - Design, test and maintenance for towbarless towing vehicles (TLTV) interfaced with nose-landing gear - Part 2 : regional aircraft.

SAE AIR5451-2005 起落架装置系统组装指南

The landing gear system is a major airframe system that needs to be integrated very efficiently to minimize the penalties of weight, cost, dispatch reliability and maintenance. As the landing gear system business develops and large scale teaming arrangements and acquisitions become increasingly common, it may be desirable in some instances to procure an Integrated Landing Gear System. This document provides guidelines and useful references for developing an integrated landing gear system for an aircraft and is divided into four sections: Landing Gear Configuration Requirements; Landing Gear Functional Requirements; Landing Gear System Integrity Requirements; Landing Gear Program Requirements. The landing gear system encompasses all landing gear structural and subsystem elements. Structural elements include shock struts, braces, fittings, pins, wheels, tires and brakes. The subsystem elements include the retraction/extension system (both normal and alternate), the steering system, the braking system (both normal and alternate, manual and automatic), the indication systems and control systems (mechanical, hydraulic, electrical and electronic).

A Guide to Landing Gear System Integration

ASTM F2242-05(2008) 动力伞降飞行器的生产验收试验系统的标准规范

1.1 The following requirements apply for the manufacture powered parachute aircraft. This specification includes the production acceptance test requirements for powered parachute aircraft. 1.2 This specification applies to powered parachute aircraft seeking civil aviation authority approval, in the form of flight certificates, flight permits, or other like documentation. 1.3 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 requirements prior to use.

Standard Specification for Production Acceptance Testing System for Powered Parachute Aircraft

SAE AMS4183-2005 溶液热处理和用拉伸法应力消除的4.4Cu 1.2Mg 0.8Mn 0.10Zr铝合金挤制型材(2027-T3511)

This specification covers an aluminum alloy in the form of extruded profiles.

Aluminum Alloy, Extruded Profiles (2027-T3511) 4.4Cu 1.2Mg - 0.8Mn 0.10Zr Solution Heat Treated and Stress Relieved by Stretching UNS A92027

DIN EN 14737-1:2004 航天工程.地面系统和操作.第1部分:原则和要求

Within the frame of the overall engineering standards for space missions, this European Standard contains the basic rules, principles and requirements to be engineering of the ground segment and mission operations, which form an integral part of the overall system implementing a space mission.#,,#

Space engineering - Ground systems and operations - Part 1: Principles and requirements; German version EN 14737-1:2004

BS EN 14776:2004 航空工程.地面设备和操作.遥测技术和遥控指令数据包应用

This document addresses the utilization of telecommand packets and telemetry source packets for the purposes of remote monitoring and control of subsystems and payloads. This document does not address mission-specific payload data packets, but the rules contained herein can be extended to suit the requirements of any mission. This document does not address audio and video data as they are not contained within either telecommand or telemetry source packets. This document is structured as follows. Firstly a set of operational concepts is identified, covering all the fundamental requirements for spacecraft monitoring and control during satellite integration, testing and flight operations. A set of services that satisfy these operational concepts is then defined. The detailed specification of these services includes the structure and contents of the associated service requests (telecommand packets) and service reports (telemetry source packets). This document is applicable to any mission, no matter what its domain of application, orbit or ground station coverage characteristics. However, it is not the intention that the PUS is applicable to a given mission in its entirety. The operational concepts and corresponding services contained in this document cover a wide spectrum of operational scenarios and, for a given mission, only a subset of these operational concepts and services is appropriate. Choices are made early in the design phase of a new mission resulting in the need to tailor the PUS to suit the requirements of the particular mission. These choices include: a) The on-board system design and architecture, in terms of the number of on-board application processes, their on-board implementation (e.g. the allocation to on-board processors) and their roles (i.e. which functions or subsystems or payloads they support). b) Which PUS services are supported by each application process. NOTE Tailoring is a process by which individual requirements or specifications, standards and related documents are evaluated and made applicable to a specific project by selection, and in some exceptional cases, modification of existing or addition of new requirements (ECSS-M-00-02A, clause 3 (Reference [11])). Each mission should document the results of this design and selection process in a space-ground interface control document (SGICD). Some missions implement a centralized architecture with a small number of application processes, whilst others have a highly-distributed architecture within which a correspondingly larger number of application processes are distributed across several on-board processors. The specification of services in this document is adapted to the expectation that different missions require, different levels of complexity and functionality from a given service. To this end, all services are optional and a given service can be implemented at one of several distinct levels, corresponding to the inclusion of one or more capability sets. The minimum capability set corresponds to the simplest possible level, which also remains sensible and coherent. At least this set is included in every implementation of a given service. The PUS should be viewed as a "Menu" from which the applicable services and service-levels are selected for a given mission. This selection process is repeated for each on-board application process, since each application process is designed to provide a specific set of tailored services.

Space engineering - Ground systems and operation - Telemetry and telecommand packet utilization

BS ISO 15389:2001 航天系统.飞行着陆脱落插头

This International Standard defines the general criteria for the development of flight-to-ground umbilical systems used by a space system. The criteria specified herein is limited to the service arms or equivalent mechanisms, umbilical carriers and plates, couplings, connectors, withdrawal and retract devices, handling mechanisms and control systems for mechanisms.

Space systems - Flight-to-ground umbilicals

SAE AIR5358-2004 着陆齿轮减震支柱液压液

This SAE Aerospace Information Report (AIR) was prepared by a panel of the SAE A-5 Committee. This document establishes the specifications for fluids used in landing gear shock struts with extreme pressure and antiwear additives that have been added for improved lubrication. This document requires qualified products.

Landing Gear Shock Strut Hydraulic Fluid

SAE AIR5885-2004 起落架装置通用检修

This document outlines the most common repairs used on landing gear components. It is not the intention of this AIR to replace Overhaul/Component Maintenance or Technical Order Manuals, but it can serve as a guide into their preparation. This document may also be used as a template to develop an MRB (Material Review Board) plan. The recommendations in this document apply to components made of metallic alloys. These recommendations are intended for new manufactured components as well as for overhauled components. The extent of repair allowed for new components as opposed to in-service components is left to the cognizant engineering authorities. Reference could be made to this document when justifying repairs on landing gears. For repairs outside the scope of this document, a detailed justification is necessary. It must be understood that all the repairs listed in this document are not to be applied without the involvement of the cognizant engineer.

Landing Gear Common Repairs

HB 8105-2002 起落架用衬套

本标准规定了起落架用衬套的结构 尺十和要求。 本标准适用于压人起落架铵链螺栓的连接。

Bush for landing gear

SAE AIR1810C-2003 (R)设计,开发和试验标准.起落架应用的固体接近开关/系统

This document examines the most important considerations relative to the use of proximity sensing systems for applications on aircraft landing gear. In general, the recommendations included are applicable to other demanding aircraft sensor installations where the environment is equially severe. The purpose of this SAE Aerospace Information Report (AIR) is to suggest specification, application, performance, and validation criteria for solid-state proximity sensing systems used for environmentally severe applications on aircraft landing gear.

(R) Design, Development and Test Criteria - Solid State Proximity Switches/Systems for Landing Gear Applications

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