V56 机场地面服务系统及设备 标准查询与下载

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 AIR5468-2000 标记飞机导线用紫外线激光器

Ultraviolet (UV) laser marking for aerospace wire and cable is now a well established and accepted process. The purpose of this report is to provide general information on the technical basis of marking systems that apply UV laser energy to the wire surface. This includes materials for UV laser marking; the key characteristics of UV lasers suitable for this application, in terms of the mark process requirements and operational requirements; the various types of UV lasers which meet the general requirements for wire marking; and the generic components of UV laser marking systems. Subjects beyond the scope of this report include other wire marking systems not utilizing UV lasers; legibility; and contrast measurement.

Ultraviolet (UV) Lasers for Aerospace Wire Marking

SAE ARP4853B-2000 无拖棒拖动车辆的设计规范

This SAE Aerospace Recommended Practice (ARP) describes the dimensions, design, layout, performance, and capability of a towbarless tow vehicle (TLTV). This tow vehicle will basically be used for aircraft listed in 1.4. Overall design of the unit is to allow operations under climatic conditions as stated under 5.1 and safe operations during day and night conditions on airport aprons, runways, taxiways, and hangars.

Design Specification for Towbarless Tow Vehicles

SAE ARP4852B-2000 无拖棒后推式拖动车辆的设计规范

This SAE Aerospace Recommended Practice (ARP) describes the dimensions, design, layout, performance, and capability of a towbarless tow vehicle (TLTV), mainly used for push-back operation on the nose gear. This tow vehicle will basically be used for aircraft listed in 1.3. Overall design of the unit is to allo operations under climatic conditions as stated under 5.1 and safe operations during day and nigh conditions on airport aprons, runways, taxiways, and in hangars.

Design Specification for Towbarless Push-Back Tow Vehicles

MH/T 6019-1999 飞机地面电源机组

本标准规定了飞机地面电源机组的技术要求、试验方法、检验规则及包装、标志、贮运。 本标准适用于由内燃机驱动发电机、向飞机供给检查和启动电能的交流400H z,1 15/200V (三相)、115 V (单相)和直流28.5 V地面电源机组，包括固定式、汽车式和挂车式电源机组。

Aircraft ground support power units

MH/T 6018-1999 地面静态电源

本标准规定了地面静态电源的技术要求、试验方法、检验规则及包装、标志、贮运。 本标准适用于向飞机及机载设备供给启动、检查和维修电能的交流400Hz、115/200V(三相)、115V(单相)、26V(单相)、36V(三相)和支流28.5V地面静态电源，包括专用于登机桥、室外或室内使用的固定式或可移动式的地面静态电源(以下简称静态电源)。

Ground solid-state power

BS Z 100:1999 空间系统.发射、着陆或回收场用地面保障设备.一般要求

This International Standard specifies the general characteristics, performance, design, test, safety, reliability, maintainability and quality requirements for ground support equipment (GSE) and systems intended for use at launch, landing, or retrieval-site installations or other locations that are the responsibility of the launch, landing and retrieval site. This International Standard does not specify how to design GSE, but establishes the minimum requirements to provide simple, robust, safe, reliable, maintainable and cost-effective GSE. This International Standard is applicable to the design of non-flight hardware and software used to support the operations of transporting, receiving, handling, assembly, inspection, test, checkout, service, launch and recovery of space vehicles and payloads at the launch, landing, or retrieval sites. As such, the requirements of this International Standard are optional for hardware used only at the manufacturing, development, or test sites prior to arrival at the launch, landing, or retrieval sites or at the mission control site. However, if such GSE is temporarily used at a launch, landing, or retrieval site, for whatever reason, this GSE shall comply with all the safety-related requirements of this International Standard, as a minimum. NOTE —In the event of conflict between the documents referenced herein and the contents of this International Standard, the contents of this International Standard supersede except where otherwise noted. The applicable contract or purchase/procurement order takes precedence over the contents of this International Standard in the event of conflicting requirements. Nothing in this International Standard supersedes applicable laws and regulations unless a specific exemption has been obtained.

Space systems - Ground support equipment for use at launch, landing, or retrieval sites - General requirements

SAE ARP1052A-1999 (R)地面支持设备所用内燃发动机的选择准则

This SAE Recommended Practice (ARP) is intended as a guide toward standard practice and is subject to change to keep pace with experience and technical advances. The purpose of this document is to establish a guideline for the selection of prime movers for use in aircraft ground support equipment. This document is recommended for use by those engaged in the design, selection, or purchase of ground support equipment. This document is applicable to both four-stroke and two-stroke spark ignition and compression ignition engines.

(R) Selection Criteria for Internal Combustion Engines Used in Ground Support Equipment

DD ENV 50231-1997 航空用地面照明电气设备.恒定电流调节器的设备规范和试验

Aeronautical ground lighting electrical installation. Constant current regulator. Equipment specifications and tests

DD ENV 50230-1997 航空用地面照明电气设备.控制监测系统的一般要求

Aeronautical ground lighting electrical installation. Control and monitoring systems. General requirements

DD ENV 50232-1997 航空地面照明电子设备.绝缘变压器的设备规范和试验

Aeronautical ground lighting electrical installation. Isolating transformer. Equipment specifications and tests

SAE AS4262A-1997 飞机地面空调服务连接

This SAE Aerospace Standard (AS) defines interface configurations for the ground air conditioning service connection on commercial transport aircraft. In addition, it defines the clearances required to accommodate the connection of ground air conditioning hose couplings. Two types of service connections are included. The Type A connection is a slotted ring with integral locking pads and is comparable to the MS33562 connection. The Type B connection is a flanged tube with external locking lugs. The Type B connection has the same interface dimensional requirements as the Type A connection. The purpose of this document is to establish uniform interface configurations on commercial transport aircraft for the ground air conditioning (conditioned air) service connection. Consideration is also given to the durability, maintainability, and repairability of the connection.

Aircraft Ground Air Conditioning Service Connection

BS M 90:1997 飞机地面支持设备 适用于大容量飞机的自走式乘客楼梯 功能要求

1 This International Standard specifies the func-tional, performance and safety requirements for self-propelled passenger boarding stairs intended for access to the cabin of all aircraft types commonly in service in international civil air transport with a cabin door sill height equal to or exceeding 2,54 m (100 in) over the ground. 2 The intent of this International Standard is not to specity equipment design, but rather to define minimum functional and performance requirements and highlight those criteria which are recognized as essential in the environment of international airports by aircraft and vehicle manufacturers as well as air-lines and handling agencies. 3 This International Standard shall be applied with due reference to national governmental regulations of the country where the vehicle is to be operated. The main though not exclusive areas in which such national regulations may apply are: — regulations concerning equipment for use by the public; — stability and other safety requirements applicable to elevating equipment.

Aircraft ground support equipment. Self-propelled passenger stairs for large capacity aircraft. Functional requirements

MH 6005-1996 飞机加油安全规范

本标准规定了飞机加油对加油设备和油品质量控制的要求以及与飞机加油作业有关人员的安全操作方法与行为准则。 本标准适用于适用石油液体燃料的各类飞机在地面加(放)燃油的操作和飞机在维修过程中的加油和放油。 本标准不适用于飞机空中加油、水陆两用飞机的水上加油、飞机燃料系统制造过程飞机燃料箱的加油和放油。

General rules for safety of aircraft fuelling

ISO 1825:1996 飞机地面加油和放油用橡胶软管和软管组件 规范

Gives requirements for six types of hose and hose assembly for use in all operations associated with the ground fuelling and defuelling of aircraft. Replaces the first edition.

Rubber hoses and hose assemblies for aircraft ground fuelling and defuelling - Specification

HB 7456-1996 Ⅱ型飞机地面系留链条组件

Type II Aircraft Ground Tethering Chain Assemblies

HB 7457-1996 飞机地面系留链条组件通用规范

本标准规定了飞机地面系留链条组件技术要求、试验方法、检验规则和标志、包装要求。 　　本标准适用于HB　7455、HB　7456飞机地面系留链条组件（以下简称系留链条组件），其它系留组件亦可参照使用。

General specification for aircraft ground tethering chain assemblies

HB 7455-1996 Ｉ型飞机地面系留链条组件

Type I Aircraft Ground Tethering Chain Assemblies

HB/Z 285-1996 机载故障诊断分系统方案设计的优化程序

本标准规定了机载故障诊断分系统方案设计的程序与方法。 　　本标准适用于机载故障诊断分系统的研制阶段。

An Optimal Program for Scheme Design of Airborne Fault Diagnosis Subsystem

GOST ISO 4116-1996 航空货运设备.与飞机集装单元装置兼容的地面设备要求

Стандарт распространяется на аэродромные и складские перегрузочные и транспортные средства и устанавливает требования к их транспортер

Air cargo equipment. Ground equipment requirements for compatibility with aircraft unit load devices