共找到 1494 条与 机上设备和仪器 相关的标准,共 100 页
Aerospace series - Connectors, optical, circular, single and multipin, coupled by threaded ring, self-locking 1,25 mm diameter ferrule with removable alignment sleeve holder - Part 003: Square flange receptacle - Product standard; German and English versi
Aerospace series - Connectors, optical, circular, single and multipin, coupled by threaded ring, self-locking 1,25 mm diameter ferrule with removable alignment sleeve holder - Part 001: Technical specification; German and English version EN 4645-001:2010
Aerospace series - Connectors, optical, circular, single and multipin, coupled by threaded ring, self-locking 1,25 mm diameter ferrule with removable alignment sleeve holder - Part 002: Specification of performance and contact arrangements; German and Eng
This specification covers all aspects from the selection through installation of wiring and wiring devices and optical cabling and termination devices used in aerospace vehicles. Aerospace vehicles include manned and unmanned airplanes, helicopters, lighter-than- air vehicles, missiles and external pods.
Wiring Aerospace Vehicle
本标准规定了安装在运输类飞机厨房和其他区域的手推车、物品箱及相关组件的最低设计和性能要求,以及供储存舱设计人员和设备安装人员使用的安装要求。 本标准适用于但不限于下列安装在运输类飞机厨房和其他区域的设备: a) 全长车和半长车(主要用于装载饮料、物品箱、食物、商品和垃圾); b) 折叠车; c) 物品箱(便携箱、标准箱和餐箱); d) 储存在手推车和(或)厨房储存舱里的非固定相关组件,如抽屉、托盘、垃圾箱衬里或其他类似组件。 本标准没有完全涵盖以下内容: a) 具有自备的机械制冷系统、电动机、其他电器部件或通过加压系统分配饮料的手推车或物品箱。 b) 延长使用寿命和持续适航的设计细则,因为这些细则可能随以下因素变化: 1) 厨房和食品(饮料)系统总体设计; 2) 营运人希望的人因工程; 3) 手推车或物品箱的使用方法和注意事项; 4) 手推车或物品箱的维护方法; c) 民用航空规章、相关公众健康规章和(或)设计细则的相关要求,该要求涵盖在客舱服务人员或飞机制造商对主要设备的规范中。
Minimum design and performance of airplane galley in-flight carts,containers,and associated components
Aerospace series - Connectors, optical, circular, single and multipin, coupled by threaded ring, self-locking 1,25 mm diameter ferrule with removable alignment sleeve holder - Part 001: Technical specification
本标准规定了民用航空空中交通管制语音通信交换系统(以下简称空管语音通信交换系统)的组成、功能、性能、技术指标和工作环境要求。 本标准适用于民用航空空中交通管理部门空管语音通信交换系统的规划、设计、建立和检验。
Civil aviation air traffic control voice communication switch system technical specification
This ARP covers the basic criteria for the design of cabin pressure control systems (CPCS) for general aviation, commercial and military pressurized aircraft.
Aircraft Cabin Pressurization Control Criteria
Errata to IEEE Specification Format for Single- Degree-of-Freedom Spring-Restrained Rate Gyros
Errata to Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros
Specification format guide and test procedure for single-degree-of-freedom rate-integrating gyros; Errata
Errata to Supplement for Strapdown Applications to IEEE Standard Specification Format Guide and Test Procedures for Single- Degree-of-Freedom Rate-Intergrating Gyros
Errata to Supplement for Strapdown Applications to IEEE Standard Specification Format Guide and Test Procedures for Single-Degree-of-Freedom Rate-Intergrating Gyros
Aerospace series - Fibres and cables, optical, aircraft use - Test methods - Part 506 : impact resistance.
This standard specifies the general characteristics, the conditions for qualification, acceptance and quality assurance, as well as the test programs and groups for threaded ring coupling circular fibre optic self-locking connectors, fire-resistant or non fire-resistant, intended for use in a temperature range from − 65 °C to 150 °C continuous.
Aerospace series - Connectors, optical, circular, single and multipin, coupled by threaded ring, self-locking 1,25 mm diameter ferrule with removable alignment sleeve holder - Technical specification
This European Standard defines the performance and contact arrangements of circular optical connectors, coupled by triple start threaded ring.
Aerospace series - Connectors, optical, circular, single and multipin, coupled by threaded ring, self-locking 1,25 mm diameter ferrule with removable alignment sleeve holder - Specification of performance and contact arrangements
Aerospace series. Connectors, optical, circular, single and multipin, coupled by threaded ring, self-locking 1,25 mm diameter ferrule with removable alignment sleeve holder. Specification of performance and contact arrangements
Aerospace series - Connectors, optical, rectangular, multicontact, rack and panel, Quadrax cavity, 2, 5 mm diameter ferrule - Operating temperatures -65 ℃ to 125 ℃ (cable dependent) - Flush contacts - Part 202: Optical contact assembly for 900 μm buffered fibre receptacle - Product standard; German and English version EN 4626-202:2009
Aerospace series - Connectors, optical, rectangular, multicontact, rack and panel, Quadrax cavity, 2,5 mm diameter ferrule - Operating temperatures -65 °C to 125 °C (cable dependent) - Flush contacts - Part 202: Optical contact assembly for 900 Šm buffere
This document provides an overview of currently available and need to be developed modeling and simulation capabilities required for implementing robust and reliable Aerospace WDM LAN applications. The purpose of this document is to provide relevant information on modeling and simulation capabilities to architects and designers of WDM LAN standards and systems. The document is intended to be utilized in conjunction with existing SAE standards documents, SAE AIR 6004 "Optical Networking Glossary Terminology" and SAE AIR 6005 "General Requirements for Wavelength Division Multiplexed (WDM) Backbone Networks".
Modeling and Simulation Capabilities for Aerospace WDM LAN Applications
This document (AIR6005) provides the framework for the specifications of a WDM OBN within the SAE AS5659 WDM LAN Specification document family, in particular, the Transparent Optical Backbone Network Specification. This framework includes potential requirements, technical background, investigation and context to support the writing of SAE's WDM LAN specifications documents. The SAE's AS6005 WDM OBN document describes a transparent optical network which contains optical components and optical interfaces to perform optical transport, optical add/drop, optical amplification, optical routing, and optical switching functions. The conforming optical signal interfaces for the data plane of the WDM OBN are defined. The conforming signal interfaces for the control and management planes of this network are also defined. The control and management plane signals may be either electrical or optical. If successful, a WDM LAN standard is anticipated to include multiple variants that may get created either as separate documents (e.g. a multimode and single-mode specification) and additional documents may be needed to specify the components from which a WDM LAN and OBN will be built. The WDM OBN specification is to be established in a future document, SAE AS5659. This AIR document is a requirements document that provides input regarding the WDM OBN to the AS5659 Aerospace Standard. Additional documents are anticipated to specify aggregation of access for multiple systems that interface to the OBN. The transition from electrical communications links to optically multiplexed networks, is anticipated to involve aggregation of slower speed signals as necessary part of a cost effective transition.
General Requirements for WDM Backbone Networks
Aerospace series - Cables, optical, 125 Šm diameter cladding - Part 001 : technical specification.
This standard specifies a method to determine the ability of an optical fibre or cable to withstand impact under specified environmental conditions.
Aerospace series - Fibres and cables, optical, aircraft use - Test methods - Part 506: Impact resistance; German and English version EN 3745-506:2009
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