V41 导航通讯系统与设备 标准查询与下载

HB 7504.14-1997 飞行模拟器设计和性能的数据要求 飞行管理、导航和通信系统

本标准规定了飞行模拟器飞行管理、导航和通信系统的数据要求。 　　本标准适用于民用飞机飞行模器，军用模拟器可参照使用。 　　本标准为飞行模拟器承制方、使用方、飞机设备的订购方和有关管理机构，提供建造和验证符合空勤人员训练要求的、足够逼真的飞行模拟器所必然的数据范围和内容。 　　本标准不是确定飞行模拟器数据要求的唯一方法。

Data requirements for flight simulator design and performance flight management, navigation and communication systems

SJ 20544-1995 仪表着陆系统（ILS）下滑信标通用规范

General specification for instrument landing system(ILS)glide slope facility

SJ 20545-1995 仪表着陆系统（ILS）下滑信标接收机通用规范

General specification for instrument landing system(ILS)glide slope facility erceiver

SJ 20546-1995 仪表着陆系统（ILS）下滑信标接收机通用规范

General specification for instrument landing system(ILS)localizer receiver

SJ 20539-1995 光纤化的飞机内部时分制指令／响应式多路传输数据总线

Fiber optics mechanization of an aircraft internal time division command/response multiplex data bus

SJ 20562-1995 机载无线电导航设备通用规范

General specification for airborne radio navegation equipment

SJ 20547-1995 仪表着陆系统（ILS）航向信标通用规范

General specification for instrument landing system(ILS)localizer

SAE AIR4886-1996(R2001) 实时通信协议(RTCP)的要求报表

The purpose of this document is to establish the requirements for Real-Time Communication Protocols(RTCP). Systems for real-time applications are characterized by the presence of hard deadlineswhere failure to meet a deadline must be considered a system fault.These requirements have been driven predominantly, but not exclusively, by aerospace type militaryplatforms and commercial aircraft, but are generally applicable to any distributed, real-time, controlsystems. These requirements are primarily targeted for the Transport and Network Layers of peer topeer protocols, as referenced in the Open System Interconnect Reference Model (2.2.1 and 2.2.2),developed by the International Standards Organization (ISO). These requirements are intended to complement SAE AS4074 (2.1.1) and AS4075 (2.1.2), and future SAE communications standards.Although information transfer objectives herein concentrate primarily on digital data flow attributes,efforts have been made such as not to preclude sensor/video and voice information transfers. This document provides evaluation criteria for selecting viable alternatives for a real-time communications protocol standard.

Statement on Requirements for Real-Time Communication Protocols (RTCP)

HB 7227-1995 军用机载座舱音频记录器通用要求

本标准规定了军用机载座舱音频记录器的通用要求。 　　本标准适用于军用飞机与直升机上装备的为提供飞行情况和飞行事故调查分析用的带有保护壳体具备防护功能的机载座舱音频记录器。

General requirements for onboard cockpit audio recorder for military use

SAE AS1773-1995 数字式时分制指令/响应型多路数据总线的光纤机械化

This document defines requirements for digital, command/response time division multiplexing (data bus) techniques for fiber optic implementation. The concept of operation and information flow on the multiplex data bus and the functional formats to be employed are also defined. When invoked in a specification or statement of work, these requirements shall apply to the multiplex data bus and associated equipment which is developed either alone or as a portion of a system or subsystem development. The contractor is responsible for invoking all of the applicable requirements of this aerospace standard on any and all subcontractors he may employ.

Fiber Optics Mechanization of a Digital Time Division Command/Response Multiplex Data Bus

SAE AS4764-1995 Mil-Std-1760飞机电台口的验证方法

This document establishes techniques for validating that an aircraft station complies with the interface requirements delineated in MIL-STD-1760. The purpose of this document is to provide methods for validating that an aircrafts store electrical interface complies with the aircraft station interface (ASI) requirements of MIL-STD-1760. This document provides a modular, independent set of methods for each of the requirements in MIL-STD-1760 that applies to aircraft requirements. The methods herein apply to the auxiliary (AUX) interface as well as the primary interface of MIL-STD-1760

Validation Methods for Mil-Std-1760 Aircraft Station Interfaces

SAE ARP4927-1995 将新系统引入驾驶舱的集成规程

This SAE Aerospace Recommended Practice (ARP) provides guidance to achieve the optimum integration of new aircraft systems which have an impact on the cockpit layout or crew operating procedures. This process may also be used for modification of existing cockpits.

Integration Procedures for the Introduction of New Systems to the Cockpit

SAE AS15531-1995 数字时分命令/响应多路传输数据总线

This SAE Aerospace Standard (AS) contains requirements for a digital time division command/response multiplex data bus, for use in systems integration, that is functionally equivalent to MIL-STD-1553B with Notice 2. Even with the use of this document, differences may exist between multiplex data buses in different system applications due to particular application requirements and the options allowed in this document. The system designer must recognize this fact and design the multiplex bus controller (BC) hardware and software to accommodate such differences. These designer selected options must exist to allow the necessary flexibility in the design of specific multiplex systems in order to provide for the control mechanism, architectural redundancy, degradation concept, and traffic patterns peculiar to the specific application requirements.

Digital Time Division Command/Response Multiplex Data Bus

SAE AS4075/1-1995 与高速环网(HSRB)相关的光学实现

This SAE Aerospace Standard (AS) has been prepared by the Ring Implementation Task Group of the SAE AS-2 Committee. It is intended as a companion document to the SAE AS4075 High Speed Ring Bus Standard. While the Standard is intended to provide as complete a description as possible of an HSRB implementation, certain parameters are system-dependent and evolutionary. This document contains those parameters. The text through Table 1 is intended to provide definitions and descriptions applicable to all applications. Table 2 contains specific parameter values for one or more implementations. This table will change as new systems are implemented or new HSRB speed options are defined.

Optical Implementation Relating to the High Speed Ring Bus (HSRB)

ISO 8668-3:1994 航空器 登机桥连接系统 第3部分:I型系统的详细规范

Specifies the particular characteristics of a terminal junction system, designated as type 1 and intended for use at temperatures between -55 鳦 and +155 鳦. The systems covered herein comprise: feedback modules and feedthrough modules in four sizes; frames adapted to these modules; module clamps and inserts; removable identification tags; removable male crimp contacts of sizes 22, 20, 16 and 12; sealing plugs.

Aircraft - Terminal junction systems - Part 3: Detail specification for type 1 system

HB/Z 254-1994 预导向定位轴与预导向定位衬套的设计与计算

Design and calculation of pre-guided positioning shaft and pre-guided positioning bushing

HB 7090-1994 机载导航设备通用规范

本规范规定了机载导航设备的研制和生产的各项技术要求及其验证要求。 　　本标准适用于机载导航设备的订购、研制和生产。

General specification for airborne navigation equipment

SJ 20403-1994 敌我识别海用应答机通用规范

General specification for IFF naval responders

SJ 20432-1994 地面海岸警戒雷达通用规范

General specification for ground-based coast guard radar

SJ 20411-1994 机载奥米加接收设备通用规范

General specification for airborne OMEGA receiving equipment