V41 导航通讯系统与设备 标准查询与下载

HB 6124-1987 机载75兆赫指点信标设备无线分系统规范

本规范对用于机载７５兆赫指点信标设备的天线分系统规定了设计、性能及试飞的一般要求。

Airborne 75 MHz Pointer Beacon Equipment Wireless Subsystem Specification

SAE AS8044-1987 飞机的起飞性能监控(TOPM)系统的最低性能标准

This Aerospace Standard (AS), establishes minimum performance standards for those sensors, computers, transponders, and airplane flight deck controls/displays which together comprise a Takeoff Performance Monitor (TOPM) System. This standard also defines functional capabilities, design requirements, and test procedures. A TOPM system is intended to monitor the progress of the takeoff and to provide advisory information which the crew may use in conjunction with other available cues to decide to continue or abort the takeoff. See Appendix A for supplementary information relating to NTSB, CAA, and ad hoc committee concerns and background information.

Takeoff Performance Monitor (TOPM) System, Airplane, Minimum Performance Standard for

ISO 8668-1:1986 航空器 登机桥连接系统 第1部分:特性

Specifies the general operating characteristics and standardization principles. Does not define a specific pattern for the connection system from the point of view of dimensions, but lays down limits for the design and performance for each system. This part lays down the basic requirements for the mechanical structure and electrical performances as well as the basic environmental conditions in service.

Aircraft; Terminal junction systems; Part 1 : Characteristics

HB 6088-1986 机载无线通用技术条件

本标准规定了机载天线的一般技术要求。 　　本标准主要供航空工业部所属有关各厂、所、机构使用。

Airborne Wireless General Specifications

NF L72-122:1986 飞机设备.电传动式转速表指示器

Aircraft equipment. Indicator for electrical transmission tachometer.

NF L72-110:1986 飞机设备.圆刻度盘机载仪表.机械传动式转速表

Aircraft equipment. On board instrument with round dials, mechanical transmission tachometer.

NF L72-310:1986 飞机设备.圆刻度盘机载压力表

Aircraft equipment. On board pressure indicator with round dials.

SAE AS8014-1986 失速警告设备的最低性能要求

This aerospace standard establishes the minimum performance requirements for Stall Warning Equipment. This aerospace standard covers two basic Stall Warning Systems; one measures air flow and pressure distribution on the airfoil and the other measures the angle of airflow with respect to an arbitrary reference line. Each type of system includes, as a minimum, a sensor and the means for activating a device which warns the pilot of an impending stall.

Minimum Performance Standard Stall Warning Equipment

HB/Z 96-1985 机载天线分系统设计和布置准则

本标准规定了飞机上使用的所有天线分系统的设计和布置通用准则，采用本标准中各种技术、工艺、材料及方法，可使飞机天线分系统设计和布置获得改善。本标准供飞机及机载天线分系统的设计、制造单位使用。

Airborne Antenna Subsystem Design and Arrangement Guidelines

SAE AS8008-1984 飞行管理设备

This Standard specifies the minimum Standards for Flight Director Equipments under standard and environmental conditions. This Aerospace Standard covers Flight Director Equipments which display to the pilot a computed command for the operation of an aircraft in accordance with selected Mode(s). The term Equipment may include controls, displays, computers, etc. and may include sensors if furnished as a part of the Flight Director.

Flight Director Equipment

NAVY MIL-STD-789 C-1983 增资部分承办技术信息编码

Contractor Technical Information Coding of Replenishment Parts. MIL -STO-789C 1, This Military Standard i s approved for use by all Departments and Beneficial comments (recommendations, additions, deletions) and any Commanding Officer, Naval A i r Engineering Center, Engineering Agencies of the Department of Defense. 2. pertinent data which may be of use i n improving This document should be addressed to: Specifications and standards Department (ESSD) Code 93, Lakehurst, New Jersey 08733 hy using the self-addressed Standardization Document Improvement Proposal (DD Form 1426) appearing at the end o f This document or by l e t t e r .

CONTRACTOR TECHNICAL INFORMATION CODING OF REPLENISHMENT PARTS

ANSI/IEEE 529:1980 单自由度速率积分陀螺规范格式指南和试验程序

Defines the requirements for a single-degree-of-freedom rate-integrating gyro to be used as a strapdown sensor for an [inertial navigation system, an attitude reference unit, ] in an aircraft, [missile, ] application.

Supplement for Strapdown Applications to IEEE Standard Specification Format Guide and Test Procedure for Single-Degree-of-Freedom Rate-Integrating Gyros

IEEE 529-1980 单自由度速率积分陀螺仪标准规范格式指南和试验程序用捷联式设备补充件

Defines the requirements for a single-degree-of-freedom rate-integrating gyro to be used as a strapdown sensor for an [inertial navigation system, an attitude reference unit, ] in an aircraft, [missile, ] application.

Supplement of strapdown applications to IEEE standard specification format guide and test procedure for single-degree-of-freedom rate integrating gyros

HB 6-38-1976 带两个纵向接头的搭铁线

Ground wire with two longitudinal connectors

SAE AS8004-1975 转弯倾斜指示仪的最低性能标准

This standard establishes the minimum performance standards for turn and slip instruments for aircraft use.

Minimum Performance Standard for Turn and Slip Instrument

SAE AS8001-1975 航空地平仪用最低性能标准

This Standard covers Bank and Pitch Instruments which measure and display the angular displacement of bank and pitch from a gyroscopic vertical referenece.This reference may be pneumatically or electrically driven and be contained within the instrument display case or located remotely.Unless otherwise specified,whenever the term"Instrument"is used,it is to be understood to be the complete system of gyro component,any auxiliary equipment and display.

Minimum Performance Standard for Bank& Pitch Instruments

ISO 3389:1975 航空器 无线电频率的挠性同轴电缆 尺寸和电气特性

Specifies these quantities for a limited range of cables. Relates to cables in two categories of operational temperature ranges, namely from -40 鳦 to +85 鳦 and from -55 鳦 to +200 鳦. An annex is included to list those cables which were in use prior to the publication of this standard. Furthermore describes the construction and manufacture and the designation.

Aircraft; Radio frequency flexible coaxial cables; Dimensions and electrical characteristics

NF L65-131:1974 标准型柔性装配机壳用机座

Pedestals for standard type flexibly mounted cases.

SAE AS8003-1974 自动压力高度数据传送码生成设备的最低性能标准

This Aerospace Standard establishes the minimum safe performance requirements for 100 foot (30.48 meters), incremental automatic pressure altitude code generating equipment. It is intended that the code generator be operated by a pressure altitude device which may also operate the pressure altitude indicator normally used to maintain flight altitude.

Minimum Performance Standard for Automatic Pressure Altitude Reporting Code Generating Equipment

ANSI/IEEE 517:1974 单自由度速率积分陀螺的规范格式指南和试验程序

Defines the requirements for a single-degree-of-freedom rate-integrating gyro to be used as a sensor in [an attitude control system, a gimbal platform, an angular displacement measuring system, an angular rate measuring system, ]

Single-Degree-of-Freedom Rate-Integrating Gyros, Specification Format Guide and Test Procedure for