V35 航空器及其附件综合 标准查询与下载

ARINC 752-1 ITEM 7.0-1995 内嵌测试设备

Built-In Test Equipment

Built-In Test Equipment

HB 7045-1994 民用飞机客舱内部装饰设计要求

本标准规定了民用飞机客舱内部装饰设计要求。 　　本标准适用于民用飞机客舱和服务舱内部装饰设计或改进设计。

Design Requirements for Civil Aircraft Cabin Interior Decoration

HB/Z 255-1994 球面浮动元件的设计与计算

本标准规定了球面浮动压块及支承头的设计计算方法。 　　本标准适用于夹具元件中的球面浮动结构的设计与计算。

Design and Calculation of Spherical Floating Element

DLA MIL-F-25173 A NOTICE 1-1994 航空器装置控制面板扣件

The General Services Administration has authorized the use of this commercial item description as a replacement for Military Specifications MIL-V-16720E and MIL-V-16721D which are cancelled.

FASTENER, CONTROL PANEL, AIRCRAFT EQUIPMENT

HB/Z 223.5-1993 飞机装配工艺涂敷密封剂的密封铆接

本标准规定了涂敷密封剂的密封铆接的工艺过程、技术要求、工艺方法及故障排除方法；同时，还规定了缝内密封所需用的常用密封剂种类和涂敷方法。 　　本标准适用于气密舱和整体油箱等密封结构的普通铆钉密封铆接。

Sealant riveting with sealant applied in aircraft assembly process

HB 6750-1993 机载武器火力控制系统校正与校靶通用要求

本标准规定了机载武器火力控制系统（以下简称机载武器火控系统）校正与校靶的程序、方法和要求。 　　本标准适用于各类机载武器火控系统的设计、制造和使用维护。

General requirements for calibration and target calibration of airborne weapon fire control system

HB/Z 249-1993 飞机装配工艺装备制造与安装要求

本标准规定了飞机装配工艺装备和标准工艺的制造与安装技术要求。 　　本标准适用于飞机装配工艺装备和标准工艺装备的制造与安装。

Requirements for the manufacture and installation of aircraft assembly process equipment

HB 6753-1993 机载武器火力控制系统误差分析通用要求

本标准规定了机载武器火力控制系统（简称机载武器火控系统）误差分析的内容和方法。 　　本标准适用于各种类型飞机与直升机的机载武器火控系统。作为机载武器火控系统的设计、地面试验和空中试验的误差分析依据。

General requirements for error analysis of airborne weapon fire control system

HB 6763-1993 攻角和侧滑角系统的安装

本标准规定了飞机攻角和侧滑角系统安装的一般要求。 　　本标准适用于飞机攻角和侧滑角系统的安装设计及验收。

Angle of attack and angle of sideslip system installation

HB 6774-1993 机载设备座舱控制板通用规范

本规范规定了两种类型机载设备座舱控制板的技术要求、试验方法和检验规则。 　　本规范主要适用于安装在军用飞机座舱内机载设备的控制板。民用飞机座舱设备控制板也可参照采用。

General specification for cockpit control panel of airborne equipment

HB 6892-1993 航空飞行器零部件的互换性和替换性

本标准规定了航空飞行器的零件、部件、组件、单元体、装置和机载设备尺寸上的互换性和替换性要求。 　　本标准适用于军用航空飞行器的研制（含改进、改型）和批生产，民用航空飞行器亦可参照使用。

Interchangeability and replaceability of aircraft parts and components

HB 6893-1993 航空飞行器雷电防护

Aviation aircraft lightning protection

AECMA PREN 3060-1994 航空航天系列飞机机架滚动轴承　镀镉钢法兰定位盖的固定单列滚珠轴承　尺寸和负荷

This "Aerospace Series" Prestandard has been drawn up under the responsibility of AECMA (Association Européenne des Constructeurs de Matériel Aérospatial). It is published on green paper for the needs of AECMA-Members. It has been technically approved by the experts of the concerned Technical Committee following comment by the Member countries.

Aerospace Series Bearings, Airframe Rolling Rigid Single Row Ball Bearings in Steel, Cadmium Plated, with Flanged Alignment Bush, Cadmium Plated Dimensions and Loads

AECMA PREN 3059-1994 航空航天系列飞机机架滚动轴承　镀镉钢法兰定位盖的固定单列滚珠轴承　尺寸和负荷

This "Aerospace Series" Prestandard has been drawn up under the responsibility of AECMA (Association Européenne des Constructeurs de Matériel Aérospatial). It is published on green paper for the needs of AECMA-Members. It has been technically approved by the experts of the concerned Technical Committee following comment by the Member countries.

Aerospace Series Bearings, Airframe Rolling Rigid Single Row Ball Bearings in Steel, with Flanged Alignment Bush, Cadmium Plated Dimensions and Loads Edition P 1

DLA MS14311 REV B-1994 250级(90度弯头T字形十字形45度耦合)线程铜管或青铜管配件

Provided by IHSNot for ResaleNo reproduction or networking permitted without license from HIS

FITTINGS, PIPE, BRASS OR BRONZE, THREADED (90-DEG. ELBOWS, TEES, CROSSES, 45-DEG. ELBOWS, AND COUPLING), CLASS 250

DLA MS14306 REV B-1994 125级(45度Y型支部封闭和开口返回弯角减速器)线程铜管或青铜管配件

Provided by IHSNot for ResaleNo reproduction or networking permitted without license from HIS

FITTINGS, PIPE, BRASS OR BRONZE, THREADED (REDUCERS, CLOSE AND OPEN RETURN BENDS, AND 45-DEG. Y-BRANCHES), CLASS 125

DLA MS14305 REV B-1994 125级(T行十字行45度弯头偶合器)线程铜管或青铜管配件

MATERIAL1 Brass or bronze in accordance with ASME B16.15. PROTECTIVE COA TINGI None,DIHENSIONSi In accordance w i t h ASME 816.15, Table 3 (Table A3>.

FITTINGS, PIPE, BRASS OR BRONZE, THREADED (TEES, CROSSES, 45-DEG. ELBOWS, AND COUPLINGS), CLASS 125

SAE AIR1780A-1994 飞机浮力分析

This document is divided into five parts. The first part deals with flotation analysis features and definitions to acquaint the engineer with elements common to the various methods and the meanings of the terms used. The second part identifies and describes the various methods used. To accomplish the minimum intent of this document, techniques could be limited to those needed for flotation analysis only; however, because of the close relation between flotation analysis and runway design, methods for the latter are also included. In fact, runway design criteria are used for flotation and evaluation in some cases, and are periodically the governing procedure in specific, if isolated, instances. From time to time, it may be necessary to deal with runways built to obsolete criteria. Therefore, a listing of most of these constitutes the third part. The fourth part of this document tabulates the recommended documents, categorizing them for commercial and civil versus military usage, by military service to be satisfied, and by type of pavement. The document concludes with brief elaborations of some concepts for broadening the analysts understanding of the subject

Aircraft Flotation Analysis

ISO 9939:1994 航空航天 滑油的压力加油接头(新型)

Specifies the basic dimensions of a pressure re-oiling connection for use with all oils for aircraft engines, and the clearance envelope to be provided.

Aerospace; pressure re-oiling connection (new type)

ISO 8668-4:1993 航空器 登机桥连接系统 第4部分:2型系统的详细规范

Specifies the particular characteristics of a TJS designated as type 2 and intended for use at temperatures from - 55 鳦 to + 155 鳦. The junction system comprises feedback modules in four sizes; feedthrough modules in four sizes; frames adapted to these modules: monolithic frame and double frame for feedback modules and double frame for feedthrough modules; spacers; removable male crimp contacts of sizes 22, 20, 16 and 12; sealing plugs.

Aircraft; terminal junction systems; part 4: detail specification for type 2 system