V38 液压、冷气系统及其附件 标准查询与下载

HB 5825-1996 航空液压过滤器通用技术条件

本标准规定了航空液压过滤器（以下简称过滤器）的一般技术要求、试验方法和检验方法和检验规则。 　　本标准适用于飞机Ⅰ、Ⅱ型液压系统使用的过滤器及滤芯的新品研制。对具体型别产品必须制订专用技术条件，本技术条件是专用技术条件的基础，专用技术条件是本技术条件的明确和补充。

General Technical Specifications for Aviation Hydraulic Filters

HB 7299-1996 飞机电动定量液压泵通用规范

本规范规定了在飞机液压系统中，由电动机驱动的定排量液压泵（以下简称“电动泵”）的基本技术要求、试验方法和检验规则。 　　本规范适用于在飞机Ⅰ型液压系统中工作的电动泵的研制及其批生产。

General specification for aircraft electric displacement hydraulic pumps

HB 7471-1996 民用飞机液压系统设计和安装要求

本标准规定了民用飞机Ⅰ型和Ⅱ型液压系统的设计和安装要求。 　　适用于民用飞机液压系统的研制及批生产。

Design and installation requirements of civil aircraft hydraulic system

HB 7504.10-1997 飞行模拟器设计和性能的数据要求 液压系统

本标准规定了飞行模拟器液压系统的数据要求。 　　本标准适用于民用飞机飞行模拟器，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须的数据范围和内容。 　　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 hydraulic systems

HB 7300-1996 飞机用液压马达驱动空气压缩机组通用规范

本规范规定了在飞机气动系统中，由液压马达驱动的空气压缩机组（以下简称“压缩机组”）的基本技术要求、试验方法和检验规则。 　　本规范适用于在飞机气动系统中工作的液压马达驱动空气压缩机组的研制及其批生产。不适用于电动机驱动的空气压缩机组、飞机发动机传动机匣驱动的空气压缩机组等。

General specification for hydraulic motor driven air compressor units for aircraft

AIR FORCE MIL-H-8890 NOTICE 1-1996 III型(负65华氏度到450华氏度)液压部件的一般规范

This notice should be filed in fiont of MIL-H-8890, dated O1 November 1961.

HYDRAULIC COMPONENTS, TYPE III, (-65 DEG. TO +450 DEG. F), GENERAL SPECIFICATION FOR

SAE AIR4922-1996 主飞行控制液压驱动系统接口定义

This SAE Aerospace Information Report (AIR) provides a description of the interfacesand their requirements for generic and specific hydraulic actuation systems used in the flight control systems of manned aircraft. Included are the basic control system characteristics and functional requirements, and the essential interfaces (structural, mechanical, hydraulic power, control input, status monitoring, and environment). Major design issues, requirements, and other considerations are presented and discussed. The primary purpose of this document is to describe the interfaces to aid in the development of Interface Control Documents (ICDs) for primary flight control servoactuation systems in future applications. Due to the variety of applications, the number of, and type of, ICDs required for a particular application is left up to the user of this document. The lessons learned from previously developed production aircraft are discussed.

Primary Flight Control Hydraulic Actuation System Interface Definition

AIR FORCE MIL-P-26191 B NOTICE 1-1995 AF/M27M-1 和 AF/M27M-2液压抽油机

This notice should be filed in fiont of MIL-P-26191B(USAF) dated 29 October 1970.

PUMPING UNIT, HYDRAULIC AF/M27M-1 AND AF/M27M-2

HB 7117-1994 民用飞机液压系统通用规范

本规范规定了民用飞机液压系统的研制要求和验证方法。 　　本规范适用于民用飞机液压系统。

General specification for civil aircraft hydraulic system

HB 5802-1994 航空液压舵机通用规范

本规范规定了航空液压舵机的性能、设计和质量保证的通用要求。 　　本规范适用于航空液压舵机的研制、试生产和批生产。 　　本规范是使用、研制、生产各单位共同遵守的准则。是制定各型航空液压舵机专用规范的指导性技术文件。如果本规范与其它有关规范有矛盾时，应优先采用本规范。本规范与专用规范有矛盾时，应以专用规范为准。

General specification for aviation hydraulic steering gear

ISO 3174:1994 航空器 用地面设备检查液压系统的连接接头 螺纹式

Cancels and replaces the first edition (1981). Specifies the requirements for connections installed in aircraft hydraulic system pressure and suction lines, intended for checking the systems by means of ground appliances.

Aircraft - Connections for checking hydraulic systems by ground appliances - Threaded type

JIS W 3102:1994 航空用气动系统部件一般规范

この規格は，MIL-P-5518に基づく航空機空気圧系統に用いる空気圧構成部品の一般的要求事項について規定する。

Pneumatic system components, aeronautical, general specification for

HB 6779-1993 航空液压过滤器设计指南

本标准规定了航空液压过滤器设计的一般要求与方法。 　　本标准适用于航空液压过滤器的设计，其他液体过滤器、民用过滤器的设计亦可参照使用。

Aviation Hydraulic Filter Design Guide

HB 6755-1993 飞机液压管路系统设计、安装要求

Aircraft hydraulic piping system design and installation requirements

SAE AIR1083B-1994 军用飞机的机载液压和控制系统的生存能力

This SAE Aerospace Information Report (AIR) provides the hydraulic system designer with the various design options and techniques currently available to enhance the survivability of hydraulic systems. A comprehensive knowledge of the hostile environment to which the air vehicle will be exposed will form the basis upon which the overall design philosophy is formulated. The designer should strive to achieve at the absolute minimum acceptable flying quality level to complete the operational mission for which the aircraft is designed; i.e., the aircraft can be controlled and the mission terminated safely, including landing. This AIR will attempt to address the following threats: a. typical small arms fire (5,56, 7.62, 12.7 and 14.5 mm AP); b. cannon (20, 30, and 40 mm API/HEI); c. NBC/EMI/EMP/beamed particle; and d. chemical/biological. Protection against missiles is beyond the scope of this AIR. Except for electronic counter-measures or evasive maneuvers, no practice technology exists which allows a hydraulic system to survive a direct hit by a missile or large caliber anti-aircraft projectile. The AIR addresses the following major topics: a. design concepts and architecture; b. design implementation; c. subsystem mechanization; and d. component design. This document provides the fluid power design engineer with information and design considerations to enhance the airborne hydraulic and control system survivability under combat conditions.

Airborne Hydraulic and Control System Survivability for Military Aircraft

HB 6754-1993 飞机液压系统通用规范

本规范规定了飞机液压系统的研制要求和验证方法。 　　本规范适用于军用飞机液压系统。

General specification for aircraft hydraulic systems

SAE AIR4725-1994 气动启动系统使用的高压气体容器长期存放的可靠性

This SAE Aerospace Information Report (AIR) provides design data reliability information relative to the long-term storage of gas containers or pressure vessels charged with nitrogen or helium at pressures ranging from 6000 to 12 000 psi. The gas containers are cylindrical, spherical, or toroidal in shape. Internal volumes range up to 1385 in3. Applications for this type cold gas actuation system include tactical missiles, guided projectiles, and smart bombs. A typical system is described.

Long-Term Storage Reliability of High Pressure Gas Containers for Pneumatic Actuation Systems

JIS W 1831:1994 航空航天.流体系统用带螺纹的和密封的联结件.尺寸

この規格は，航空宇宙産業において用いる継手部のポート接続部におけるシール方式について規定する。

Aerospace -- Couplings, threaded and sealed, for fluid systems -- Dimensions

JIS W 1841:1994 航空航天.气动、压力补偿式变量传送泵.一般要求

この規格は，航空機の油圧系統で使用するのに適した圧力補償式可変容量形油圧ポンプに対すろ一般的要求事項について規定する。

Aerospace -- Hydraulic, pressure compensated, variable delivery pumps -- General requirements

ISO 11217:1993 航空航天 液压系统液体污染物 取样点位置和取样准则

Specifies location and criteria for hydraulic system fluid particulate contamination in aeroplanes, helicopters and space vehicles, and provides indirectly related references. Requirements are specified in SAE ARP 4268 which is adopted as a de facto ISO international Standard. For the purposes of international standardization, the outlined modification shall apply to clause 2 of AS4059A.

Aerospace; hydraulic system fluid contamination; location of sampling points and citeria for sampling