V37 操纵系统及其附件 标准查询与下载

NAVY QPL-16383-27-2005 CO2可充气的水下摧毁系统救生用具

This list has been prepared for use by or for the Government in the acquisition of products covered by the subject specification and such listing of a product is not intended to and does not connote endorsement of the product by he Department of Defense. All products listed herein have been qualified under the requirements for the product as specified in the latest effective issue of the applicable specification. This list is subject to change without notice; revision or amendment of this list will be issued as necessary. The listing of a product does not release the contractor from compliance with the specification requirements.

LIFE PRESERVER, CO2 INFLATABLE, UNDERWATER DEMOLITION TEAM

NF L90-336:2004 空间工程.机械的.第6部分:烟火制造术

Space engineering - Mechanical - Part 6 : pyrotechnics.

NF L90-337:2004 空间工程.机械的.第7部分:机械部件

Space engineering - Mechanical - Part 7 : mechanical parts.

NAVY MIL-PRF-32098 A-2004 每分10加仑油性废物隔膜(OWMS-10)超滤系统

This specification covers a fully automated, electrically operated, self-contained oily waste membrane system (OWMS) capable of providing secondary treatment of the effluent (see 6.7.4) from 10-gallon per minute (gpm) oil/water separators (OWS) in Naval shipboard installations.

ULTRAFILTRATION SYSTEM, 10-GALLON PER MINUTE OILY WASTE MEMBRANE (OWMS-10)

NAVY MIL-PRF-32168-2004 同步感应电动机的变速传动系统

This specification covers an electronic variable speed drive (VSD) system (see 6.3.12) used to control 3-phase alternating current induction and synchronous machines.

VARIABLE SPEED DRIVE SYSTEM FOR INDUCTION AND SYNCHRONOUS MACHINES

DOD MIL-STD-2401 ADMIN NOTICE 1-2004 国防部世界测地系统(WGS)

The purpose of this notice is to inform users of the change in name of the preparing activity from the Defense and Mapping Agency (DMA) to the National Geospatial-Intelligence Agency (NGA).

DEPARTMENT OF DEFENSE WORLD GEODETIC SYSTEM (WGS)

NAVY MIL-PRF-23236 C-2003 船舶结构的油漆系统

This specification covers five types of air pollution regulated ship and structure coatings that comply with the National Emission Standards for Hazardous Air Pollutants (NESHAP) for shipbuilding for state and federal regulations (except Type VIII and VIIIA). There are 17 classes of coating systems. There are four grades of coating systems based on temperature of application and cure.

COATING SYSTEMS FOR SHIP STRUCTURES

NAVY MIL-PRF-32007-2003 每分6.7加仑海军综合隔膜系统(NIMS)油废物分离系统

This specification covers a fully automated and self-contained Navy Integrated Membrane System (NIMS) capable of providing treatment of oily wastewater found onboard Naval vessels at a rate of 6.7 gallons per minute (gpm).

OILY WASTEWATER SEPARATION SYSTEM, 6.7-GALLON PER MINUTE NAVY INTEGRATED MEMBRANE SYSTEM (NIMS)

ARINC 735A-1 ITEM 3.0-2003 TCAS功能描述

TCAS Functional Description

TCAS Functional Description

ASTM F2295-03 轻型运动飞机的连续操作安全监控的标准实施规程

1.1 This document establishes the standard practice for the continued operational safety monitoring of a light sport airplane.1.2 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.

Standard Practice for Continued Operational Safety Monitoring of a Light Sport Airplane

SAE AS1614C-2003 主线飞机牵引杆附属零件界面

This SAE AErospace Standard (AS) specifies the interface requirements for tow bar attachment fittings on the nose gear (when towing operations are performed from the nose gear) of conventional tricycle type landing gears and of commercial civil transport aircraft with a maximum ramp weight higher than 50 000 kg (110 000 lb), commonly designated as main line aircraft. Its purpose is to achieve tow bar attachment fittings interface standardization by aircraft weight category (which determines tow bar forces) in order to ensure that one single type of tow bar with a standard connection can be used for all aircraft types within or near that weight category, so as to assist operators and airport handling companies in reducing the number of different tow bar types used.

Main Line Aircraft Tow Bar Attach Fitting Interface

HB 7708-2002 飞机滑油系统安装和试验要求

本标准规定了有人驾驶飞机，无人驾驶飞机滑油系统安装和试验的通用要求。 本标准适用于发动机滑油系统的部分功能部件装在飞机上从而构成飞机滑油系统的有人驾驶飞机、 无人驾驶飞机等。

Requirements for oil systems aircarft installattion and test

SAE ARP1281C-2002 (R)液压动力操作式飞机飞行控制装置执行机构的一般规范

This aerospace recommended practice provides a framework and suggested procedures or values for requirements for the design, performance, and test of hydraulically powered servoactuators for use in aircraft flight control systems. The original version of this document was intended for military usage: consequently, the requirements still often reflect such use. However, the basic requirements of this ARP may and should be applicable to commercial usage as well, provided that appropriate considerations are given for the applicable FAR/JAR 25 regulations, hydraulic fluids, and environmental controls. This recommended practice is a guide and surrogate specification for preparing a detail specification for a particular servoactuator application.

(R) Actuators: Aircraft Flight Controls, Power Operated, Hydraulic, General Specification For

ARINC 627-2 ITEM 5.0-2002 利用ARINC 626构造指南

Guidance for Using Selected ARINC 626 Constructs

Guidance for Using Selected ARINC 626 Constructs

ARMY MIL-STD-1477 C VALID NOTICE 1-2002 军用系统演示符号(公制)

MIL-STD-1477C(MI), dated 30 September 1996, has been reviewed and determined to be valid for use in acquisition.

SYMBOLS FOR ARMY SYSTEMS DISPLAYS (METRIC)

SAE AIR4253A-2001 带有遥控自动驾驶仪飞行操纵系统的飞机用传动系统的描述

This information report (AIR) provides design information of various contemporary aircraft fly-by-wire flight control actuation systems that may be useful in the design of future actuation systems for similar applications. This AIR provides a description of representative state-of-the-art, fly-by-wire (FBW) actuation systems used in flight control systems of manned aircraft. It presents the basic characteristics, hardware descriptions, redundancy concepts, functional schematics, and discussions of the servo controls, failure monitoring, and fault tolerance. All existing FBW actuation systems are not described herein; however, those most representing the latest designs are included. While this AIR is intended as a reference source of information for future aircraft actuation system designs, the exclusion or omission of any other appropriate actuation system or subsystem should not limit consideration of their use on future aircraft.

Description of Actuation Systems for Aircraft with Fly-By-Wire Flight Control Systems

ARMY MIL-HDBK-765 NOTICE 2-2001 用于安全设计的多相电力系统指导方针

This notice should be filed in front of MIL-HDBK-765(MI), dated 14 July 1988.

GUIDELINES FOR SAFE DESIGN OF POLYPHASE ELECTRICAL SYSTEMS

ARINC 622-4 ITEM 1.0-2001 ACARS之上的ATS数据传输器程序

ATS Data Link Processes over ACARS

ATS Data Link Processes over ACARS

ARINC 429 DISKETTE-2001 微软Word和Excel形式数据记录单电子磁盘

Electronic Diskette Copy of Data Labels in Microsoft Word and Excel Formats ***To Purchase: Contact IHS at 1-800-854-7179 USA/Canada or 303-397-7956 Worldwide***

Electronic Diskette Copy of Data Labels in Microsoft Word and Excel Formats

ISO 9763:1999 航空航天 航空器操纵钢丝绳组件 技术规范

This International Standard specifies the characteristics, inspections and test methods as well as the quality assurance requirements for aircraft control wire rope assemblies equipped with swaged end fittings. This International Standard is applicable to control wire rope assemblies as defined in ISO 9762.

Aerospace - Aircraft control wire rope assemblies - Technical specification