V45 航空仪表 标准查询与下载



共找到 902 条与 航空仪表 相关的标准,共 61

Standard Specification Format Guide and Test Procedure for Coriolis Vibratory Gyros - Corrigendum 1: Figure 1 - Gyro Axes and Misalignment Angles

ICS
49.090
CCS
V45
发布
2008
实施

This document provides information regarding ice detector technology, design and operating requirements. The SAE document SAE AS 5498 provides detailed information regarding the requirement, specifications, qualification, and certification of icing detection systems. This document is not meant to repolace SAE AS 5498 but to enhance it by considering unique aspects of sensing technology and in particular those that may not be certificated at the time of this revision. To that end an effort has been made not to duplicate information contained in SAE AS 5498. Icing rate information is included where applicable. The primary application is associated with ice forming on the leading edges of airfoils and inlets while the aircraft is in flight. Information related to detection of ice over cold fuel tanks and icing at low velocity operation is included. The material is primarily applicable to fixed-wing aircraft. Unique requirements for engine inlets and rotorcraft are also provided. The purpose of this document is to provide information regarding various in situ icing sensing technologies and issues a user of these technologies should consider regarding the method of operation, performance, design, verification, and installation of aircraft ice detectors and icing rate indicators. The intent is not to duplicate SAE AS 5498 but to supplement it in areas that may not have been deemed appropriate for such a standards document.

(R) Aircraft Inflight Ice Detectors and Icing Rate Measuring Instruments

ICS
49.045;49.090
CCS
V45
发布
2007-07-01
实施

The purpose of this document is to recommend to the designer the various criteria and to familiarize him with techniques associated with white incandescent lighted aerospace instruments. This SAE Aerospace Recommended Practice (ARP) covers the general requirements and test procedures recommended for use with white incandescent integrally lighted instruments. Its use should provide uniformity of illumination from instrument to instrument and legibility under daylight operation. An appendix is provided to familiarize the designer with some of the techniques used to obtain uniformity of color and illumination in various types of instruments.

(R) Design Criteria for White Incandescent Lighted Aerospace Instruments

ICS
49.090
CCS
V45
发布
2007-03-01
实施

This specification covers fault locating indicators which display the operational status of electrical and electronic equipment.

INDICATORS, FAULT LOCATING, GENERAL SPECIFICATION FOR

ICS
49.090
CCS
V45
发布
2007-02-15
实施

MIL-DTL-6856 was made "Inactive for New Design" with no superseding specification on 24 March 1999.

INDICATOR, PRESSURE, SYNCHRO, 1-1/2 INCH

ICS
49.090
CCS
V45
发布
2007-01-11
实施

This specification covers two types of indicators for measuring combustible gas and oxygen.

INDICATOR, COMBUSTIBLE GAS AND OXYGEN

ICS
49.090
CCS
V45
发布
2007-01-04
实施

Defines the specification and test requirements for a single-axis laser gyro for use as a sensor in attitude control systems, angular displacement measuring systems, or angular rate measuring systems, including the electronics necessary to operate the gyro and to condition the output signals.

Standard Specification Format Guide and Test Procedure for Single-Axis Laser Gyros

ICS
31.260;31.020
CCS
V45
发布
2006-08-08
实施

This SAE Aerospace Standard (AS) will specify what type night vision goggles are required, minimum requirements for compatible crew station lighting, aircraft exterior lighting such as anticollision lights and position/navigation lights that are NVG compatible. Also, this document is intended to set standards for NVG utilization for aircraft so that special-use aircraft such as the Coast Guard, Border Patrol, Air Rescue, Police Department, Medivacs, etc., will be better equipped to chase drug smugglers and catch illegal immigrants, rescue people in distress, reduce high-speed chases through city streets by police, etc. Test programs and pilot operator programs are required. For those people designing or modifying civil aircraft to be NVG compatible, the documnets listed in 2.1.3 are essential.

Night Vision Goggles (NVG) Compatible Lighting for Civil Aircraft

ICS
49.090
CCS
V45
发布
2006-06-01
实施

本规范规定了机载航空电子启动装置的功能、性能、质量保证规定和交货准备等通用要求。 本规范适用于机载航空电子启动装置。

General specification for airborne aviation activation panel

ICS
CCS
V45
发布
2006-05-17
实施
2006-10-01

本标准规定了机载电子设备交联试验的一般程序、内容和要求,作为机载电子设备设计定型试验中实施交联试验的基本依据。 本标准适用于设计定型阶段军用飞机机载电子设备的地面和空中交联试验,其它阶段的机载电子设备交联试验也可参照使用。

Test code for interconnection of airborne electronic equipments

ICS
CCS
V45
发布
2006-05-17
实施
2006-10-01

本规范规定了机载光学成像侦察吊舱的设计、制造、质量保证和交货准备的通用要求。 本规范适用于在固定翼飞机上挂载的光学成像侦察吊舱(以下简称吊舱)。

General specification for airborne optics imaging reconnaissance

ICS
CCS
V45
发布
2006-05-17
实施
2006-10-01

A-A-59462, dated 31 January 2000, has been reviewed and determined to be valid for use in acquisition.

INDICATOR, SIGHT, LIQUID, REFRIGERANT

ICS
49.090
CCS
V45
发布
2006-05-15
实施

1.1 Scope. This specification covers three hermetically sealed clamp-mounted 1-1/2 inch single synchro pressure indicators.

INDICATOR, PRESSURE, SYNCHRO, 1-1/2 INCH

ICS
49.090
CCS
V45
发布
2006-03-16
实施

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 is not intended to and does not connote endorsement of the product by the 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.

INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, MULTIFUNCTION, -70 DEGREES TO +150 DEGREES C 2 INCH SIZE

ICS
49.090
CCS
V45
发布
2006-02-27
实施

本规程适用于民用航空系统飞机维修中应用的PSD60-2R型燃油油量测试仪MOD2(以下简称测试仪)的首次检定、后续检定和使用中检验。

PSD60-2R Fuel Quantity Test Set

ICS
CCS
V45
发布
2006-01-20
实施
2006-05-01

本规程适用于民用航空系统飞机维修中应用的T60系列C8型和C9型钢索张力表(以下简称张力表)的首次检定、后续检定和使用中检验。

T60 Series Cable Tensiometer

ICS
CCS
V45
发布
2006-01-20
实施
2006-05-01

MIL-I-83245A remains inactive for new design, however, the document is valid for use.

INDICATOR SET, OIL PRESSURE A/A24J-17

ICS
49.090
CCS
V45
发布
2006-01-19
实施

MS25331C, dated 27 September 2001, has been reviewed and determined to be valid for use in acquisition.

LIGHT ASSEMBLY, PRESS TO TEST INDICATOR

ICS
49.090
CCS
V45
发布
2006
实施

This specification covers the requirements for one type of hermetically sealed, remote indicating, synchro-style, integrally lighted, oil pressure indicator, designated EGU-2/A.

INDICATOR, PRESSURE EGU-2/A, OIL, 0-100 PSI

ICS
49.090
CCS
V45
发布
2006
实施

MIL-DTL-27190 was made "Inactive for New Design" with no superseding specification on 24 March 1999.

INDICATOR, PRESSURE AGU-3/A, HYDRAULIC, 0-4,000 PSI

ICS
49.090
CCS
V45
发布
2006
实施



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