V45 航空仪表 标准查询与下载

AIR FORCE QPL-9443-12-2002 MJ-2型发动机排气热电偶温度指示器

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 the Department of Defense.

INDICATOR, TEMPERATURE, THERMOCOUPLE, ENGINE EXHAUST, TYPE MJ-2

SAE AS8039A-2002 一般航空飞行记录器最低性能标准

The standards contained herein apply to recording equipment intended primarily for installation in multi-engine, turbine powered aircraft (fixed and rotary wing) for automatically recording flight data parameters and audio information. This standard is not intended for large aircraft operating under Code of Federal Regulations Title 14, Aeronautics & Space, part 121. This Aerospace Standard (AS) specifies minimum performance standards for recording automatically aircraft flight par ammeters and (or) aural communication between flight crew members, aural warning sounds, and communications to and from aircraft necessary for flight operations. It is the intent of this standard to allow for the use of individual Cockpit Voice Recorder (CVR) or Flight Data Recorder (FDR) equipment, or a combination CVR/FDR.

Minimum Performance Standard General Aviation Flight Recorder

SAE AS5391-2002 健康和使用监控系统的加速度计接口规范

Accelerometers are transducers, or sensors, that convert acceleration into an electrical signal which can be used for vibration monitoring and analysis. This document defines interface requirements for accelerometers and associated interfacing electronics for use in a helicopter Health and Usage Monitoring System (HUMS). The purpose is to standardize the accelerometer-to-electronics interface with the intent of increasing interchangeability among HUMS sensors/systems and reducing the cost of HUMS accelerometers. Although this interface was specified with an internally amplified piezoelectric accelerometer in mind, this does not preclude the use of any other sensor technology that meets the requirements given in this specification. These SAE HUMS Interface Specifications include the minimal interface and performance requirements for interoperability with the Rotorcraft Industry Technology Association (RITA) compliant HUMS. Compliance with these Interface Specifications can be referenced in more comprehensive procurement and device specifications.

Health and Usage Monitoring System Accelerometer Interface Specification

SAE AS5393-2002 健康和使用监控系统的叶片跟踪器接口规范

Blade trackers measure: (a) rotor blade height and (b) lead- lag for use in a rotor track and balance (RT&B) function in a health and usage monitoring system (HUMS). HUMS is a generic term for a system used to measure, monitor, process, and store information relating to the functioning and usage of an aircrafts on-board primary systems, including the engine(s).

Health and Usage Monitoring System, Blade Tracker Interface Specification

JJG(民航) 0068-2001 856A1214P03型发动机可调静子叶片位置传感测试仪

856A1214P03 Generator Variable Stator Vane Transmitter Indicator Test Set

DLA MS25331 REV C VALID NOTICE 2-2001 打样试验指示器的灯装置

MS25331C, dated 14 September 2001, has been reviewed and determined to be valid for use in acquistion

LIGHT ASSEMBLY, PRESS TO TEST INDICATOR

DLA MS25331 REV C VALID NOTICE 1-2001 打样试验指示器的灯装置

MIL-DTL-11589/55E, dated 21 January 1999, is hereby reactivated and may be used for either new or existing design acquisition.

LIGHT ASSEMBLY, PRESS TO TEST INDICATOR

SAE ARP794A-2001 气流偏差指示仪(ADI)

This Aerospace Recommended Practice recommends the industry standards for an Airstream Deviation Instrument primarily for use with turbine-powered, subsonic transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Paragraph 3.4. This recommended practice covers an instrument which measures and displays angle of deviation of the airstream dependent on mounting location on the aircraft.

Airstream Deviation Instrument (ADI)

SAE AS404C-2001 电动转速针:磁阻力(指示器&发生器)

To specify minimum requirements for Electric Tachometers primarily for use in reciprocating engine powered civil transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.3. This Aeronautical Standard covers magnetic drag tachometers with or without built-in synchroscopes.

Electric Tachometer: Magnetic Drag (Indicator& Generator)

SAE AS407C-2001 燃料流量计

To specify minimum requirements for Fuel Flowmeters for use primarily in reciprocating engine powered civil transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.3. This Aeronautical Standard covers two basic types of instruments, or combinations thereof, intended for use in indicating fuel consumption of aircraft engines as follows: TYPE I - Measure rate of flow of fuel used. TYPE II - Totalize amount of fuel consumed or remaining.

Fuel Flowmeters

SAE AIR818D-2001 飞机仪表和仪表系统标准:措辞术语,表达方式,环境设计标准

This Aerospace Information Report, (AIR) is intended to provide the sponsors of Aerospace Standards, (AS), with standard wording, formatting, and minimum environment and design requirements for use in the preparation of their document. The individual shall use only those parts of this AIR which apply to their particular document. The individual sponsor may expand the standard wording, especially under Sections 4, 5, and 6 as required. The paragraphs of this AIR shall be used verbatim wherever possible. Unless otherwise directed by SAE, cross referenced documents shall be called out by specific revision letter, e.g. shall be in accordance with AS XXXXB. In addition, all non-SAE documents called out shall include the document title when initially identified. However, every effort shall be made to keep cross-referencing to an absolute minimum.

Aircraft Instrument and Instrument System Standards: Wording Terminology, Phraseology, Environment and Design Standards For

SAE AS412B-2001 一氧化碳检测仪器

To specify minimum requirements for carbon monoxide detector instruments for use in aircraft, the operation of which may subject the instrument to the environmental conditions specified in Paragraph 3.3. This standard is not intended to cover fire detectors. This Aeronautical Standard covers the basic type of carbon monoxide detector instrument used to determine toxic concentrations of carbon monoxide by the measurement of heat changes through catalytic oxidation.

Carbon Monoxide Detector Instruments

SAE AS398B-2001 非稳定型磁性方向仪(磁罗盘)

To specify minimum requirements for non-stabilized magnetic direction instruments for use in aircraft, the operation of which may subject the instrument to the environmental conditions specified in Paragraph 3.3. This Aeronautical Standard covers two basic types of instruments as follows: Type I - Direct Reading, Type II - Remote Indicating.

Direction Instrument, Magnetic, Non-Stabilized Type (Magnetic Compass)

SAE ARP427A-2001 压力比仪器

To recommend requirements for electrical Pressure Ratio Indicating Instruments for use in aircraft, the operation of which may subject the instruments to the environmental conditions specified in Para. 3.3. This recommended practice is to be considered as being currently applicable and necessarily subject to revision from time to time due to rapid development in the aircraft industry. This Aeronautical Recommended Practice covers two types of two unit Pressure Ratio Instruments each of which consist of a Transducer and an Indicator. The Transducer computes the ratio of two pressures and converts this ratio to a synchro electrical signal which is transmitted to the Indicator. TYPE I - All material in this document applies to this classification only. TYPE II - Additional material for this classification will be added to superseding issues as the state of the art permits.

Pressure Ratio Instruments

SAE AS402B-2001 自动驾驶仪

To specify minimum requirements for Automatic Pilots primarily for use in reciprocating engine powered civil transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.3. This Aeronautical Standard covers Automatic Pilots intended for use on aircraft to automatically operate the aerodynamic controls to maintain flight and/or to provide maneuvering about the three axes through servo control.

Automatic Pilots

SAE AS408C-2001 测压仪表.燃料,油和液压(装有活塞式发动机的飞机)

This Aerospace Standard establishes the essential minimum safe performance standards for fuel, oil and hydraulic pressure instruments primarily for use with reciprocating engine powered transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.3. This Aerospace Standard covers two basic types of fuel, oil and hydraulic pressure instruments as follows: Type I - Direct Indicating, Type II - Remote Indicating. This Aerospace Standard does not apply to engine mounted torque meter systems.

Pressure Instruments - Fuel, Oil and Hydraulic (Reciprocating Engine Powered Aircraft)

NAVY QPL-22075-17 NOTICE 1-2001 ID-663D/U型方位一距离一航向指示器

Qualified Products List QPL-22075-16, dated 22 May 2000, is hereby inactive for new design.Military Specification MIL-I-22075C(AS), which covered the products listed thereon was inactivated on 17 September 1997.

INDICATOR, BEARING-DISTANCE-HEADING ID-663D/U

NAVY MIL-I-81454 (3)-2001 ID-1481(*)/A型垂直陀螺仪指示器

This amendment forms a part of MIL-I-81454(AS), dated 15 January 1967, and is approved for use by the Naval Air Systems Command, Department of the Navy and is available for use by all Departments and Agencies of the Department of Defense.

INDICATOR, GYROSCOPE, VERTICAL REFERENCE ID-1481 (*)/A

NAVY MIL-I-22126 B (3)-2001 螺旋桨发动机扭矩指示器

This amendment forms a part of MIL-I-22126B(AS), dated 17 August 1972, and has been approved by the Naval Air Systems Command, Department of the Navy. It is available for use by all Departments and Agencies of the Department of Defense.

INDICATOR, TORQUEMETER, ENGINE, TURBOPROP

NAVY MIL-I-8974 A (2)-2001 事件指示器一般规范

This amendment forms a part of MIL-I-8974A, dated 15 July 1981, and is approved for use by all Departments and Agencies of the Department of Defense.

INDICATOR, EVENT COUNTING, GENERAL SPECIFICATION FOR