V45 航空仪表 标准查询与下载

HB 6-76-1976 航空仪表通用技术条件

本标准适用于飞机上使用的仪表专业产品。制订产品的专业技术条件和专用技术条件时，均应按产品使用条件和特点选用本标准的有关项目和类别。

General Technical Conditions for Aviation Instruments

AIR FORCE MIL-I-27304 E-1977 流速指示器

This specification covers the requirements for type sofher meticallys ealed indicators for indicating the flow . rate of engine fuelin pounds per hour (pph). receiver .The indicator is a remote second-harmonic selsyn

INDICATOR, RATE OF FLOW

NF L74-170:1977 ３８０－５８０赫兹电流互感器

Current transformers, 380 hertz - 580 hertz.

AIR FORCE MIL-I-7065 A-1976 副翼调整片位置指示器

This specification covers one type of aileron trim tabposition indicator.

INDICATOR, POSITION, AILERON TRIM TAB

AIR FORCE MIL-A-83212 A-1976 AAU-27/A型压力高度计

This specification covers the requirements for one type of counter-drum-pointer, integrally lighted, pressure altimeter having a range of -1,000 to +50,000 feet, designated AAU-27/A.

ALTIMETER, PRESSURE AAU-27/A

ARMY MIL-L-52039 D-1976 着陆机场滑翔角度指示

This specification covers an a i r p o r t approach glide-angle 1i.ght designed t o project three separate beams of l i g h t,one red, one green, and one yellow.

LIGHT, GLIDE ANGLE, AIRPORT APPROACH

2G 117-1975 压力驱动的空气速度表规范

Specification for pressure-driven airspeed indicators

BS 2G 182:1975 航空用压力驱动马赫表规范

This British Standard specifies the general design requirements and test procedures for machmeters of the following types. 1 Type A. Machmeter indicating a Mach scale range of at least 0.5 M up to a maximum scale reading of 1.0 M and of altitude range up to 50 000 ft, with maximum accuracy from 20 000 ft to 40 000 ft, unless otherwise required by the individual specifi-cation. 2 Type B. Machmeter indicating a range extending above 1.0 M and of altitude range up to 60 000 ft with maximum accuracy in the region between the altitude limits 20 000 ft and 40 000 ft and in the indicated range of 0.7 M to 0.9 M.

Specification for pressure-driven machmeters for aircraft

BS 2G 117:1975 压力驱动空速指示器规范

This British Standard specifies the general design requirements and test procedures for airspeed indicators operated directly by the aircraft pitot and static pressures. It relates to indicators with ranges partly or wholly up to 800 knots.

Specification for pressure-driven airspeed indicators

AIR FORCE MIL-I-7062 C-1975 28伏特直流电操纵表位置指示器的一般规范

This specification covers the general requirements for 28-V, d-c controlsurface electrical position irkdicators.The moving element is a nonenergized permanent magnet, and the stator is electrically connected to a position transmitter and energized with di

INDICATOR, POSITION, CONTROL SURFACES, 28 VOLT DC, GENERAL SPECIFICATION FOR

NAVY MIL-T-81988-1975 AN/ARM-155指示器试验装置

Referenced specifications - Any referenced specifications shall have precedence over all applicable subsidiary specifications referenced therein. All referenced specifications shall apply to the extent specified.

TEST SET, INDICATOR, AN/ARM-155

HB 6-62-1975 航空仪表圆形刻度盘

本标准适用于航空仪表中具有圆形（或圆弧形）的向心式刻度盘和离心式刻度盘的设计。

Aviation Instrument Circular Dial

AIR FORCE MIL-I-27619 G-1974 指引地平仪指示器

This specification covers three types of remote attitude-director indicators.with superimposed flight-director information.

INDICATORS, ATTITUDE DIRECTOR

ARMY MIL-I-58099-1974 一般规格的电压比式直升机压力指示器

This specification covers one type of hermetically sealed, remote indicating, vol tage ratio type, oil pressure indicator designated Type TB-1.

INDICATOR, PRESSURE, HELICOPTER, VOLTAGE RATIO TYPE, GENERAL SPECIFICATION FOR

AIR FORCE MIL-I-38263 VALID NOTICE 1-1974 ARU-17/A型遥控飞行姿态指示器

This datice should be filedin front of Military Specification MIL-1-38263 dated 28 February 1964.

INDICATOR, ATTITUDE ARU-17/A, REMOTE

AIR FORCE MIL-I-6447 C-1974 M-1A型真空速指示器

This specification covers one type of Pitot - statictrue air speed indicator , range. 100-450 knots , designated type M-1A.

INDICATOR, TRUE AIRSPEED, TYPE M-1A

AIR FORCE MIL-I-83152 B-1974 AVU-22/A型(指示传感器)指示空速指示器

This specification covers an integrally white lighted, 3-inch, round-dial, Pitot-static, indicated airspeed indicator and transducer, designated AW-22/A.

INDICATOR, INDICATED-AIRSPEED AVU-22/A (INDICATOR-TRANSDUCER)

AIR FORCE MIL-I-83449-1974 A/A24J-21液氧量指示器装置

The following documents, of the issue in effect on date of invitation for bids or requests for proposal, form a part of this specification to the extent specified herein,

INDICATOR SET, LIQUID OXYGEN QUANTITY, A/A24J-21

NF L70-132:1973 机载仪表盘和驾驶舱记录用字母和数字

Letter and figure designs for flight instrument dials and for inscriptions in the cockpit.

ARMY MIL-I-14868 (1)-1973 10559241.数字显示指示器

This amendment forms a part of Military Specification MIL-I-l4868(MU),dated 2 March 1970.

INDICATOR, DIGITAL, DISPLAY, 10559241