V06 环境条件 标准查询与下载

NAVY MIL-S-29398 C NOTICE 1-1998 40,000磅容量外部货物直升飞机投掷系统

SLING SYSTEM, HELICOPTER: EXTERNAL CARGO, 40,000 POUND CAPACITY

SLING SYSTEM, HELICOPTER: EXTERNAL CARGO, 40,000 POUND CAPACITY

DLA A-A-59266-1998 中央型外部圆柱形通用砂轮机 [代替:DLA MIL-G-23823 E CANC 通用 1,DLA MIL-G-23823 E,DLA MIL-G-23823 D,DLA MIL-G-23823 C,DLA MIL-G-23823 B,DLA MIL-G-23823 A,DLA MIL-G-23823]

This commercial item description (CID) covers cylindrical universal grinding machines intended for grinding workpieces where uniform tolerances for size, roundness, and finish on a wide variety of materials are required.

GRINDING MACHINE, UNIVERSAL, CYLINDRICAL, EXTERNAL, CENTER-TYPE [Superseded: DLA MIL-G-23823 E CANC NOTICE 1, DLA MIL-G-23823 E, DLA MIL-G-23823 D, DLA MIL-G-23823 C, DLA MIL-G-23823 B, DLA MIL-G-23823 A, DLA MIL-G-23823]

DLA A-A-59332-1998 电脑数字控制(CNC)中央型外部圆柱形砂轮机 [代替:DLA MIL-G-80278 CANC 通告 1,DLA MIL-G-80278]

This commercial item description (CID) covers computer numerical control (CNC)center-type external cylindrical grinding machines. The grinding machines covered by this CIDare intended for use in operations where multiple workpieces aregroundfromworkpieceprograms to close tolerances for outside diameter, straightness, tapers, steps, and faces.

GRINDING MACHINE, CYLINDRICAL, EXTERNAL, CENTER-TYPE, COMPUTER NUMERICAL CONTROL (CNC) [Superseded: DLA MIL-G-80278 CANC NOTICE 1, DLA MIL-G-80278]

NAVY MIL-T-81838 NOTICE 1-1996 AERO-1D型外部辅助300加仑飞行器油箱

This notice should be filed in front of MIL-T-8 1838(AS), dated 30 November 1971, and Amendment - 1 , dated 8 March 1976.

TANK, FUEL, AIRCRAFT, AUXILIARY EXTERNAL 300 GALLON, TYPE AERO-1D

BS 4G 229:1996 机载设备环境条件和测试程序一览表

This International Standard lists the different environ-mental conditions and test procedures for airborne equipment and is primarily intended for civil and/or transport aircraft applications. This International Standard is an endorsement of sections of publications EUROCAE/ED-14C and RTCA/DO-160C, which supplement several ISO International Standards. note:1) These publications can be obtained from the following addresses: EUROCAE (European Organization for Civil Aviation Electronics), 11 rue Hamelin, 75783 Paris Cedex 16, France. RTCA (Radio Technical Commission for Aeronautics), 1140 Connecticut Avenue, N.W., Suite 1020, Washington, DC 20036, USA.

Schedule for environmental conditions and test procedures for airborne equipment

BS G 260:1996 飞机设备的环境测试 稳态加速度

This International Standard specifies two types of steady-state acceleration test and establishes five severity grades of acceleration forces used to simu-late a gradually changing acceleration environment representative of that which civil aircraft equipment can encounter in operational use. The emergency landing case is not within the scope of this International Standard; reference should be made to ISO 7137 for this case.

Environmental tests for aircraft equipment. Steady-state acceleration

BS G 259:1996 飞机设备 机载设备的环境和操作条件 湿度、温度和压力测试

This International Standard, which is applicable pri-marily to civil and transport aircraft, specifies the test requirements for aerospace equipment which could be subjected to moisture ingress, frosting and condensation, resulting from the passage through at-mospheric conditions of high humidity, in combination with or induced by changing temperature and press-ure. It specifies various test procedures which can be in-voked when required by an equipment design and requirement specification. This International Standard permits the selection of specific test conditions and methods that define ac-ceptance requirements for aerospace equipment which may be subject to induced condensation and humidity. The conditions are more likely to occur in an uncon-ditioned bay but may also occur in a conditioned bay when the equipment has a short thermal transmission path to an external airframe structure. The incidence of this form of condensation is also influenced by the duty cycle of the equipment and its thermal charac-teristics. This test is not intended to reveal the defects ensuing from prolonged exposure to high humidity such as may occur on the ground in tropical climates, a suit-able test for this environment is given in ISO 7137. Also this test is not intended to simulate the hazards of local ice formation, in which case reference should be made to the icing tests defined in ISO 7137, test procedure 1.4.

Aircraft equipment. Environmental and operating conditions for airborne equipment. Humidity, temperature and pressure tests

ARMY ADS-37 A-PRF-1996 电磁环境效应的性能及检验要求

This document establishes electromagnetic environmental effects(E3) performance and verification requirements for aircraft systems.

ELECTROMAGNETIC ENVIRONMENTAL EFFECTS (E3) PERFORMANCE AND VERIFICATION REQUIREMENTS

DD ENV 50196-1995 现场作业.额定绝缘水准和相关空中距离.计算方法

Provides a guide to the minimum safe distances of a worker from electrical parts at different potential.

Live working. Required insulation level and related air distances. Calculation method

DLA DESC-DDL-103-33-1995 环境法方案要求和制表描述图纸编写述的准则述绘图程序方针

When an immediate need for a part has been shown and insufficient time exists for preparation of a complete specification, a "skeleton" document in the form of a DESC drawing is prepared.

GUIDELINES FOR DESC DRAWINGS PROCEDURES, REQUIREMENTS AND TABULATION OF DESC DRAWINGS PREPARED BY DESC-ELP

DLA MS90708 REV C-1995 [由以下代替: 美国机械工程师协会 B18.24.3, 美国机械工程师协会 B18.24.3]外部联锁保留环

UNLESS OTHERWISE SPECIFIED, ALL DIMENSION ARE IN INCHES.

RING, RETAINING, EXTERNAL INTERLOCKING [Superseded By: ASME B18.24.3, ASME B18.24.3]

ISO 7137:1995 航空器 机载设备的环境条件和试验程序

Cancels and replaces the third edition (1992). Lists the different environmental conditions and test procedures for airborne equipment and is primarily intended for civil and/or transport aircraft applications.

Aircraft - Environmental conditions and test procedures for airborne equipment

HB 7122.1-1994 民用飞机机载设备气候环境试验箱（室）检定方法 总则

本标准规定了《民用飞机机载设备气候环境试验箱（室）检定方法》系列标准中所用的术语、检定条件、检定用仪器要求、检定周期以及检定工作其他基本要求。 　　本系列标准包括： 　　ＨＢ ７１２２．１ 民用飞机机载设备气候环境试验箱（室）检定方法 总则 　　ＨＢ ７１２２．２ 民用飞机机载设备气候环境试验箱（室）检定方法 温度和高度试验箱（室） 　　ＨＢ ７１２２．３ 民用飞机机载设备气候环境试验箱（室）检定方法 温度湿度试验箱（室） 　　ＨＢ ７１２２．４ 民用飞机机载设备气候环境试验箱（室）检定方法 防水试验箱（室） 　　ＨＢ ７１２２．５ 民用飞机机载设备气候环境试验箱（室）检定方法 砂尘试验箱（室） 　　ＨＢ ７１２２．６ 民用飞机机载设备气候环境试验箱（室）检定方法 盐雾试验箱（室） 　　本标准适用于《民用飞机机载设备气候环境试验箱（室）检定方法》系列标准中的所有标准。《民用飞机机载设备气候环境试验箱（室）检定方法》系列标准规定的检定方法也适用于按ＨＢ ６１６７进行试验时所用的气候环境试验箱（室）的检定。对于民用飞机机载设备按其他标准进行时所用的气候环境试验箱（室）的检定亦可参照使用。

General rules for verification methods of climate and environment test chambers (rooms) for airborne equipment of civil aircraft

HB 7122.6-1994 民用飞机机载设备气候环境试验箱（室）检定方法 盐雾试验箱（室）

本标准规定了盐雾试验箱（室）的检定方法。本标准是《民用飞机机载设备气候环境试验箱（室）检定方法》系列标准的组成部分。 　　本标准适用于按HB 6167.12《民用飞机机载设备环境条件和试验方法 盐雾试验》进行试验时所用的试验箱（室）的检定。

Civil aircraft airborne equipment climate environment test chamber (room) verification method Salt spray test chamber (room)

HB 7122.5-1994 民用飞机机载设备气候环境试验箱（室）检定方法 砂尘试验箱（室）

本标准规定了砂尘试验箱（室）的检定方法。本标准是《民用飞机机载设备气候环境试验箱（室）检定方法》系列标准的组成部分。 　　本标准适用于按HB 6167.10《民用飞机机载设备环境条件和试验方法 砂尘试验》进行试验时所用的试验箱（室）的检定。

Civil aircraft airborne equipment climate environment test box (room) verification method sand dust test box (room)

HB 7122.3-1994 民用飞机机载设备气候环境试验箱（室）检定方法 温度湿度试验箱（室）

本标准规定了湿热试验箱（室）和霉菌试验箱（室）的检定方法。 　　本标准是《民用飞机机载设备气候环境试验箱（室）检定方法》系列标准的组成部分。 　　本标准适用于按ＨＢ ６１６７．４《民用飞机机载设备环境条件和试验方法 湿热试验》和ＨＢ ６１６７．１１《民用飞机机载设备环境条件和试验方法 霉菌试验》进行试验时所用试验箱（室）的检定。

Civil aircraft airborne equipment climate environment test chamber (room) verification method temperature and humidity test chamber (room)

HB 7122.2-1994 民用飞机机载设备气候环境试验箱（室）检定方法 温度和高度试验箱（室）

本标准规定了温度和高度、温度变化试验箱（室）的检定方法。本标准是《民用飞机机载设备气候环境试验箱（室）检定方法》系列标准的组成部分。 　　本标准适用于按ＨＢ ６１６７．２《民用飞机机载设备环境条件和试验方法 温度和高度试验》、ＨＢ ６１６７．３《民用飞机机载设备环境条件和试验方法 温度变化试验》进行试验时所用试验箱（室）的规定。

Civil Aircraft Airborne Equipment Climatic Environment Test Chamber (Chamber) Verification Method Temperature and Altitude Test Chamber (Chamber)

ISO 2669:1995 航空器设备的环境试验 稳态加速度

Cancels and replaces the first edition (1978). Lays down two types of steady-state acceleration test and establishes five severity grades of acceleration forces used to simulate a gradually changing acceleration environment representative of that which civil aircraft equipment can encounter in operational use. Does not apply to emergency landing case.

Environmental tests for aircraft equipment - Steady-state acceleration

JIS W 0813:1995 飞行器.机载设备的环境条件和试验程序.指定防火区内的耐火性

この規格は，特定防火区域内にあり，規定した最低水準よりも高い耐火性をもつように作られるすべての構成部品。機器及び構造物に対する要求事項について規定する。

Aircraft -- Environmental conditions and test procedures for airborne equipment -- Resistance to fire in designated fire zones

JIS W 0203:1995 航空和航天用标准大气

この規格は，地表(地球表面)から高度80kmまでの大気の特性の季節，緯度，経度及び日々による変化についてのモデルを示す。

Reference atmospheres for aerospace use