49.120 货运设备 标准查询与下载

SAE AS5135-1997 干燥剂通道和干燥剂容器

This SAE Aerospace Standard (AS) describes the characteristics of a desiccant port installed through the flat wall of a shipping and storage container. With the cover removed, the desiccant port shall provide access to the interior of the container for installation and removal of desiccant.

Desiccant Port and Desiccant Holder

BS M 91:1997 飞机 货舱容积计算方法

This International Standard covers the methodology of defining and determining the internal volumes of both the main deck and lower deck aircraft cargo compartments. The minimum required clearance between the compartment envelope and the unit load devices (ULDs) is also stated in order to provide the maximum ULD external contour and the methodology to define the ULD internal volumes.

Aircraft. Methodology of calculating cargo compartment volumes

AIR FORCE MIL-P-83037 A NOTICE 1-1997 A/E29H-1空中运载货运平台

MIL-P-83037A (USAF) is inactive for new design and is no longer used, except for replacement purposes. Custodians:

PLATFORM, CARGO, AERIAL DELIVERY A/E29H-1

SAE AIR1811A-1997 液体冷却系统

This publication is applicable to liquid cooling systems of the closed loop type and the expendable coolant type in which the primary function is transporting of heat from its source to a heat sink. Most liquid cooling system applications are oriented toward the cooling of electronics. Liquid cooling techniques, heat sinks, design features, selection of coolants, corrosion control, and servicing requirements for these systems are presented. Information on vapor compression refrigeration systems, which are a type of cooling system, is found in Reference 1. The purpose of this Aerospace Information Report (AIR) is to provide guidelines for the selection and design of airborne liquid cooling systems.

Liquid Cooling Systems

SAE AIR4359-1997 悬重(如挂衣箱)对集装箱性能的影响

This SAE Aerospace Information Report (AIR) provides information on the subject of Air Mode containers used for transporting Hanging Loads such as Garment-On-Hangers (GOH), or other roof supported cargo. It suggests considerations and recommendations for roof loaded containers to transport hanging loads efficiently and safely by air and to protect the aircraft floor and cargo system from damage due to overload conditions.

Effects of Hanging Loads (e.g., GOH) on ULD Performance

SAE AIR806B-1997 飞机货运的空气调节

The report presents air conditioning data for aircraft cargo which is affected by temperature, humidity, ventilation rate and atmospheric pressure. The major emphasis is on conditioning of perishable products and warm-blooded animals. The report also covers topics peculiar to cargo aircraft or which are related to the handling of cargo. The purpose of this Aerospace Information Report (AIR) is to provide design information related to the air conditioning of cargo transported by commercial and military aircraft. Affected cargo includes perishable products, live animals and hazardous materials.

Air Conditioning of Aircraft Cargo

ISO 10046:1996 航空器 货舱容积的计算方法

Covers the methodology of calculating for the determination of the internal volumes of both the main deck and the lower deck aircraft cargo compartments. The minimum required clearance between the compartment envelope and the unit load devices (ULDs) is also stated in order to provide the maximum ULD external contour and the methodology to define the ULD internal volumes.

Aircraft - Methodology of calculating cargo compartment volumes

BS M 88:1996 航空货运设备 货物集装箱的压力平衡要求

Since most modern civil transport aircraft capable of carrying air cargo unit load devices or large-size shipping containers have pressurized cabins and cargo compartments, two different cases must be con-sidered: a) normal (low airflow) pressure equalization during climb and descent —from the departure airport pressure down to the cruise flight cabin pressure, up to the landing airport pressure; b) emergency (rapid decompression) pressure equalization in the event of a sudden (possibly "explosive") depressurization of the aircraft fuselage occurring at cruise altitude: this case re-quires very fast (high airflow) pressure equaliz-ation between cruise flight cabin pressure and outer ambient pressure. This International Standard defines the minimum safety requirements to be met by containers used to transport cargo by civil transport aircraft in either case a) or b) above. The flight safety requirements specified in this Inter-national Standard are applicable to the design of — aircraft containers for general cargo, as covered by · ISO 4118 for non-certified lower deck con-tainers, · ISO 6517 for base-restrained certified con-tainers exclusively for the lower deck of high-capacity aircraft, · ISO 8323 for air/surface intermodal containers, · ISO 10327 for certified containers for air cargo; — air mode insulated containers, as covered by ISO 8058; — any airtight shipping containers with an internal volume of 1 m (35 ft) or more. NOTE 1 Most shipping containers/packagings used for air cargo are made of sufficiently low-strength material (e.g. fibreboard) or provide sufficient air leakage (e.g. wooden crates) that they cannot be considered airtight and do not present any significant hazard as a result of pressure equalization. There are however a number of special containers, notably for the carriage of satellites/space hardware, aircraft spares, sensitive scientific or technical equipment, etc., which are airtight per design (in order to protect the contents against atmospheric pollution) or per construction (because of the quality of sealing and materials used).

Air cargo equipment. Pressure equalization requirements for cargo containers

SAE AIR822A-1996 通用航空氧气系统R(2001)

This specification has been declared "NONCURRENT" as of June 2006. It is recommended, therefore, that this document not be specified for new designs. This SAE Aerospace Information Report (AIR) provides a general overview of oxygen systems for general aviation use. Included are a brief review of the factors and effects of hypoxia, system descriptions and mission explanations for system or component selection, and techniques for safe handling of oxygen distribution systems.

Oxygen Systems for General Aviation R(2001)

SAE AS8040A-1996 飞机内燃换热器型加热器

This SAE Aerospace Standard (AS) covers internal combustion heat exchanger type heaters used in the following applications: a) cabin heating (all occupied regions and windshield heating); b) wing and empennage anti-icing; c) engine and accessory heating (when heater is installed as part of the aircraft); d) aircraft de-icing. This document details the minimum safety, performance, design, and testing requirements for internal combustion heaters and certain auxiliary devices that are considered necessary for the utilization of heaters in fixed and rotary wing aircraft. This standard is to be considered currently applicable and necessarily subject to revision from time to time due to advances in the aircraft industry. This standard is based on practical engineering requirements for aircraft heaters currently in use and is applicable to aircraft heaters that shall be developed to meet future requirements. The requirements of this standard are primarily intended to be applicable to civil aircraft whose primary function is transporting passengers or cargo.

Heater, Aircraft Internal Combustion Heat Exchanger Type

SAE ARP1532A-1996 飞机氧气系统线路的制造,测试和安装

This ARP covers procedures or methods to be used for fabricating, handling, testing, and installation of oxygen lines in an aircraft oxygen system. The purpose of this recommended practice is to establish and/or outline the methods for fabricating, handling, and testing of oxygen lines and their installation into an aircraft oxygen system. Compliance with this practice should enhance satisfactory operation of the oxygen system.

Aircraft Oxygen System Lines, Fabrication, Test and Installation

SAE AS8026A-1996 运输类飞机乘务人员用氧气面罩

This standard covers oxygen masks and breathing valves used with both panel mounted and mask mounted demand and pressure-demand oxygen regulators. Mask mounted oxygen regulators are covered under other standards, but when the mask mounted regulator incorporates an integral exhalation valve, the performance of this valve shall meet the requirements of this standard. This standard establishes the minimum performance standards for the manufacturer of demand type crewmember oxygen masks to be used with straight demand, diluter-demand and pressure-demand oxygen systems.

Crewmember Demand Oxygen Mask for Transport Category Aircraft

SAE AS916B-1996 氧流量指标

This SAE Aerospace Standard (AS) defines the overall requirements applicable to oxygen flow indicating devices intended to operate in conjunction with an oxygen regulator and mask system. Flow indicators covered by this document are for use with pressure demand, diluter-demand and continuous flow oxygen systems.

Oxygen Flow Indicators

ISO 11242:1996 航空器 货运集装箱压力均衡要求

Describes the minimum safety requirements to be met by containers used to transport cargo by civil transport aircraft under normal pressure equalization during climb and descent and under emergency pressure equalization in the event of a sudden depressurization.

Aircraft - Pressure equalization requirements for cargo containers

SAE AIR1823A-1996 飞机ECS动态分析的(R)工程分析系统 (EASY)计算程序

The Engineering Analysis System (EASY) computer program is summarized in this report. It provides techniques for analysis of steady-state and dynamic (transient) environmental control system (ECS) performance, control system stability, and for synthesis of optimal ECS. General uses of a transient analysis computer program for ECS design and development, and general features of EASY relative to these uses, are presented. This report summarizes the nine analysis options of EASY, EASY program organization for analyzing ECS, data input to the program and resulting data output, and a discussion of EASY limitations. A generalized computer program for determining transient thermodynamic performance of aircraft ECS, and methods for dynamic analysis of aircraft ECS are discussed in this report.

(R) Engineering Analysis System (EASY) Computer Program for Dynamic Analysis of Aircraft ECS

SAE AS1304A-1996 持续气流化学氧生成器

This SAE Aerospace Standard (AS) applies to performance and testing of solid chemical oxygen generators which produce oxygen at essentiall ambient pressure for use aboard aircraft whose cabin pressure altitude does not exceed 40,000 ft (about 12,200 m). Portable chemical oxygen devices are covered by AS1303.

Continuous Flow Chemical Oxygen Generators

GOST ISO 4116-1996 航空货运设备.与飞机集装单元装置兼容的地面设备要求

Стандарт распространяется на аэродромные и складские перегрузочные и транспортные средства и устанавливает требования к их транспортер

Air cargo equipment. Ground equipment requirements for compatibility with aircraft unit load devices

SAE AIR5145-1996 数据库目录第一部分.全身人体测量调查

This SAE Aerospace Information Report (AIR) lists whole body anthropometric surveys and provides current sources for the survey raw data and summary statistics. The purpose of this directory is to provide a single source for accessing anthropometric survey data for human modelers, human factors specialists, and other interested in anthropometric data. It is not meant to provide detailed data on each survey, but to provide readers with enough information to allow them to make a decision about which surveys are of possible application to their work. The reader can then obtain further information and actual data from the listed points of contact.

Directory of Databases Part I - Whole Body Anthropometry Surveys

SAE AS1214A-1996 阀门、高压氧气、线路关闭、手动操作的最低标准

This standard covers all types of manually operated high pressure oxygen line shut off valves utilizing either metallic or nonmetallic valve seats for use in general and commercial type aircraft. It is intended that the line valve should be installed in a position accessible in flight, when the cylinder mounted oxygen valves are not. The line shutoff valve may also be used optionally in large systems as a maintenance aid where only a portion of the system need be opened up and purged after repair or replacement of one or more parts. The purpose of this Aerospace Standard is to define general minimum standards for the design, fabrication, test and packaging of manually operated, high pressure oxygen line shut off valves.

Minimum Standards for Valve, High Pressure Oxygen, Line Shut Off, Manually Operated

SAE AS1303A-1996 便携式化学氧气

This SAE Aerospace Standard (AS) applies to a portable chemical oxygen generator assembly intended for the following uses: a. First aid treatment of aircraft occupants after an emergency descent following a decompression or other emergency condition; and b. use by cabin attendants to maintain their mobility after a decompression.

Portable Chemical Oxygen