V44 生命保障系统与设备 标准查询与下载

GJB 6988-2010 飞行人员救生信号弹规范

本规范规定了飞行人员救生信号弹的技术要求、质量保证规定和交货准备等内容。 本规范适用于飞行人员救生信号弹的研制、生产、验收和使用。

Specification for aircrew survival signal cartridge

SAE AIR825/14-2010 基础航空器氧气系统设计

This slash document collects general reference material related to gaseous oxygen system flow requirements and sizing calculations. This document will assist oxygen system equipment designers and operators to establish systems and equipment requirements. The document consists of charts, tables, system schematics, system requirements, and sample calculations for system sizing.

Basic Aircraft Oxygen Systems Design

MH/T 6061-2010 飞机厨房手推车、物品箱及相关组件的最低设计和性能

本标准规定了安装在运输类飞机厨房和其他区域的手推车、物品箱及相关组件的最低设计和性能要求，以及供储存舱设计人员和设备安装人员使用的安装要求。 本标准适用于但不限于下列安装在运输类飞机厨房和其他区域的设备： a) 全长车和半长车(主要用于装载饮料、物品箱、食物、商品和垃圾)； b) 折叠车； c) 物品箱(便携箱、标准箱和餐箱)； d) 储存在手推车和(或)厨房储存舱里的非固定相关组件，如抽屉、托盘、垃圾箱衬里或其他类似组件。 本标准没有完全涵盖以下内容： a) 具有自备的机械制冷系统、电动机、其他电器部件或通过加压系统分配饮料的手推车或物品箱。 b) 延长使用寿命和持续适航的设计细则，因为这些细则可能随以下因素变化： 1) 厨房和食品(饮料)系统总体设计； 2) 营运人希望的人因工程； 3) 手推车或物品箱的使用方法和注意事项； 4) 手推车或物品箱的维护方法； c) 民用航空规章、相关公众健康规章和(或)设计细则的相关要求，该要求涵盖在客舱服务人员或飞机制造商对主要设备的规范中。

Minimum design and performance of airplane galley in-flight carts,containers,and associated components

SAE AS5402A-2010 飞机应急斧设计与性能标准

This SAE Aerospace Standard (AS) provides design criteria and performance tests for crash axes intended for use by aircraft crew members to assist in evacuation, extrication, fire fighting, or other emergency activities.

Design and Performance Criteria Aircraft Crash Axes

SAE ARP5403A-2010 航空器应急斧

This SAE Aerospace Recommended Practice (ARP) recommends general criteria for availability, location, accessibility, stowage, use, and crew member training needed for aircraft crash axes.

Aircraft Crash Axes

CFR 14-135.621-2014 航空和航天. 第135部分:操作要求:通勤人员和随需应变操作和规则架这样的飞机. 第135.621节:简报医务人员.

(a) Except as provided in paragraph (b) of this section, prior to each helicopter air ambulance operation, each pilot in command, or other flight crewmember designated by the certificate holder, must ensure that all medical personnel have been briefed on the following—

Aeronautics and Space. Part135:Operating requirements: Commuter and on demand operations and rules governing persons on board such aircraft. Section135.621: Briefing of medical personnel.

ASTM F320-10 航空航天用透明外壳的抗冰雹撞击性能的标准试验方法

This test method may be used to determine the hail impact resistance of windshields for acceptance, design, service, or research purposes. By coupling this method with the installed angle and velocity of a specific aerospace vehicle, design allowables, criteria, and tolerances can be established for that vehicle''s windshield.1.1 This test method covers the determination of the impact resistance of an aerospace transparent enclosure, hereinafter called windshield, during hailstorm conditions using simulated hailstones consisting of ice balls molded under tightly controlled conditions. 1.2 The values stated in inch-pound units are to be regarded as standard. The values given in parentheses are mathematical conversions to SI units that are provided for information only and are not considered standard. 1.3 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use. For specific hazard statements see Section 7.

Standard Test Method for Hail Impact Resistance of Aerospace Transparent Enclosures

GJB 6850.220-2009 水面舰船系泊和航行试验规程 第220部分：舰载直升机目视助降系统试验

Surface ship mooring and sailing test procedures part 220: shipboard helicopter visual landing aid system test

GJB 6850.228-2009 水面舰船系泊和航行试验规程 第228部分：舰载直升机格栅、防滑网装置试验

Surface warship mooring and sailing test procedures part 228: shipboard helicopter grille, anti-skid net device test

KS W ISO 1465:2009 航空器.液态氧充填接头.相配尺寸

이 표준은 항공기 액체 산소 보급용 커플링의 결합 및 간극 치수를 규정한다.

Aircraft-Liquid oxygen replenishment couplings-Mating dimensions

BS EN 4618:2009 航空航天系列.飞机内部空气质量规格,标准和测定方法

This standard specifies requirements and determination methods for newly certificated commercial passenger aircraft programmes. This standard applies to newly certificated commercial passenger aircraft programmes. It may also apply to current production aircraft if it does not carry significant penalties, i.e. if it can be shown to be technically feasible and economically justifiable. This standard covers the period from first crew embarkation to last crew disembarkation. NOTE 1 During embarkation and disembarkation, reduced temperatures in the cabin may be desirable due to increased metabolic activity of the occupants. In some ground cases, the aircraft environmental control system (ECS) may not be able to compensate for the external conditions influencing the cabin comfort conditions, such as open doors, extreme hot/cold ground/air temperatures or radiant heat. In this case, external air-conditioning systems, for example conditioned low-pressure ground air or high-pressure supply, may be used to supplement the aircraft ECS. If the temperature range stated in this standard is regularly exceeded (either above or below the stated range), changes to airline and/or airport procedures and/or aircraft design should be introduced. NOTE 2 During ground operations, the external air quality may adversely influence the air quality within the aircraft cabin. Contamination produced as a result of servicing activities or ground operations vehicles may enter the aircraft directly, for example via open doors, and the ECS may not be able to effectively control contaminant levels in the cabin. Airline and airport operational procedures should be organised so as to avoid direct contamination of the cabin from these pollutant sources. If the contaminant ranges stated in this standard are regularly exceeded, changes to airline and/or airport procedures and/or aircraft design should be introduced. Outside air quality levels would usually be regulated by national authorities. The population under consideration – passengers and crew – excludes individuals with pre-existing infirmity or ill health conditions. All values given in this document are sea-level equivalent (see Clause 4). According to the Air Quality Guidelines WHO 1999, paragraph 2.2.3, ‘For gaseous pollutants, no increase in effects over those experienced at sea level would be expected as a result of the increase of the inhalation, as the partial pressures of the pollutant gases will fall in line with that of oxygen.’ The limit concentrations at flight altitude can therefore be defined using pressure ratios. Annex A provides the formula for calculating allowable concentrations at flight altitude. There are many potential sources of contamination, which could affect the aircraft cabin environment. It would be impractical to set limits for all the chemical constituents of these sources. The presence of marker compounds in concentrations that exceed the cabin air quality comfort, health or safety limits set in the standard may indicate that maintenance, procedural or operational change or design change is required to bring the air quality back within the limits set in this standard. Several sources have been considered to identify contaminants produced during normal operation. The possible sources have been analysed to identify which chemical groupings are related to each one. At least one compound from each grouping identified for each potential source has been chosen as representative of that source.

Aerospace series. Aircraft internal air quality standards, criteria and determination methods

KS W ISO 2046:2009 航空器上呼吸用气态氧的供应

이 표준은 항공기에서 사용되는 호흡용 기체산소의 압력과 특성을 규정하고 일차적으로 제조자에

Gaseous breathing oxygen sopplies for aircraft

SAE AS8057-2008 电气/受压的飞机厨房内部设备的最低设计和性能

1.1 GeneralThis SAE Aerospace Standard (AS) establishes minimum design and performance requirements for galley insert equipment with an electrical and/or pressure system, as well as associated components intended for installation in galleys and other areas (e.g., bars) of transport category airplanes.1.2 Purpose1.2.1 This standard applies to the following equipment intended for installation in galleys and other areas (e.g., bars) within transport category airplanes, such as but not limited to the following:a. Ovens (e.g., convection, steam, induction, microwave, bun warmer, plate warmer)b. Beverage makers (e.g., coffee makers, coffee warmers, water heaters, espresso makers)c. Beverage cups and jugs (so-called hot cups and jugs)d. Self contained refrigeration equipment (e.g., refrigerators, freezers, wine chillers, water coolers, air chillers)e. Trash compactorsf. Rail assembliesg. Associated components, such as oven racks and trays, beverage servers1.2.2 This standard does not:a. Address equipment covered in AS8056 “Minimum Design and Performance of Airplane Galley In-Flight Carts,Containers, and Associated Components”.b. Fully address design details that provide extended service life and continued airworthiness, since these are a functionof: (1) total galley and food/beverage system design, (2) human factors engineering desired by individual operators,(3) techniques of care in servicing, and (4) maintenance philosophy. However, references to these considerations are included as appropriate.c. Fully address requirements that are covered by national aviation regulations, pertinent U.S. Public Health regulations and/or design details, which should be covered by galley operator/airplane manufacturer specifications for the subjectequipment.d. Fully address requirements for equipment utilizing hydraulic systems (e.g., Trash compactors).1.2.3 When the term “equipment” is used in this standard, it refers to all of the items identified in the Purpose（2）unless specifically identified otherwise.1.3 Mandating and Recommendation Phrasesa. “Shall”The word “shall” indicates a mandatory criterion.b. “Should”The word “should” indicates a criterion for which an alternative, including non-compliance, may be applied if it is documented and justified.

Minimum Design and Performance of Airplane Galley Insert Equipment, Electrical/Pressurized

SAE ARP5374A-2008 预处理空气设备的测试方法

This SAE Aerospace Recommended Practice (ARP) applies to Point-Of-Use, Central, and Mobile Pre- Conditioned Air Equipment. It does not apply to aircraft mounted equipment. This document provides a consistent and uniform test method for determining the cooling and/or heating capacity of Pre-Conditioned Air (PCA) equipment.

Method of Testing Pre-Conditioned Air Equipment

SAE AMS3801B-2008 低模数间位芳香族降落伞织物

This specification covers a low modulus meta-aramid in the form of cloth. This product has been used typically for use in construction of parachutes, but usage is not limited to such applications.

Cloth, Parachute - Meta-Aramid, Low Modulus

ASTM F2316-08(2010) 轻型娱乐飞行器机身紧急情况降落伞的标准规范

1.1 This specification covers minimum requirements for the design, manufacture, and installation of parachutes for light sport aircraft. 1.2 The values stated in SI units are to be regarded as standard. There may be values given in parentheses that are mathematical conversions to inch-pound units. Values in parentheses are provided for information only and are not considered standard. 1.2.1 Note that within the aviation community mixed units are appropriate in accordance with International Civil Aviation Organization (ICAO) agreements. While the values stated in SI units are regarded as standard, certain values such as airspeeds in knots and altitude in feet are also accepted as standard. 1.3 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory requirements prior to use.

Standard Specification for Airframe Emergency Parachutes for Light Sport Aircraft

BS ISO 22538-1:2007 航空航天系统.氧气安全性.氧气系统及组件的设计

ISO 22538-1:2007 describes a process for the design of oxygen systems and their components. ISO 22538-1:2007 applies equally to ground support equipment, launch vehicles and spacecraft.

Space systems. Oxygen safety. Design of oxygen systems and components

BS ISO 22538-2:2007 航空航天系统.氧气安全性.氧气系统及组件用金属材料的选择

ISO 22538-2:2007 describes a process for the selection of metallic materials for oxygen systems and their components. ISO 22538-2:2007 applies equally to ground support equipment, launch vehicles and spacecraft.

Space systems. Oxygen safety. Selection of metallic materials for oxygen systems and components

ISO 22538-2:2007 航天系统.氧气安全.第2部分:氧气系统及组件用金属材料的选择

This part of ISO 22538 describes a process for the design of oxygen systems and their components. This part of ISO 22538 applies equally to ground support equipment, launch vehicles and spacecraft.

Space systems - Oxygen safety - Part 2: Selection of metallic materials for oxygen systems and components

ISO 22538-1:2007 航天系统.氧气安全.第1部分:氧气系统及组件的设计

This part of ISO 22538 describes a process for the design of oxygen systems and their components. This part of ISO 22538 applies equally to ground support equipment, launch vehicles and spacecraft.

Space systems - Oxygen safety - Part 1: Design of oxygen systems and components