BS ISO 11077-2014 Aircraft ground equipment De-icers Functional requirements《航空器地面设备 除冰器 功能要求》.pdf

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1、BSI Standards PublicationBS ISO 11077:2014Aircraft ground equipment De-icers Functional r e q u i r e mentsBS ISO 11077:2014 BRITISH STANDARDNational forewordThis British Standard is the UK implementation of ISO 11077:2014. It supersedes BS M 77:1994 which is withdrawn.The UK participation in its pr

2、eparation was entrusted to Technical Committee ACE/57, Air cargo and ground support equipment.A list of organizations represented on this committee can be obtained on request to its secretary.This publication does not purport to include all the necessary provisions of a contract. Users are responsib

3、le for its correct application. The British Standards Institution 2014.Published by BSI Standards Limited 2014ISBN 978 0 580 80628 5ICS 49.100Compliance with a British Standard cannot confer immunity from legal obligations.This British Standard was published under the authority of the Standards Poli

4、cy and Strategy Committee on 31 May 2014.Amendments/corrigenda issued since publicationDate Text affectedBS ISO 11077:2014 ISO 2014Aircraft ground equipment De-icers Functional requirementsMatriel au sol pour aronefs Dgivreuses Exigences fonctionnellesINTERNATIONAL STANDARDISO11077Second edition2014

5、-06-01Reference numberISO 11077:2014(E)BS ISO 11077:2014ISO 11077:2014(E)ii ISO 2014 All rights reservedCOPYRIGHT PROTECTED DOCUMENT ISO 2014All rights reserved. Unless otherwise specified, no part of this publication may be reproduced or utilized otherwise in any form or by any means, electronic or

6、 mechanical, including photocopying, or posting on the internet or an intranet, without prior written permission. Permission can be requested from either ISO at the address below or ISOs member body in the country of the requester.ISO copyright officeCase postale 56 CH-1211 Geneva 20Tel. + 41 22 749

7、 01 11Fax + 41 22 749 09 47E-mail copyrightiso.orgWeb www.iso.orgPublished in SwitzerlandBS ISO 11077:2014ISO 11077:2014(E) ISO 2014 All rights reserved iiiContents PageForeword ivIntroduction v1 Scope . 12 Normative references 13 Terms and definitions . 24 Requirements 24.1 General . 24.2 Functions

8、 34.3 Vehicle. 44.4 Aerial device 54.5 Fluids system 64.6 Controls . 64.7 Mobility and stability . 74.8 Personnel protection . 84.9 Emergency 85 Information for use 95.1 Manufacturers instructions 95.2 Markings . 96 Options 96.1 General . 96.2 Fluid heater 96.3 Fluid mixing system . 106.4 Spraying b

9、oom . 106.5 Fire extinguishing system . 106.6 One person operation 107 Quality assurance .107.1 Manufacturers quality assurance . 107.2 Users quality assurance 11Annex A (informative) Toxicological aspects of using de-icing/anti-icing equipment12Annex B (informative) Environmental aspect of de-icing

10、/anti-icing at airports 16Bibliography .21BS ISO 11077:2014ISO 11077:2014(E)ForewordISO (the International Organization for Standardization) is a worldwide federation of national standards bodies (ISO member bodies). The work of preparing International Standards is normally carried out through ISO t

11、echnical committees. Each member body interested in a subject for which a technical committee has been established has the right to be represented on that committee. International organizations, governmental and non-governmental, in liaison with ISO, also take part in the work. ISO collaborates clos

12、ely with the International Electrotechnical Commission (IEC) on all matters of electrotechnical standardization.The procedures used to develop this document and those intended for its further maintenance are described in the ISO/IEC Directives, Part 1. In particular the different approval criteria n

13、eeded for the different types of ISO documents should be noted. This document was drafted in accordance with the editorial rules of the ISO/IEC Directives, Part 2 (see www.iso.org/directives). Attention is drawn to the possibility that some of the elements of this document may be the subject of pate

14、nt rights. ISO shall not be held responsible for identifying any or all such patent rights. Details of any patent rights identified during the development of the document will be in the Introduction and/or on the ISO list of patent declarations received (see www.iso.org/patents). Any trade name used

15、 in this document is information given for the convenience of users and does not constitute an endorsement.For an explanation on the meaning of ISO specific terms and expressions related to conformity assessment, as well as information about ISOs adherence to the WTO principles in the Technical Barr

16、iers to Trade (TBT) see the following URL: Foreword - Supplementary informationThe committee responsible for this document is ISO/TC 20, Aircraft and space vehicles, Subcommittee SC 9, Air cargo and ground equipment.This second edition cancels and replaces the first edition (ISO 11077:1993),which ha

17、s been technically revised.iv ISO 2014 All rights reservedBS ISO 11077:2014ISO 11077:2014(E)IntroductionThis International Standard specifies the functional and personnel safety requirements to be taken into account by manufacturers for the design of aircraft de-icing and anti-icing vehicles (de-ice

18、rs).The requirements of this International Standard were determined based on generally recognized assumptions as toa) the normally intended use of aircraft ground support equipment on the ramp of international civil airports in order to handle, service, or maintain civil transport aircraft, orb) the

19、 environmental (surface, slope, weather, lighting, operating rules, staff qualification, etc.) conditions prevailing on the ramp area of the majority of international civil airports. In addition to customary environment conditions in this context, it is to be assumed that de-icers will be operated o

20、n snowy, icy, muddy, or slushed ramp surfaces and under freezing precipitation conditions.It is assumed that the manufacturers of de-icers define in the relevant documentation the specifically intended conditions of use and environment for their equipment, and the purchasers systematically review th

21、eir own specific conditions of use and environment in order to determine whether those stated are adequate or negotiate with the manufacturer appropriate modifications to ensure they are.NOTE Negotiation between manufacturer and purchaser/user is considered essential to establish or verify the adequ

22、ate conditions of use and design parameters.The requirements of this International Standard are expressed in the applicable SI units, with approximate inch-pound unit conversion between brackets for convenience in those countries using that system. Where it is deemed necessary to use exact values, t

23、he SI unit ones are to be used. ISO 2014 All rights reserved vBS ISO 11077:2014BS ISO 11077:2014Aircraft ground equipment De-icers Functional requirements1 ScopeThis International Standard specifies the general functional, performance, and safety requirements for a self-propelled vehicle equipped wi

24、th a boom type aerial device and aircraft de-icing/anti-icing fluid (ADF) spraying systems, hereinafter designated as “de-icer”.This International Standard does not specify a comprehensive set of technical design criteria for aircraft de-icing/anti-icing vehicles, but only those relating to the main

25、 functional, safety, and performance requirements.This International Standard is not applicable to stationary equipment, e.g. gantries, cranes, used to perform de-icing/anti-icing operations on aircraft.Throughout this International Standard, the minimum essential criteria are identified by use of t

26、he key word “shall”. Recommended criteria are identified by use of the key word “should” and, while not mandatory, are considered to be of primary importance in providing safe, economical, and usable aircraft de-icers. Deviation from recommended criteria should only occur after careful consideration

27、 and thorough service evaluation have shown alternate methods to provide an equivalent level of safety.2 Normative referencesThe following documents, in whole or in part, are normatively referenced in this document and are indispensable for its application. For dated references, only the edition cit

28、ed applies. For undated references, the latest edition of the referenced document (including any amendments) applies.ISO 6966-1, Aircraft ground equipment Basic requirements Part 1: General design requirementsISO 6966-2, Aircraft ground equipment Basic requirements Part 2: Safety requirementsISO 700

29、0, Graphical symbols for use on equipment Registered symbolsISO 10254, Air cargo and ground equipment VocabularyISO 11075, Aircraft De-icing/anti-icing fluids ISO type IISO 11076, Aircraft De-icing/anti-icing methods on the groundISO 11078, Aircraft De-icing/anti-icing fluids ISO types II, III and I

30、VISO 11532, Aircraft ground equipment Graphical symbolsISO 13849-1, Safety of machinery Safety-related parts of control systems Part 1: General principles for designEN 1915-2, Aircraft ground support equipment General requirements Part 2: Stability and strength requirements, calculations and test me

31、thodsEN 12312-6, Aircraft ground support equipment Specific requirements Part 6: De-icers and de-icing/anti-icing equipmentDIN 51130:2010, Testing of floor coverings Determination of the anti-slip property Workrooms and fields of activities with slip danger, walking method Ramp testINTERNATIONAL STA

32、NDARD ISO 11077:2014(E) ISO 2014 All rights reserved 1BS ISO 11077:2014ISO 11077:2014(E)NOTE DIN 51130 can be obtained from Deutsches Institut fr Normen, Burggrafenstrasse 6, D-10787 Berlin, Germany.3 Terms and definitionsFor the purposes of this document, the terms and definitions given in ISO 1025

33、4 and the following apply.3.1de-icerself-propelled mobile unit, used to perform de-icing or anti-icing operations by means of fluids spraying on aircraft on the groundNote 1 to entry: It is fitted with an operator cabin or basket mounted on a boom in order to raise the operator at the height of airc

34、raft surfaces to be sprayed.3.2driverperson located in the cabin (driving station) of a de-icers chassis and driving the vehicle around the aircraft3.3operatorperson(s) located in the boom mounted operators cabin or basket, operating its movements relative to the de-icers chassis as well as the flui

35、d spraying system(s)3.4cabin (operators)completely enclosed work station at the end of the de-icers boom, where the operator is located to perform de-icing/anti-icing operations on the aircraft3.5basket (operators)non-enclosed work station at the end of the boom where the operator stands alternative

36、ly to a cabin3.6boomstructural element supporting the operators cabin or basket at a heightNote 1 to entry: Not to be mistaken for “spraying boom”, an element extending from the operators station to support spraying hoses and brings the nozzles as close as possible to the aircraft being de-iced, whi

37、ch does not support persons.4 Requirements4.1 General4.1.1 The de-icers design and construction shall meet the applicable requirements of ISO 6966-1 and ISO 6966-2, and the requirements stated hereafter. Where these requirements are in excess of those in the general aircraft ground equipment standar

38、ds, they shall take precedence.NOTE For operation in Europe, the EU Machinery Directive essential safety requirements legally apply. They can be met by complying with the requirements of the following European Standards (see Clause 2 and Bibliography): EN 1915-1, Aircraft ground support equipment Ge

39、neral requirements Part 1: Basic safety requirements EN 1915-2, Aircraft ground support equipment General requirements Part 2: Stability and strength requirements, calculations and test methods2 ISO 2014 All rights reservedBS ISO 11077:2014ISO 11077:2014(E) EN 1915-3, Aircraft ground support equipme

40、nt General requirements Part 3: Vibration measurement methods and reduction EN 1915-4, Aircraft ground support equipment General requirements Part 4: Noise measurement methods and reduction EN 12312-6, Aircraft ground support equipment General requirements Part 6: De-icers and de-icing equipment4.1.

41、2 The de-icers structural strength shall meet the applicable stability and strength requirements of EN 1915-2 and EN 12312-6 and be demonstrated by testing in accordance with them.4.1.3 Particular attention shall be paid to the fatigue strength requirements for the boom and attachments thereto, whic

42、h shall be based on minimum 2 104stress cycles or 10 000 h operating life expectancy, whichever is highest.NOTE Consultation between manufacturer and purchaser is required to substantiate a realistic life expectancy, stress cycle definition, and fatigue spectrum.4.1.4 The de-icer and all associated

43、systems shall be designed and constructed to operate satisfactorily between temperatures of 30 C and 50 C (20 F and 120 F) and in continuous relative humidity of up to 95 % or as stipulated between purchaser and manufacturer.NOTE Lower temperatures, requiring special design and operating measures, c

44、an be agreed between manufacturer and purchaser. See Note in the Introduction.4.2 Functions4.2.1 The primary function of the de-icer shall be to apply heated de-icing/anti-icing fluid from a variable height boom to the surfaces of stationary aircraft while traversing their perimeter. A hose shall al

45、so be fitted for ground use. The vehicle shall be acceptable for use around terminal gate areas, airport service roads, and aircraft service ramps.NOTE A secondary function can also be to provide access when required to high elevation parts of the aircraft.4.2.2 The maximum width and overall height

46、with the boom in the stowed position shall be kept to a minimum. The maximum overall width should be minimum compatible with stability objectives, and the overall height in the stowed position shall not exceed 4,0 m (13 ft, 1 in). Overall turning radius in this position should not exceed 12 m (40 ft

47、), though maximum possible manoeuvrability is recommended.NOTE Over the road regulations in a majority of states allow a maximum width of 2,5 m (8 ft 2 1/2 in). A number of states allow 2,6 m (8 ft) width. Conversely, some local road traffic regulations can require narrower widths. Depending on the

48、airport of use, a lower height can also be necessary. See Note in the Introduction.4.2.3 On an appropriate self-propelled chassis with an enclosed drivers cabin, meeting the requirements of 4.3, the de-icer shall providea) an aerial device with operators cabin or basket, including safe access means

49、from the ground in the stowed position, meeting the requirements of 4.4,b) (a) fluid storage and supply tank(s), large enough to accommodate the fluid capacity necessary for servicing standard-body and/or wide-body or large capacity aircraft as required by the purchaser, meeting the requirements of 4.5.2, andc) fluid pumping systems for applying heated de-icing fluid and heated or unheated anti-icing fluid to aircraft surfaces, meeting the requirements o