BS ISO 9206-2016 Aerospace series Constant displacement hydraulic motors General specifications《航空航天系列 恒流量液压马达 一般规范 》.pdf

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1、BSI Standards Publication BS ISO 9206:2016 Aerospace series Constant displacement hydraulic motors General specificationsBS ISO 9206:2016 BRITISH STANDARD National foreword This British Standard is the UK implementation of ISO 9206:2016. It supersedes BS ISO 12333:2000 which is withdrawn. The UK par

2、ticipation in its preparation was entrusted to Technical Committee ACE/69, Aerospace hydraulic systems, fluids and com- ponents. 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 provision

3、s of a contract. Users are responsible for its correct application. The British Standards Institution 2016. Published by BSI Standards Limited 2016 ISBN 978 0 580 82185 1 ICS 49.080 Compliance with a British Standard cannot confer immunity from legal obligations. This British Standard was published

4、under the authority of the Standards Policy and Strategy Committee on 31 March 2016. Amendments issued since publication Date Text affectedBS ISO 9206:2016 ISO 2016 Aerospace series Constant displacement hydraulic motors General specifications Srie arospatiale Moteurs hydrauliques cylindre fixe Spci

5、fications gnrales INTERNATIONAL STANDARD ISO 9206 Second edition 2016-03-01 Reference number ISO 9206:2016(E)BS ISO 9206:2016ISO 9206:2016(E)ii ISO 2016 All rights reserved COPYRIGHT PROTECTED DOCUMENT ISO 2016, Published in Switzerland All rights reserved. Unless otherwise specified, no part of thi

6、s publication may be reproduced or utilized otherwise in any form or by any means, electronic or 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 th

7、e country of the requester. ISO copyright office Ch. de Blandonnet 8 CP 401 CH-1214 Vernier, Geneva, Switzerland Tel. +41 22 749 01 11 Fax +41 22 749 09 47 copyrightiso.org www.iso.orgBS ISO 9206:2016ISO 9206:2016(E)Foreword vi 1 Scope . 1 2 Normative references 1 3 Terms and definitions . 2 4 Class

8、ification 6 5 General requirements . 6 5.1 Order of precedence . 6 5.2 Hydraulic system characteristics 6 5.3 Airworthiness regulations 6 5.4 Qualification 6 6 Functional requirements . 7 6.1 Hydraulic fluid . 7 6.2 Pressures 7 6.2.1 Rated supply pressure. 7 6.2.2 Rated differential pressure . 7 6.2

9、.3 No-load break-out pressure . 7 6.2.4 Motor return port pressure 7 6.2.5 Case port pressure 7 6.3 Flows 8 6.3.1 Rated consumption 8 6.3.2 Case drain flow 8 6.3.3 Shaft seal leakage flow 8 6.3.4 External leakage . 8 6.4 Speed and direction of rotation 9 6.4.1 Speed 9 6.5 Torque . 9 6.5.1 Rated torq

10、ue 9 6.5.2 Break-out torque 9 6.5.3 Stalling torque 9 6.5.4 Torque pulsations . 9 6.6 Motor overall efficiency 11 6.7 Dynamic characteristics .12 6.7.1 General.12 6.7.2 Dynamic braking .12 6.7.3 Rapid reversals .12 6.8 Passive operation .12 6.9 Rated temperature 12 6.10 Acoustic noise level 12 6.11

11、Rated endurance .12 6.12 Environmental requirements 13 7 Detail design requirements .13 7.1 Dimensionally critical components 13 7.2 Maintainability features .13 7.3 Seals .14 7.4 Lubrication 14 7.5 Balance 14 7.6 Self-contained failure .14 7.7 Safety wire sealing 14 7.8 Electro-conductive bonding 1

12、4 7.9 Marking 14 7.9.1 Nameplate .14 7.9.2 Fluid identification 15 ISO 2016 All rights reserved iii Contents PageBS ISO 9206:2016ISO 9206:2016(E)7.9.3 Ports .15 8 Strength requirements 15 8.1 General 15 8.2 Proof pressure 15 8.2.1 Motor case 15 8.2.2 Motor inlet port .15 8.2.3 Motor return port .15

13、8.3 Ultimate pressure 16 8.3.1 Motor case 16 8.3.2 Motor inlet port .16 8.3.3 Motor return port .16 8.4 Pressure impulse (fatigue) 16 8.5 Port strength 16 9 Construction requirements 16 9.1 Materials 16 9.1.1 General.16 9.1.2 Metals .17 9.2 Corrosion protection .17 9.2.1 General.17 9.2.2 Ferrous and

14、 copper alloys 17 9.2.3 Aluminium alloys 18 9.3 Castings 18 10 Installation requirements18 10.1 Dimensions 18 10.2 Mass .18 10.3 Mounting .18 10.4 Orientation 19 10.5 Drive shaft 19 10.6 Ports 19 11 Maintenance requirements 19 11.1 Maintenance concept 19 11.2 Service life limitations and storage spe

15、cifications 19 12 Reliability requirements .20 12.1 Equipment compliance .20 12.2 Requirements 20 13 Quality assurance provisions .20 13.1 Responsibility for inspection .20 13.2 Classification of tests 20 13.3 Test stand requirements 20 14 Acceptance tests .21 14.1 General 21 14.2 Examination of the

16、 product 21 14.3 Test programme 21 14.3.1 General.21 14.3.2 External leakage requirements 22 14.3.3 Break-in run 22 14.3.4 Proof pressure and overspeed tests .22 14.3.5 Operational tests at rated conditions 22 14.3.6 Break-out torque test 23 14.3.7 Teardown inspection examination 23 14.3.8 Run-in .2

17、3 14.3.9 Performance data .23 14.3.10 Fluid contamination test 24 14.3.11 Electro-conductive bonding 25 14.4 Storage and packaging .25 iv ISO 2016 All rights reservedBS ISO 9206:2016ISO 9206:2016(E)15 Qualification procedures 25 15.1 General 25 15.2 Qualification procedure 25 15.2.1 Qualification by

18、 analogy .25 15.2.2 Motor qualification test report .25 15.2.3 Samples and program of qualification tests 25 15.3 Qualification testing 26 15.3.1 Dimensional check 26 15.3.2 Expanded envelope acceptance tests 26 15.3.3 Overspeed test 27 15.3.4 Operational test at overpressure 27 15.3.5 Calibration 2

19、7 15.3.6 Endurance testing 28 15.3.7 Environmental tests .31 15.3.8 Structural tests .32 15.3.9 Supplementary tests 33 Bibliography .34 ISO 2016 All rights reserved vBS ISO 9206:2016ISO 9206:2016(E) Foreword ISO (the International Organization for Standardization) is a worldwide federation of nation

20、al standards bodies (ISO member bodies). The work of preparing International Standards is normally carried out through ISO technical 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. Internatio

21、nal organizations, governmental and non-governmental, in liaison with ISO, also take part in the work. ISO collaborates closely with the International Electrotechnical Commission (IEC) on all matters of electrotechnical standardization. The procedures used to develop this document and those intended

22、 for its further maintenance are described in the ISO/IEC Directives, Part 1. In particular the different approval criteria needed 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

23、.org/directives). Attention is drawn to the possibility that some of the elements of this document may be the subject of patent 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

24、 be in the Introduction and/or on the ISO list of patent declarations received (see www.iso.org/patents). Any trade name used 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 express

25、ions related to conformity assessment, as well as information about ISOs adherence to the WTO principles in the Technical Barriers to Trade (TBT) see the following URL: Foreword - Supplementary information The committee responsible for this document is ISO/TC 20, Aircraft and space vehicles, Subcomm

26、ittee SC 10, Aerospace fluid systems and components. This second edition cancels and replaces the first edition (ISO 9206:1990) and ISO 12333:2000. The entire document has been rewritten and it incorporates requirements from ISO 12333:2000.vi ISO 2016 All rights reservedBS ISO 9206:2016INTERNATIONAL

27、 ST ANDARD ISO 9206:2016(E) Aerospace series Constant displacement hydraulic motors General specifications 1 Scope This International Standard establishes the general requirements for constant displacement hydraulic motors, suitable for use in aircraft hydraulic systems at pressures up to 35 000 kPa

28、 (5 000 psi). Primary and secondary function motors (see Clause 4) are covered in this International Standard; however, actuators with internal rotation angle limits and low-speed motors are not covered. This International Standard is to be used in conjunction with the detail specification that is p

29、articular to each application. 2 Normative references The 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 cited applies. For undated references, the latest edition of the reference

30、d document (including any amendments) applies. ISO 2093, Electroplated coatings of tin Specification and test methods ISO 2669, Environmental tests for aircraft equipment Steady-state acceleration ISO 2671, Environmental tests for aircraft equipment Part 3.4 : Acoustic vibration ISO 2685, Aircraft E

31、nvironmental test procedure for airborne equipment Resistance to fire in designated fire zones ISO 3323, Aircraft Hydraulic components Marking to indicate fluid for which component is approved ISO 3601-1:2012, Fluid power systems O-rings Part 1: Inside diameters, cross-sections, tolerances and desig

32、nation codes ISO 7137, Aircraft Environmental conditions and test procedures for airborne equipment ISO 7320, Aerospace Couplings, threaded and sealed, for fluid systems Dimensions ISO 8078, Aerospace process Anodic treatment of aluminium alloys Sulfuric acid process, undyed coating ISO 8079, Aerosp

33、ace process Anodic treatment of aluminium alloys Sulfuric acid process, dyed coating ISO 8081, Aerospace process Chemical conversion coating for aluminium alloys General purpose ISO 8399-1, Aerospace Accessory drives and mounting flanges (Metric series) Part 1: Design criteria ISO 8399-2, Aerospace

34、Accessory drives and mounting flanges (Metric series) Part 2: Dimensions ISO 8625-1, Aerospace Fluid systems Vocabulary Part 1: General terms and definitions related to pressure ISO 8625-2, Aerospace Fluid systems Vocabulary Part 2: General terms and definitions relating to flow ISO 8625-3, Aerospac

35、e Fluid systems Vocabulary Part 3: General terms and definitions relating to temperature ISO 2016 All rights reserved 1BS ISO 9206:2016ISO 9206:2016(E) ISO 11218: 1) , Aerospace Cleanliness classification for hydraulic fluids 3 Terms and definitions For the purposes of this document, the terms and d

36、efinitions given in ISO 8625-1, ISO 8625-2, ISO 8625-3, and the following apply. 3.1 fixed displacement hydraulic motor mechanical actuator that converts hydraulic pressure and flow into torque and angular displacement (rotation) 3.2 purchaser organization that has the engineering responsibility for

37、 the hydraulic system that includes the motor Note 1 to entry: Typically, the purchaser is an aircraft manufacturer, an equipment manufacturer that has the actuation system responsibility or a modification centre. Note 2 to entry: The purchaser is responsible for the compilation of the detail specif

38、ication. 3.3 detail specification document compiled by the purchaser (3.2) that specifies the following: a) technical requirements; b) acceptance and qualification test requirements; c) reliability requirements; d) quality requirements; e) packaging requirements; f) other requirements 3.4 supplier o

39、rganization that provides the motor Note 1 to entry: Typically, the supplier is the manufacturer of the motor who will be responsible for the design, production, and qualification of the motor 3.5 ports of the hydraulic motor3.5.1 motor inlet port port that receives flow from the hydraulic system to

40、 supply the motor 3.5.2 motor return port port that returns flow back to the system 3.5.3 motor case drain port port that drains internal leakage flow to the reservoir 1) To be published. (Revision of ISO 11218:1993)2 ISO 2016 All rights reservedBS ISO 9206:2016ISO 9206:2016(E) 3.5.4 shaft seal port

41、 port that routes any shaft seal leakage from the motor to an overboard drain, collector tank, etc. 3.6 temperature terms3.6.1 rated temperature maximum continuous temperature of the fluid to be supplied at the inlet port of the motor Note 1 to entry: It is expressed in degrees centigrade. 3.6.2 min

42、imum continuous temperature minimum temperature of the fluid to be continuously supplied at the supply port of the motor Note 1 to entry: It is expressed in degrees centigrade. Note 2 to entry: This temperature is generally higher than the survival temperature. 3.7 pressure terms3.7.1 design operati

43、ng pressure normal maximum steady pressure Note 1 to entry: Excluded are reasonable tolerances, transient pressure effects such as may arise from the following: pressure ripple; reactions to system functioning; demands that may affect fatigue. 3.7.2 rated supply pressure system rated pressure, which

44、 is normally the hydraulic power generation system design operating pressure (3.7.1) 3.7.3 rated differential pressure differential pressure measured between the motor inlet and outlet ports required to produce rated torque (3.11.1) 3.7.4 no-load break-out pressure differential pressure required for

45、 starting the output shaft, without interruption, with the case drain port at the rated return pressure 3.7.5 motor return pressure3.7.5.1 nominal motor return pressure pressure generated at the return port as the motor returns flow back to the system ISO 2016 All rights reserved 3BS ISO 9206:2016IS

46、O 9206:2016(E) 3.7.5.2 rated motor return pressure maximum pressure at the return port Note 1 to entry: This is applicable to uni-directional motors only. Note 2 to entry: This is a stressing term only as the nominal motor pressure is generally considerably less than the rated motor return pressure.

47、 3.7.6 case drain pressure3.7.6.1 rated case drain pressure nominal pressure at which the motor case is required to operate continuously in the system 3.7.6.2 maximum case pressure maximum of either the maximum pressure peak that may be imposed by the hydraulic system on the motor case drain port (3

48、.5.3), or the pressure resulting from integral bypassing of the rated flow towards the outlet and drain ports in order to take into account the accidental transitory separation of the components 3.8 rated consumption flow rate measured at the motor inlet port (3.5.1) under conditions of the followin

49、g: rated fluid temperature; rated differential pressure (3.7.3); rated speed (3.10.1); using the hydraulic fluid specified in the detail specification (3.3) 3.9 rated displacement maximum theoretical volume of fluid generated by one revolution of its output shaft Note 1 to entry: It shall be expressed in cubic centimetres per revolution (cubic inches per revolution). Note 2 to entry: The rated displacement shall be calculated from the geometrical