1、 IEC/TR 62131-2 Edition 1.0 2011-02 TECHNICAL REPORT Environmental conditions Vibration and shock of electrotechnical equipment Part 2: Equipment transported in fixed wing jet aircraft IEC/TR 62131-2:2011(E) colour inside THIS PUBLICATION IS COPYRIGHT PROTECTED Copyright 2011 IEC, Geneva, Switzerlan
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10、1 22 919 03 00 IEC/TR 62131-2 Edition 1.0 2011-02 TECHNICAL REPORT Environmental conditions Vibration and shock of electrotechnical equipment Part 2: Equipment transported in fixed wing jet aircraft INTERNATIONAL ELECTROTECHNICAL COMMISSION W ICS 19.040 PRICE CODE ISBN 978-2-88912-383-4 Registered t
11、rademark of the International Electrotechnical Commission colour inside 2 TR 62131-2 IEC:2011(E) CONTENTS FOREWORD . 4 1 Scope . 6 2 Normative references . 6 3 Data source and quality 7 3.1 Lockheed Tristar KC Mk 1 . 7 3.2 BAe VC10 K 7 3.3 Boeing 747 Combi (freight and passengers) 8 3.4 Supplementar
12、y data 10 3.4.1 McDonnell Douglas DC8 cargo 10 3.4.2 Lockheed C5A (Galaxy), Lockheed C-141 (Starlifter) and Boeing NC- 135 (707) . 10 4 Intra data source comparison . 10 4.1 General remark . 10 4.2 Lockheed Tristar KC Mk 1 . 10 4.2.1 Relative severity of flight conditions . 10 4.2.2 Position within
13、the cargo hold 11 4.2.3 Relative severity of measurement axes 11 4.3 BAe VC10 K 11 4.3.1 Relative severity of flight conditions . 11 4.3.2 Position within the cargo hold 11 4.3.3 Relative severity of measurement axes 12 4.4 Boeing 747 Combi (freight and passengers) 12 4.4.1 Relative severity of meas
14、urement axes 12 4.4.2 Relative severity of flight conditions . 12 5 Inter data source comparison . 12 6 Environmental description 13 6.1 Lockheed Tristar KC Mk 1 . 13 6.2 BAe VC10 K 13 6.3 Boeing 747 Combi (freight and passengers) 13 7 Supplementary data . 13 7.1 McDonnell Douglas DC8 Cargo . 13 7.2
15、 Lockheed C5A (Galaxy), Lockheed C-141 (Starlifter) and Boeing NC-135 (707) . 14 8 Comparison with IEC 60721 . 14 9 Recommendations 15 Bibliography 40 Figure 1 Schematic of Tristar aircraft . 17 Figure 2 Tristar noise measurements . 18 Figure 3 Tristar vibration measurements Take-off, power and roll
16、 . 18 Figure 4 Tristar vibration measurements Low altitude climb 19 Figure 5 Tristar vibration measurements High altitude cruise 19 Figure 6 Tristar vibration measurements Landing 20 Figure 7 Tristar vibration measurements Low altitude decent 20 Figure 8 Tristar vibration measurements C of G Take-of
17、f/climb . 21 TR 62131-2 IEC:2011(E) 3 Figure 9 Tristar vibration measurements Forward take-off/climb 21 Figure 10 Tristar vibration measurements Centre of gravity cruise 22 Figure 11 Tristar vibration measurements Forward cruise . 22 Figure 12 Tristar vibration measurements Centre of gravity landing
18、 23 Figure 13 Tristar vibration measurements Forward landing . 23 Figure 14 Tristar vibration measurements Cruise environment 24 Figure 15 Tristar vibration measurements Take-off/landing environment . 24 Figure 16 Schematic of VC10 aircraft . 25 Figure 17 VC10 vibration measurements Cruise 27 Figure
19、 18 VC10 vibration measurements Maximum airframe severity 27 Figure 19 VC10 vibration measurement Forward container during reverse thrust 28 Figure 20 VC10 vibration measurement Rear container during reverse thrust . 28 Figure 21 VC10 measurements Overlaid worst case spectra . 29 Figure 22 Vibration
20、 Measurements on a pallet in a Boeing 747 Combi aircraft (transducer V1) . 31 Figure 23 Vibration measurements on a pallet in a Boeing 747 Combi aircraft (Transducer V2) 31 Figure 24 DC8 vibration measurements reverse thrust . 32 Figure 25 DC8 vibration measurements acceleration and take-off 33 Figu
21、re 26 DC8 vibration measurements cruise . 33 Figure 27 Foley representation of environment for NC-135, C-141 and C-5A aircraft 34 Figure 28 Foley landing shock environment . 34 Figure 29 Foley test severity for take-off/landing 35 Figure 30 Foley test severity for cruise 36 Figure 31 IEC 60721-3-2 (
22、1997) Stationary vibration random 37 Figure 32 IEC 60721-3-2 (1997) Non-stationary vibration including shock . 37 Figure 33 Test severities ASTM D 4728-91 . 38 Figure 34 Test severities Mil Std 810 issue F and G 38 Figure 35 Test severities AECTP 400 (Edition 2 any IEC National Committee interested
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32、of a different kind from that which is normally published as an International Standard, for example “state of the art“. IEC/TR 62131-2, which is a technical report, has been prepared by IEC technical committee 104: Environmental conditions, classification and methods of test. TR 62131-2 IEC:2011(E)
33、5 The text of this technical report is based on the following documents: Enquiry draft Report on voting 104/507/DTR 104/536/RVC Full information on the voting for the approval of this technical report can be found in the report on voting indicated in the above table. This publication has been drafte
34、d in accordance with the ISO/IEC Directives, Part 2. A list of all the parts in the IEC 62131 series, under the general title Environmental conditions Vibration and shock of electrotechnical equipment, can be found on the IEC website. The committee has decided that the contents of this publication w
35、ill remain unchanged until the stability date indicated on the IEC web site under “http:/webstore.iec.ch“ in the data related to the specific publication. At this date, the publication will be reconfirmed, withdrawn, replaced by a revised edition, or amended. A bilingual version of this standard may
36、 be issued at a later date. IMPORTANT The colour inside logo on the cover page of this publication indicates that it contains colours which are considered to be useful for the correct understanding of its contents. Users should therefore print this document using a colour printer. 6 TR 62131-2 IEC:2
37、011(E) ENVIRONMENTAL CONDITIONS VIBRATION AND SHOCK OF ELECTROTECHNICAL EQUIPMENT Part 2: Equipment transported in fixed wing jet aircraft 1 Scope IEC/TR 62131-2, which is a technical report, reviews the available dynamic data relating to electrotechnical equipment transported in fixed wing jet tran
38、sport aircraft. The intent is that from all the available data an environmental description will be generated and compared to that set out in IEC 60721. For each of the sources identified the quality of the data is reviewed and checked for self consistency. The process used to undertake this check o
39、f data quality and that used to intrinsically categorize the various data sources is set out in IEC/TR 62131-1. This technical report primarily addresses data extracted from a number of different sources for which reasonable confidence exist as to their quality and validity. The report also presents
40、 data for which the quality and validity cannot realistically be reviewed. These data are included to facilitate validation of information from other sources. The report clearly indicates when it utilizes information in this latter category. This technical report addresses data from several differen
41、t transport aircraft 1 . Although one of these aircraft is no longer used commercially, data from it are included to facilitate validation of information from other sources. Relatively little of the data reviewed has been made available in electronic form. To permit comparison, a quantity of the ori
42、ginal (non-electronic) data have been manually digitized in this technical report. 2 Normative references The following referenced documents are indispensable for the application of this document. For dated references, only the edition cited applies. For undated references, the latest edition of the
43、 referenced document (including any amendments) applies. IEC 60721 (all parts), Classification of environmental conditions IEC 60721-3-2:1997, Classification of environmental conditions Part 3: Classification of groups of environmental parameters and their severities Section 2: Transportation _ 1Loc
44、kheed Tristar KC Mk 1, Lockheed Tristar L-1011, BAe VC10 K, Boeing 747 Combi, McDonnel Douglas DC8 Cargo, Lockheed C5A (Galaxy), Lockheed C-141 (Starlifter), Boeing NC-135 (707) are the trade names of products supplied by Lockheed, BAe, McDonnel Douglas and Boeing, respectively. This information is given for the convenience of users of this technical report and does not constitute anendorsement by IEC of the products named.
