{"id":239527,"date":"2024-10-19T15:40:09","date_gmt":"2024-10-19T15:40:09","guid":{"rendered":"https:\/\/pdfstandards.shop\/product\/uncategorized\/bsi-pd-iec-tr-62131-62017\/"},"modified":"2024-10-25T10:22:30","modified_gmt":"2024-10-25T10:22:30","slug":"bsi-pd-iec-tr-62131-62017","status":"publish","type":"product","link":"https:\/\/pdfstandards.shop\/product\/publishers\/bsi\/bsi-pd-iec-tr-62131-62017\/","title":{"rendered":"BSI PD IEC\/TR 62131-6:2017"},"content":{"rendered":"

This part of IEC 62131 reviews the available dynamic data relating to the transportation of electrotechnical equipment. The intent is that from all the available data an environmental description will be generated and compared to that set out in IEC 60721 (all parts)[11] 1<\/sup> .<\/p>\n

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 of data quality and that used to intrinsically categorize the various data sources is set out in IEC TR 62131-1[18].<\/p>\n

This document primarily addresses data extracted from a number of different sources for which reasonable confidence exist in its quality and validity. The report also reviews some data for which the quality and validity cannot realistically be verified. These data are included to facilitate validation of information from other sources. The document clearly indicates when utilizing information in this latter category.<\/p>\n

This document addresses data from a number of data gathering exercises. The quantity and quality of data in these exercises varies considerably as does the range of conditions encompassed.<\/p>\n

Not all of the data reviewed were made available in electronic form. To permit comparison to be made, in this assessment, a quantity of the original (non-electronic) data has been manually digitized.<\/p>\n

PDF Catalog<\/h4>\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n
PDF Pages<\/th>\nPDF Title<\/th>\n<\/tr>\n
2<\/td>\nNational foreword <\/td>\n<\/tr>\n
4<\/td>\nCONTENTS <\/td>\n<\/tr>\n
7<\/td>\nFOREWORD <\/td>\n<\/tr>\n
9<\/td>\n1 Scope
2 Normative references
3 Terms and definitions <\/td>\n<\/tr>\n
10<\/td>\n4 Data source and quality
4.1 Vibration survey of four different propeller driven aircraft <\/td>\n<\/tr>\n
11<\/td>\n4.2 Britten-Norman Islander aircraft flight measurements
Tables
Table 1 \u2013 Record durations and error estimates for measured data for Britten-Norman Islander aircraft flight measurements <\/td>\n<\/tr>\n
12<\/td>\n4.3 Lockheed C130 flight vibration measurements <\/td>\n<\/tr>\n
13<\/td>\nTable 2 \u2013 Record durations and error estimates for measured data for Lockheed C130 flight vibration measurements <\/td>\n<\/tr>\n
14<\/td>\n4.4 Lockheed C130 landing shock measurements
4.5 Supplementary data <\/td>\n<\/tr>\n
16<\/td>\n5 Intra data source comparison
5.1 General
5.2 Vibration survey of four propeller driven aircraft <\/td>\n<\/tr>\n
17<\/td>\n5.3 Britten-Norman Islander aircraft flight measurements <\/td>\n<\/tr>\n
18<\/td>\n5.4 Lockheed C130 flight vibration measurements
5.5 Lockheed C130 landing shock measurements
6 Inter data source comparison <\/td>\n<\/tr>\n
19<\/td>\n7 Environmental description
7.1 Physical sources producing mechanical vibrations <\/td>\n<\/tr>\n
21<\/td>\n7.2 Environmental characteristics and severities
7.3 Derived test severities <\/td>\n<\/tr>\n
22<\/td>\n8 Comparison with IEC 60721 (all parts) <\/td>\n<\/tr>\n
25<\/td>\n9 Recommendations <\/td>\n<\/tr>\n
26<\/td>\nFigures
Figure 1 \u2013 Instrumentation locations for Britten-Norman Islander aircraft [1]
Figure 2 \u2013 Instrumentation locations for BAe Jetstream aircraft [1] <\/td>\n<\/tr>\n
27<\/td>\nFigure 3 \u2013 Instrumentation locations for BAe HS 748 aircraft [1]
Figure 4 \u2013 Instrumentation locations for Lockheed C130 Aircraft Islander [1] <\/td>\n<\/tr>\n
28<\/td>\nFigure 5 \u2013 Comparison of relative overall rms severities for different aircrafts [1] <\/td>\n<\/tr>\n
29<\/td>\nFigure 6 \u2013 Comparison of relative overall rms severities forvarious flight conditions [1] <\/td>\n<\/tr>\n
30<\/td>\nFigure 7 \u2013 Comparison of relative overall rms severities for various locations [1] <\/td>\n<\/tr>\n
31<\/td>\nFigure 8 \u2013 Typical cruise vibration spectrum forBritten-Norman Islander aircraft [1]
Figure 9 \u2013 Typical cruise vibration spectrum forBAe Jetstream aircraft [1] <\/td>\n<\/tr>\n
32<\/td>\nFigure 10 \u2013 Typical cruise vibration spectrum forBAe HS 748 aircraft [1]
Figure 11 \u2013 Typical cruise vibration spectrum forLockheed C130 aircraft [1] <\/td>\n<\/tr>\n
33<\/td>\nFigure 12 \u2013 Britten-Norman Islander vibration at cabinduring cruise [2]
Table 3 \u2013 Overall rms severities for Britten-Norman Islander [2] <\/td>\n<\/tr>\n
34<\/td>\nFigure 13 \u2013 Britten-Norman Islander vibration at plane ofpropeller during take\u00adoff [2]
Figure 14 \u2013 Britten-Norman Islander vibration at middle offuselage during take\u00adoff [2] <\/td>\n<\/tr>\n
35<\/td>\nFigure 15 \u2013 Britten-Norman Islander vibration at middle offuselage during cruise [2]
Figure 16 \u2013 Britten-Norman Islander vibration at rear offuselage during cruise [2] <\/td>\n<\/tr>\n
36<\/td>\nFigure 17 \u2013 Comparison of vibration severities forLockheed C130 \u2013 Take-off [3]
Figure 18 \u2013 Comparison of vibration severities forLockheed C130 \u2013 Climb [3] <\/td>\n<\/tr>\n
37<\/td>\nFigure 19 \u2013 Comparison of vibration severities forLockheed C130 \u2013 Cruise [3]
Figure 20 \u2013 Comparison of vibration severities forLockheed C130 \u2013 Reverse thrust [3] <\/td>\n<\/tr>\n
38<\/td>\nFigure 21 \u2013 Comparison of vibration severities forLockheed C130 at blade passing frequency [3] <\/td>\n<\/tr>\n
39<\/td>\nFigure 22 \u2013 Comparison of vibration severities forLockheed C130 background random overall rms [3] <\/td>\n<\/tr>\n
40<\/td>\nTable 4 \u2013 Overall rms severities for Lockheed C130 \u2013 Flight 3 [3] <\/td>\n<\/tr>\n
41<\/td>\nTable 5 \u2013 Overall rms severities for Lockheed C130 \u2013 Flight 4 [3] <\/td>\n<\/tr>\n
42<\/td>\nFigure 23 \u2013 Lockheed C130 vibration at forward fuselageduring take-off \u2013 Flight 3 [3]
Figure 24 \u2013 Lockheed C130 vibration at forward fuselage(Frame 257) during cruise \u2013 Flight 3 [3] <\/td>\n<\/tr>\n
43<\/td>\nFigure 25 \u2013 Lockheed C130 vibration at forward fuselage(Frame 317) during cruise \u2013 Flight 3 [3]
Figure 26 \u2013 Lockheed C130 vibration at aft fuselageduring cruise \u2013 Flight 3 [3] <\/td>\n<\/tr>\n
44<\/td>\nFigure 27 \u2013 Lockheed C130 vibration at forward fuselageduring landing \u2013 Flight 3 [3]
Figure 28 \u2013 Lockheed C130 vibration at forward fuselageduring take-off \u2013 Flight 4 [3] <\/td>\n<\/tr>\n
45<\/td>\nFigure 29 \u2013 Lockheed C130 vibration at plane of propellerduring take-off \u2013 Flight 4 [3]
Figure 30 \u2013 Lockheed C130 vibration at plane of propellerduring climb \u2013 Flight 4 [3] <\/td>\n<\/tr>\n
46<\/td>\nFigure 31 \u2013 Lockheed C130 vibration at plane of propellerduring cruise \u2013 Flight 4 [3]
Figure 32 \u2013 Lockheed C130 vibration at plane of propellerduring landing \u2013 Flight 4 [3] <\/td>\n<\/tr>\n
47<\/td>\nFigure 33 \u2013 Landing shocks from Lockheed C130 vertical [4]
Figure 34 \u2013 Landing shocks from Lockheed C130 lateral [4] <\/td>\n<\/tr>\n
48<\/td>\nFigure 35 \u2013 Landing shocks from Lockheed C130 longitudinal [4]
Table 6 \u2013 Overall rms severities for Transall C160 [7] <\/td>\n<\/tr>\n
49<\/td>\nFigure 36 \u2013 Transall C160 vibration at fuselage floorduring take-off [7]
Figure 37 \u2013 Transall C160 vibration at fuselage floorduring cruise [7] <\/td>\n<\/tr>\n
50<\/td>\nFigure 38 \u2013 Transall C160 vibration at fuselage floorduring landing [7]
Figure 39 \u2013 Lockheed C130J variant vibration at planeof propeller during cruise <\/td>\n<\/tr>\n
51<\/td>\nFigure 40 \u2013 Airbus A400M vibration on fuselage floorduring cruise conditions
Figure 41 \u2013 IEC\u00a060721-3-2 [13] \u2013 Stationary vibrationrandom severities <\/td>\n<\/tr>\n
52<\/td>\nFigure 42 \u2013 IEC\u00a0TR\u00a060721-4-2 [14] \u2013 Stationary vibrationrandom severities
Figure 43 \u2013 IEC\u00a060721-3-2 [13] \u2013 Stationary vibrationsinusoidal severities <\/td>\n<\/tr>\n
53<\/td>\nFigure 44 \u2013 IEC\u00a0TR\u00a060721-4-2 [14] \u2013 Stationary vibrationsinusoidal severities
Figure 45 \u2013 IEC\u00a060721-3-2 [13] \u2013 Shock severities <\/td>\n<\/tr>\n
54<\/td>\nFigure 46 \u2013 IEC\u00a0TR\u00a060721-4-2 [14] \u2013 Shock severities forIEC\u00a060068-2-29 [17] test procedure
Figure 47 \u2013 IEC\u00a0TR\u00a060721-4-2 [14] \u2013 Shock severities forIEC\u00a060068-2-27 [15] test procedure <\/td>\n<\/tr>\n
55<\/td>\nFigure 48 \u2013 Comparison of four propeller aircraft vibrations [1]with IEC\u00a060721-3-2 [13]
Figure 49 \u2013 Comparison of Britten-Norman Islander aircraftvibrations [1] with IEC\u00a060721\u00ad3\u00ad2 [13] <\/td>\n<\/tr>\n
56<\/td>\nFigure 50 \u2013 Comparison of Lockheed C130 aircraftvibrations [3] with IEC\u00a060721-3-2 [13]
Figure 51 \u2013 Comparison of Transall C160 aircraftvibrations [7] with IEC\u00a060721-3-2 [13] <\/td>\n<\/tr>\n
57<\/td>\nFigure 52 \u2013 Comparison of Britten-Norman Islander aircraftcruise vibrations [1] with IEC\u00a060721-3-2 [13]
Figure 53 \u2013 Comparison of Britten-Norman Islander aircrafttake-off\/landing vibrations [1] with IEC\u00a060721-3-2 [13] <\/td>\n<\/tr>\n
58<\/td>\nFigure 54 \u2013 Comparison of Lockheed C130 aircraft cruisevibrations [3] with IEC\u00a060721\u00ad3-2 [13]
Figure 55 \u2013 Comparison of Lockheed C130 aircraft take-off\/landing vibrations [3] with IEC\u00a060721-3-2 [13] <\/td>\n<\/tr>\n
59<\/td>\nFigure 56 \u2013 Comparison of Lockheed C130J variant cruisevibrations with IEC\u00a060721\u00ad3-2 [13]
Figure 57 \u2013 Comparison of Airbus A400M cruise vibrationswith IEC\u00a060721\u00ad3-2 [13] <\/td>\n<\/tr>\n
60<\/td>\nFigure 58 \u2013 Comparison of Lockheed C130 landing shocks [4]with IEC\u00a060721-3-2 [13] <\/td>\n<\/tr>\n
61<\/td>\nBibliography <\/td>\n<\/tr>\n<\/table>\n","protected":false},"excerpt":{"rendered":"

Environmental conditions. Vibration and shock of electrotechnical equipment – Transportation by propeller aircraft<\/b><\/p>\n\n\n\n\n
Published By<\/td>\nPublication Date<\/td>\nNumber of Pages<\/td>\n<\/tr>\n
BSI<\/b><\/a><\/td>\n2017<\/td>\n64<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n","protected":false},"featured_media":239532,"template":"","meta":{"rank_math_lock_modified_date":false,"ep_exclude_from_search":false},"product_cat":[2641],"product_tag":[],"class_list":{"0":"post-239527","1":"product","2":"type-product","3":"status-publish","4":"has-post-thumbnail","6":"product_cat-bsi","8":"first","9":"instock","10":"sold-individually","11":"shipping-taxable","12":"purchasable","13":"product-type-simple"},"_links":{"self":[{"href":"https:\/\/pdfstandards.shop\/wp-json\/wp\/v2\/product\/239527","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/pdfstandards.shop\/wp-json\/wp\/v2\/product"}],"about":[{"href":"https:\/\/pdfstandards.shop\/wp-json\/wp\/v2\/types\/product"}],"wp:featuredmedia":[{"embeddable":true,"href":"https:\/\/pdfstandards.shop\/wp-json\/wp\/v2\/media\/239532"}],"wp:attachment":[{"href":"https:\/\/pdfstandards.shop\/wp-json\/wp\/v2\/media?parent=239527"}],"wp:term":[{"taxonomy":"product_cat","embeddable":true,"href":"https:\/\/pdfstandards.shop\/wp-json\/wp\/v2\/product_cat?post=239527"},{"taxonomy":"product_tag","embeddable":true,"href":"https:\/\/pdfstandards.shop\/wp-json\/wp\/v2\/product_tag?post=239527"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}