AECMA CTI 81 11760-1980 Report on Aircraft Weight Terms and Definitions《飞机重量术语和定义的报告》.pdf
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1、88, Boulevard Malesherbes, 75008 PARIS Tlphone : 563.82.85 I Telex : 210311 F PUBLI CODE 731 I 9 I Rapport sur la ( Masse des avions : terminologie et dfinitions 1) Report on ( Aircraft weight terms and definitions ) Bericht ber ( Gewichtsbegriffe -und Definitionen bei Flugzeugen ) .- -. 5 -, - - z
2、- -. RECOMMANDATION No : CT1181111760 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-THIS DOCUMENT IS FILMED IN THE ENGLISH LANGUAGE VERSION ONLY. THE
3、 ORIGINAL PAGE NUMBERS ARE DISCONTINUOUS. FOR THIS REASON O Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-.-. . REPORT on “AIRCRAFT WEIGHT TERMS AND
4、DEFINITIONS“ I BERICHT ber “GEWICHTSBEGRIFFE UND DEFINITIONEN BEI FLUGZEUGEN RAPPORT SUR LA “WEE DES AVIONS : TERlINOLIE Ei DEFIMITIiiS“ Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permi
5、tted without license from IHS-,-,-June 1980 CONTENTS I. I ntroducti on I II, Compari sons 1. Tabu1 ated comparison of the weight standards a) in the respective original language b) in English language c) in German language - Nor FIAHED d) in French language - Nya T FrcFic 3 2. Definition of the stan
6、dards associated with the tabulated comparison a) b) in English language in the respective original language c) in German language- Alor FILfiED d) in French language- FILIEP 3. Detailed Comparison 3.1 Comparison of weight standards MIL-STD-1374 with AIR 2001/C a) in English language b) in German la
7、nguage- dor c) in French language- rror rzIng3 3.2 Comparison of weight standards MIL-STD-1374 A with DIN 9020 a) in English language b) in German language- do7 ILHSP c) in French language- FtflEa. . 4 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under li
8、cense with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MARCH 1981 I. INTRODUCTION The present recommendation is the recul t of the working group “Aircraft Weight and Definitions which was founded by the “Commission Technique et Industrielle“ of the AECMA a
9、nd includes broad and detail comparisons in tabular forni of the following standards : German standard : DIN 9020 Edition 1978 Eng1 ish standard : AvNin Form 2492 Edition 1964 French standard : AIR 2001/C Edition 1962 USA standard : MIL-STD-1374 A Edition 1977 ATA 100 Edition 1974 The recommendation
10、 has the short term objective of simplifying the compari son between different weight standards and therefore faci 1 i tating international co-operation on common programmes. This aim was achieved by interpretation of the differences between individual weight standard by weights experts from the cou
11、ntry of origin of the national standards. Thus errors due to linguistic misinterpretation, which may have been included in unofficial weight comparisons used so far, have been eliminated. Additionally the classification of the comparisons has been standardised. In the long run.the European Industry
12、should be encouraged, in the opinion of all the working group members, to formulate a common standard of weight terms and definitions. Furthermore, the intensive work with these standards has contributed to the fact that mutual understanding has been significantly improved. Referring to Great Britai
13、n and Germany, where the national standards are currently being revised, co-operation in this work has resulted in a German represen- tative on the British Committee and British Expert in the German Committee. This will lead to an ajustment of standards and result in a considerable step forward towa
14、rds a European Standard. It is proposed that AECNA will periodically review the need to update this recommendation in the light of any changes that have occurred. In order to facilitate this task National Associations are requested to inform AECMA of any future changes to their Nati onal Weight Stan
15、dards. ! 5 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AECMA CTI/B1/L1760 80 m 1012311 OOOOq28 . 5 II. COMPARISONS VERGLEICHE COMPARAISONS 7 Copyri
16、ght Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-1. TABULATED COMPARISON OF THE WEIGHT STANDARDS TABELLARISCHER VERGLEICH DER GEWICHTSNORMEN COMPARAISON DES N
17、ORMES SOUS FORME DE TABLEAU 8 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-1. Tabulated comparison of the weight standards Concerning the following
18、tables in English it has to be underlined that the national standards have been literally translated and therefore they are not necessarily identical e.g. weight empty (MIL-STD-1374 A) is not identical with weight empty (AIR 2001/C). Furthermore we would like to state that it is always to be underst
19、ood mass by weight and not force. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AECMA CTI/1/117bO 0 M 1012311 OOOOL131 5 I 1. a) IN THE RESPECTIVE OR
20、IGINAL LANGUAGE IN DER JEWEILIGEN ORIGINALSPRACHE EN LANGUE DU PAYS .CONCERNE Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,- - AECMA CTI/BL/L17bO ATA
21、 100 (1974) Structure powerpl ant f urni s hi ngs sys terns + other items of equipment that are an integral part of a particular aircraft configuration. (it is essentially a iidryII weight, including only those fluids, contained in closed systems). Unusable fuel and other unusable fluids engine oil
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