AECMA TR 4661-2009 Aerospace series Hinges flight controls materials and surface treatments Edition 1《航空航天系列.铰链 飞行控制材料及表面处理.版本1》.pdf

1、 ASD Technical Report Rapport Technique ASD ASD Fachbericht TR 4661 Edition 1 October 2009 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATION Avenue de Tervuren, 270 - B-1150 Brussels - Tel. + 32 2 775 8126 - Fax. + 32 2 775 8131 - www.asd-stan.orgICS: 49.025.0

2、1/49.030.01/49.020.30/49.030.99 Descriptors: aircraft industry, material, hinge Descripteurs : industrie aronautique, matriau, articulation Deskiptoren: Luftfahrzeug, Werkstoff, Gelenk ENGLISH VERSION Aerospace series Hinges, flight controls materials and surface treatments Srie arospatiale Articula

3、tions, commandes de vol matriaux et traitements de surface Luft- und Raumfahrt Lager, Flugsteuerungen Werkstoffe und Oberflchenschutz This Technical report was drawn up by ASD-STAN in cooperation with ASD-CERT. The reason which led to the publication of the document as a Technical Report is explaine

4、d in the foreword. Ce Rapport Technique a t labor par ASD-STAN en coopration avec ASD-CERT. Les raisons pour lesquelles le document a t publi sous forme de Rapport Technique sont donnes dans lavant-propos. Dieser Fachbericht wurde von ASD-STAN in Zusammenarbeit mit ASD-CERT erarbeitet. Die Grnde, di

5、e zur Verffentlichung dieses Dokumentes als Fachbericht gefhrt haben, sind im Vorwort angegeben. Edition approved for publication 31 October 2009 Copyright 2009 by ASD-STAN Copyright ASD-STAN Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without licen

6、se from IHS-,-,-Page/Page/Seite 2 TR 4661:10-09 Foreword The main task of ASD-STAN Domains is to prepare EN standards. In exceptional circumstances, however, the publication of a Technical Report of one of the following types may be proposed: type 1, the subject is still under technical development

7、requiring wider exposure; type 2, a Domain has collected data of a different kind from that which is normally published as a European Standard. Mechanical Domain decided to publish this document in the form of a Technical Report of type 2 in order to facilitate the updating of this document. Avant-p

8、ropos La tche principale des Domaines ASD-STAN est dlaborer des normes EN. Cependant, titre exceptionnel, la publication dun Rapport Technique de lun des types suivants peut tre propose : type 1, le sujet en question est encore en cours de dveloppement technique et requiert une plus grande exprience

9、 ; type 2, un Domaine a runi des donnes de nature diffrente de celles qui sont normalement publies comme norme europenne. Le Domaine Mcanique a dcid de publier ce document sous la forme dun Rapport Technique de type 2 pour en faciliter la mise jour. Vorwort Die Hauptaufgabe der Domain der ASD-STAN i

10、st es, EN-Normen zu erarbeiten. In Sonderfllen kann jedoch die Verffentlichung eines Fachberichtes folgender Typen beantragt werden: Typ 1, das betroffene Thema befindet sich noch in technischer Entwicklung und bentigt weitere Erfahrung; Typ 2, das Domain hat Angaben zusammengetragen, die blicherwei

11、se nicht Gegenstand einer europischen Norm sind. Das Mechanik Domain hat beschlossen, dieses Dokument in Form eines Fachberichtes von Typ 2 zu verffentlichen, um dessen berarbeitung zu erleichtern. Copyright ASD-STAN Provided by IHS under license with AECMA Not for ResaleNo reproduction or networkin

12、g permitted without license from IHS-,-,-Page/Page/Seite 3 TR 4661:10-09 1 Scope This Technical Report gives the EN standardized materials or, on the national level, the materials standardized by ASD member countries to be used for manufacturing the relevant products to insure their functional inter

13、changeability. This Technical Report is not to be taken as a table of equivalent materials. The use of EN standardized materials shall be given priority. This Technical Report applies when it is referenced. 1 Domaine dapplication Le prsent Rapport Technique indique les matriaux normaliss EN ou, sur

14、le plan national, les matriaux normaliss par les pays membres de lASD utiliser pour la fabrication des produits concerns afin dassurer leur interchangeabilit fonctionnelle. Il ne sagit pas dune table dquivalence de matriaux. Les matriaux normaliss EN doivent tre utiliss en priorit. Le prsent Rapport

15、 technique sapplique chaque fois quil est cit en rfrence. 1 Anwendungsbereich Dieser Fachbericht fhrt die EN genormten Werkstoffe und die von den ASD Lndern auf nationaler Ebene genormten Werkstoffe auf, die angewandt werden, um Erzeugnisse herzustellen, die ihre funktionelle Austauschbarkeit gewhrl

16、eisten. Er ist nicht als ein Verzeichnis austauschbarer Werkstoffe zu verwenden. EN- genormte Werkstoffe sind vorrangig zu verwenden. Dieser Fachbericht ist immer dann anzuwenden, wenn auf ihn verwiesen wird. Copyright ASD-STAN Provided by IHS under license with AECMA Not for ResaleNo reproduction o

17、r networking permitted without license from IHS-,-,-Page/Page/Seite 4 TR 4661:10-09 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 th

18、e referenced document (including any amendments) applies. EN ISO 683-17, Heat-treated steels, alloy steels and free-cutting steels Part 17: Ball and roller bearing steels. ISO 4618, Paints and varnishes Terms and definitions. ISO 8074, Aerospace Surface treatment of austenitic stainless steel parts.

19、 ISO 8075, Aerospace Surface treatment of hardenable stainless steel parts. EN 2030, Steel FE-PM43 Hardened and tempered Bars D 150 mm Aerospace series. 1)EN 2031, Steel FE-PL31 Hardened and tempered Bars Aerospace series. 1)EN 2099, Aerospace series Steel FE-PL52S Rm 690 MPa Bar De 250 mm. 2)EN 213

20、2, Electrodeposition of chromium for engineering purposes Aerospace series. 1)EN 2133, Aerospace series Cadmium plating of steels with specified tensile strength 1 450 MPa, copper, copper alloys and nickel alloys. EN 2135, Aerospace series Steel FE-PL61 Carburized, hardened and tempered Bar De 40 mm

21、. 6)EN 2137, Steel FE-PL75 1 100 MPa Rm 1 250 MPa Bars De 100 mm Aerospace series. 1)EN 2159 3), Steel FE-PM44 Hardened and tempered Bars D 150 mm Aerospace series. 1)EN 2221, Steel FE-PL31 Hardened and tempered Hollow bars 3,5 mm a 55 mm Aerospace series. 1)EN 2222, Steel FE-PL31 Hardened and tempe

22、red Hand and die forgings Aerospace series. 1)EN 2227, Steel FE-PM44 Hardened and tempered Hand and die forgings De 150 mm Aerospace series. 1)EN 2249, Aerospace series Steel FE-PL71 Carburized, hardened and tempered Bars De 100 mm. 2)1) Published as ASD-STAN Standard at the date of publication of t

23、his standard. 2) In preparation at the date of publication of this standard. 3) Inactive for New Design, see EN 3492. Copyright ASD-STAN Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page/Page/Seite 5 TR 4661:10-09 EN 2438

24、, Aerospace series Steel FE-PL2102 (35NiCr6) 900 MPa Rm 1 100 MPa Bars De 40 mm. EN 2471, Steel FE-PL74 1 250 MPa Rm 1 450 MPa Bars De 40 mm Aerospace series. 1)EN 2473 4), Steel FE-PL74 900 MPa Rm 1 100 MPa Bars De 150 mm Aerospace series. 1)EN 2475, Aerospace series Steel FE-PL2106 (30CrNiMo8) Air

25、 melted Hardened and tempered Bar for machining De 100 mm 1 100 MPa Rm 1 300 MPa. 6)EN 2815, Aerospace series Steel FE-PM1802 (X5CrNiCu15-5) Consumable electrode remelted Solution treated and precipitation treated Bar for machining a or D 200 mm Rm 965 MPa. 6)EN 2817, Aerospace series Steel FE-PM180

26、2 (X5CrNiCu15-5) Consumable electrode remelted Solution treated and precipitation treated Bar for machining a or D 200 mm Rm 1 070 MPa. 6)EN 2821, Aerospace series Steel FE-PM1802 (X5CrNiCu15-5) Consumable electrode remelted Solution treated and precipitation treated Bar for machining a or D 200 mm

27、Rm 1 310 MPa. EN 3161, Aerospace series Steel FE-PM3801 (X5CrNiCu17-4) Air melted Solution treated and precipitation treated Bar a or D 200 mm Rm 930 MPa. EN 3353 5), Aerospace series Titanium alloy TI-P63 Solution treated and aged Rm 1 100 MPa Bar and wire for fasteners machined De 25 mm. 6)EN 3458

28、 5), Aerospace series Titanium alloy TI-P63 Annealed 900 Rm 1 160 MPa Bar and wire for fasteners machined De 25 mm. 6)EN 3521, Aerospace series Steel FE-PL2106 (30CrNiMo8) Air melted - Hardened and tempered Bar for machining De 150 mm 900 MPa Rm 1 100 MPa. 6)EN 3813, Aerospace series Titanium alloy

29、TI-P64001 Annealed Bar and wire for forged fasteners De 25 mm. 6)EN 10027-1, Designation systems for steel Part 1: Steel names. TR 3900, Aerospace series Metallic materials Relationship between AECMA designation systems.7)AMS4928, Titanium Alloy Bars, Wire, Forgings, Rings, and Drawn Shapes, 6Al - 4

30、V, Annealed. 8)4) Inactive for New Design, see EN 3521. 5) Inactive for New Design, see EN 3813. 6) Published as ASD-STAN Prestandard at the date of publication of this standard. 7) Published as ASD-STAN Technical Report at the date of publication of this technical report. Copyright ASD-STAN Provide

31、d by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page/Page/Seite 6 TR 4661:10-09 AMS4965, Titanium Alloy, Bars, Wire, Forgings, and Rings, 6.0AI - 4.0V, Solution Heat Treated and Aged. 8)AMS4967, Titanium Alloy, Bars, Wire, Forgings

32、, and Rings, 6.0Al - 4.0V, Annealed, Heat Treatable. 8)AMS5618, Steel, Corrosion-Resistant, Bars, Wire, and Forgings, 17Cr - 0.52Mo (0.95 - 1.20C) (SAE 51440C), Consumable Electrode Vacuum Melted. 8)AMS5622, Steel, Corrosion-Resistant, Bars, Wire, Forgings, Tubing, and Rings, 16Cr - 4.0Ni - 0.30Cb -

33、 4.0Cu, Solution Heat Treated, Precipitation Hardenable, Consumable Electrode Remelted. 8)AMS5630, Steel, Corrosion-Resistant, Bars, Wire, and Forgings, 17Cr - 0.52Mo (0.95 - 1.20C) (SAE 51440C). 8)AMS5643, Steel, Corrosion-Resistant, Bars, Wire, Forgings, Tubing, and Rings 16Cr - 4.0Ni - 0.30Cb - 4

34、.0Cu Solution Heat Treated, Precipitation Hardenable. 8)AMS5659, Steel, Corrosion Resistant, Bars, Wire, Forgings, Rings, and Extrusions 15Cr - 4.5Ni - 0.30Cb (Nb) - 3.5Cu, Consumable Remelted, Precipitation Hardenable. 8)AMS5828, Nickel Alloy, Corrosion and Heat Resistant, Welding Wire, 57Ni - 19.5

35、Cr - 13.5Co - 4.2Mo - 3.1Ti - 1.4Al - 0.006B, Vacuum Induction Melted, Solution Heat Treated. 8)AMS6263, Steel Bars, Forgings, and Tubing, 1.2Cr - 3.2Ni - 0.12Mo (0.11 - 0.17C) (SAE 9315). 8)AMS6440, Steel, Bars, Forgings, and Tubing, 1.45Cr (0.93 - 1.05C) (SAE 52100), for Bearing Applications. 8)AS

36、TM-B 348-83, Standard Specification for Titanium and Titanium Alloy Bars and Billets. 9)MIL-S-7420B, Steel Bars, Alloy, Chromium, High Carbon e52100 (Aircraft Quality). 8)MIL-S-18732D, Steel Bars, Wire, Forging Stock, Forgings Tubing (431), Special Quality. 10)DIN 17230, Ball and Roller Bearing Stee

37、ls; Technical Conditions of Delivery. 11)8) Published by: Society of Automotive Engineers, Inc. (SAE), 400 Commonwealth Drive, Warrendale, PA 15096-0001, USA. 9) Published by: American Society for Testing and Materials (ASTM), 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959 USA.

38、 10) Published by: Department of Defense (DoD), the Pentagon, Washington, DC 20301, USA. 11) Inactive for New Design, see EN ISO 683-17. Copyright ASD-STAN Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page/Page/Seite 7 TR

39、 4661:10-09 2 Rfrences normatives Les documents de rfrence suivants sont indispensables pour lapplication du prsent document. Pour les rfrences dates, seule ldition cite sapplique. Pour les rfrences non dates, la dernire dition du document de rfrence sapplique (y compris les ventuels amendements). E

40、N ISO 683-17, Aciers pour traitement thermique, aciers allis et aciers pour dcolletage Partie 17 : Aciers pour roulements. ISO 8074, Aronautique et espace Traitement de surface des lments en acier inoxydable austnitique. ISO 8075, Aronautique et espace Traitement de surface des lments en acier inoxy

41、dable durcissement structural. EN 2030, Acier FE-PM43 Tremp et revenu Barres D 150 mm Srie arospatiale. 1)EN 2031, Acier FE-PL31 Tremp et revenu Barres Srie arospatiale. 1)EN 2099, Srie arospatiale Acier FE-PL52S Rm 690 MPa Barres De 250 mm. 2)EN 2132, Dpt lectrolytique de chrome pour usages mcaniqu

42、es Srie arospatiale. 1)EN 2133, Srie arospatiale Cadmiage lectrolytique des aciers de rsistance 1 450 MPa, du cuivre, des alliages de cuivre et des alliages de nickel. EN 2135, Srie arospatiale Acier FE-PL61 Cment, tremp et revenu Barres De 40 mm. 6)EN 2137, Acier FE-PL75 1 100 MPa Rm 1 250 MPa Barr

43、es De 100 mm Srie arospatiale. 1)EN 2159 3), Acier FE-PM44 Tremp et revenu Barres D 150 mm Srie arospatiale. 1)EN 2221, Acier FE-PL31 Tremp et revenu bauches tubulaires 3,5 mm a 55 mm Srie arospatiale. 1)EN 2222, Acier FE-PL31 Tremp et revenu Pices forges et matrices Srie arospatiale. 1)EN 2227, Aci

44、er FE-PM44 Tremp et revenu Pices forges et matrices De 150 mm Srie arospatiale. 1)EN 2249, Srie arospatiale Acier FE-PL71 Cment, tremp et revenu Barres De 100 mm. 2)1) Publie comme norme ASD-STAN la date de publication de la prsente norme. 2) En prparation la date de publication de la prsente norme.

45、 3) Ne pas Appliquer pour tudes Nouvelles, voir lEN 3492. Copyright ASD-STAN Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page/Page/Seite 8 TR 4661:10-09 EN 2438, Srie arospatiale Acier FE-PL2102 (35NiCr6) 900 MPa Rm 1 10

46、0 MPa Barres De 40 mm. EN 2471, Acier FE-PL74 1 250 MPa Rm 1 450 MPa Barres De 40 mm Srie arospatiale. 1)EN 2473 4), Acier FE-PL74 900 MPa Rm 1 100 MPa Barres De 150 mm Srie arospatiale. 1)EN 2475, Srie arospatiale Acier FE-PL2106 (30CrNiMo8) labor lair Durci par trempe et revenu Barre pour usinage

47、De 100 mm 1 100 MPa Rm 1 300 MPa. 6)EN 2815, Srie arospatiale Acier FE-PM1802 (X5CrNiCu15-5) Refondu llectrode consommable Mis en solution et vieilli Barres pour usinage a ou D 200 mm Rm 965 MPa. 6)EN 2817, Srie arospatiale Acier FE-PM1802 (X5CrNiCu15-5) Refondu llectrode consommable Mis en solution et vieilli Barres pour usinage a ou D 200 mm Rm 1 070 MPa. 6)