1、BRITISH STANDARD AEROSPACE SERIESBS EN 4497:2005Screws, pan head, offset cruciform recess, close tolerance normal shank, short thread, in titanium alloy, anodized, with aluminium pigmented coating Classification: 1 100 MPa (at ambient temperature) / 315 CThe European Standard EN 4497:2005 has the st
2、atus of a British StandardICS 49.030.20g49g50g3g38g50g51g60g44g49g42g3g58g44g55g43g50g56g55g3g37g54g44g3g51g40g53g48g44g54g54g44g50g49g3g40g59g38g40g51g55g3g36g54g3g51g40g53g48g44g55g55g40g39g3g37g60g3g38g50g51g60g53g44g42g43g55g3g47g36g58Licensed Copy: Wang Bin, na, Fri Apr 14 07:24:08 BST 2006, Un
3、controlled Copy, (c) BSIBS EN 4497:2005This British Standard was published under the authority of the Standards Policy and Strategy Committee on 31 January 2006 BSI 31 January 2006ISBN 0 580 47217 5National forewordThis British Standard is the official English language version of EN 4497:2005. The U
4、K participation in its preparation was entrusted to Technical Committee ACE/12, Aerospace fasteners and fastening systems, which has the responsibility to: A list of organizations represented on this committee can be obtained on request to its secretary.Cross-referencesThe British Standards which im
5、plement international or European publications referred to in this document may be found in the BSI Catalogue under the section entitled “International Standards Correspondence Index”, or by using the “Search” facility of the BSI Electronic Catalogue or of British Standards Online.This publication d
6、oes not purport to include all the necessary provisions of a contract. Users are responsible for its correct application. Compliance with a British Standard does not of itself confer immunity from legal obligations. aid enquirers to understand the text; present to the responsible international/Europ
7、ean committee any enquiries on the interpretation, or proposals for change, and keep UK interests informed; monitor related international and European developments and promulgate them in the UK.Summary of pagesThis document comprises a front cover, an inside front cover, the EN title page, pages 2 t
8、o 9 and a back cover.The BSI copyright notice displayed in this document indicates when the document was last issued.Amendments issued since publicationAmd. No. Date CommentsLicensed Copy: Wang Bin, na, Fri Apr 14 07:24:08 BST 2006, Uncontrolled Copy, (c) BSIEUROPEAN STANDARD NORME EUROPENNE EUROPIS
9、CHE NORM EN 4497 December 2005 ICS 49.030.20 English Version Aerospace series - Screws, pan head, offset cruciform recess, close tolerance normal shank, short thread, in titanium alloy, anodized, with aluminium pigmented coating - Classification: 1 100 MPa (at ambient temperature) / 315 C Srie arosp
10、atiale - Vis tte cylindrique, empreinte cruciforme dporte, ft normal tolrance serre, filetage court, en alliage de titane, anodises, avec revtement alumino-organique - Classification : 1 100 MPa ( temprature ambiante) / 315 C Luft- und Raumfahrt - Flachkopf-Paschrauben, mit Flgelkreuzschlitz, kurzes
11、 Gewinde, aus Titanlegierung, anodisiert, mit Aluminium pigmenttete Beschichtung - Klasse: 1 100 MPa (bei Raumtemperatur) / 315 C This European Standard was approved by CEN on 26 October 2005. CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions fo
12、r giving this European Standard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such national standards may be obtained on application to the Central Secretariat or to any CEN member. This European Standard exists in three official
13、 versions (English, French, German). A version in any other language made by translation under the responsibility of a CEN member into its own language and notified to the Central Secretariat has the same status as the official versions. CEN members are the national standards bodies of Austria, Belg
14、ium, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION CO
15、MIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG Management Centre: rue de Stassart, 36 B-1050 Brussels 2005 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 4497:2005: ELicensed Copy: Wang Bin, na, Fri Apr 14 07:24:08 BS
16、T 2006, Uncontrolled Copy, (c) BSI2 Contents Page Foreword 3 1 Scope .4 2 Normative references .4 3 Required characteristics 5 4 Designation .8 5 Marking 8 6 Technical specification.9 7 Oversized bolts .9 EN 4497:2005Licensed Copy: Wang Bin, na, Fri Apr 14 07:24:08 BST 2006, Uncontrolled Copy, (c) B
17、SI3 Foreword This European Standard (EN 4497:2005) has been prepared by the European Association of Aerospace Manufacturers - Standardization (AECMA-STAN). After enquiries and votes carried out in accordance with the rules of this Association, this Standard has received the approval of the National
18、Associations and the Official Services of the member countries of AECMA, prior to its presentation to CEN. This European Standard shall be given the status of a national standard, either by publication of an identical text or by endorsement, at the latest by June 2006, and conflicting national stand
19、ards shall be withdrawn at the latest by June 2006. Attention is drawn to the possibility that some of the elements of this document may be the subject of patent rights. CEN and/or CENELEC shall not be held responsible for identifying any or all such patent rights. According to the CEN/CENELEC Inter
20、nal Regulations, the national standards organizations of the following countries are bound to implement this European Standard: Austria, Belgium, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Nether
21、lands, Norway, Poland, Portugal, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. EN 4497:2005Licensed Copy: Wang Bin, na, Fri Apr 14 07:24:08 BST 2006, Uncontrolled Copy, (c) BSI4 1 Scope This standard specifies the characteristics of screws, pan head, offset cruciform recess,
22、 close tolerance normal shank, short thread, in titanium alloy, anodized, with aluminium pigmented coating. Classification: 1 100 MPa 1) / 315 C 2)2 Normative references The following referenced documents are indispensable for the application of this document. For dated references, only the edition
23、cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. ISO 3353-1, Aerospace Lead and runout threads Part 1: Rolled external threads. ISO 5855-2, Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts. ISO 7913, Aerospace Bo
24、lts and screws, metric Tolerances of form and position. ISO 7994, Aerospace Internal drive, offset cruciform recess (Torq-Set ) for rotary fastening devices Metric series. ISO 9152, Aerospace Bolts, with MJ threads, in titanium alloys, strength class 1 100 MPa Procurement specification. EN 2424, Aer
25、ospace series Marking of aerospace products. EN 4016, Aerospace series Oversized bolts.3)EN 4474, Aerospace series Aluminium pigmented coatings Coating methods.3) EN 9100, Aerospace series Quality management systems Requirements (based on ISO 9001:2000) and Quality systems Model for quality assuranc
26、e in design, development, production, installation and servicing (based on ISO 9001:1994). EN 9133, Aerospace series Quality management systems Qualification Procedure for aerospace standard parts. MIL-L-87132B, Lubricant, Cetyl Alcohol, 1-Hexadecanol, Application to Fasteners.4)TR 3775, Aerospace s
27、eries Bolts and pins Materials.5)1) Minimum tensile strength of the material at ambient temperature. 2) Maximum temperature that the screw can withstand without continuous change in its original characteristics, after return to ambient temperature. The maximum temperature is determined by the coatin
28、g. 3) Published as AECMA Prestandard at the date of publication of this standard. 4) Published by: Department of Defense (DoD), the Pentagon, Washington, D.C.20301, USA. 5) Published as AECMA Technical Report at the date of publication of this standard. EN 4497:2005Licensed Copy: Wang Bin, na, Fri A
29、pr 14 07:24:08 BST 2006, Uncontrolled Copy, (c) BSI5 3 Required characteristics 3.1 Configuration Dimensions Masses See Figure 1 and Table 1. Dimensions and tolerances are expressed in millimetres and apply after coating (tolerance on shank diameter before coating is also specified). Details of form
30、 not stated are left to the manufacturers discretion. 3.2 Tolerances of form and position See ISO 7913 3.3 Materials See TR 3775 (titanium alloy, strength class 1 100 MPa) 3.4 Surface treatments See EN 4474 Lubrication with cetylic alcohol (chlorine free) according to MIL-L-87132 EN 4497:2005License
31、d Copy: Wang Bin, na, Fri Apr 14 07:24:08 BST 2006, Uncontrolled Copy, (c) BSI6 Values in micrometres apply prior to surface treatment. Break sharp edges 0,1 to 0,4. Key 1 One hole diameter D5(optional) 2 Thread 3 Marking 4 Drive: see Table 3. 5 Conforms to ISO 3353-1 aShape optional Figure 1 3,2 0,
32、8 EN 4497:2005Licensed Copy: Wang Bin, na, Fri Apr 14 07:24:08 BST 2006, Uncontrolled Copy, (c) BSI7 Table 1 D1D2D3D4D5E nom. Tol. Diameter code Thread a before coating after coating 0 0,3 min. nom. Tol. H13 nom. Tol. 030 MJ30,5-4h6h 3 0,026 0,041 0,006 0,031 6 4,7 2,3 1,8 040 MJ40,7-4h6h 4 8 6,7 3
33、0 0,5 1,1 2,4 050 MJ50,8-4h6h 5 10 8,7 3,4 3 0 0,2 060 MJ61-4h6h 6 0,030 0,045 0,010 0,035 12 10,7 4,2 1,5 3,6 070 MJ71-4h6h 7 14 12,7 5,2 4,2 080 MJ81-4h6h 8 16 14,7 6,2 1,9 4,8 100 MJ101,25-4h6h 10 0,033 0,048 0,013 0,038 20 18,7 7,9 6 120 MJ121,25-4h6h 12 0,036 0,051 0,016 0,041 24 22,7 9,8 0,5 2
34、,4 7,2 0 0,3 L1 0,2 b c L2 L3 R S Mass dDiameter code Code nom. nom. Tol. max. min. e f 030 002 to 030 2 to 30 6 1,2 0,3 0,38 0,03 040 002 to 040 2 to 40 7,5 5 0,4 1,6 0,4 0,92 0,06 050 003 to 050 3 to 50 9 6 0,5 2 0,5 1,88 0,08 060 003 to 060 3 to 60 10 2,4 0,6 3,10 0,12 070 004 to 070 4 to 70 11 7
35、 2,8 0,7 5,31 0,17 080 004 to 080 4 to 80 11,5 7,5 0,7 3,2 0,8 7,23 0,22 100 005 to 100 5 to 100 14,5 9 0,8 0 0,2 4 1 14,24 0,35 120 006 to 120 6 to 120 16 10 0,9 0 0,3 4,8 1,2 25,17 0,50 aIn accordance with ISO 5855-2, except the thread major diameter “d max.“ which shall be equal to D1min. 0,025.
36、bIncrements: 1 for L1 30 2 for 30 100 cIf greater lengths are required, they shall be chosen using the above increments. The length code corresponds to length L1, completed by one or two zeros to the left, where necessary, to obtain a three digit code. dApproximate values (kg/1 000 pieces), calculat
37、ed on the basis of 4,45 kg/dm3, for information purposes only. They apply to screws without holes. eValue for head and first L4fIncrease for each additional millimetre of L4. EN 4497:2005Licensed Copy: Wang Bin, na, Fri Apr 14 07:24:08 BST 2006, Uncontrolled Copy, (c) BSI8 4 Designation EXAMPLE Desc
38、ription block SCREW Identity block EN4497D050010ANumber of this standard Hole code (see Table 2) Diameter code (see Table 1) Length code (see Table 1) Drive code (see Table 3) NOTE If necessary, the code I9005 shall be placed between the description block and the identity block. Table 2 Holes Code W
39、ith DWithout (hyphen) Table 3 Drive Code ISO 7994 RISO 7994 unribbedA 5 Marking See Table 4 and Figure 1, indented. Table 4 Diameter code EN 2424 Style 030 and 040 N 050 to 120 C + MJ EN 4497:2005Licensed Copy: Wang Bin, na, Fri Apr 14 07:24:08 BST 2006, Uncontrolled Copy, (c) BSI9 6 Technical speci
40、fication ISO 9152, except for clauses: Approval of manufacturers: see EN 9100; Qualification of screws: see EN 9133. 7 Oversized bolts See EN 4016 EN 4497:2005Licensed Copy: Wang Bin, na, Fri Apr 14 07:24:08 BST 2006, Uncontrolled Copy, (c) BSIBS EN 4497:2005BSI389 Chiswick High RoadLondonW4 4ALBSI
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