1、ASD STANDARD NORME ASD ASD NORM prEN 4673-005 Edition P 1 December 2009 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATIONAvenue de Tervuren, 270 - B-1150 Brussels - Tel. 32 2 775 8126 - Fax. 32 2 775 8131 - www.asd-stan.orgICS: Descriptors: ENGLISH VERSION Aer
2、ospace series Inserts, UNJ threads, self-locking, with self-broaching keys Part 005: In heat resisting nickel base alloy Ni-P101HT (WASPALOY), silver plating Srie arospatiale Douilles filetes, filetage UNJ, freinage interne, clavettes autobrochantes Partie 005 : En alliage rsistant chaud base nickel
3、 Ni-P101HT (WASPALOY), argentage Luft- und Raumfahrt Gewindeeinstze, UNJ-Gewinden, selbstsichernd, mit selbstrumenden Stiften Teil 005: selbstrumenden Stiften, aus Hochwarmfeste Nickellegierung Ni-P101HT (WASPALOY), Versilbern This “Aerospace Series“ Prestandard has been drawn up under the responsib
4、ility of ASD-STAN (The AeroSpace and Defence Industries Association of Europe - Standardization). It is published for the needs of the European Aerospace Industry. It has been technically approved by the experts of the concerned Domain following member comments. Subsequent to the publication of this
5、 Prestandard, the technical content shall not be changed to an extent that interchangeability is affected, physically or functionally, without re-identification of the standard. After examination and review by users and formal agreement of ASD-STAN, it will be submitted as a draft European Standard
6、(prEN) to CEN (European Committee for Standardization) for formal vote and transformation to full European Standard (EN). The CEN national members have then to implement the EN at national level by giving the EN the status of a national standard and by withdrawing any national standards conflicting
7、with the EN. Edition approved for publication 15 December 2009 Comments should be sent within six months after the date of publication to ASD-STAN Mechanical Domain Copyright 2009 by ASD-STAN prEN 4673-005:2009 (E) 2 White page prEN 4673-005:2009 (E) 3 Contents Page Foreword .3 Introduction.4 1 Scop
8、e4 2 Normative references4 3 Required characteristics.4 4 Insert definition5 5 Designation 8 6 Marking.8 7 Technical specification.8 Foreword This standard was reviewed by the Domain Technical Coordinator of ASD-STANs Mechanical Domain. After inquiries and votes carried out in accordance with the ru
9、les of ASD-STAN defined in ASD-STANs General Process Manual, this standard has received approval for Publication. prEN 4673-005:2009 (E) 4 Introduction For design and installation procedures see EN 4673-002 1)and EN 4673-001 1)1 Scope This standard specifies the characteristics of self-locking, inse
10、rts for Inch series, self-broaching keys, in NI-P101HT, silver plated, for aerospace applications. Classification: 1 210 MPa 2)/ 760 C 3)2 Normative references The following referenced documents are indispensable for the application of this document. For dated references, only the edition cited appl
11、ies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 2424, Aerospace series Marking of aerospace products EN 2786, Aerospace series Electrolytic silver plating of fasteners EN 2959, Aerospace series Heat resisting alloy NI-PH1302 (NiCr20Co
12、13Mo4Ti3Al) Solution treated and cold worked Bar for forged fasteners 3 mm D 30 mm EN 3220, Aerospace series Heat resisting nickel base alloy (Ni-P101HT) - Cold worked and softened Bar and wire for continuous forging or extrusion for fasteners 3 D 30 mm EN 4673-001, Aerospace series Inserts, UNJ thr
13、eads, self-locking, with self-broaching keys Part 001: Installation and removal procedure 1)EN 4673-002, Aerospace series Inserts, UNJ threads, self-locking, with self-broaching keys Part 002: Design standard 1)EN 4673-003, Aerospace series Inserts, UNJ threads, self-locking, with self-broaching key
14、s Part 003: Technical specification 1)ISO 3161, UNJ threads general requirements and limit dimensions TR 3198, Aerospace series Manufacturers identification monograms and marks for EN aerospace products 4)3 Required characteristics 3.1 Configuration Dimensions Tolerances Masses See Figure 1 and Tabl
15、es 1, 2, 3 and 4. 1) Published as ASD-STAN Prestandard at the date of publication of this standard. 2) Corresponds to the minimum tensile stress which the material is able to withstand at ambient temperature. 3) Maximum temperature that the insert is able to withstand, without permanent alteration t
16、o its original characteristics, after ambient temperature has been restored. The maximum temperature is conditioned by the silver plating. 4) Published as ASD-STAN Technical Report at the date of publication of this standard. prEN 4673-005:2009 (E) 5 Dimensions and tolerances are in millimetres. The
17、y apply after silver plating. 3.2 Material Insert: EN 3220 and EN 2959 treated for 335 HV to 427 HV Keys: Stainless steel or Nickel alloy treated for HV 600 3.3 Surface treatment See EN 2786. 4 Insert definition See Figure 1. only for key grooves and keys Values apply after silver plating. Remove sh
18、arp edges 0,1 mm to 0,4 mm. Key 1 N keys equally spaced. 2 form out-of-round in this area to achieve the self-locking requirement. Mark of tools allowed. 3 pitch diameters. 4 marking area or on keys left to producers option. 5 total length of the key shall not exceed E min. Dimensions and location o
19、f keys shall meet EN 4673-003 requirements. Details of form not stated are left to the producers discretion. Figure 1 5Ra3,2 Ra1,6 prEN 4673-005:2009 (E) 6 4.1 Normal size insert See Table 1. Table 1 A Internal thread aCode Designation B External thread bDesignation Ccmax. D 0 - 0,2 E max. F max. G
20、max. N Mass kg/1 000 3-0 .190 0-32UNJF-3B .312 5-18UNS-2A 6,30 7,9 6,0 7,7 2 1,4 4-0 .250 0-28UNJF-3B .375 0-16UNS-2A 7,90 9,5 8,0 10,0 2 2,4 5-0 .312 5-24UNJF-3B .437 5-16UNS-2A 9,50 11,1 9,5 12,3 2 3,7 6-0 .375 0-24UNJF-3B .500 0-16UNS-2A 11,05 12,7 11,5 14,5 4 5,2 7-0 .437 5-20UNJF-3B .562 5-16UN
21、S-2A 12,65 14,2 13,5 17,1 4 7,3 8-0 .500 0-20UNJF-3B .625 0-16UNS-2A 14,25 15,8 15,5 4,35 19,4 4 9,5 aIn accordance with ISO 3161. bSee Table 4. cAfter deformation.4.2 First repair size insert See Table 2. Table 2 A Internal thread aCode Designation B External thread bDesignation Ccmax. D 0 - 0,2 E
22、max. F 0 - 0,2 G max. N Mass kg/1 000 3-1 .190 0-32UNJF-3B .375 0-16UNS-2A 7,90 9,5 6,0 7,7 2 2,5 4-1 .250 0-28UNJF-3B .437 5-16UNS-2A 9,50 11,1 8,0 10,0 2 4,3 5-1 .312 5-24UNJF-3B .500 0-16UNS-2A 11,05 12,7 9,5 12,3 2 6,4 6-1 .375 0-24UNJF-3B .562 5-16UNS-2A 12,65 14,2 11,5 14,5 4 8,8 7-1 .437 5-20
23、UNJF-3B .625 0-16UNS-2A 14,25 15,8 13,5 17,1 4 12,2 8-1 .500 0-20UNJF-3B .687 5-16UNS-2A 15,80 17,4 15,5 4,35 19,4 4 15,6 aIn accordance with ISO 3161. bSee Table 4. cAfter deformation.prEN 4673-005:2009 (E) 7 4.3 Second repair size insert See Table 3. Table 3 A Internal thread aCode Designation B E
24、xternal thread bDesignation Ccmax. D 0 - 0,2 E max. F 0 - 0,2 G max. N Mass kg/1 000 3-2 .190 0-32UNJF-3B .437 5-16UNS-2A 9,50 11,1 6,0 7,7 2 4,0 4-2 .250 0-28UNJF-3B .500 0-16UNS-2A 11,05 12,7 8,0 10,0 2 6,5 5-2 .312 5-24UNJF-3B .562 5-16UNS-2A 12,65 14,2 9,5 12,3 2 9,5 6-2 .375 0-24UNJF-3B .625 0-
25、16UNS-2A 14,25 15,8 11,5 14,5 4 13,0 7-2 .437 5-20UNJF-3B .687 5-16UNS-2A 15,80 17,4 13,5 17,1 4 17,6 8-2 .500 0-20UNJF-3B .750 0-16UNS-2A 17,40 19,0 15,5 4,35 19,4 4 22,4 aIn accordance with ISO 3161. bSee Table 4. cAfter deformation.4.4 External thread dimension See Table 4. Table 4 Major diameter
26、 Pitch diameter Minor diameter External thread Designation min. max. min. max. min. max. .312 5-18UNS-2A 7,69 7,91 6,89 6,99 6,32 6,50 .375 0-16UNS-2A 9,25 9,49 8,35 8,46 7,92 8,13 .437 5-16UNS-2A 10,84 11,08 9,93 10,05 9,50 9,72 .500 0-16UNS-2A 12,43 12,67 11,51 11,63 11,09 11,30 .562 5-16UNS-2A 14
27、,01 14,25 13,10 13,22 12,67 12,89 .625 0-16UNS-2A 15,60 15,84 14,69 14,81 14,26 14,48 .687 5-16UNS-2A 17,19 17,43 16,27 16,39 15,84 16,07 .750 0-16UNS-2A 18,77 19,01 17,85 17,98 17,42 17,65 prEN 4673-005:2009 (E) 8 5 Designation EXAMPLE Description block Identity block INSERTS, SELF-LOCKING, SELF-BR
28、OACHING KEYS EN4673-005-5-0 Number of this standard Thread code (see Tables 1 to 3) NOTE The last digit corresponds to: Oversize code: 0 = Normal size 1 = First repair size 2 = Second repair size NOTE If necessary, the code I9005 shall be placed between the description block and the identity block. 6 Marking EN 2424, style F Manufacturers identification marks in accordance with the list for special identification marks in TR 3198. 7 Technical specification EN 4673-003
