1、ASD STANDARD NORME ASD ASD NORM prEN 4623 Edition P 1 June 2008 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATIONAvenue de Tervuren, 270 - B-1150 Brussels - Tel. + 32 2 775 8126 - Fax. + 32 2 763 3565 - www.asd-stan.orgICS: 49.030.20 Descriptors: Aircraft indu
2、stry ENGLISH VERSION Aerospace series Inserts, MJ threads, self-locking, with self-broaching keys, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated Srie arospatiale Douilles filetes, filetage MJ, freinage interne, clavettes auto-brochantes, en alliage rsistant chaud base de
3、 nickel NI-PH2601 (Inconel 718), argentes Luft- und Raumfahrt Gewindeeinstze, MJ-Gewinden, selbstsichernd, mit selbstrumenden Stiften, aus hochwarmfeste Nickellegierung NI-PH2601 (Inconel 718), Versilbert This “Aerospace Series“ Prestandard has been drawn up under the responsibility of ASD-STAN (The
4、 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 Prestandard, the tech
5、nical 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 (prEN) to CEN (Europea
6、n 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 with the EN. Edition a
7、pproved for publication 30 June 2008 Comments should be sent within six months after the date of publication to ASD-STAN Mechanical Domain Copyright 2008 by ASD-STAN Copyright ASD-STAN Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from
8、 IHS-,-,-prEN 4623:20082 Contents Page Foreword2 Introduction.3 1 Scope 3 2 Normative references 3 3 Required characteristics.4 4 Insert definition4 5 Designation 7 6 Marking and identification 7 7 Technical specification .7 Foreword This standard was reviewed by the Domain Technical Coordinator of
9、ASD-STANs Mechanical Domain. After inquiries and votes carried out in accordance with the rules of ASD-STAN defined in ASD-STANs General Process Manual, this standard has received approval for Publication. Copyright ASD-STAN Provided by IHS under license with AECMA Not for ResaleNo reproduction or n
10、etworking permitted without license from IHS-,-,-prEN 4623:20083 Introduction For design and installation procedures, see EN 4620 and EN 4619. 1 Scope This standard specifies the characteristics of self-locking, MJ thread inserts, self-broaching keys, in NI-PH2601, silver plated, for aerospace appli
11、cations. Classification: 1 550 MPa 1)/ 600 C 2)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 the referenced document (including any
12、amendments) applies. ISO 5855-1, Aerospace MJ threads Part 1: General requirements. ISO 5855-2, Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts. EN 2424, Aerospace series Marking of aerospace products. EN 2786, Aerospace series Electrolytic silver plating of fasteners. 3)EN 2952, Ae
13、rospace series Heat resisting alloy NI-PH2601 Solution treated and cold worked Bar for forged fasteners D 50 mm 1 270 MPa Rm 1 550 MPa. 3)EN 4619, Aerospace series Inserts, MJ threads, self-locking, with self-broaching keys Installation and removal procedure. 3)EN 4620, Aerospace series Inserts, MJ
14、threads, self-locking, with self-broaching keys Design standard. 3)EN 4621, Aerospace series Inserts, MJ threads, self-locking, self-broaching keys Technical specification. 3)TR 3198, Aerospace series Manufacturers identification monograms and marks for EN aerospace products. 4)1) Corresponds to the
15、 minimum tensile stress which the insert is able to withstand at ambient temperature without breaking or craking when tested with a bolt of a higher strength class. 2) Maximum temperature that the insert is able to withstand, without permanent alteration to its original characteristics, after ambien
16、t temperature has been restored. The maximum temperature is conditioned by the MoS2lubricant. 3) Published as ASD Prestandard at the date of publication of this standard. 4) Published as ASD Technical Report at the date of publication of this standard. Copyright ASD-STAN Provided by IHS under licens
17、e with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4623:20084 3 Required characteristics 3.1 Configuration Dimensions Tolerances Masses See Figure 1 and Tables 1, 2, 3 and 4. Dimensions and tolerances are in millimetres. They apply after silver plati
18、ng. 3.2 Material Insert: EN 2952 treated for 370 HV to 480 HV Keys: Stainless steel or Nickel alloy treated for HV 600 3.3 Surface treatment See EN 2786. 4 Insert definition See Figure 1. Values apply after silver plating. Remove sharp edges 0,1 mm to 0,4 mm. Key 1 N keys equally spaced 2 form out-o
19、f-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 of keys shall meet EN 4623 requirements Details of form not stated are le
20、ft to the producers discretion. Figure 1 5Ra3,2 only for key grooves and keys Ra1,6 Copyright ASD-STAN Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4623:20085 4.1 Normal size insert See Table 1. Table 1 A B CcD E F G
21、 N Internal thread aExternal thread bMass kg/1 000parts Code Designation Designation max. 0 0,2 max. 0 0,2 max. 050-0 MJ5x0,8-4H6H MJ9x1-4h6h 7,5 9 5 8 2 2,3 060-0 MJ6x1-4H5H MJ10x1-4h6h 8,5 10 6,5 10 2 3,4 070-0 MJ7x1-4H5H MJ11x1-4h6h 9,5 11 8 11,5 2 4,5 080-0 MJ8x1-4H5H MJ12x1-4h6h 10,5 12 9,5 13,
22、5 4 5,9 100-0 MJ10x1,25-4H5H MJ14x1-4h6h 12,5 14 12 4,35 16,5 4 9,2 aIn accordance with ISO 5855-2. bIn accordance with ISO 5855-1. cAfter deformation. 4.2 First repair size insert See Table 2. Table 2 A B CcD E F G N Internal thread aExternal thread bMass kg/1 000parts Code Designation Designation
23、max. 0 0,2 max. 0 0,2 max. 050-1 MJ5x0,8-4H6H MJ10x1-4h6h 7,5 10 5 8 2 2,8 060-1 MJ6x1-4H5H MJ11x1-4h6h 8,5 11 6,5 10 2 4,2 070-1 MJ7x1-4H5H MJ12x1-4h6h 9,5 12 8 11,5 2 5,6 080-1 MJ8x1-4H5H MJS13x1-4h6h 10,5 13 9,5 13,5 4 7,4 100-1 MJ10x1,25-4H5H MJ15x1-4h6h 12,5 15 12 4,35 16,5 4 11,3 aIn accordanc
24、e with ISO 5855-2. bIn accordance with ISO 5855-1 except MJS13x1-4h6h thread which shall be in accordance with Table 4. cAfter deformation. Copyright ASD-STAN Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4623:20086 4
25、.3 Second repair size insert See Table 3. Table 3 A B CcD E F G N Internal thread aExternal thread bMass kg/1 000parts Code Designation Designation max. 0 0,2 max. 0 0,2 max. 050-2 MJ5x0,8-4H6H MJ11x1-4h6h 7,5 11 5 8 2 3,5 060-2 MJ6x1-4H5H MJ12x1-4h6h 8,5 12 6,5 10 2 5,1 070-2 MJ7x1-4H5H MJS13x1-4h6
26、h 9,5 14 8 11,5 2 6,8 080-2 MJ8x1-4H5H MJ14x1-4h6h 10,5 15 9,5 13,5 4 8,9 100-2 MJ10x1,25-4H5H MJ16x1-4h6h 12,5 16 12 4,35 16,5 4 13,6 aIn accordance with ISO 5855-2. bIn accordance with ISO 5855-1 except MJS13x1-4h6h thread which shall be in accordance with Table 4. cAfter deformation. 4.4 Special
27、thread dimensions See Table 4. Table 4 Major diameter Pitch diameter Minor diameter Root radius External thread a max. min. max. min. max. min. max. min. MJS131-4h6h 13 12,888 12,350 12,275 11,845 11,709 0,18 0,15 aProfile in accordance with ISO 5855-1. Copyright ASD-STAN Provided by IHS under licen
28、se with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4623:2008 7 5 Designation EXAMPLE Description block INSERTS, SELF-LOCKING, SELF-BROACHING KEYS Identity block EN4623-050-0 Number of this standard Thread code (see Tables 1 to 3) NOTE The last digit
29、 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 and identification EN 2424, style F Manufacturers identification marks in accordance with the list for special identification marks in TR 3198. 7 Technical specification EN 4621 Copyright ASD-STAN Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-
