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    ASD-STAN PREN 4710-06-2014 Aerospace series Quick release fastening systems for non-structural applications Part 06 Stud - quick-release and locking (Edition P 1).pdf

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    ASD-STAN PREN 4710-06-2014 Aerospace series Quick release fastening systems for non-structural applications Part 06 Stud - quick-release and locking (Edition P 1).pdf

    1、ASD-STAN STANDARD NORME ASD-STAN ASD-STAN NORM prEN 4710-06 Edition P 1 February 2014 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATIONRue Montoyer 10 - 1000 Brussels - Tel. + 32 2 775 8126 - Fax. + 32 2 775 8131 - www.asd-stan.orgICS: Descriptors: ENGLISH VER

    2、SION Aerospace series Quick release fastening systems for non-structural applications Part 06: Stud - quick-release and locking Srie arospatiale Fixations rapides filetes pour applications non-structurales Partie 06 : Pion dmontage et verrouillage rapide Luft- und Raumfahrt Druckverschlsse nicht-str

    3、ukturelle Anwendungen Teil 06: Bolzen - Schnell Auslsend und Schlieend This “Aerospace Series“ Prestandard has been drawn up under the responsibility of ASD-STAN (The AeroSpace and Defence Industries Association of Europe - Standardization). It is published for the needs of the European Aerospace In

    4、dustry. It has been technically approved by the experts of the concerned Domain following member comments. Subsequent to the publication of this Prestandard, the technical content shall not be changed to an extent that interchangeability is affected, physically or functionally, without re-identifica

    5、tion 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 (European Committee for Standardization) for formal vote and transformation to full European Standard (EN). The CEN national members have then

    6、 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 approved for publication 28 February 2014 Comments should be sent within six months after the date of publication to ASD-STAN Mechanica

    7、l Domain Copyright 2014 by ASD-STAN prEN 4710-06:2014 (E) 2 Contents Page Foreword 2 1 Scope 3 2 Normative references 3 3 Requirements . 4 4 Designation 7 5 Marking . 7 6 Technical specification . 8 Foreword This standard was reviewed by the Domain Technical Coordinator of ASD-STANs Mechanical Domai

    8、n. 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. prEN 4710-06:2014 (E) 3 1 Scope This standard specifies the dimensions, mass, tolerances and static values of stud - qui

    9、ck-release and locking for use in fuselage interior equipment and non- structural or secondary structural area. This standard part shall be used in conjunction with EN 4710-03, EN 4710-04, EN 4710-05 and EN 4710-07 as described in EN 4710-02. The applicable temperature range is 55 C to 85 C. 2 Norma

    10、tive 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 amendments) applies. EN 2424, Aerospace series Marking

    11、 of aerospace products EN 2516, Aerospace series Passivation of corrosion resistant steels and decontamination of nickel base alloys EN 4710-01, Aerospace series Quick release fastening systems for non-structural applications Part 01: Technical specification 1)EN 4710-02, Aerospace series Quick rele

    12、ase fastening systems for non-structural applications Part 02: Stud spring clamp family 1)EN 4710-03, Aerospace series Quick release fastening systems for non-structural applications Part 03: Spring clamp 1)EN 4710-04, Aerospace series Quick release fastening systems for non-structural applications

    13、Part 04: Spring clamp One way tolerance compensation 1)EN 4710-05, Aerospace series Quick release fastening systems for non-structural applications Part 05: Spring clamp Two ways tolerance compensation 1)EN 4710-07, Aerospace series Quick release fastening systems for non-structural applications Par

    14、t 07: Retaining grommet 1)EN 10088-3, Stainless steels Part 3: Technical delivery conditions for semi-finished products, bars, rods, wire, sections and bright products of corrosion resisting steels for general purposes EN 12165, Copper and copper alloys Wrought and unwrought forging stock ISO 1456,

    15、Metallic coatings Electrodeposited coatings of nickel plus chromium and of copper plus nickel plus chromium ISO 2768-1:1989, General tolerances Part 1: Tolerances for linear and angular dimensions without individual tolerance indications ISO 2768-2:1989, General tolerances Part 2: Geometrical tolera

    16、nces for features without individual tolerance indications 1) Published as ASD-STAN Prestandard at the date of publication of this standard. http:/www.asd-stan.org/ prEN 4710-06:2014 (E) 4 3 Requirements 3.1 Configuration, dimensions, tolerances and mass The configuration, dimensions, tolerances and

    17、 mass shall conform with Figure 1 and Table 1. Tolerances not specified, shall be in accordance with ISO 2768-mK (ISO 2768-1:1989 and ISO 2768-2:1989). Dimensions are unless otherwise specified per manufacturers option. Figure 1 Configuration pin Px prEN 4710-06:2014 (E) 5 Figure 2 shows an example

    18、of installation of EN 4710-06 (1), EN 4710-07 (2) and EN 4710-03 to EN 4710-05 (3). H shows the maximum thickness of parts assembled with the used pin. Key 1 Stud as per EN 4710-06 (1) 2 Grommet as per EN 4710-07 (2) 3 Spring Clamp as per EN 4710-03 to EN 4710-05 (3) Figure 2 Grip range H prEN 4710-

    19、06:2014 (E) 6 Table 1 Dimensions and mass Dimensions in millimetres Type code Length code b D1 D2 D3h1h2l1l2l3H r1r2r3Mass Aprox. 0,1 0 0 0,1 0,1 0,1 max. min. g PS 020 1,0 8,0 2,6 3,9 2,2 1,0 11,2 7,9 9,3 2,9 1,0 0,5 0,1 1,4 025 11,6 9,7 3,3 1,4030 12,2 10,3 3,9 1,4035 12,6 10,7 4,3 1,4040 13,0 11,

    20、1 4,7 1,5045 13,4 11,5 5,1 1,5 050 13,9 12,0 5,6 1,5060 15,0 13,1 6,7 1,6070 16,0 14,1 7,7 1,6080 17,2 15,3 8,9 1,7090 18,2 16,3 9,9 1,7 100 19,2 17,3 10,9 1,8120 21,2 19,3 12,9 1,9PM 020 1,5 11,0 4,5 6,3 2,4 1,0 15,6 11,9 13,4 3,3 1,6 1,0 3,9 030 16,6 14,4 4,3 4,0040 17,6 15,4 5,3 4,2050 18,6 16,4

    21、6,3 4,4060 19,8 17,6 7,5 4,6070 20,6 18,4 8,3 4,7080 21,8 19,6 9,5 4,8090 22,6 20,4 10,3 4,9100 23,6 21,4 11,3 5,0110 24,6 22,4 12,3 5,2120 25,8 23,6 13,5 5,4130 26,8 24,6 14,5 5,6 140 27,6 25,4 15,3 5,9160 29,6 27,4 17,3 6,0180 31,6 29,4 19,3 6,2200 33,8 31,6 21,5 6,5220 35,6 33,4 23,3 6,8 PL 040 2

    22、,0 16,0 6,5 9,4 3,3 1,5 22,2 15,7 18,4 6,1 2,5 1,5 10,9 050 23,2 19,4 7,1 11,2060 24,2 20,4 8,1 11,5080 26,2 22,4 10,1 12,1100 28,1 24,3 12,0 12,7120 30,1 26,3 14,0 13,3 140 32,4 28,6 16,3 13,9160 34,1 30,3 18,0 14,5180 36,0 32,2 19,9 15,1200 38,1 34,3 22,0 15,7prEN 4710-06:2014 (E) 7 3.2 Mechanical

    23、 characteristics Ultimate loads, see Table 2. Table 2 Loads Type code Ultimate tensile loads Ultimate share loads Push-in loads Torque-out Material code N N N max. N cm PS 500 300 30 5 - 15 C B PM 900 600 30 5 - 15 C B PL 2 000 1 500 80 30 - 50 C B 3.3 Material and surface treatment Materials and fi

    24、nished shall be in accordance with the Table 3. Table 3 Materials and surface treatment Material code Material Surface treatment C Stainless steel 1.4301 per EN 10088-3 Passivated per EN 2516 B CuZn39Pb3 or CuZn39Pb2 per EN 12165 Electrodeposited coatings per ISO 1456 4 Designation EXAMPLE Descripti

    25、on block STUD - QUICK RELEASE AND LOCKING Identity block EN4710-06PM080C Number of the basic standard Standard family number Type code (see Table 1) Length code (see Table 1) Material code (see Table 3) 5 Marking EN 2424, style F prEN 4710-06:2014 (E) 8 6 Technical specification Required tests for a

    26、cceptance and qualification shall be in accordance to Table 4. Table 4 Requirements, inspections and tests Characteristic Requirements Requirements as per EN 4710-01 Inspections and tests as per EN 4710-01 A aQ bMaterials In accordance with Table 3. 4.1 5.4.1 X X Dimensions and masses In accordance

    27、with Table 1. 4.2 5.4.2 X X Surface defects Refer to EN 4710-01. 4.3.1 5.4.3.1 X X Surface treatment In accordance with Table 3. 4.3.2 5.4.3.2 X X Ultimate tensile loads In accordance with Table 2. 4.4.1 5.4.4.1 X Ultimate share loads In accordance with Table 2. 4.4.2 5.4.4.2 X Push-in load In accor

    28、dance with Table 2. 4.4.3 5.4.4.3 X Torque-out In accordance with Table 2. 4.4.4 5.4.4.4 X Corrosion resistance Refer to EN 4710-01. 4.5 5.4.5 X Functionality Refer to EN 4710-01. 4.7.1 5.4.7.1 X Endurance Material code C per Table 3: 500 cycles.Material code B per Table 3: 1 500 cycles. 4.7.2 5.4.7.2 X Identification marking of the product Refer to EN 4710-01. 4.8.1 5.4.8.1 X X Identification marking of the package Refer to EN 4710-01. 4.8.2 5.4.8.2 X X aAcceptance test. bQualification test.


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