ASD-STAN PREN 3833-2015 Aerospace series Bolts MJ threads in heat resisting nickel base alloy NI-PH2601 (Inconel 718) passivated Classification 1 550 MPa (at ambient temperature) .pdf
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1、ASD-STAN STANDARD NORME ASD-STAN ASD-STAN NORM prEN 3833 Edition P 2 September 2015 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATION Rue Montoyer 10 - 1000 Brussels - Tel. 32 2 775 8126 - Fax. 32 2 775 8131 - www.asd-stan.org ICS: 49.030.20 Supersedes edition
2、 P 1 of July 1997 and will supersede EN 3833:2004 Descriptors: Aircraft industry, fastener, MJ-threads, nickel alloy, surface treatment, bolt, procurement, specification, characteristic, mechanical properties, test, mechanical test, quality assurance, qualification ENGLISH VERSION Aerospace series B
3、olts, MJ threads, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), passivated Classification: 1 550 MPa (at ambient temperature) / 650 C Technical specification Srie arospatiale Vis filetage MJ, en alliage rsistant chaud base de nickel NI-PH2601 (Inconel 718), passives Classification : 1
4、 550 MPa ( temprature ambiante) / 650 C Spcification technique Luft- und Raumfahrt Schrauben, MJ-Gewinde, aus hochwarmfester Nickelbasislegierung NI-PH2601 (Inconel 718), passiviert Klasse: 1 550 MPa (bei Raumtemperatur) / 650 C Technische Lieferbedingungen This “Aerospace Series“ Prestandard has be
5、en 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 Industry. It has been technically approved by the experts of the concerned Domain following member comments. Subseq
6、uent 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-identification of the standard. After examination and review by users and formal agreement of ASD-STAN, it will be submitte
7、d 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 to implement the EN at national level by giving the EN the status of a national standard and by withdrawing any
8、national standards conflicting with the EN. Edition approved for publication 1st September 2015 Comments should be sent within six months after the date of publication to ASD-STAN Mechanical Domain Copyright 2015 by ASD-STAN prEN 3833:2015 (E) 2 Contents Page Foreword 2 1 Scope 3 2 Normative referen
9、ces 3 3 Terms and definitions . 4 4 Quality assurance 5 5 Requirements . 6 Annex A (normative) Passivation treatment for bolts26 A.1 Pre-treatment26 A.2 Passivation .26 A.3 Water rinse .26 A.4 Finish 26 Annex B (informative) Tensile, stress rupture and tension fatigue Areas and loads formulae .27 B.
10、1 Cross sectional area values .27 B.2 Formulae .27 Annex C (informative) Standard evolution form .29 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 rules of ASD-STAN defined in ASD-S
11、TANs General Process Manual, this standard has received approval for Publication. prEN 3833:2015 (E) 3 1 Scope This standard specifies the characteristics, qualification and acceptance requirements for bolts with MJ threads in NI-PH2601, passivated, for aerospace applications. Classification: 1 550
12、MPa 1) /650 C 2) It is applicable whenever referenced. 2 Normative references The following documents, in whole or in part, are normatively referenced in this document and are indispensable for its application. For dated references, only the edition cited applies. For undated references, the latest
13、edition of the referenced document (including any amendments) applies. EN 9133, Aerospace series Quality management systems Qualification procedure for aerospace standard parts EN ISO 3452-1, Non-destructive testing Penetrant testing Part 1: General principles EN ISO 4288, Geometrical Product Specif
14、ications (GPS) Surface texture: Profile method Rules and procedures for the assessment of surface texture EN ISO 6508-1, Metallic materials Rockwell hardness test Part 1: Test method (scales A, B, C, D, E, F, G, H, K, N, T) EN ISO 6892-1, Metallic materials Tensile testing Part 1: Method of test at
15、room temperature EN ISO 6892-2, Metallic materials Tensile testing Part 2: Method of test at elevated temperature EN ISO 9227, Corrosion tests in artificial atmospheres Salt spray tests ISO 2859-1, Sampling procedures for inspection by attributes Part 1: Sampling schemes indexed by acceptance qualit
16、y limit (AQL) for lot-by-lot inspection ISO 5855-2, Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts ISO 7961, Aerospace Bolts Test methods ASTM E112-13, Standard Test Methods for Determining Average Grain Size 3). 1) Minimum tensile strength of the material at ambient temperature 2)
17、 Maximum test temperature of the parts 3) Published by: ASTM National (US) American Society for Testing and Materials. http:/www.astm.org prEN 3833:2015 (E) 4 3 Terms and definitions For the purposes of this standard, the following terms and definitions apply. 3.1 batch quantity of finished parts, o
18、f the same type and same diameter, produced from the same material obtained from the same melt, manufactured in the course of the same production cycle, following the same manufacturing route and having undergone all the relevant heat treatments and surface treatments 3.2 inspection lot quantity of
19、parts from a single production batch with the same part number which completely defines the part 3.3 Surface discontinuities 3.3.1 crack rupture in the material which may extend in any direction and which may be intercrystalline or transcrystalline in character 3.3.2 seam open surface defect 3.3.3 l
20、ap surface defect caused by folding over metal fins or sharp corners and then rolling or forging them into the surface 3.3.4 inclusions non-metallic particles originating from the material manufacturing process Note 1 to entry: These particles may be isolated or arranged in strings. 3.4 test tempera
21、ture ambient temperature unless otherwise specified 3.5 simple random sampling the taking of n items from a population of N items in such a way that all possible combinations of n items have the same probability of being chosen 3.6 critical defect a defect that, according to judgement and experience
22、, is likely to result in hazardous or unsafe conditions for individuals using, maintaining, or depending upon the considered product, or that is likely to prevent performance of the function of a major end item 3.7 major defect a defect other than critical, that is likely to result in a failure or t
23、o reduce materially the usability of the considered product for its intended purpose prEN 3833:2015 (E) 5 3.8 minor defect a defect that is not likely to reduce materially the usability of the considered product for its intended purpose, or that is a departure from established specification having l
24、ittle bearing on the effective use or operation of this product 3.9 sampling plan a plan according to which one or more samples are taken in order to obtain information and possibly to reach a decision 3.10 Limiting Quality LQ10 in a sampling plan, the quality limit which corresponds to a specified
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