ASD-STAN PREN 4836-2017 Aerospace series - Adaptor Pipe coupling 24 ne up to 35 000 kPa (5 080 psi) Ringlocked fitting Reducer-Flareless End - Inch Series - Extra Fine Thread Pitch.pdf

《ASD-STAN PREN 4836-2017 Aerospace series - Adaptor Pipe coupling 24 ne up to 35 000 kPa (5 080 psi) Ringlocked fitting Reducer-Flareless End - Inch Series - Extra Fine Thread Pitch.pdf》由会员分享，可在线阅读，更多相关《ASD-STAN PREN 4836-2017 Aerospace series - Adaptor Pipe coupling 24 ne up to 35 000 kPa (5 080 psi) Ringlocked fitting Reducer-Flareless End - Inch Series - Extra Fine Thread Pitch.pdf（13页珍藏版）》请在麦多课文档分享上搜索。

1、 ASD-STAN STANDARD NORME ASD-STAN ASD-STAN NORM ASD-STAN prEN 4836 Edition P1 2017-01 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: Descriptors: ENGLISH V

2、ERSION Aerospace series Adaptor, Pipe coupling 24Cone up to 35 000 kPa (5 080 psi) Ring-locked fitting Reducer- Flareless End Inch Series - Extra Fine Thread Pitch Luft- und Raumfahrt Adapter, Rohrverschraubung 24Konus bis 35 000 kPa (5 080 psi) gerade Anschlussverschraubung, reduziertes Rohrende mi

3、t Sicherungsring Inch Reihe - extra feine Gewindesteigung Srie arospatiale Adapteur, Systme de raccordement interface conique 24 jusqu 3500 kPa (5080 psi) Implantation pour raccord avec bague de scurit Sries inch - Filetage pas extra-fin Filetage pas extra-fin This “Aerospace Series” Prestandard has

4、 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 Industry. It has been technically approved by the experts of the concerned Domain following member comments. Sub

5、sequent 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, the ASD-STAN prE

6、N 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 to implement the EN at national level by giving the EN the status of a national standard and b

7、y withdrawing any national standards conflicting with the EN. ASD-STAN Technical Committee approves that: “This document is published by ASD-STAN for the needs of the European Aerospace Industry. The use of this standard is entirely voluntary and its applicability and suitability for any particular

8、use, including any patent infringement arising therefrom, is the sole responsibility of the user.” ASD-STAN reviews each standard and technical report at least every five years at which time it may be revised, reaffirmed, stabilized or cancelled. ASD-STAN invites you to send your written comments or

9、 any suggestions that may arise. All rights reserved. No parts of this publication may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording or otherwise, without prior written permission of ASD-STAN. Order details: E

10、-mail: salesasd-stan.org Web address: http:/www.asd-stan.org/ Edition approved for publication 1st January 2017 Comments should be sent within six months after the date of publication to ASD-STAN Mechanical domain Copyright 2017 ASD-STAN prEN 4836:2017 (E) 2 Contents Page Foreword 3 Introduction 3 1

11、 Scope . 4 2 Normative references . 4 3 Requirements 5 3.1 Configuration, Dimensions, Tolerances and Mass . 5 3.2 Material, Heat and Surface Treatment . 5 3.3 Surface texture 5 3.3.1 General . 5 3.3.2 Surface roughness 6 3.4 Sealing areas 6 3.5 Installation 6 3.6 Working pressure 6 4 Quality Assuran

12、ce . 10 5 Designation 11 6 Marking . 12 7 Packaging . 12 7.1 Packaging . 12 7.2 Labelling . 12 8 Technical Specification . 12 9 REACH 12 Bibliography . 13 prEN 4836:2017 (E) 3 Foreword This standard was reviewed by the Domain Technical Coordinator of ASD-STANs Mechanical Domain. After inquiries and

13、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. Introduction This standard is co-owned standard and a functional equivalent of AS5865. There should be no technical objection to use AS5865 as

14、replacement of EN 4836 parts. Table 3 shows the equivalent cross reference of EN 4836 part numbers to AS5865 part numbers. Further revisions to this standard shall be coordinated with the SAE committee. European Standards use the International System of units (SI); however, large segments of the aer

15、ospace industry make use of other measurement systems as a matter of common working practice. All dimensions and units used in this Standard are given in SI units, with other units also indicated for the convenience of the user. The decimal sign used in European Standards is the comma (“,”); however

16、, the comma is not used in common working practice with non-SI dimensions. Therefore, in common with many other aerospace standards, the decimal point (“.”) is used in this Standard when providing dimensions in inch-pound units. NOTE The use of non-SI units and the decimal point in this Standard doe

17、s not constitute general acceptance of measurement systems other than SI within European Standards. prEN 4836:2017 (E) 4 1 Scope This standard specifies the dimensions, tolerances, required characteristics and the mass of a reducer, flareless tube end EN 6123, ring locked type, for use in 35 000 kPa

18、 (5 080 psi) working pressure systems. 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 edition of the r

19、eferenced document (including any amendments) applies. EN 2424, Aerospace series Marking of aerospace products EN 3311, Aerospace series Titanium alloy TI-P64001 (Ti-6Al-4V) Annealed Bar for machining D 110 mm EN 3314, Aerospace series Titanium alloy TI-P64001 solution treated and aged Bar for machi

20、ning D 75 mm EN 4315, Aerospace series Heat resistance alloy FE-PA2601 (X6NiCrTiMoV26-15) Solution treated and precipitation treated, bar and section a or D 100 mm; Rm 900 MPa EN 4317, Aerospace series Heat resistance alloy FE-PA2601 (X6NiCrTiMoV26-15) Non heat treated, forging stock a or D 200 mm E

21、N 4832, Aerospace series Adaptor, Pipe coupling 24Cone up to 35 000 kPa (5 080 psi) Ring-locked fitting and Ring-locked fitting-reducer Inch Series Technical specification1)EN 4835, Aerospace series Installation and removal requirements for Ring locked fitting and reducer, 24Cone up to 35 000 kPa (5

22、 080 psi) Inch Series1) EN 6123, Aerospace series Fitting end, 24 internal cone, external thread, flareless type Extra fine thread pitch Inch series Design standard ISO 1302, Geometrical Product Specifications (GPS) Indication of surface texture in technical product documentation ISO 3161, Aerospace

23、 UNJ threads General requirements and limit dimensions ISO 4287, Geometrical Product Specification (GPS) Surface texture: Profile method Terms, definitions and surface texture parameters AMS 2486, Conversion coating of titanium alloys fluoride-phosphate type2)AMS 2488, Anodic treatment of titanium a

24、nd titanium alloys2)AMS 2700, Passivation of corrosion resistant steels2)AMS 5731, Steel bars, forgings, tubing and rings, corrosion and heat resistant 15Cr-25.5Ni-1.2Mo-2.1Ti-0.006B-0.30V solution heat treated2)1) Published as ASD-STAN Prestandard at the date of publication of this standard (www.as

25、d-stan.org). 2) Published by: SAE International (www.sae.org). prEN 4836:2017 (E) 5 AMS 5732, Steel bars, wire, forgings, tubing and rings, corrosion and heat resistant 15Cr-25.5Ni-1.2Mo-2.1Ti-0.006B-0.30V consumable electrode melted, 1 800 F (982 C), solution and precipitation heat treated2)AMS 573

26、4, Steel bars, forgings and tubing, corrosion and heat resistant 15Cr-25.5Ni-1.2Mo-2.1Ti-0.006B-0.30V consumable electrode melted, 1 650 F (900 C), solution and heat treated2)AMS 5737, Steel, corrosion and heat resistant, bars, wire, forgings, and tubing, and rings 15Cr-25.5Ni-1.2Mo-2.1Ti-0.006B-0.3

27、0V Consumable electrode melted, 1 650 F (900 C), solution and precipitation heat treated2)AMS 5853, Steel, corrosion and heat resistant, bars and wire 15Cr-25.5Ni-1.2Mo-2.1Ti-0.006B-0.30V consumable electrode melted. 1 650 F (900 C), solution treated and work-strengthened 160 ksi (1 103 MPa) tensile

28、 strength2)3 Requirements 3.1 Configuration, Dimensions, Tolerances and Mass The configuration, dimensions, tolerances and mass shall conform to Figure 1 and Table 2. Dimensions are expressed in millimetres (inch). Unless otherwise specified, the following tolerances are applicable: Linear dimension

29、s 0,13 mm ( 0.0050 inch). Angular tolerances 0 degrees 30 minutes. Break edges 0,08 mm to 0,38 mm (0.0030 inch to 0.0150 inch). 3.2 Material, Heat and Surface Treatment The material, heat and surface treatment shall be in accordance with Table 1. Table 1 Material, Heat and Surface Treatment Element

30、Material Heat Treatment Surface Treatment Adapter Titanium alloy type Ti-6Al-4V according to EN 3311 or EN 3314a130 KSI UTS min. Anodic treatment according to AMS 2488, type 2 or fluoride-phosphate conversion according to AMS 2486 Lockring CRES A286 according to AMS 5731, AMS 5732, or EN 4315, EN 43

31、17; AMS 5734, AMS 5737 or AMS 5853 34 to 40 HRC Passivated according to AMS 2700, Type 2 or 8. White color PTFE Coating for pressure class identification aStandards are equivalent to AMS 4928 or AMS 4965 or AMS 4967. 3.3 Surface texture 3.3.1 General Surface texture shall be in accordance with ISO 4

32、287. Symbols shall be in accordance with ISO 1302. prEN 4836:2017 (E) 6 3.3.2 Surface roughness Unless otherwise specified, the following surface roughness is applicable: Machined surfaces shall be 3,175 m (125 in) Ramax. Sealing surface shall be 1,6 m (63 in) Ramax. 3.4 Sealing areas Sealing surfac

33、es shall have no visible defects. 3.5 Installation Fitting assembly shall be installed according to EN 4835 (equivalent to AS5551). 3.6 Working pressure This part shall be designed for use in 35 000 kPa (5 080 psi) working pressure systems compatible with titanium. Key 1 Thread A 2 Thread B 3 Lockri

34、ng captivated 0 0.015 (0 0,381) from flange chamfer 4 End asper EN 6123 Style E 5 M (No. of serration) a Dimensions meet the minimum requirements of specification EN 6123 style E for pipe connection. b Sealing surfaces c Manufacturers identification marking location optional Lockring shall be retain

35、ed on fitting by controlled interference fit. Figure 1 Configuration prEN 4836:2017 (E) 7 Table 2 Dimensions, Tolerances and Mass (1 of 4) Dimensions in millimetres (inches) Size codea Nominal Tube Size Thread A ISO 3161 Class 3AbThread B ISO 3161 Class 3AbC D 06-04 6,350 (0.250 0) 0.4375-28UNJEF 0.

36、4375-20UNJF 17,78 (0.700 0) 6,93 7,62 (0.273 0 0.300 0) 08-06 9,525 (0.375 0) 0.5625-24UNJEF 0.5625-18UNJF 20,68 (0.814 0 ) 9,58 10,36 (0.377 0 0.408 0) 10-08 12,700 (0.500 0) 0.7500-20UNJEF 0.6875-24UNJEF 26,42 (1.040 0) 12,12 12,78 (0.477 0 0.503 0) 12-10 15,875 (0.625 0) 0.8750-20UNJEF 0.8125-20U

37、NJEF 29,72 (1.170 0) 14,63 15,60 (0.576 0 0.614 0) 16-12 19,050 (0.750 0) 1.0625-18UNJEF 1.1250-18UNJEF 36,98 (1.456 0) 20,42 21,62 (0.804 0 0.851 0) 20-16 25,400 (1.000 0) 1.3125-16UNJ 1.3125-18UNJEF 45,26 (1.782 0) 25,43 26,39 (1.001 0 1.039 0) 24-20 31,750 (1.250 0) 1.6250-16UNJ 1.6250-18UNJEF 51

38、,59 (2.031 0) 31,60 31,75 (1.244 1.250 0) a Size code corresponds to the nominal tube diameter in 1/16 inch b For Information only, please refer to EN 6123 c Tolerances K and N dimensions listed in Table 2 shall be used from May 2004. Before this date, tolerances of K and N dimensions were respectiv

39、ely + 0,25 mm / - 0,13 mm (+ 0.010 0 inch / - 0.005 0 inch ) and 0,51 mm ( 0.020 0 inch). prEN 4836:2017 (E) 8 Table 2 Dimensions, Tolerances and Mass (2 of 4) Dimensions in millimetres (inches) Size codea Nominal Tube Size E (+ 0,13 - 0,05) (+ 0.005 0 - 0.002 0) F min. G Ref. H 0,18 (0.007 0) 06-04

40、 6,350 (0.250 0) 9,25 (0.364 0) 11,58 (0.456 0) 13,82 (0.544 0) 5,33 (0.210 0) 08-06 9,520 (0.375 0) 12,24 (0.482 0) 14,58 (0.574 0) 17,02 (0.670 0) 10-08 12,700 (0.500 0) 15,88 (0.625 0) 18,21 (0.717 0) 20,93 (0.824 0) 12-10 15,875 (0.625 0) 18,72 (0.737 0) 22,63 (0.891 0) 24,92 (0.981 0) 5,59 (0.2

41、20 0) 16-12 19,050 (0.750 0) 25,40 (1.000 0) 29,31 (1.154 0) 31,78 (1.251 0) 20-16 25,400 (1.000 0) 31,12 (1.225 0) 35,03 (1.379 0) 37,24 (1.466 0) 6,10 (0.240 0) 24-20 31,750 (1.250 0) 38,15 (1.502 0) 42,06 (1.656 0) 44,91 (1.768 0) a Size code corresponds to the nominal tube diameter in 1/16 inch.

42、 b For Information only, please refer to EN 6123. c Tolerances K and N dimensions listed in Table 2 shall be used from May 2004. Before this date, tolerances of K and N dimensions were respectively + 0,25 mm / - 0,13 mm (+ 0.010 0 inch / - 0.005 0 inch ) and 0,51 mm ( 0.020 0 inch). prEN 4836:2017 (

43、E) 9 Table 2 Dimensions, Tolerances and Mass (3 of 4) Dimensions in millimetres (inches) Size codea Nominal Tube Size J + 0,25 - 0,13 (+ 0.010 0 - 0.005 0) Kc 0,13 ( 0.005 0) L - 0,38 (- 0.015 0) M 06-04 6,350 (0.250 0) 3,18 (0.125 0) 23,24 (0.915 0) 10,03 (0.395 0) 36 08-06 9,520 (0.375 0) 23,65 (0

44、.931 0) 10,92 (0.430 0) 40 10-08 12,700 (0.500 0) 26,04 (1.025 0) 11,81 (0.465 0) 38 12-10 15,875 (0.625 0) 3,99 (0.157 0) 27,53 (1.084) 13,39 (0.527 0) 40 16-12 19,050 (0.750 0) 29,44 (1.159 0) 14,33 (0.564 0) 36 20-16 25,400 (1.000 0) 29,62 (1.166 0) 14,45 (0.569 0) 56 24-20 31,750 (1.250 0) 30,15

45、 (1.187 0) 15,44 (0.608 0) 81 a Size code corresponds to the nominal tube diameter in 1/16 inch. b For Information only, please refer to EN 6123. c Tolerances K and N dimensions listed in Table 2 shall be used from May 2004. Before this date, tolerances of K and N dimensions were respectively + 0,25

46、 mm / - 0,13 mm (+ 0.010 0 inch / - 0.005 0 inch ) and 0,51 mm ( 0.020 0 inch). prEN 4836:2017 (E) 10 Table 2 Dimensions, Tolerances and Mass (4 of 4) Dimensions in millimetres (inches) Size codea Nominal Tube Size Mass max. (kg / part) 06-04 6,350 (0.250 0) 0,015 1 08-06 9,520 (0.375 0) 0,020 0 10-

47、08 12,700 (0.500 0) 0,035 9 12-10 15,875 (0.625 0) 0,046 4 16-12 19,050 (0.750 0) 0,074 9 20-16 25,400 (1.000 0) 0,100 8 24-20 31,750 (1.250 0) 0,143 7 a Size code corresponds to the nominal tube diameter in 1/16 inch. b For Information only, please refer to EN 6123. c Tolerances K and N dimensions

48、listed in Table 2 shall be used from May 2004. Before this date, tolerances of K and N dimensions were respectively + 0,25 mm / - 0,13 mm (+ 0.010 0 inch / - 0.005 0 inch ) and 0,51 mm ( 0.020 0 inch). 4 Quality Assurance Responsibility for Inspection Unless otherwise specified in the contract or pu

49、rchase order, the supplier is responsible for carrying out all inspections as required in this standard and qualification tests in accordance with the requirements of EN 9133 and EN 4832. The manufacturers operations shall be an approved production organisation for aerospace products and shall demonstrate that it has implemented and is able to maintain a quality system (e.g. according to EN 9100 or a