ASD-STAN PREN 4833-2017 Aerospace series - Pipe coupling 24 one up to 35 000 kPa (5 080 psi) Ring locked fitting - Flareless End - Inch Series - Extra Fine Thread Pitch (Edition P1.pdf

1、 ASD-STAN STANDARD NORME ASD-STAN ASD-STAN NORM ASD-STAN prEN 4833 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 Pipe coupling 24 Cone up to 35 000 kPa (5 080 psi) Ring locked fitting Flareless End Inch Series Extra Fine Thread Pitch Luft- und Raumfahrt Rohrverschraubung 24 Konus bis 35 000 kPa (5 080 psi) gerade Anschlussverschraubung mit Sicherungsring Inch-Reihe extra feine Gewindest

3、eigung Srie arospatiale Systme de raccordement interface conique 24 jusqu 35 000 kPa (5 080 psi) Raccord implanter avec bague de scurit Srie inch Filetage pas extra-fin This “Aerospace Series” Prestandard has been drawn up under the responsibility of ASD-STAN (The AeroSpace and Defence Industries As

4、sociation 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 technical content shall not be changed t

5、o 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 prEN will be submitted as a draft European Standard (prEN) to CEN (European Committee for Stand

6、ardization) 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. ASD-STAN Technical Committee a

7、pproves 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 use, including any patent infringement arising therefrom, is the sole responsibility of the

8、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 any suggestions that may arise. All rights reserved. No parts of this publication may be re

9、produced, 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-mail: salesasd-stan.org Web address: http:/www.asd-stan.org/ Edition approved for publicati

10、on 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 4833:2017 (E) 2 Contents Page Foreword 3 Introduction 3 1 Scope . 4 2 Normative references . 4 3 Requirements 5 3.1 Configuration, Dimensions, Tolera

11、nces 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 Assurance . 10 5 Designation 11 6 Marking . 11 7 Preparation for delivery . 12 7.1 Packaging . 12 7

12、.2 Labelling . 12 8 Technical Specification . 12 9 REACH 12 Bibliography . 13 prEN 4833:2017 (E) 3 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-STA

13、Ns General Process Manual, this standard has received approval for Publication. Introduction This standard is co-owned standard and a functional equivalent of AS5550. There should be no technical objection to use AS5550 as replacement of EN 4833 parts. Table 3 shows the equivalent cross reference of

14、 EN 4833 part numbers to AS5550 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 aerospace industry make use of other measurement systems as a matter of common w

15、orking 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, the comma is not used in common working practice with non-SI dimensions. Th

16、erefore, 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 does not constitute general acceptance of measurement systems other than SI with

17、in European Standards. prEN 4833:2017 (E) 4 1 Scope This standard specifies the dimensions, tolerances, required characteristics and the mass of an adaptor, flareless tube end EN 6123, ring locked type, for use in 35 000 kPa (5 080 psi) working pressure systems. 2 Normative references The following

18、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 referenced document (including any amendments) applies. EN 2424, Aerospace se

19、ries 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 machining D 75 mm EN 4315, Aerospace series Heat resistance alloy FE-PA2601 (X6Ni

20、CrTiMoV26-15) 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 EN 4832, Aerospace series Pipe coupling 24Cone up to 35 000 kPa (5 080 psi) R

21、ing-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 (5 080 psi) Inch Series1)EN 6123, Aerospace series Fitting end, 24 internal cone, exter

22、nal thread, flareless type Extra fine thread pitch Inch series Design standardISO 1302, Geometrical Product Specifications (GPS) Indication of surface texture in technical product documentation ISO 3161, Aerospace UNJ threads General requirements and limit dimensions ISO 4287, Geometrical Product Sp

23、ecification (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 and titanium alloys2)AMS 2700, Passivation of corrosion resistant steels2)AMS 5731, Stee

24、l 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.asd-stan.org) 2)Published by: SAE International (www.sae.org) prEN 4833:2017 (E) 5 AMS 573

25、2, 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 5734, Steel bars, forgings and tubing, corrosion and heat resistant 15Cr-25.5Ni-1.2Mo-2.1Ti-0.

26、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-0.30V - Consumable electrode melted, 1 650 F (899 C), solution and precipitation heat treated2

27、)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 800F (982 C), solution treated and work-strengthened 160 ksi (1 103 MPa) tensile strength2)3 Requirements 3.1 Configuration, Dimensions, Tolerances and Mass The configura

28、tion, 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 dimensions 0,13 mm ( 0.0050 in); Angular tolerances 0 degrees 30 minutes; Break edges 0,08 mm (0.00

29、30 in ) to 0,38 mm (0.0150 in). 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 Material Heat Treatment Surface Treatment Adapter Titanium alloy type Ti-6Al-4V according to EN

30、3311 or EN 3314a 130 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 4317; AMS 5734, AMS 5737 or AMS 5853 34 to 40 HRC Passivated according to AMS 2700, Type 2 or 8.

31、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 4287. Symbols shall be in accordance with ISO 1302. prEN 4833:2017 (E) 6 3.3.2 Surface roughness

32、 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 surfaces shall have no visible defects. 3.5 Installation Fitting assembly shall be installed accordin

33、g 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 Lockring captivated 0 mm 0,381 mm (0 in - .015 in) from A thread chamfer 4 End according to EN 6123 S

34、tyle B 5 M (No. of Serration), see Table 2 a Dimensions meet the minimum requirements of EN 6123 Style B for pipe connection. Lockring shall be retained on fitting by controlled interference fit. b Sealing surfaces c Manufacturers identification marking location optional Figure 1 Configuration prEN

35、4833:2017 (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 04 6,35 (0.250 0) 0.4375 - 28UNJEF 0.3125 - 24UNJF 13,06 (0.514 0) 4,67 4,83 (0.184 0 0.190 0) 06 9,52 (0.375 0)

36、0.5625 - 24UNJEF 0.4375 - 20UNJF 17,78 (0.700 0) 7,47 7,62 (0.294 0 0.300 0) 08 12,700 (0.500 0) 0.7500 - 20UNJEF 0.5625 - 18UNJF 20,68 (0.814 0) 10,64 10,79 (0.419 0 0.425 0) 10 15,875 (0.625 0) 0.8750 - 20UNJEF 0.6875 - 24UNJEF 26,42 (1.040 0) 12,62 12,78 (0.497 0 0.503 0) 12 19,050 (0.750 0) 1.06

37、25 - 18UNJEF 0.8125 - 20UNJEF 29,72 (1.170 0) 16,59 16,74 (0.653 0 0.659 0) 16 25,400 (1.000 0) 1.3125 - 16UNJ 1.1250 - 18UNJEF 36,98 (1.456 0) 22,15 22,30 (0.872 0 0.878 0) 20 31,750 (1.250 0) 1.6250 - 16UNJ 1.3125 - 18UNJEF 45,26 (1.782 0) 27,69 27,84 (1.090 1.096 0) aSize code corresponds to the

38、nominal tube diameter in 1/16 inch. bFor Information only, please refer to EN 6123. cSuppliers may qualify with a reduced range within these dimensions. Refer to individual qualification reports for exact dimensions. prEN 4833:2017 (E) 8 Table 2 Dimensions, Tolerances and Mass (2 of 4) Dimensions in

39、 millimetres (inches) Size codea Nominal Tube Size DDcE +0,13 -0,05 ( +0.005 0 -0.002 0) F min. G Ref. H 0,13 ( 0.005) 04 6,35 (0.250 0) 4,06 4,44 (0.160 0 0.175 0) 6,07 (0.239 0) 8,41 (0.331 0) 10,16 (0.400 0) 19,10 (0.752 0) 06 9,52 (0.375 0) 6,93 7,62 (0.273 0 0.300 0) 9,25 (0.364 0) 11,58 (0.456

40、 0) 13,82 (0544 0) 20,04 (0.789 0) 08 12,700 (0.500 0) 9,58 10,36 (0.377 0 0.408 0) 12,24 (0.482 0) 14,58 (0.574 0) 17,02 (0.670 0) 22,40 (0.882 0) 10 15,875 (0.625 0) 12,12 12,78 (0.477 0 0.503 0) 15,87 (0.625 0) 18,21 (0.717 0) 20,93 (0.824 0) 24,00 (0.945 0) 12 19,050 (0.750 0) 14,63 15,60 (0.576

41、 0 0.614 0) 18,72 (0.737 0) 22,63 (0.891 0) 24,92 (0.981 0) 25,86 (1.018 0) 16 25,400 (1.000 0) 20,42 21,62 (0.804 0 0.851 0) 25,40 (1.000 0) 29,31 (1.154 0) 31,78 (1.251 0) 20 31,750 (1.250 0) 25,43 26,39 (1.001 0 1.039 0) 31,11 (1.225 0) 35,03 (1.379 0) 37,24 (1.466 0) 26,54 (1.045 0) aSize code c

42、orresponds to the nominal tube diameter in 1/16 inch. bFor Information only, please refer to EN 6123. cSuppliers may qualify with a reduced range within these dimensions. Refer to individual qualification reports for exact dimensions. prEN 4833:2017 (E) 9 Table 2 Dimensions, Tolerances and Mass (3 o

43、f 4) Dimensions in millimetres (inches) Size codea Nominal Tube Size J -0,38 (-0.015 0) K +0,25 -0,13 (+0.010 0 -0.005 0) L 0,18 (0.007 0) M 04 6,35 (0.250 0) 9,02 (0.355 0) 3,18 (0.125 0) 4,88 (0.192 0) 30 06 9,52 (0.375 0) 10,03 (0.395 0) 5,33 (0.210 0) 36 08 12,700 (0.500 0) 10,92 (0.430 0) 40 10

44、 15,875 (0.625 0) 11,81 (0.465 0) 38 12 19,050 (0.750 0) 13,39 (0.527 0) 3,99 (0.157 0) 5,59 (0.220 0) 40 16 25,400 (1.000 0) 14,33 (0.564 0) 36 20 31,750 (1.250 0) 14,45 (0.569 0) 6,10 (0.240 0) 56 aSize code corresponds to the nominal tube diameter in 1/16 inch. bFor Information only, please refer

45、 to EN 6123. cSuppliers may qualify with a reduced range within these dimensions. Refer to individual qualification reports for exact dimensions. prEN 4833:2017 (E) 10 Table 2 Dimensions, Tolerances and Mass (4 of 4) Dimensions in millimetres (inches) Size codea Nominal Tube Size Mass (kg / part) ma

46、x. 04 6,35 (0.250 0) 0,008 2 06 9,52 (0.375 0) 0,015 0 08 12,700 (0.500 0) 0,022 7 10 15,875 (0.625 0) 0,037 2 12 19,050 (0.750 0) 0,052 2 16 25,400 (1.000 0) 0,075 7 20 31,750 (1.250 0) 0,112 5 aSize code corresponds to the nominal tube diameter in 1/16 inch. bFor Information only, please refer to

47、EN 6123. cSuppliers may qualify with a reduced range within these dimensions. Refer to individual qualification reports for exact dimensions. 4 Quality Assurance Unless otherwise specified in the contract or purchase order, the supplier is responsible for carrying out all inspections as required in

48、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

49、 EN 9100 or another in aerospace accepted and established quality management system). Unless otherwise specified, the supplier may use his own facilities or any commercial laboratory acceptable to the procuring activity. The purchaser reserves the right to perform any of the inspections set out in the procurement specification where such inspections are deemed necessary to ensure