ASD-STAN PREN 4510-2017 Aerospace series - Pipe coupling 60 spherical in titanium alloy TIP64001 port adapter straight double end with locking ring (Edition P1).pdf

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1、 ASD-STAN STANDARD NORME ASD-STAN ASD-STAN NORM ASD-STAN prEN 4510 Edition P1 2017-09 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.orgICS: Descriptors: ENGLISH VE

2、RSION Aerospace series Pipe coupling, 60, spherical, in titanium alloy TI-P64001, port adapter, straight, double end, with locking ring Luft- und Raumfahrt Rohrverschraubung mit Kugelbuchse, 60, aus Titanlegierung TI-P64001, gerade Anschluverschraubung mit Sicherungsring Srie arospatiale Raccord sph

3、rique, 60, en alliage de titane TI-P64001, raccord droit, planter, avec bague de freinage 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 Eu

4、ropean 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 to an extent that interchangeability is affected, physically or functionally, wi

5、thout 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 Standardization) for formal vote and transformation to full European Standard (EN).

6、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 approves that: “This document is published by ASD-STAN for the needs of the Euro

7、pean 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 user.” ASD-STAN reviews each standard and technical report at least every five

8、 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 reproduced, stored in a retrieval system or transmitted, in any form or by any m

9、eans, 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 publication 1stSeptember 2017 Comments should be sent within six months after the date

10、 of publication to ASD-STAN Mechanical Domain prEN 4510:2017 (E) 2 Contents Page Foreword 3 Introduction 4 1 Scope 5 2 Normative references 5 3 Requirements characteristics 6 4 Quality Assurance Responsibility for Inspection . 9 5 Designation. 10 6 Identification marking . 10 7 Preparation for deliv

11、ery 10 8 Technical Specification 10 Bibliography . 11 prEN 4510:2017 (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-STANs General Process Manua

12、l, this standard has received approval for Publication. prEN 4510:2017 (E) 4 Introduction This standard is a co-owned standard and a functional equivalent of SAE MA 2113. Further revisions to this standard shall be coordinated with the SAE committee. prEN 4510:2017 (E) 5 1 Scope This standard specif

13、ies the characteristics of the pipe coupling adapter, 60 spherical sealing face manufactured in titanium alloy with locking ring, for installing in a boss for aerospace applications. These adapters shall be installed into port connections manufactured in accordance with EN 2602 using ISO 3601-1 seal

14、ing O-rings selected sizes. O-ring material depends on the system fluid and operation conditions. The installation shall be performed in accordance with EN 2608. Nominal working pressure: up to 28 000 kPa. Temperature range: limited by elastomeric sealing ring, 54 C to +135 C 2 Normative references

15、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 referenced document (including any amendments) applies. EN 2424

16、, Aerospace series Marking of aerospace products EN 2491, Aerospace series Molybdenum disulphide dry lubricants Coating methods EN 2602, Aerospace series Ports for adaptors, threaded, with lockring Geometric configuration EN 2603, Aerospace series Port ends for adaptors, threaded, with lockring Geom

17、etric configuration EN 2606, Aerospace series 60 interface for adaptors, threaded, with lockring Geometric configuration EN 2608, Aerospace series Installation and removal requirements for 830 adaptors, threaded, with lockring EN 2645, Aerospace series Lockrings for adaptors, threaded, with lockring

18、 Dimensions EN 3079, Aerospace series Pipe coupling 830 up to 28 000 kPa Adaptors Metric series Technical specification 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; ba

19、r for machining D 75 mm EN 4315, Aerospace series Heat resisting 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 resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) Non heat treated, forging stock a or D

20、 200 mm EN ISO 286-2, Geometrical product specifications (GPS) ISO code system for tolerances on linear sizes Part 2: Tables of standard tolerance classes and limit deviations for holes and shafts prEN 4510:2017 (E) 6 ISO 3601-1, Fluid power systems O-rings Part 1: Inside diameters, cross-sections,

21、tolerances and designation codes ISO 5855-3, Aerospace MJ threads Part 3: Limit dimensions for fittings for fluid systems ISO 7169, Aerospace Separable tube fittings for fluid systems, for 24 cones, for pressures up to 3 000 psi or 21 000 kPa. Procurement specification, inch/metric 3 Requirements ch

22、aracteristics 3.1 Configuration Dimensions Tolerances Mass According to Figure 1 and Figure 2 and Table 1 and Table 2. Dimensions are in mm and apply before lubricating or anodizing. The dimensions specified are those required by design to meet installation and system requirements. The dimensions no

23、t specified are at manufactures option providing that the qualification and acceptance requirements of EN 3079, type II are met. 3.2 Surface roughness According to Figure 1 and Figure 2 unless otherwise specified in the design documentation. Sealing surfaces roughness 1,6 m. 3.3 Material Adapter: EN

24、 3311 or EN 3314; Alternative: AMS 4928, AMS 4965 or AMS 4967. Heat treatment to 900 MPa, minimum. Locking ring: EN 4315 or EN 4317. Alternative: AMS 5731 or AMS 5734. 3.4 Surface treatment Adapter: Lubrication: according to EN 2491, on all surfaces except in the flow hole; Prior to application of t

25、he lubricant, the surface shall be abrasive blasted using non-metallic grit; Film thickness: 0,005 mm to 0,013 mm. Alternative: Anodizing according to AMS 2488 type 2. Locking ring: prEN 4510:2017 (E) 7 Passivated as per AMS 2700, type 2 or type 8. NOTE Type 2 is chromate loaded, affected by REACH r

26、egulation. Dimensions in millimetres Key Fitted Dimension For design use only 1 Thread C 2 Identity Marking 3 Fitting end per EN 2606 for tube size specified 4 Locking ring per EN 2645 for ring size specified. Located 0 to 0,4 from thread “A” chamfer. 5 Port end per EN 2603 for tube size specified.

27、6 Thread D7 a Sealing surface: No visible defects. To be protected for shipment. b Sealing surface: No visible defects. To be protected for shipment. Figure 1 Adapter Assembly prEN 4510:2017 (E) 8 For dimensions not specified refer to the following specifications: For tube end EN 2606; For Port end

28、EN 2603; For locking ring EN 2645. Figure 2 Configuration for sizes 06, 16, 18 and 20 Table 1 Dimensions Dimensional size codea Nominal tube Thread Thread A ref D D1 DD D10ref D18ref Cb D7b4g6g 4h6h 0,09 +0,20+0,200,050,2 +0,150,05min. 0604 4,0 MJ10 1 MJ6 1 12,90 2,50 4,50 7,10 0806 6,0 MJ12 1,25 MJ

29、8 1 14,75 4,50 4,40 12,85 6,50 9,05 1208 8,0 MJ16 1,5 MJ12 1,25 19,50 7,70 10,20 12,78 1410 10,0 MJ18 1,5 MJ14 1,5 21,00 9,00 11,90 14,38 1612 12,0 MJ20 1,5 MJ16 1,5 22,60 10,70 13,90 16,36 1814 14,0 MJ22 1,5 MJ18 1,5 26,40 12,50 15,90 18,37 2016 16,0 MJ24 1,5 MJ20 1,5 28,00 14,50 14,20 15,05 17,90

30、20,37 2218 18,0 MJ27 1,5 MJ22 1,5 30,20 16,50 15,90 16,00 19,90 22,38 2420 20,0 MJ30 1,5 MJ24 1,5 33,70 18,50 17,65 16,00 21,90 24,35 aDimensional size code: Thread diameter of port end (thread D7) and nominal tube diameter of nut end (thread C). bIn accordance with ISO 5855-3. prEN 4510:2017 (E) 9

31、Table 2 Dimensions and weights Dimensionalsize codeaJ H L14ref L16ref G ref Weight kg/ea NcLocking ring codeb0,2 +0,050+0,150,100,2 max. 0604 9,37 16,35 7,95 3,00 5,3 0,007 10,8 077 0806 11,53 18,85 8,60 3,00 6,1 0,010 12,75 098 1208 15,37 21,60 10,00 3,00 7,0 0,019 15,0 136 1410 17,12 21,65 10,65 3

32、,00 7,0 0,022 15,0 153 1612 18,77 21,85 11,30 3,00 7,0 0,025 15,2 170 1814 20,93 21,85 12,00 3,00 7,0 0,033 15,2 192 2016 23,85 22,65 12,70 3,00 7,0 0,037 15,0 214 2218 24,92 23,25 13,35 3,00 7,0 0,044 15,6 281 2420 27,41 23,25 14,00 3,00 7,0 0,050 15,6 253 aDimensional size code: Thread diameter of

33、 port end (thread D7) and nominal tube diameter of nut end (thread C). bLocking ring retained an union by interference fit, dimensional details in accordance with EN 2645. cAdapters to be installed in accordance with EN 2608, into port cavities produced in accordance with EN 2602. Dimension “N” for

34、design only. Tolerance in accordance with ISO 286-2. Dimensions marked ref are for reference only and should be checked in the EN standard from which they are taken: EN 2603 for EN 2603 for D7, D10, D18, L14and L16; EN 2645 for A and G. 4 Quality Assurance Responsibility for Inspection Unless otherw

35、ise specified in the contract or purchase 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 the technical specification. The manufacturers operations shall be an approved product

36、ion 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 another in aerospace accepted and established quality management system). prEN 4510:2017 (E) 10 5 Designation EXAMPLE NOTE If necessary, the co

37、de I9005 shall be placed between the description block and the identity marking. 6 Identification marking The adaptors shall be legibly and permanently marked as per EN 2424 style A as indicated in Figure 1 with the following: Manufacturers name; or trademark: or cage code Manufacture identification

38、 stamp on the locking ring shall be, either on the upper surface or in the groove. The method of marking shall be laser marking or impression stamping. 7 Preparation for delivery 7.1 Packaging All parts shall be delivered individually in suitable bags. Bags and tags shall be marked as per EN 2424 st

39、yle G. Sealing surfaces shall be protected for shipment. 7.2 Labelling All packages shall be legibly marked with the following: part number and name; trademark and cage code. 8 Technical Specification EN 3079 in combination with ISO 7169. All products supplied to this specification shall be manufact

40、ured by a manufacture listed in the Qualified Products List (QPL) of the appropriate accrediting body, e.g. ASD-CERT, or Performance Review Institute (PRI). prEN 4510:2017 (E) 11 Bibliography 1 EN 9100, Quality Management Systems Requirements for Aviation, Space and Defence Organizations 2 EN 9133,

41、Aerospace series Quality management systems Qualification procedure for aerospace standard parts 3 AMS 2488, Anodic Treatment Titanium and Titanium Alloys Solution pH 13 or Higher1)4 AMS 4928, Titanium Alloy Bars, Wire, Forgings, Rings, and Drawn Shapes 6Al - 4V Annealed1)5 AMS 4965, Titanium Alloy,

42、 Bars, Wire, Forgings, and Rings, 6.0AI - 4.0V, Solution Heat Treated and Aged1)6 AMS 4967, Titanium Alloy, Bars, Wire, Forgings, and Rings 6.0Al - 4.0V Annealed, Heat Treatable1)7 AMS 5731, Steel, Steel, Corrosion and Heat Resistant, Bars, Wire, Forgings, Tubing, and Rings 15Cr 25.5Ni 1.2Mo 2.1Ti 0

43、.006B 0.30V, Consumable Electrode Melted, 1 800 F (982 C) Solution Heat Treated1)8 AMS 5734, Steel, Corrosion and Heat Resistant, Bars, Wire, Forgings, and Tubing 15Cr 25.5Ni 1.2Mo 2.1Ti 0.006B 0.30V, Consumable Electrode Melted, 1 650 F (899 C) Solution Heat Treated1)1) Published by: Society of Automotive Engineers, Inc (SAE), 400 Commonwealth Drive, Warrendale; PA 15096-001.