1、 ASD-STAN STANDARD NORME ASD-STAN ASD-STAN NORM ASD-STAN prEN 6096 Edition P2 February 2018 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: ENGL
2、ISH VERSION Aerospace series Bearing, spherical plain with self-lubricating liner, extra wide inner ring in corrosion resisting steel Dimensions and loads Inch series Luft- und Raumfahrt Gelenklager mit selbst schmierender Beschichtung, extra breitem Innenring aus korrosionsbestndigem Stahl Mae und
3、Belastungen Inch Reihe Srie arospatiale Rotule garniture autolubrifiante avec bague intrieure extra large en acier rsistant la corrosion Dimensions et charges Srie en inches This “Aerospace Series“ Prestandard has been drawn up under the responsibility of ASD-STAN (The AeroSpace and Defence Industri
4、es 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. Subsequent to the publication of this Prestandard, the technical content shall not be chan
5、ged 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 prEN will be submitted as a draft European Standard (prEN) to CEN (European Committee for
6、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 national standards conflicting with the EN. ASD-STAN Technical Commit
7、tee 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 use, including any patent infringement arising therefrom, is the sole responsibility o
8、f 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 any suggestions that may arise. All rights reserved. No parts of this publication may
9、 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-mail: salesasd-stan.org Web address: http:/www.asd-stan.org/ Edition approved for pu
10、blication 1st February 2018 Comments should be sent within six months after the date of publication to ASD-STAN Mechanical Domain prEN 6096:2018 (E) 2 Contents Page Foreword 3 Introduction 4 1 Scope 5 2 Normative references 5 3 Symbols and definitions . 6 4 Requirements . 6 4.1 Configuration, dimens
11、ions, tolerances and mass 6 4.2 Surface roughness . 6 4.3 Material 11 4.4 Surface treatment 11 4.5 Swaging groove . 11 4.6 Liner technology . 11 4.7 Loads . 11 4.8 Starting torque values 12 4.9 Temperature range . 13 5 Designation. 14 6 Marking 14 7 Technical specification . 14 8 Quality management
12、system 14 (informative) Standard evolution form . 15 Annex ABibliography . 16 prEN 6096:2018 (E) 3 Foreword This document (prEN 6096:2018) has been prepared by the Aerospace and Defence Industries Association of Europe Standardization (ASD-STAN). After enquiries and votes carried out in accordance w
13、ith the rules of this Association, this Standard has received the approval of the National Associations and the Official Services of the member of ASD, prior to its presentation to CEN. This document is currently submitted to the CEN Enquiry. prEN 6096:2018 (E) 4 Introduction This document is publis
14、hed at edition P2. Former P1 and drafts may exist of Airbus development only but without any ASD-STAN official publication. In consequence configuration management discrepancies with these unofficial documents are under Airbus responsibility. prEN 6096:2018 (E) 5 1 Scope This European standard speci
15、fies general characteristics of spherical plain bearings in corrosion resisting steel with self-lubricating liner, extra wide inner ring, inch series. They are intended for use in fixed or moving parts of the aircraft structure and control mechanisms. 2 Normative references The following documents a
16、re referred to in the text in such a way that some or all of their content constitutes requirements 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 2030, Aerospace ser
17、ies Steel X105CrMo17 (1.3544) Hardened and tempered Bars De 150 mm1)EN 2133, Aerospace series Cadmium plating of steels with specified tensile strength 1 450 MPa, copper, copper alloys and nickel alloys EN 2424, Aerospace series Marking of aerospace products EN 2755, Aerospace series Bearings, spher
18、ical plain in corrosion resisting steel with self-lubricating liner Elevated load at ambient temperature Technical specification2)EN 3161, Aerospace series Steel FE-PM3801 (X5CrNiCu17-4) Air melted, solution treated and precipitation treated, bar a or D 200 mm, Rm 930 MPa2) ISO 1101, Geometrical pro
19、duct specifications (GPS) Geometrical tolerancing Tolerances of form, orientation, location and run-out ISO 1132-1, Rolling bearings Tolerances Part 1: Terms and definitions ISO 1302, Geometrical product specifications (GPS) Indication of surface texture in technical product documentation ISO 1302,
20、Technical drawings Method of indicating surface texture ISO 8075, Aerospace-Surface treatment of hardenable stainless steel parts TR 4475, Aerospace series Bearings and mechanical transmissions for airframe applications Vocabulary 1) Published as ASD-STAN Standard at the date of publication of this
21、European standard (www.asd-stan.org). 2) Published as ASD-STAN Prestandard at the date of publication of this European standard (www.asd-stan.org). prEN 6096:2018 (E) 6 3 Symbols and definitions Symbols of limit deviations are in accordance with definitions of ISO 1132-1. maximum angle of tilt of th
22、e outer ring with respect to the inner ring, with the spherical surface of the outer ring being completely in contact with the inner ring Capermissible static axial load Cspermissible static radial load C25permissible dynamic radial load by 25 000 cycles dmpsingle plane mean bore diameter deviation
23、Dmpsingle plane mean outside diameter deviation dsdeviation of a single bore diameter Dsdeviation of a single outside diameter For definitions and vocabulary, see TR 4475. 4 Requirements 4.1 Configuration, dimensions, tolerances and mass Configuration, dimensions, tolerances and mass should be accor
24、ding to Figure 1, Figure 2 and Table 1. Table 1: dimensions and tolerances are expressed in millimetres (inches). Figure 1: dimensions and tolerances for Ra max. are expressed in m (in). Values apply after surface treatment. 4.2 Surface roughness Surface roughness should be according to Figure 1 and
25、 Figure 2. Values in micrometer (micro inches), apply prior to surface treatment. prEN 6096:2018 (E) 7 Key a) set-back b) optional from to permit grinding undercut c) TFE liner d) cadmium plated 1 type code D 2 type code E Figure 1 Code S without swaging groove prEN 6096:2018 (E) 8 Key a) swaging gr
26、oove b) set-back c) TFE liner d) cadmium plated e) optional form to permit grinding undercut 1 type code D 2 type code E Figure 2 Code R with swaging groove prEN 6096:2018 (E) 9 Table 1 Dimensions, tolerances and mass Diameter codeaDiameter B C D2 d3 D2 d D Limit deviation 0 +0,25 0 0 0,05 0 0,200 0
27、,200 dmpdsDmpDs(0 (+0.010 Ref. (0 (0 0.002) 0) 0.008) 0.008) 03 4,826 (0.1900) 14,288 (0.5625) 12,700 (0.500) 5,207 (0.205) 11,024 (0.434) 12,649 (0.498) 8,001 (0.315) 0 04 6,350 (0.2500) 18,796 (0.7400) 0,008 15,062 (0.593) 6,350 (0.250) 15,0602 (0.593) 17,170 (0.676) 9,703 (0.382) (0 0.0003) 05 7,
28、937 (0.3125) 23,012 (0.9060) 20,650 (0.813) 8,636 (0.340) 19,837 (0.781) 21,387 (0.842) 12,853 (0.506) 06 9,525 (0.3750) 13,259 (0.522) 0 0 07 11,113 (0.4375) 25,400 (1.0000) 0,013 0 0,013 22,225 (0.875) 22,225 (0.875) 22,809 (0.898) 15,545 (0.612) (0 0,010 (0 0.0005) (0 0.0005) 08 12,700 (0.5000) 2
29、8,575 (1.1250) 0.0004) 23,800 (0.937) 10,058 (0.396) 25,400 (1.000) 25,984 (1.023) 18,288 (0.720) 0 10 15,875 (0.6250) 34,925 (1.3750) 0,013 30,480 (1.200) 14,275 (0.562) 31,750 (1.250) 32,330 (1.273) 21,463 (0.845) (0 12 19,050 (0.7500) 39,688 (1.5625) 0.0005) 0 32,512 (1.280) 15,621 (0.615) 34,925
30、 (1.375) 36,500 (1.437) 24,257 (0.955) 0,010 14 22,225 (0.8750) 44,450 (1.7500) (0 35,560 (1.400) 15,748 (0.620) 38,887 (1.531) 41,275 (1.625) 28,296 (1.114) 0.0004) 16 25,400 (1.0000) 53,975 (2.1250) 47,625 (1.875) 21,082 (0.830) 47,625 (1.875) 50,800 (2.000) 32,055 (1.262) 20 31,750 (1.2500) 63,50
31、0 (2.5000) +0,003 0 +0,003 25,400 (1.000) 57,150 (2.250) 60,325 (2.375) 38,506 (1.516) 0,015 0,013 0,015 24 38,100 (1.5000) 76,200 (3.0000) (+0.0001 (0 (+0.0001 57,150 (2.250) 29,718 (1.170) 67,869 (2.672) 73,025 (2.875) 45,466 (1.790) 0.0006) 0.0005) 0.0006) 28 44,450 (1.7500) 90,488 (3.5625) 73,02
32、5 (2.875) 31,750 (1.250) 82,550 (3.250) 87,325 (3.438) 51,511 (2.028) prEN 6096:2018 (E) 10 Dia-meter codead4 P E L1 L2 r1 r2 r3 r4 r5 N bT Mass 0 0 +0,500 +0,20 0 +0,18 +0,20 +0,20 0,5 g/piece 0,20 0,254 0 0 0,25 0 0 0 (0 (0 (+0.020 (+0.008 (0 max. (+0.007 (+0.008 (+0.008 (0.02) max. min 0.008) 0.0
33、10) 0) 0) 0.010) 0) 0) 0) 03 5,230 (0.206) 0,635 (0.025) 2,032 (0.08) 0,127 (0.005) 0,610 (0.024) 0,130 (0.005) 0,127 (0.005) 0,508 (0.020) 0,508 (0.020) 0,508 (0.020) 20 0,508 (0.02) 15 0,076 (0.003) 8 04 6,750 (0.266) 24 17 05 8,340 (0.328) 3,048 (0.12) 30 23 36 06 9,930 (0.391) 0,711 (0.028) 21,5
34、 0,127 (0.005) 33 07 11,510 (0.453) 0,889 (0.035) 2,540 (0.100) 0,254 (0.010) 22 42 08 13,100 (0.516) 3,556 (0.14) 20 61 10 16,280 (0.641) 3,048 (0.12) 0,889 (0.035) 117 12 19,450 (0.766) 1,397 (0.055) 4,064 (0.16) 0,991 (0.039) 1,143 (0.045) 19 153 14 22,630 (0.891) 4,318 (0.17) 195 16 25,800 (1.01
35、6) 6,096 (0.24) 21 390 20 32,150 (1.266) 2,794 (0.11) 595 24 38,500 (1.516) 3,302 (0.13) 1020 28 44,850 (1.766) 4,318 (0.17) 28,5 1740 a The diameter code corresponds to bore diameter d in 1/16 inch. b The acceptance value is the maximum value for the user.prEN 6096:2018 (E) 11 4.3 Material Inner ri
36、ng: see EN 2030; hardness 55 HRC 62. Outer ring: see EN 3161, hardness 28 HRC 38; before swaging. Liner: self-lubricating liner per EN 2755. 4.4 Surface treatment Surface treatment should be as defined in chapter 5 (designation) with following codes: Code T: surface treatment according to ISO 8075 f
37、or inner ring before swaging. Outer ring: no treatment. Code P: surface treatment according to ISO 8075 for inner ring before swaging. Cadmium plating of outer ring according to EN 2133, 5 m to 8 m (0.2 in to 0.3 in). 4.5 Swaging groove Swaging groove should be described in chapter 5 (designation) w
38、ith following codes: Without swaging groove code S: Surface treatment according to ISO 8075 for inner ring before swaging. Cadmium plating of outer ring: 5 m to 8 m (0.2 in to 0.3 in) according to EN 2133. (Cylindrical surface area, chamfers and both end surfaces at manufactures option), followed by
39、 chromating. With swaging groove code R: Surface treatment according to ISO 8075 for inner ring before swaging. Cadmium plating of outer ring: 5 m to 8 m (0.2 in to 0.3 in) according to EN 2133. (cylindrical surface area, broken angles and radii, respectively, as well as both end surfaces up to the
40、swaging grooves), followed by chromating. 4.6 Liner technology Liner technology should be as defined in chapter 5 (designation) with following codes: code A : bonded liner technology; code B: injected or molded liner technology. without code: both technologies can be used. 4.7 Loads Loads should be
41、according to Table 2. prEN 6096:2018 (E) 12 Table 2 Loads Diameter codeaPermissible static load kN Ultimate static load kN Dynamic loadd kNradialb, e Csaxialb, c, f CaradialbaxialbradialgC2503 9,4h2,1 14,1h3,1 9,4h04 18,0h3,4 27,0h5,1 17,7 05 25,7h6,9 38,5h10,3 25,7h06 44,4h66,6h33,3 07 65,5h98,2h37
42、,4 08 91,3h9,7 136,9h14,5 50,6 10 139,2h27,6 208,8h41,4 87,3 12 209,7 31,4 314,5 47,2 102,5 14 235,7 32,1 353,6 48,1 115,2 16 364,8h62,5 547,2h93,7 197,0 20 594,6 94,5 891,9 141,7 290,7 24 838,0 133,1 1257,1 199,6 409,7 28 1094,7 153,5 1642,1 230,2 535,2 aThe diameter code corresponds to bore diamet
43、er d in 1/16 inch. bDefinition and testing for permissible and ultimate static loads according to EN 2755 and TR 4475. cThese values apply to loose spherical bearings. For installed bearings, the push-out loads may be smaller than these values. dDefinition and testing for dynamic radial load accordi
44、ng to EN 2755. ePermissible surface pressure 450 MPa, definition per TR 4475. fPermissible surface pressure for diameter code 03 to 08 150 MPa and for diameter code 10 to 28 225 MPa. gSurface pressure 220 MPa, definition per TR 4475. hLimit by bolt bending. Definition: solid shaft; rigid clamping on
45、 both sides; uniform load; permissible bending stress 1 350 MPa; pemissible shear stress 1 200 MPa. 4.8 Starting torque values Starting torque values should be according to Table 3. prEN 6096:2018 (E) 13 Table 3 Starting torque values Diameter codeaStarting torqueb Nm normal Code N reduced Code R 03
46、 0,06 0,34 0 0,11 04 0,11 0,56 05 06 07 0,03 0,15 08 10 12 14 0,23 0,90 0,04 0,25 16 20 0,23 1,50 0,05 0,32 24 0,11 0,32 28 a The diameter code corresponds to nominal diameter d in 1/16 inch. bDefinition and testing for starting torque according to EN 2755. 4.9 Temperature range They shall be used i
47、n the temperature range 55 C to 163 C. prEN 6096:2018 (E) 14 5 Designation EXAMPLE NOTE If necessary, the code I9005 shall be placed between the description block and the identity block. 6 Marking Marking should be according to EN 2424, style A. The marking position as per manufacturers option. Bear
48、ings ordered without technology code shall be delivered marked in accordance with its technology code. 7 Technical specification Technical specification should be according to EN 2755. 8 Quality management system The manufacturers operations shall be an approved production organisation for aerospace
49、 products and shall demonstrate that it has implemented and is able to maintain a quality management system (e. g. according to EN 9100 or another in aerospace accepted and established quality management system). The qualification procedure for aerospace standard products (e. g. according to EN 9133 or another in aerospace accepted and established qualification procedure) shall be
