EN 4535-2:2016

Aerospace series - Bushes, flanged in aluminium alloy with self-lubricating liner, elevated load - Part 2: Dimensions and loads - Inch series

This European Standard specifies the characteristics of bushes flanged in aluminium alloy with self-lubricating liner elevated load for aerospace applications.
The bushes are intended for use in fixed or moving parts of the aircraft structure and control mechanisms.
They shall be used in the temperature range -55 °C to 121 °C.

Luft- und Raumfahrt - Buchsen mit Flansch aus Aluminiumlegierung, mit selbstschmierender Beschichtung, erhöhte Belastung - Teil 2: Maße und Belastungen - Inch-Reihe

Diese Europäische Norm legt die Eigenschaften von Buchsen mit Flansch aus Aluminiumlegierung, mit selbstschmierender Beschichtung, erhöhter Belastung, für die Anwendung in der Luft- und Raumfahrt fest.
Die Buchsen sind für den Einsatz in starren oder beweglichen Teilen der Luftfahrzeugstruktur und der Betätigungsvorrichtungen vorgesehen.
Sie sind für den Einsatz im Temperaturbereich von −55 °C bis 121 °C bestimmt.

Série aérospatiale - Bagues à épaulement en alliage d'aluminium à garniture autolubrifiante, charge élevée - Partie 2: Dimensions et charges - Série en inches

Aeronavtika - Puše s prirobnico iz aluminijeve zlitine s samomazalno oblogo, serija za večje obremenitve - 2. del: Mere in nosilnosti - Colski tip

Ta evropski standard določa lastnosti puš s prirobnico iz aluminijeve zlitine s samomazalno oblogo, serija za večje obremenitve za uporabo v aeronavtiki.
Puše so namenjene za uporabo v fiksnih ali premikajočih se delih ogrodja letala in nadzornih mehanizmih.
Uporabljati jih je treba v temperaturnem razponu –55 °C do 121 °C.

General Information

• Status: Published
• Publication Date: 06-Sep-2016
• Withdrawal Date: 30-Mar-2017
• ICS: 49.035 - Components for aerospace construction
• Technical Committee: ASD-STAN - Aerospace
• Drafting Committee: ASD-STAN/D 3 - Mechanical
• Current Stage: 6060 - Definitive text made available (DAV) - Publishing
• Start Date: 07-Sep-2016
• Completion Date: 07-Sep-2016
• Ref Project: SIST EN 4535-2:2016 - Aerospace series - Bushes, flanged in aluminium alloy with self-lubricating liner, elevated load - Part 2: Dimensions and loads - Inch series

Relations

• Replaces: EN 4535-2:2009 - Aerospace series - Bushes, flanged in aluminium alloy with self-lubricating liner, elevated load - Part 2: Dimensions and loads - Inch series
• Effective Date: 04-Feb-2015

Standards Content (Sample)

2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Luft- und Raumfahrt - Buchsen mit Flansch aus Aluminiumlegierung, mit selbstschmierender Beschichtung, erhöhte Belastung - Teil 2: Maße und Belastungen - Inch-ReiheSérie aérospatiale - Bagues à épaulement en alliage d'aluminium à garniture autolubrifiante, charge élevée - Partie 2: Dimensions et charges - Série en inchesAerospace series - Bushes, flanged in aluminium alloy with self-lubricating liner, elevated load - Part 2: Dimensions and loads - Inch series49.035Sestavni deli za letalsko in vesoljsko gradnjoComponents for aerospace construction49.025.20AluminijAluminiumICS:Ta slovenski standard je istoveten z:EN 4535-2:2016SIST EN 4535-2:2016en,fr,de01-november-2016SIST EN 4535-2:2016SLOVENSKI
STANDARDSIST EN 4535-2:20091DGRPHãþD

EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 4535-2
September
t r s x ICS
v {ä r u w Supersedes EN
v w u wæ tã t r r {English Version
Aerospace series æ Bushesá flanged in aluminium alloy with selfælubricating linerá elevated load æ Part
tã Dimensions and loads æ Inch series Sßrie aßrospatiale æ Bagues à ßpaulement en alliage d 5aluminium à garniture autolubrifianteá charge ßlevße æ Partie
tã Dimensions et charges æ Sßrie en inches
Luftæ und Raumfahrt æ Buchsen mit Flansch aus Aluminiumlegierungá mit selbstschmierender Beschichtungá erhöhte Belastung æ Teil
tã Maße und Belastungen æ InchæReihe This European Standard was approved by CEN on
v March
t r s xä
egulations which stipulate the conditions for giving this European Standard the status of a national standard without any alterationä Upætoædate lists and bibliographical references concerning such national standards may be obtained on application to the CENæCENELEC Management Centre or to any CEN memberä
translation under the responsibility of a CEN member into its own language and notified to the CENæCENELEC Management Centre has the same status as the official versionsä
CEN members are the national standards bodies of Austriaá Belgiumá Bulgariaá Croatiaá Cyprusá Czech Republicá Denmarká Estoniaá Finlandá Former Yugoslav Republic of Macedoniaá Franceá Germanyá Greeceá Hungaryá Icelandá Irelandá Italyá Latviaá Lithuaniaá Luxembourgá Maltaá Netherlandsá Norwayá Polandá Portugalá Romaniaá Slovakiaá Sloveniaá Spainá Swedená Switzerlandá Turkey andUnited Kingdomä
EUROPEAN COMMITTEE FOR STANDARDIZATION COMITÉ EUROPÉEN DE NORMALISATION EUROPÄISCHES KOMITEE FÜR NORMUNG
CEN-CENELEC Management Centre:
Avenue Marnix 17,
B-1000 Brussels
t r s x CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Membersä Refä Noä EN
v w u wæ tã t r s x ESIST EN 4535-2:2016

Standard evolution form . 23
The bushes are intended for use in fixed or moving parts of the aircraft structure and control mechanisms.
They shall be used in the temperature range -55 °C to 121 °C. 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 referenced document (including any amendments) applies.
EN 2101, Aerospace series — Chromic acid anodizing of aluminium and wrought aluminium alloys EN 2284, Aerospace series — Sulphuric acid anodizing of aluminium and wrought aluminium alloys EN 2311, Aerospace series — Bushes with self-lubricating liner — Technical specification EN 2318, Aerospace series — Aluminium alloy AL-P2024-T3511 — Extruded bars and sections
1,2 mm ≤ a or D ≤ 150 mm EN 2424, Aerospace series — Marking of aerospace products EN 4704, Aerospace series — Tartaric-Sulphuric-Acid anodizing of aluminium and aluminium wrought alloys for corrosion protection and paint pre-treatment (TSA) ISO 2768-1, General tolerances — Part 1: Tolerances for linear and angular dimensions without individual tolerance indications AECMA TR 4475, Aerospace series — Bearings and mechanical transmissions for airframe applications — Vocabulary 1)
3 Terms and definitions For the purposes of this document, the terms and definitions given in TR 4475 apply. 4 Requirements
4.1 Configuration, dimensions and mass According to Figures 1 and 2 and Tables 1, 2, 3, 5 and 6. Dimensions apply after surface treatment. Dimensions and tolerances are expressed in millimetres (inches). Except for roughness given in micrometres (micro inches).
General tolerances shall be ISO 2768-m in accordance with ISO 2768-1.
1) Published as ASD-STAN Technical Report at the date of publication of this European Standard. http://www.asd-stan.org/ SIST EN 4535-2:2016

Liner: Self-lubricating wear resistant material consistent with the requirements of EN 2311.
4.4 Surface treatment See Table 1 and Figure 1. Table 1 — Surface treatment Code Surface treatment Remarks R Chromic acid anodizing according to EN 2101 Type A or Sulphic acid anodizing according to EN 2284 Type A Pre-treatment for painting S Chromic acid anodizing according to EN 2101 Type A (unsealed) Pre-treatment for painting T Chromic acid anodizing according to EN 2101 Type B (sealed) Corrosion protection U Sulphic acid anodizing according to EN 2284 Type A (unsealed) Pre-treatment for painting V Sulphic acid anodizing according to EN 2284 Type B (sealed) Corrosion protection N Tartaric-Sulphuric-Acid anodizing according to EN 4704 (unsealed) Pre-treatment for painting M Tartaric-Sulphuric-Acid anodizing according to EN 4704 (sealed) Corrosion protection
Key a chamfer machined before bonding b chamfer or radius at manufacturers option c chamfer machined after bonding d at manufacturer's option Figure 1 — Configuration – Type D SIST EN 4535-2:2016

Diameter code a d D D1 g1 g2 L2 f1 a α R Nominal diameter 00,025− ± 0,013 00,51− max. max. 00,13− max.
± 2° 00,25+ −00.0010 (± 0.000 5) −0.0200 −0.0050 +00,010 04 6,350 (0.250 0) 6,388 (0.251 5) 9,550 (0.376 0) 19,05 (0.750) 0,70 (0.028) 0,70 (0.028) 1,60 (0.063) 1,20 (0.047) 0,50 to 0,70 (0.020 to 0.030) 15° 0,13 (0.005) 05 7,938 (0.312 5) 7,976 (0.314 0) 11,140 (0.438 6) 20,64 (0.813) 06 9,525 (0.375 0) 9,563 (0.376 5) 12,730 (0.5012) 22,23 (0.875) 07 11,113 (0.437 5) 11,151 (0.439 0) 14,321 (0.563 8) 23,81 (0.938) 08 12,700 (0.500 0) 12,738 (0.501 5) 15,913 (0.626 5) 25,40 (1.000) 09 14,288 (0.562 5) 14,326 (0.564 0) 17,506 (0.689 2) 28,58 (1.125) 10 15,875 (0.625 0) 15,913 (0.626 5) 20,681 (0.814 2) 31,75 (1.250) 11 17,463 (0.687 5) 17,501 (0.689 0) 22,268 (0.876 7) 34,93 (1.375) 12 19,050 (0.750 0) 19,088 (0.751 5) 23,858 (0.939 3) 38,10 (1.500) 14 22,225 (0.875 0) 22,263 (0.876 5) 27,038 (1.064 5) 41,28 (1.625) 1,00 (0.039) 1,00 (0.039) 16 25,400 (1.000 0) 25,438 (1.001 5) 30,221 (1.189 8) 44,45 (1.750) 18 28,575 (1.125 0) 28,613 (1.126 5) 33,396 (1.314 8) 47,63 (1.875) 2,39 (0.094) 20 31,750 (1.250 0) 31,788 (1.251 5) 36,571 (1.439 8) 50,80 (2.000) 22 34,925 (1.375 0) 34,963 (1.376 5) 39,746 (1.564 8) 53,98 (2.125) 24 38,100 (1.500 0) 38,138 (1.501 5) 44,508 (1.752 3) 57,15 (2.250) 26 41,275 (1.625 0) 41,313 (1.626 5) 47,683 (1.877 3) 60,33 (2.375) 28 44,450 (1.750 0) 44,488 (1.751 5) 50,858 (2.002 3) 63,50 (2.500) 32 50,800 (2.000 0) 50,838 (2.001 5) 57,208 (2.252 3) 69,85 (2.750) a Diameter code corresponds to nominal diameter d in 1/16 inch.
006 007 008 009 010 011 012 014 016 018 020 022 024 028 032
L1 0,100,40−− −−0.0160,004
4,76 5,56 6,35 7,14 7,94 8,73 9,53 11,11 12,70 14,29 15,88 17,46 19,05 22,23 25,40
(0.188) (0.219) (0.250) (0.281) (0.313) (0.344) (0.375) (0.438) (0.500) (0.563) (0.625) (0.688) (0.750) (0.875) (1.000)
04 1,48 1,57 1,66 1,75 1,84 1,92 2,01 2,19 2,36 — — — — — —
05 1,70 1,80 1,91 2,01 2,12 2,22 2,33 2,54 2,75 2,96 3,17 — — — —
06 1,91 2,03 2,15 2,28 2,40 2,52 2,65 2,89 3,14 3,39 3,63 3,88 4,13 — —
07 2,12 2,26 2,40 2,54 2,68 2,82 2,96 3,25 3,53 3,81 4,09 4,37 4,66 5,22 —
08 2,33 2,49 2,65 2,81 2,97 3,13 3,28 3,60 3,92 4,24 4,55 4,87 5,19 5,83 —
09 2,86 3,03 3,21 3,39 3,56 3,74 3,92 4,27 4,62 4,98 5,33 5,68 6,04 6,74 7,45
10 3,87 4,17 4,48 4,78 5,09 5,39 5,70 6,31 6,91 7,52 8,13 8,74 9,35 10,57 11,79
11 — — 5,20 5,53 5,86 6,19 6,52 7,18 7,84 8,50 9,17 9,83 10,49 11,81 13,14
12 — — 5,97 6,32 6,68 7,04 7,40 8,11 8,83 9,54 10,26 10,97 11,69 13,12 14,55
14 — — 6,71 7,12 7,53 7,94 8,35 9,18 10,00 10,82 11,64 12,46 13,29 14,93 16,57
16 — — 7,46 7,92 8,39 8,85 9,32 10,24 11,17 12,10 13,03 13,96 14,89 16,75 18,61
18 — — — — 11,23 11,75 12,27 13,30 14,34 15,37 16,41 17,44 18,48 20,55 22,62
20 — — — — — — 13,38 14,52 15,66 16,80 17,94 19,08 20,22 22,51 24,79
22 — — — — — — 14,49 15,73 16,98 18,23 19,48 20,72 21,97 24,47 26,96
24 — — — — — — 17,78 19,61 21,45 23,29 25,13 26,97 28,80 32,48 36,16
26 — — — — — — — — 23,00 24,98 26,96 28,94 30,92 34,88 38,84
28 — — — — — — — — 24,55 26,67 28,80 30,92 33,04 37,28 41,52
32 — — — — — — — — 27,66 30,06 32,46 34,87 37,27 42,07 46,88
Diameter code a Length code b
036 040 044 048 052 056 060 064 068 072 076 080 088 096
L1 0,100,40−− −−0.0160,004
28,58 31,75 34,93 38,10 41,28 44,45 47,63 50,80 53,98 57,15 60,33 63,50 69,85 76,20
(1.125) (1.250) (1.375) (1.500) (1.625) (1.750) (1.875) (2.000) (2.125) (2.250) (2.375) (2.500) (2.750) (3.000)
04 — — — — — — — — — — — — — —
05 — — — — — — — — — — — — — —
06 — — — — — — — — — — — — — —
07 — — — — — — — — — — — — — —
08 — — — — — — — — — — — — — —
09 8,16 — — — — — — — — — — — — —
10 13,01 14,22 — — — — — — — — — — — —
11 14,46 15,79 17,11 — — — — — — — — — — —
12 15,98 17,41 18,84 20,27 — — — — — — — — — —
14 18,22 19,86 21,50 23,15 24,79 — — — — — — — — —
16 20,47 22,33 24,18 26,04 27,90 29,76 31,62 — — — — — — —
18 24,69 26,76 28,83 30,90 32,97 35,04 37,11 39,19 — — — — — —
20 27,07 29,36 31,64 33,92 36,20 38,49 40,77 43,05 45,34 — — — — —
22 29,46 31,95 34,45 36,94 39,44 41,93 44,43 46,92 49,41 — — — — —
24 39,83 43,51 47,18 50,86 54,54 58,21 61,89 65,56 69,24 72,92 76,59 80,27 87,62 —
26 42,80 46,75 50,71 54,67 58,63 62,59 66,55 70,50 74,46 78,42 82,38 86,34 94,26 102,17
28 45,76 50,00 54,24 58,48 62,72 66,96 71,20 75,45 79,69 83,93 88,17 92,41 100,89 109,37
32 51,69 56,49 61,30 66,10 70,91 75,71 80,52 85,33 90,13 94,94 99,74 104,55 114,16 123,77
a Diameter code corresponds to nominal diameter d in 1/16 inch. b Length code corresponds to length L1 in 1/32 inch.
code Permissible radial load Radial
load Axial
static load
Diameter code a Length
code Permissible radial load Radial
load Axial static load kN
kN Static
Cs b Dynamic
C25 c Ca d
Static
Cs b Dynamic
C25 c Ca d 04 006 2,15 1,92 37,05
08 009 13,09
11,69 54,85 007 3,62
3,24
010 16,02
14,31 008
5,09
4,55
011 18,95
16,93 009 6,56 5,86
21,89
19,55 010 8,04
7,18
014 27,75 24,78 011 9,51
8,49
016 33,62
30,02 012 10,98
9,80
018 39,48
35,26 014 13,92
12,43
020 45,34
40,50 016 16,86
15,06
022 51,21
45,73 05 006 2,69
2,40 41,50
024 57,07
50,97 007 4,52
4,04
028 68,80
61,45 008 6,36
5,68
09 006 4,83
4,31 72,80 009
8,20
7,32
007 8,13
7,26 010 10,03 8,96
008 11,42
10,20 011 11,87
10,60
009 14,72
13,15 012 13
...