EN 4695:2017
(Main)Aerospace series - Tie Rod with integrated bolts - Assembly Code G, H and K
Aerospace series - Tie Rod with integrated bolts - Assembly Code G, H and K
This standard specifies the dimensions and tolerances of rod assemblies for aerospace applications with two adjustable ends with integrated bolts for interior and sub structure in the temperature range − 55 °C to 85 °C. The rod ends should not be screwed completely apart.
Luft- und Raumfahrt - Zug-Druck-Stange mit integrierten Bolzen - Variante G, H und K
Série aérospatiale - Bielle avec axes intégrés - Code assemblage G, H et K
Aeronavtika - Zglobna ročica z vgrajenim sornikom - Montažne kode G, H in K
Ta standard določa mere in tolerance sestavov ročic z dvema nastavljivima končnikoma z vgrajenimi sorniki za uporabo v aeronavtiki v notranjosti ali podstrukturah v temperaturnem razponu od –55 °C do 85 °C. Končnika ročice ne smeta biti privita tako, da sta povsem narazen.
General Information
Standards Content (Sample)
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Luft- und Raumfahrt - Zug-Druck Stange mit integrierten Bolzen - Zusammenbaucode G, H und KSérie aérospatiale - Bielle avec axes intégrés - Code assemblage G, H et KAerospace series - Tie Rod with integrated bolts - Assembly Code G, H and K49.035Sestavni deli za letalsko in vesoljsko gradnjoComponents for aerospace constructionICS:Ta slovenski standard je istoveten z:EN 4695:2017SIST EN 4695:2017en,fr,de01-december-2017SIST EN 4695:2017SLOVENSKI
STANDARD
EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 4695
October
t r s y ICS
v {ä r u w English Version
Aerospace series æ Tie Rod with integrated bolts æ Assembly Code Gá H and K Série aérospatiale æ Bielle avec axes intégrés æ Code assemblage Gá H et K
Luftæ und Raumfahrt æ ZugæDruck Stange mit integrierten Bolzen æ Variante Gá H und K This European Standard was approved by CEN on
t w June
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 Serbiaá Slovakiaá Sloveniaá Spainá Swedená Switzerlandá Turkey and United 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 y CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Membersä Refä Noä EN
v x { wã t r s y ESIST EN 4695:2017
Standard evolution form . 19
USA: US 8371767
China: CN 10104431
Japan: JP 4885140
Russia: RU 2389914
South Africa: ZA 2007/03913
Canada: 2584387
South Korea: 7011559 ASD-STAN takes no position concerning the evidence, validity and scope of this patent right. The holder of this patent right has assured ASD-STAN that he/she is willing to negotiate licences under reasonable and non-discriminatory terms and conditions with applicants throughout the world. In this respect, the statement of the holder of this patent right is registered with ASD-STAN. Information may be obtained from: GMT Gummi-Metall-Technik GmbH Liechtersmatten 5 D-77815 Bühl TRIGUM Engineering GmbH Brunskamp 4 D-21220 Seevetal/Maschen Attention is drawn to the possibility that some of the elements of this document may be the subject of patent rights other than those identified above. ASD-STAN shall not be held responsible for identifying any or all such patent rights. SIST EN 4695:2017
« 55 °C to 85 °C. The rod ends should not be screwed completely apart. 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.
DIN 6799, Retaining washers for shafts1) DIN 65038-1, Aerospace — Steel, nickel- and cobalt-alloy bars — Technical specification1) 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 4614, Aerospace series — Spherical plain bearings in corrosion resisting steel with self-lubricating liner wide series — Dimensions and loads — Inch series EN 4691-1, Aerospace series — Tie rod with integrated bolts — Part 1: Technical specification EN 4692, Aerospace series — Tie rod with integrated bolts — Locking clip EN 10088-3, Stainless steels — Part 3: Technical delivery conditions for semifinished products, bars, rods, wire, sections and bright products of corrosion resisting steels for general purposes ISO 2768-1, General tolerances — Part 1: Tolerances for linear and angular dimensions without individual tolerance indications ISO 2768-2, General tolerances — Part 2: Geometrical tolerances for features without individual tolerance indications ISO 8075, Aerospace series — Surface treatment of hardenable stainless steel parts LN 9368-4, Aerospace — Designation of surface treatments — Part 4: Codes numbers for methods of anodic treatment1) LN 9368-7, Aerospace — Designation of surface treatments — Part 7: Codes numbers for methods of organic coating1) LN 9499-1, Aerospace series — Inserts, helical
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