EP 3532313 A1 20190904 - AIRCRAFT TYRE CROWN REINFORCEMENT
Title (en)
AIRCRAFT TYRE CROWN REINFORCEMENT
Title (de)
GÜRTELVERSTÄRKUNG FÜR FLUGZEUGREIFEN
Title (fr)
ARMATURE DE SOMMET DE PNEUMATIQUE POUR AVION
Publication
Application
Priority
- FR 1660380 A 20161026
- FR 2017052917 W 20171024
Abstract (en)
[origin: WO2018078268A1] The subject of the present invention is an aircraft tyre crown reinforcement and the object of the present invention is to increase the mechanical strength thereof so as to increase the bursting pressure of the tyre during a pressure test in accordance with prescribed standards. An aircraft tyre comprises a working reinforcement consisting of a strip (5) wound continuously in a zigzag from a starting end (51) to a finishing end (52) in a circumferential direction (XX') of the tyre, according to a periodic curve (7) that, with the circumferential direction (XX') of the tyre and in an equatorial plane (XZ) of the tyre, makes a non-zero angle A. According to the invention, the respective starting end (51) and finishing end (52) of the strip (5) are positioned, axially from an axial end (E1, E2) of the working reinforcement, at a distance (DI, DF) at most equal to 0.25 times the axial width WT of the working reinforcement.
IPC 8 full level
B29D 30/30 (2006.01); B60C 9/20 (2006.01)
CPC (source: EP US)
B29D 30/3035 (2013.01 - EP US); B60C 9/0042 (2013.01 - US); B60C 9/0057 (2013.01 - US); B60C 9/2003 (2013.01 - EP US); B60C 9/263 (2013.01 - EP US); B60C 2009/2016 (2013.01 - EP US); B60C 2009/2032 (2013.01 - EP US); B60C 2009/2035 (2013.01 - US); B60C 2200/02 (2013.01 - EP US)
Citation (search report)
See references of WO 2018078268A1
Designated contracting state (EPC)
AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR
Designated extension state (EPC)
BA ME
DOCDB simple family (publication)
FR 3057809 A1 20180427; CN 109843605 A 20190604; EP 3532313 A1 20190904; US 2019263182 A1 20190829; WO 2018078268 A1 20180503
DOCDB simple family (application)
FR 1660380 A 20161026; CN 201780064511 A 20171024; EP 17797403 A 20171024; FR 2017052917 W 20171024; US 201716344267 A 20171024