JP2013514218A5 - - Google Patents

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Publication number
JP2013514218A5
JP2013514218A5 JP2012543601A JP2012543601A JP2013514218A5 JP 2013514218 A5 JP2013514218 A5 JP 2013514218A5 JP 2012543601 A JP2012543601 A JP 2012543601A JP 2012543601 A JP2012543601 A JP 2012543601A JP 2013514218 A5 JP2013514218 A5 JP 2013514218A5
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JP
Japan
Prior art keywords
theoretical
radially outer
filling element
radially
outer end
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JP2012543601A
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English (en)
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JP2013514218A (ja
JP5856567B2 (ja
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Publication date
Priority claimed from FR0959046A external-priority patent/FR2953763B1/fr
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Publication of JP2013514218A publication Critical patent/JP2013514218A/ja
Publication of JP2013514218A5 publication Critical patent/JP2013514218A5/ja
Application granted granted Critical
Publication of JP5856567B2 publication Critical patent/JP5856567B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Description

充填要素の理論的な半径方向外側の端は、充填要素の半径方向最も外側の箇所であり、この充填要素の半径方向外側では、カーカス補強材層及び／又はカーカス補強材折り返し部分が互いに合体すると共に２つずつ隣り合っている。本発明の意味の範囲内において、充填要素の半径方向外側の端は、理論的な半径方向外側の端の付近において、ビード外側フェース上への正投影像がビード外側フェースとカーカス補強材外側層との間の最大距離を形成する箇所を意味している。「〜の付近」という表現は、半径方向外側の端と理論的な半径方向外側の端との間の距離が多くても１０ｍｍに等しいことを意味している。換言すると、製造公差を考慮に入れると、ビード外側フェースとカーカス補強材外側層との間の最大距離は、０〜１０ｍｍの上述の理論的な半径方向外側の端からの距離のところで、且つ、充填要素の半径方向外側の端と呼ばれていると共に理論的な半径方向外側の端の半径方向内側に位置した、充填要素上の箇所で得られる。
JP2012543601A 2009-12-16 2010-12-07 航空機用タイヤのためのカーカス補強材 Expired - Fee Related JP5856567B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0959046A FR2953763B1 (fr) 2009-12-16 2009-12-16 Armature de carcasse pour pneumatique d'avion
FR0959046 2009-12-16
PCT/EP2010/069081 WO2011073059A1 (fr) 2009-12-16 2010-12-07 Armature de carcasse pour pneumatique d'avion

Publications (3)

Publication Number Publication Date
JP2013514218A JP2013514218A (ja) 2013-04-25
JP2013514218A5 true JP2013514218A5 (ja) 2015-11-19
JP5856567B2 JP5856567B2 (ja) 2016-02-10

Family

ID=42312620

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2012543601A Expired - Fee Related JP5856567B2 (ja) 2009-12-16 2010-12-07 航空機用タイヤのためのカーカス補強材

Country Status (8)

Country Link
US (1) US9056529B2 (ja)
EP (1) EP2512835B1 (ja)
JP (1) JP5856567B2 (ja)
CN (1) CN102656028B (ja)
BR (1) BR112012014329B1 (ja)
CA (1) CA2783335C (ja)
FR (1) FR2953763B1 (ja)
WO (1) WO2011073059A1 (ja)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2989633B1 (fr) * 2012-04-24 2015-02-27 Michelin & Cie Armature de carcasse pour pneumatique d'avion
FR3083742B1 (fr) * 2018-07-11 2020-07-17 Compagnie Generale Des Etablissements Michelin Pneumatique comportant des flancs renforces
CN110341382B (zh) * 2019-07-22 2021-06-01 三角轮胎股份有限公司 子午线航空轮胎

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL299910A (ja) * 1962-10-31
JP2807489B2 (ja) * 1989-07-06 1998-10-08 株式会社ブリヂストン 航空機用ラジアルタイヤ
US6427741B1 (en) * 1997-07-25 2002-08-06 The Goodyear Tire & Rubber Company Aircraft tire
JP4242956B2 (ja) 1998-10-27 2009-03-25 株式会社ブリヂストン 重荷重用空気入りラジアルタイヤ
US6374883B1 (en) * 2000-05-19 2002-04-23 The Goodyear Tire & Rubber Company Aircraft tire with two aquachannels
FR2823698B1 (fr) 2001-04-19 2004-05-07 Michelin Soc Tech Armatures de pneumatique pour avion
US6648041B2 (en) * 2001-08-31 2003-11-18 The Goodyear Tire & Rubber Company Aircraft tire with improved bead structure
JP5159575B2 (ja) 2008-11-18 2013-03-06 株式会社ブリヂストン 航空機用ラジアルタイヤ

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