• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    A tire, particularly for aircraft, has a crown reinforcement formed of plies of circumferential cables having a relative extensibility upon rupture of at least 8%, preferably between 10% and 26%, when the vulcanized tire is mounted on its service rim but not yet inflated, and a relative contraction under the effect of the heat at the temperature of vulcanization of at least 1.25%, preferably between 2% and 8%.
    公开号:SU1277885A3
    申请号:SU823394403
    申请日:1982-02-12
    公开日:1986-12-15
    发明作者:Мюзи Жак
    申请人:Мишлен Э Ко (Компани Женераль Дез Этаблиссман Мишлен) (Фирма)；
    IPC主号:
    专利说明:

    rim 17 and relative compression for vulcanization of 1.25-8%. The deflection of the tread 2 tires 1 in the mold 16 differs by at least 10% from the deflection tread of the tread 2 tires mounted on the rim 7, but not reduced. This implementation pshnya
    This makes it easier to remove the tire from the mold and to avoid pressure effects on the breaker, occurring when the tire is deformed and inflated during rolling, leading to premature tire wear. 10 hp f-ly, 4 ill.
    The invention relates to tire industry, in particular to the belt construction of radial tires.
    The purpose of the invention is to increase the service life.
    FIG. Figure 1 shows the halves of the radial section of the tire in a vulcanization form and mounted on a wheel rim in the unloaded state; in fig. 2 is a portion of the radial section of the tire belt in FIG. one; in fig. 3 is a cross section of an inflated tire mounted on a rim; in fig. 4 is a schematic representation of a portion of a protective belt layer.
    The pneumatic tire 1 comprises a tread 2, a radial carcass .3 fixed in each side 4 around the bead ring 5, and a belt 6, located radially outside the carcass 3.
    Breaker. 6 consists of three layers of 7, 8 and 9 cords of aliphatic polyamide type tex with elongation at break. Approximately 22% with a force of 60 dec, under the effect of temperature, the cords are compressed by 6-7%. In each of these sin layers, cords are arranged in a circumferential direction.
    Layer 9, located radially outside of Layers 7 and 8, has a width of 108 mm, and layers 7 and 8, respectively, of 214 and .212 mm and extend to the shoulders 10 of the tire.
    The belt 6 may also contain layers 11 and 12 located radially outside layers 7, 8 and 9 at an angle of 60 with respect to the circumferential direction, made of aliphatic polyamide of type 94x3 tex with an approximate 22% elongation at break with c 15 dan, under by temperature, these cords are compressed by 3-5%, the cords of layers 11 and 12 intersect from one layer to another. The layer 11 has a width of 155 mm, a layer of 12152 mm.
    The frame is made of three layers 13,
    14 and 15, each centimeter wide, contains twelve cords of aliphatic polyamide type 188x2 tex with approximately 24% elongation at break with a strength of 29 dan, under the effect of temperature these cords are compressed by 5%.
    Tire 1, extracted from the ForLf 16, mounted on the rim 17 of the wheel
    in the non-pumped state, it has a bend along the radius of the tread 2 and in the middle plane 18 is significantly increased due to the stresses in the cords of the belt 6 layers. While the top 19
    the mold 16 has a concavity of 25 mm; the top 20 of the tire 1 mounted on the rim 17 after vulcanisation in the non-compacted state has a large concavity f 5.75 mm. In the shoulder area 10
    Tire 1 sediment d relative to the radius of the form in the same zone is equal to 4.1%, and in the zone of the middle plane - 4.6%. In the state that is not inflated to the working pressure, the tire 1 of the tread has a slightly convex shape due to stretching of the breaker cords 6. ./
    Breaker 6 may contain a highly expandable protective shield of a layer 21 of undulating cords 22 with a diameter of 1 mm of steel filaments.
    The amplitude A of the sinusoid is 5 mm, the wavelength is 5 mm, the middle axes of the parallel cords are located at a distance of 1.5 mm at an angle of 90 relative to the circumferential direction.
    权利要求:
    Claims (11)
    [1]
    1. High pressure pneumatic tire, in particular for airplanes, comprising a tread having a radial negative curvature when the tire is mounted on the wheel rim in the empty state, a frame with radially arranged yarns fixed at least around one bead of the ring in each a breaker consisting of at least two layers of circumferential cords stacked on top of each other, located radially outside the frame, characterized in that, in order to increase the service life, The circumferential cords have an elongation at break of 8-26% when the vulcanized tire is installed on the wheel rim and the relative compression when vulcanized is 1.25-8%.
    [2]
    2. Tire according to claim 1, characterized in that in the axial direction, layers of circumferential cords are located at least between the tread arms,
    [3]
    3. Tire according to pp1 and 2, characterized in that the axial width of the layers of circumferential cords decreases in the radially outward direction.
    [4]
    4. Tire according to claim 3, characterized in that the widest layer of circumferential cords is located from one side to the other.
    [5]
    5. Tire pop. 4 and 3, differing from the fact that at least the circumferential cords of the widest layer have a relative compression of the vulcanization temperature less than the relative compression of cords of other layers of the circumferential cords.
    [6]
    6. Tire on PP. 1-5, about a t of l and h and shcha so that the breaker includes at least two additional layers of cords located radially outside the layers of circumferential cords at an angle of 45-90 relative to the circumferential direction parallel to the calodes layer intersected from the layer jc to the layer and the extended elongated and compressed iMH when heated.
    [7]
    7. Tire according to claim 6, characterized in that the cords of the additional layers have a relative stretch when the gap is smaller, and the relative compression at the vulcanization temperature is greater than the corresponding characteristics of the circumferential cords.
    [8]
    8. Tire according to PP.-6 and 7, from l that with the fact that the stretching of additional layers when breaking the cords is smaller, the greater the angle of inclination of these cords,
    [9]
    9. Tire on PP. 1-8, that is, with the fact that the cords of the frame are arranged and compressible at the vulcanization temperature. t
    [10]
    10. Tire on PP. 1–8, of which it is obvious that} the cords of the framework are incompressible and incompressible at the temperature of vulcanisation.
    [11]
    11. A pneumatic tire according to claim 1, characterized in that. At least one layer of wave-like cords with parallel axes parallel to the angle of 0-90 is located outside the breaker, the distance between the axes is 50-100% of the wave amplitude, the wavelength is 100-200% from their amplitude. Priority points: .12.02,81 on PP. 1-10, except for the sign of item 1: circumferential cords have an elongation at break of 8-10% when installing a vulcanized tire on the wheel rim; 12/23/81 on item 11 and the indicated feature of item 1.
    789
    17
    /.J
    类似技术:
    公开号 | 公开日 | 专利标题
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    US4142930A|1979-03-06|Method of fabricating large tires
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    同族专利:
    公开号 | 公开日
    IT1191165B|1988-02-24|
    NO153327B|1985-11-18|
    AT388137B|1989-05-10|
    IT8267125D0|1982-02-03|
    OA07013A|1983-08-31|
    AU547433B2|1985-10-17|
    CH646652A5|1984-12-14|
    ES8402760A1|1984-02-16|
    ES519268A0|1984-02-16|
    NZ199690A|1985-09-13|
    BR8200746A|1982-12-21|
    GR76056B|1984-08-03|
    DE3202008C2|1990-10-25|
    AR225718A1|1982-04-15|
    IE52538B1|1987-12-09|
    ATA51982A|1988-10-15|
    DD208943A5|1984-04-18|
    ES273338Y|1984-06-01|
    EG15695A|1987-10-30|
    IE820318L|1982-08-12|
    GB2092963A|1982-08-25|
    DK151069B|1987-10-26|
    DE3202008A1|1982-09-23|
    DK62482A|1982-08-13|
    NO153327C|1986-02-26|
    SE8200811L|1982-08-13|
    NO820410L|1982-08-13|
    ES273338U|1983-11-16|
    MX159332A|1989-05-17|
    CA1155739A|1983-10-25|
    US4402356A|1983-09-06|
    LU83937A1|1982-07-07|
    SE452970B|1988-01-04|
    NL8200505A|1982-09-01|
    DK151069C|1988-06-13|
    GB2092963B|1985-02-13|
    AU8043282A|1982-08-19|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    NL269848A|1960-10-07|
    NL299910A|1962-10-31|
    US3643723A|1966-03-11|1972-02-22|Bridgestone Tire Co Ltd|Pneumatic tire having a belt member|
    FR2082137A5|1970-03-04|1971-12-10|Englebert|
    US3693690A|1970-06-29|1972-09-26|Goodyear Tire & Rubber|Pneumatic aircraft tire|
    US3735791A|1971-06-07|1973-05-29|Goodyear Tire & Rubber|Pneumatic tire|
    FR2437945B1|1978-10-05|1981-07-10|Michelin & Cie|
    FR2446193B1|1979-01-11|1982-06-18|Kleber Colombes|DE3580076D1|1984-08-29|1990-11-15|Sumitomo Rubber Ind|PLANE TIRES.|
    GB8501647D0|1985-01-23|1985-02-27|Sp Tyres Uk Ltd|Motor cycle tyres|
    GB2171067B|1985-02-04|1989-06-07|Bridgestone Corp|Heavy duty pneumatic tire|
    JPH0717129B2|1986-12-27|1995-03-01|住友ゴム工業株式会社|Radial tire|
    JPH0545441B2|1987-06-17|1993-07-09|Bridgestone Corp|
    US4934428A|1987-12-07|1990-06-19|Bridgestone Corporation|Heavy duty pneumatic radial tire|
    JP2690531B2|1987-12-07|1997-12-10|株式会社ブリヂストン|Pneumatic radial tire for aircraft|
    JP2612330B2|1988-02-29|1997-05-21|住友ゴム工業株式会社|Aircraft tires|
    JPH01223004A|1988-03-01|1989-09-06|Bridgestone Corp|Pneumatic tyre for high internal pressure and heavy load|
    US5078191A|1988-04-14|1992-01-07|Bridgestone Corporation|Off-the-road heavy duty pneumatic radial tires for decreasing inner rubber peeling and cracking in the vicinity of the shoulder portion|
    US5271445A|1988-09-19|1993-12-21|Bridgestone Corporation|Pneumatic tire including wave-shaped cords or filaments|
    JP3009670B2|1988-09-19|2000-02-14|株式会社ブリヂストン|Pneumatic tires for passenger cars|
    DE68912253T2|1988-09-19|1994-05-11|Bridgestone Corp|Tire.|
    EP0364291B1|1988-10-14|1994-12-21|Bridgestone Corporation|Radial tire for aircraft|
    EP0392117B1|1989-04-11|1994-01-19|Sumitomo Rubber Industries Limited|Pneumatic tyre|
    FR2652311B1|1989-09-25|1991-11-29|Michelin & Cie|TREAD PROVIDED WITH CELLS.|
    US5088538A|1990-10-29|1992-02-18|The Goodyear Tire & Rubber Company|Radial ply tire with shoulder reinforcement between belt and carcass|
    JP2859959B2|1991-01-07|1999-02-24|コンパニーゼネラールデエタブリッスマンミシュラン―ミシュランエコムパニー|Motorcycle tires|
    JPH05338406A|1992-06-05|1993-12-21|Bridgestone Corp|Pneumatic radial tire for construction vehicle|
    DE69418563T2|1993-10-12|1999-11-18|Bridgestone Corp|Vulcanizing mold for tires|
    JP4523722B2|1999-02-19|2010-08-11|ソシエテドテクノロジーミシュラン|Motorcycle tire having a crown reinforcement with a ply comprising circumferential elements|
    DE10326895A1|2003-06-14|2004-12-30|Continental Aktiengesellschaft|Radial tire for automobiles comprises a carcass layer whose steel cords within the tire belt zone form a wavy surface|
    US8056596B2|2007-10-22|2011-11-15|The Goodyear Tire + Rubber Company, Inc.|Multiple ply modular construction|
    FR2933031B1|2008-06-30|2011-08-19|Michelin Soc Tech|SUMMIT FOR TIRE AIRCRAFT|
    FR3029458B1|2014-12-08|2016-12-09|Michelin & Cie|PNEUMATIC PROTECTION TOP REINFORCEMENT FOR AIRCRAFT|
    FR3029460B1|2014-12-08|2016-12-09|Michelin & Cie|PNEUMATIC PROTECTION TOP REINFORCEMENT FOR AIRCRAFT|
    法律状态:
    优先权:
    申请号 | 申请日 | 专利标题
    FR8102787A|FR2499475B1|1981-02-12|1981-02-12|
    FR8124262A|FR2518462B2|1981-12-23|1981-12-23|
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