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公开(公告)号：US20050274443A1
公开(公告)日：2005-12-15
申请号：US11159243
申请日：2005-06-23
Applicant: Christian Monnerie
Inventor： Christian Monnerie
CPC classification number: B60C15/0018 , B60C9/023 , B60C15/024 , B60C15/04 , B60C2200/02 , Y10T152/10819 , Y10T152/10846 , Y10T152/10855 , Y10T152/10864
Abstract: The invention relates to an aircraft tire, the inflation pressure of which is greater than 9 bar and the deflection of which is greater than 30%, comprising a crown, two sidewalls and two beads, a carcass reinforcement anchored in the two beads and a crown reinforcement, in which the carcass reinforcement comprises at least one circumferential alignment of reinforcement elements and in which the means for anchoring said reinforcement elements within each bead comprise circumferentially oriented reinforcement elements axially bordering said circumferential aligmnents of said reinforcement elements of the carcass reinforcement, said reinforcement elements of the carcass reinforcement and said circumferentially oriented reinforcement elements being separated by a bonding rubber mix of very high elasticity modulus. According to the invention, said circumferentially oriented reinforcement elements are cables having a penetrability of between 80 and 100%, the breaking load of the cables being greater than 150 daN and said cables having an elongation at break greater than 4%.
Abstract translation: 本发明涉及一种飞机轮胎，其充气压力大于9巴，其偏差大于30％，包括冠，两个侧壁和两个珠，锚固在两个珠中的胎体增强件和冠 加强件，其中胎体增强件包括加强元件的至少一个圆周对准，并且其中用于将所述加强元件固定在每个胎圈内的装置包括沿着周向定向的加强元件，所述加强元件轴向地邻接所述胎体增强件的所述加强件的周向凹槽， 胎体增强件和所述周向取向的增强件的元件由非常高的弹性模量的粘合橡胶混合物分离。 根据本发明，所述周向取向的增强元件是具有80-100％渗透性的电缆，电缆的断裂载荷大于150dN，所述电缆的断裂伸长率大于4％。
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公开(公告)号：US09027618B2
公开(公告)日：2015-05-12
申请号：US12405873
申请日：2009-03-17
Applicant: Christian Monnerie
Inventor： Christian Monnerie
IPC: B60C15/00 , B60C15/06 , B60C9/02 , B60C15/024 , B60C15/04
CPC classification number: B60C15/0018 , B60C9/023 , B60C15/024 , B60C15/04 , B60C2200/02 , Y10T152/10765 , Y10T152/10819 , Y10T152/10846
Abstract: A mounted assembly of a wheel and a tire. The tire inflation pressure is greater than 9 bar, and a relative deflection of the tire greater than 30%. The rim comprises a drop-center functionality and is of monobloc type. A carcass reinforcement includes a circumferential alignment of carcass reinforcement elements anchored in the beads by a stack of circumferentially oriented reinforcement elements, and by an anchoring rubber mix having an elasticity modulus of less than 30 MPa at 10% deformation.
Abstract translation: 轮和轮胎的安装组件。 轮胎充气压力大于9巴，轮胎的相对挠度大于30％。 边缘包括液滴中心功能并且是单体型的。 胎体增强件包括通过周向取向的增强元件的堆叠锚固在胎圈中的胎体增强件的圆周对准，以及在10％变形下具有小于30MPa的弹性模量的锚固橡胶混合物。
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公开(公告)号：US07278457B2
公开(公告)日：2007-10-09
申请号：US11159243
申请日：2005-06-23
Applicant: Christian Monnerie
Inventor： Christian Monnerie
CPC classification number: B60C15/0018 , B60C9/023 , B60C15/024 , B60C15/04 , B60C2200/02 , Y10T152/10819 , Y10T152/10846 , Y10T152/10855 , Y10T152/10864
Abstract: An aircraft tire has an inflation pressure greater than 9 bar and a deflection greater than 30%. The tire includes a crown, two sidewalls and two beads, a carcass reinforcement anchored in the two beads and a crown reinforcement. The carcass reinforcement includes at least one circumferential alignment of reinforcement elements and the mechanism for anchoring the reinforcement elements within each bead includes circumferentially oriented reinforcement elements axially bordering the circumferential alignments of said reinforcement elements of the carcass reinforcement. The reinforcement elements of the carcass reinforcement and the circumferentially oriented reinforcement elements are separated from each other by a bonding rubber mix of very high elasticity modulus. The circumferentially oriented reinforcement elements are in the form of cables having a penetrability of between 80 and 100%, the breaking load of the cables being greater than 150 daN, and the cables having an elongation at break greater than 4%.
Abstract translation: 飞机轮胎的充气压力大于9巴，偏转大于30％。 轮胎包括冠部，两个侧壁和两个胎圈，锚固在两个胎圈中的胎体增强件和胎冠加强件。 胎体增强件包括加强元件的至少一个圆周对准，并且用于将增强元件固定在每个胎圈内的机构包括沿着与胎体增强件的所述加强件的圆周对准轴向接合的周向取向的加强元件。 胎体增强件的加强件和周向取向的加强件通过非常高弹性模量的粘合橡胶混合物相互分离。 周向取向的增强元件是电缆的形式，具有80-100％的穿透性，电缆的断裂载荷大于150daN，断裂伸长率大于4％的电缆。
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公开(公告)号：US20050252593A1
公开(公告)日：2005-11-17
申请号：US11182860
申请日：2005-07-18
Applicant: Christian Monnerie
Inventor： Christian Monnerie
IPC: B60C15/024 , B60C19/00 , B60C3/04 , B60B21/02 , B60C3/00 , B60C9/20 , B60C9/22 , B60C15/00 , B60C15/02 , B60C15/06
CPC classification number: B60C15/0018 , B60C9/023 , B60C15/024 , B60C15/04 , B60C2200/02 , Y10T152/10765 , Y10T152/10819 , Y10T152/10846
Abstract: The invention relates to mounted assemblies for aircraft and to the wheels and tires which constitute them. The mounted assemblies for aircraft to which the invention relates are characterized in particular by the combination of an inflation pressure greater than 9 bar and a relative deflection of the tire greater than 30%, the wheel comprising a rim for receiving the tire and more specifically seats receiving the beads of said tire. According to the invention, the rim comprises a drop-centre functionality and is advantageously of monobloc type.
Abstract translation: 本发明涉及用于飞行器和构成它们的轮子和轮胎的安装组件。 本发明涉及的用于飞行器的安装组件特别地特征在于大于9巴的充气压力和轮胎的相对偏差大于30％的组合，该轮包括用于接收轮胎的轮辋，更具体地说是座椅 接收所述轮胎的珠子。 根据本发明，轮辋包括液滴中心功能并且有利地是单体型。
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