Geometric parametric modeling method for meridian aircraft tire

A technology of aviation tires and geometric parameters, applied in geometric CAD, tire parts, reinforcement layers of pneumatic tires, etc., can solve the problems of time-consuming and complex tire geometry drawing, and achieve the effect of promoting ability improvement and shortening research and development cycle.

Pending Publication Date: 2022-07-15
JILIN UNIV
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Problems solved by technology

[0004] Aiming at the complex and time-consuming problem of tire geometric drawing, the pr

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  • Geometric parametric modeling method for meridian aircraft tire
  • Geometric parametric modeling method for meridian aircraft tire
  • Geometric parametric modeling method for meridian aircraft tire

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Embodiment Construction

[0020] The present invention realizes above-mentioned technical purpose through the following steps:

[0021] The geometric parametric modeling method of radial aviation tires, the method is: according to the maximum diameter R of the tire vertical 、Maximum width of tire section W max , rim diameter R rim , the thickness of the inner liner T IL , sidewall thickness T SideWall , Bead taper A taper , the ratio of rim width to tire section width W ratio , Tread thickness T tread 、 Lateral thickness T of tire heel HealH , the longitudinal thickness of the tire heel T HealV , Reinforcing layer thickness T PP , diameter of traveler R bead , carcass ply thickness T CP , Belt thickness T BP , the lateral distance D between the vertex of the apex and the center of the traveler circle apexH , the longitudinal distance D between the vertex of the apex and the center of the traveler apexV , to build a 3D model of radial aeronautical tires. According to the above 16 parameter...

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Abstract

The invention discloses a meridian aircraft tire geometric parametric modeling method, relates to the technical field of aircraft tire design, and solves the problem that existing tire geometric drawing is complex and time-consuming. The method comprises the following steps: according to the maximum diameter of the tire, the maximum width of the section of the tire, the diameter of a rim, the thickness of an inner liner, the thickness of a sidewall, the taper of a tire bead, the ratio of the width of a hub to the width of the section of the tire, the thickness of a tread, the transverse thickness of a bead heel, the longitudinal thickness of the bead heel, the thickness of a reinforcing layer, the diameter of a bead ring, the thickness of a carcass ply and the thickness of a belted layer; and establishing a three-dimensional model of the meridian aircraft tire according to the transverse distance between the apex and the center of the bead ring and the longitudinal distance between the apex and the center of the bead ring. According to the method, the geometric model of the meridian aircraft tire can be quickly and accurately established through 16 geometric information parameters, so that the research and development period of the meridian aircraft tire is shortened, and the capability of independent design of the meridian aircraft tire is promoted to be improved.

Description

technical field [0001] The invention relates to the field of aviation tire design, in particular to a geometric parameterized modeling method of radial aviation tires. Background technique [0002] Aviation tires are known as the "jewel in the crown" of the tire industry. Foreign tires can fly 250 sorties, while domestic tires can only fly 50 sorties. And domestic tires only account for 5% of the domestic market. Therefore, it is necessary to break through the technical barriers of foreign aviation tires as soon as possible and improve the ability of independent design. The emergence of radial aviation tires not only opens up a new development direction, but will also be a milestone in the development of aircraft tire technology. Compared with bias tires, radial tires have the advantages of low heat generation, long service life, low tire weight, high tire retreading rate and low running cost. However, due to the small radial rigidity of radial aviation tires and the lar...

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Application Information

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IPC IPC(8): G06F30/15G06F30/20B60C9/00
CPCG06F30/15G06F30/20B60C9/00
Inventor 左文杰靳金鑫王东禹石玉彪
Owner JILIN UNIV
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