CN219544431U - Aviation tire with inner belt structure - Google Patents

Aviation tire with inner belt structure Download PDF

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Publication number
CN219544431U
CN219544431U CN202223140635.0U CN202223140635U CN219544431U CN 219544431 U CN219544431 U CN 219544431U CN 202223140635 U CN202223140635 U CN 202223140635U CN 219544431 U CN219544431 U CN 219544431U
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CN
China
Prior art keywords
tire
fixedly connected
tread
carcass
belt structure
Prior art date
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Active
Application number
CN202223140635.0U
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Chinese (zh)
Inventor
秦龙
林文龙
秦靖博
佟伟
盛春敬
李延磊
常慧敏
范全江
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Qingdao Sentury Tire Co Ltd
Original Assignee
Qingdao Sentury Tire Co Ltd
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Publication date
Application filed by Qingdao Sentury Tire Co Ltd filed Critical Qingdao Sentury Tire Co Ltd
Priority to CN202223140635.0U priority Critical patent/CN219544431U/en
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Publication of CN219544431U publication Critical patent/CN219544431U/en
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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/80Technologies aiming to reduce greenhouse gasses emissions common to all road transportation technologies
    • Y02T10/86Optimisation of rolling resistance, e.g. weight reduction 

Abstract

The utility model provides an aircraft tire with an inner belt structure, which belongs to the technical field of tires, and comprises; a carcass; a tread fixedly connected to the circumferential inner wall of the carcass; a resistance mechanism comprising: the two elastic rubber rings are fixedly connected to the circumferential inner wall of the tire body; the two fixed sleeves are fixedly connected to the inner wall of the enlarged circumference of the carcass; the two mounting pipe grooves are respectively arranged in the two fixed sleeves; and two support rings are respectively connected in two installation tube slots in a rotating way, the facility can support the tread through the support rings arranged in the tire body, the effect of the stability of the tire is improved, the stress of the support rings can be reduced to cause deformation through the elastic rubber rings arranged in the tire body, the service life of the tire is prolonged, and the overall installation stability of the tire is improved through the fixed ring frame arranged in the tire body.

Description

Aviation tire with inner belt structure
Technical Field
The utility model belongs to the technical field of tires, and particularly relates to an aviation tire with an inner belt structure.
Background
Tires are ground-engaging rolling, annular elastomeric rubber articles assembled on a variety of vehicles or machines. The automobile body is usually arranged on a metal rim, can support the automobile body, buffer external impact, realize contact with a road surface and ensure the running performance of the automobile.
The authority publication number CN211684524U records that a snowfield tire pattern relates to a tire pattern, in particular to a snowfield tire pattern, which comprises 3-5 pattern folding grooves which are longitudinally arranged, knife grooves are respectively arranged between every two adjacent pattern folding grooves, the knife grooves are longitudinally arranged, the knife grooves are respectively connected with the pattern folding grooves positioned at two sides of the knife grooves through a plurality of 3D wavy fine grooves, and the 3D wavy fine grooves are respectively transversely arranged; the longitudinal grooves are designed by adopting the folding grooves, the depth is the same, and the two side walls of the flower-shaped groove are provided with a plurality of fine cutter grooves, so that the braking force of the tire is improved; the angle between the middle pattern folding groove and the vertical normal line of the tread is 10-20 degrees, the angle between the edge pattern folding groove and the vertical normal line of the tread is designed to be a variable angle, the variable angle range is 10-20 degrees, and the adjacent first pattern blocks and the adjacent second pattern blocks are combined to be arranged at variable pitches, so that resonance of air of the pattern groove during tire running is effectively reduced, and tire noise is reduced. "
The noise of the tire can be effectively reduced by the aid of the air tire fixing frame, but in the prior art, when the air tire is used, the supporting ring is easy to deform under pressure after the tire is stressed, so that the air tire fixing frame deforms, and the service life of the tire is shortened.
Disclosure of Invention
The utility model aims to provide an aviation tire with an inner belt structure, and aims to solve the problems that in the prior art, when the aviation tire is used, a supporting ring is easy to deform under pressure after the tire is stressed, so that an aviation tire fixing frame deforms, and the service life of the tire is shortened.
In order to achieve the above purpose, the present utility model provides the following technical solutions:
an inner belt structure aircraft tire comprising:
a carcass;
a tread fixedly connected to the circumferential inner wall of the carcass;
a resistance mechanism, the resistance mechanism comprising:
two elastic rubber rings fixedly connected to the circumferential inner wall of the carcass;
the two fixed sleeves are fixedly connected to the inner wall of the enlarged circumference of the carcass;
the two mounting pipe grooves are respectively arranged in the two fixing sleeves; and
the two supporting rings are respectively and rotatably connected in the two mounting pipe grooves.
As a preferable scheme of the utility model, the circumferential inner wall of the carcass is fixedly connected with a fixed ring frame, and the circumferential surface of the fixed ring frame is provided with an adhesive layer.
As a preferable scheme of the utility model, the two side ends of the tread are fixedly connected with the fixing attachment rings, and the two fixing attachment rings are made of rubber materials.
As a preferable scheme of the utility model, veneers are fixedly connected to two side ends of the tread, and the veneers are both made of synthetic resin materials.
As a preferable mode of the present utility model, the elastic rubber ring is made of a rubber material, and the fixing sleeve is made of a carbon material.
As a preferable scheme of the utility model, one side ends of the two veneers are fixedly connected with mounting rings, and one side ends of the two mounting rings are provided with mounting sliding grooves.
As a preferable aspect of the present utility model, the circumferential surface of the tread is provided with an anti-slip layer.
Compared with the prior art, the utility model has the beneficial effects that:
1. in this scheme, through setting up the holding ring in the child, can support the tread, increase the effect of tire stability, through setting up the elastic rubber ring in the child, reducible holding ring atress causes the deformation, increases tire life's effect, through setting up the fixed ring frame in the child, has played the effect that increases tire overall installation stability.
2. In this scheme, through the fixed ring that pastes of setting in tread both sides, the effect of multiplicable tread fixity through the collar of setting in wainscot one side, has played the effect of protecting the tread, through the installation spout that sets up in collar one side, can place the effect of tire information.
Drawings
The accompanying drawings are included to provide a further understanding of the utility model and are incorporated in and constitute a part of this specification, illustrate the utility model and together with the embodiments of the utility model, serve to explain the utility model. In the drawings:
FIG. 1 is a perspective view of a first view of the present utility model;
FIG. 2 is an exploded view of the present utility model;
FIG. 3 is a cross-sectional view of the tread of FIG. 1 in accordance with the present utility model;
FIG. 4 is an enlarged view of the retaining sleeve of FIG. 2 in accordance with the present utility model;
fig. 5 is a perspective view of a second view of the present utility model.
In the figure: 1. a tread; 2. a fixed ring frame; 3. fixing the sticking ring; 4. veneering; 5. a mounting ring; 6. installing a chute; 7. a carcass; 8. fixing the sleeve; 9. an elastic rubber ring; 10. a support ring; 11. and (5) installing a pipe groove.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Example 1
Referring to fig. 1-5, the present utility model provides the following technical solutions:
an inner belt structure aircraft tire comprising:
a carcass 7;
a tread 1 fixedly connected to the circumferential inner wall of the carcass 7;
a resistance mechanism comprising:
two elastic rubber rings 9 fixedly connected to the circumferential inner wall of the carcass 7;
two fixed sleeves 8 fixedly connected to the enlarged circumferential inner wall of the carcass 7;
the two mounting tube slots 11 are respectively arranged in the two fixed sleeves 8; and
the two support rings 10 are respectively rotatably connected in the two mounting tube slots 11.
In the specific embodiment of the utility model, the tread 1 arranged on the surface of the carcass 7 plays a role in increasing the friction force of the tire, the elastic rubber ring 9 arranged in the carcass 7 plays a role in increasing the elasticity of the supporting ring 10, the supporting ring 10 arranged in the fixed sleeve 8 plays a role in supporting the whole tread 1, the fixed attaching rings 3 arranged on two sides of the tread 1 play a role in increasing the fixity of the tread 1, the fixed ring frames 2 arranged in the carcass 7 play a role in increasing the fixity of the tire, the attaching rings 4 arranged on two sides of the carcass 7 play a role in reducing damage caused by abrasion of the side edges of the tire, the mounting rings 5 arranged on one side of the attaching rings 4 play a role in fixing the whole information of the tire, the elastic rubber ring 9 is made of rubber materials, the elastic rubber ring 9 can be arranged according to the situation, the fixed sleeve 8 is reduced to deform due to compression, the attaching rings 4 are made of synthetic resin materials play a role in reducing abrasion, and the adhesive layers arranged on the surface of the fixed ring frames 2 play a role in fixing rings 7 and the fixed ring frames 2.
Referring to fig. 2 and 3 specifically, a fixing ring frame 2 is fixedly connected to the circumferential inner wall of the carcass 7, and an adhesive layer is provided on the circumferential surface of the fixing ring frame 2.
In this embodiment: the tire body 7 and the wheels of the tire can be fixed through the fixing ring frame 2 arranged in the tire body 7, and the fixing ring frame 2 and the tire body 7 can be fixed through the adhesive layer arranged on the surface of the fixing ring frame 2.
Referring to fig. 2 specifically, two side ends of the tread 1 are fixedly connected with fixing rings 3, and both fixing rings 3 are made of rubber material.
In this embodiment: through the fixed ring 3 that pastes that set up in tread 1 both sides, played the effect of fixing tread 1, fixed ring 3 is made through the rubber material, has played the effect of fitting tread 1 material.
Referring to fig. 2 specifically, the tread 1 is fixedly connected with two facing surfaces 4 at both ends, and both facing surfaces 4 are made of synthetic resin material.
In this embodiment: through the wainscot 4 that sets up in tread 1 both sides, played the effect of protecting matrix 7, wainscot 4 has played the effect that increases wainscot 4 use wearing and tearing through synthetic resin material.
Referring specifically to fig. 3 and 4, the elastic rubber ring 9 is made of a rubber material, and the fixing sleeve 8 is made of a carbon material.
In this embodiment: the elastic rubber ring 9 is made of rubber materials, the elasticity of the elastic rubber ring 9 can be selected according to actual conditions, the effect of increasing deformation of the support ring 10 after being pressed is achieved, and the stability of the tire body 7 can be increased by the aid of carbon materials in the fixing sleeve 8.
Referring to fig. 2 specifically, one side ends of the two veneers 4 are fixedly connected with mounting rings 5, and one side ends of the two mounting rings 5 are provided with mounting sliding grooves 6.
In this embodiment: through setting up the collar 5 in wainscot 4 one side, played the effect of protecting tread 1 one side, through setting up the installation spout 6 in collar 5 one side, played the effect of setting up tire body information.
Referring specifically to fig. 2, the circumferential surface of the tread 1 is provided with an anti-slip layer.
In this embodiment: through the anti-skid layer arranged on the surface of the tread 1, the function of increasing the friction force between the tire body and the ground is achieved.
The working principle and the using flow of the utility model are as follows: when the tire is in use, the fixing ring frame 2 is sleeved on the wheels, after the tire body is stressed, the elastic rubber ring 9 is pressed outside the supporting ring 10 under force, so that the compression can be reduced, the tire tread 1 can be supported by the tire through the supporting ring 10 arranged in the tire body 7, the effect of the stability of the tire is improved, the deformation caused by the stress of the supporting ring 10 can be reduced through the elastic rubber ring 9 arranged in the tire body 7, the service life of the tire is prolonged, and the overall installation stability of the tire is improved through the fixing ring frame 2 arranged in the tire body 7.
Finally, it should be noted that: the above is only a preferred embodiment of the present utility model, and the present utility model is not limited thereto, but it is to be understood that the present utility model is described in detail with reference to the foregoing embodiments, and modifications and equivalents of some of the technical features described in the foregoing embodiments may be made by those skilled in the art. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present utility model should be included in the protection scope of the present utility model.

Claims (7)

1. An aircraft tire of inner belt structure comprising:
a carcass (7);
a tread (1) fixedly connected to the circumferential inner wall of the carcass (7);
a resistance mechanism, the resistance mechanism comprising:
two elastic rubber rings (9) fixedly connected to the circumferential inner wall of the carcass (7);
two fixed sleeves (8) fixedly connected to the enlarged circumferential inner wall of the carcass (7);
the two mounting pipe grooves (11) are respectively arranged in the two fixing sleeves (8); and
the two support rings (10) are respectively and rotatably connected in the two mounting pipe grooves (11).
2. An aircraft tire with an inner belt structure according to claim 1, wherein: the tire body (7) is characterized in that a fixing ring frame (2) is fixedly connected to the circumferential inner wall of the tire body (7), and an adhesive layer is arranged on the circumferential surface of the fixing ring frame (2).
3. An aircraft tire with an inner belt structure according to claim 2, wherein: both side ends of tread (1) are all fixedly connected with and are pasted ring (3), and two fixed ring (3) are made by rubber material.
4. An aircraft tire of inner belt structure as in claim 3, wherein: veneers (4) are fixedly connected to two side ends of the tread (1), and the veneers (4) are made of synthetic resin materials.
5. An aircraft tire with an inner belt structure as in claim 4, wherein: the elastic rubber ring (9) is made of rubber material, and the fixed sleeve (8) is made of carbon material.
6. An aircraft tire with an inner belt structure as in claim 5, wherein: one side ends of the two veneers (4) are fixedly connected with mounting rings (5), and one side ends of the two mounting rings (5) are provided with mounting sliding grooves (6).
7. An aircraft tire with an inner belt structure as in claim 5, wherein: the circumferential surface of the tread (1) is provided with an anti-slip layer.
CN202223140635.0U 2022-11-25 2022-11-25 Aviation tire with inner belt structure Active CN219544431U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202223140635.0U CN219544431U (en) 2022-11-25 2022-11-25 Aviation tire with inner belt structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202223140635.0U CN219544431U (en) 2022-11-25 2022-11-25 Aviation tire with inner belt structure

Publications (1)

Publication Number Publication Date
CN219544431U true CN219544431U (en) 2023-08-18

Family

ID=87732013

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202223140635.0U Active CN219544431U (en) 2022-11-25 2022-11-25 Aviation tire with inner belt structure

Country Status (1)

Country Link
CN (1) CN219544431U (en)

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