CN213200154U

CN213200154U - Aircraft tire mooring device

Info

Publication number: CN213200154U
Application number: CN202021920704.8U
Authority: CN
Inventors: 何湘飞; 缪海沿; 赵鹏; 王天龙; 符棉
Original assignee: Grand China Aviation Maintenance Services Co ltd
Current assignee: Grand China Aviation Maintenance Services Co ltd
Priority date: 2020-09-04
Filing date: 2020-09-04
Publication date: 2021-05-14
Anticipated expiration: 2030-09-04

Abstract

The utility model provides an aircraft tire mooring device, including binding device and two fixing device. The two fixing devices are respectively arranged on two sides of the binding device. When the binding device is used, the binding device is sleeved on the surface of the airplane tire and is fixed through the two fixing devices. The aircraft tire mooring device is provided with the binding device and the two fixing devices, the binding device is sleeved on the aircraft tire, the two fixing devices are utilized for fixing, so that the aircraft tire is fixed on the ground instead of being fixed by static friction between the aircraft tire and the ground, and the stability of the aircraft tire is enhanced.

Description

Aircraft tire mooring device

Technical Field

The utility model belongs to the aviation field especially relates to an aircraft tire mooring device.

Background

Aircraft tires are commonly known as aircraft tires. Aircraft tires are important components on aircraft where safety and reliability requirements are high. Safe takeoff and landing of an aircraft must rely on the various unique functions of the aircraft tires. The airplane needs to be fixed when the airplane stays on the ground, and in the prior art, the airplane fixes the tire through a brake device, but the fixation is not firm enough depending on the static friction of the tire, so that a space for improving the fixation performance exists.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to overcome the shortcoming and not enough among the prior art, provide an aircraft tire mooring device.

The utility model relates to an aircraft tire mooring device of embodiment, include:

the binding device comprises a net body, a first upper connecting ring, a first lower connecting ring, a second upper connecting ring, a second lower connecting ring, a first upper leading-out rope, a first lower leading-out rope, a second upper leading-out rope and a second lower leading-out rope, the first upper connecting ring and the first lower connecting ring are both positioned at one end of the net body, the second upper connecting ring and the second lower connecting ring are both positioned at the other end of the net body, the first upper leading-out rope is led out from the first upper connecting ring and penetrates through the second upper connecting ring, the first lower leading-out rope is led out from the first lower connecting ring and penetrates through the second lower connecting ring, the second upper leading-out rope is led out from the second upper connecting ring and penetrates through the first upper connecting ring, the second lower leading-out rope is led out from the second lower connecting ring and penetrates through the first lower connecting ring;

the two fixing devices are respectively arranged on two sides of the binding device, the first upper leading-out rope and the first lower leading-out rope are both connected with one fixing device, and the second upper leading-out rope and the second lower leading-out rope are both connected with the other fixing device.

The utility model relates to an aircraft tire mooring device of embodiment is provided with and bindes device and two fixing device, it establishes on the aircraft tire to bind the device cover, and utilize two fixing device fixes for the aircraft tire is fixed subaerial, and not only utilize the aircraft tire to fix with the static friction on ground, has strengthened the steadiness of aircraft tire.

In a preferred or optional embodiment, the net body comprises a plurality of warp ropes and a plurality of weft ropes, the warp ropes and the weft ropes are arranged in a staggered mode, and knots are formed at the joints of the warp ropes and the weft ropes.

In a preferred or optional embodiment, the net body further comprises a plurality of reinforcing rings, and the reinforcing rings are arranged at knots on the edge of the net body.

In a preferred or alternative embodiment, the first upper connecting ring, the first lower connecting ring, the second upper connecting ring and the second lower connecting ring are each provided with two perforations.

In a preferred or optional embodiment, the fixing device includes a fixing ring, an earth anchor and a connecting band, the first upward-leading rope and the first downward-leading rope are connected with one of the fixing rings, the second upward-leading rope and the second downward-leading rope are connected with the other fixing ring, one end of the connecting band is connected with the fixing ring, and the other end of the connecting band is connected with the earth anchor.

In a preferred or optional embodiment, both ends of the connecting band are respectively connected with the ground anchor and the fixing ring through shackles.

In a preferred or alternative embodiment, the connecting strap is provided with a length tightening unit.

In a preferred or alternative embodiment, the connecting band is a woven band.

In order to make the present invention more clearly understood, the following description will be made in conjunction with the accompanying drawings.

Drawings

FIG. 1 is a first schematic view of a mounting arrangement for an aircraft tire tie-down apparatus of the present invention;

FIG. 2 is a second schematic view of the mounting structure of the aircraft tire tie down apparatus of the present invention;

fig. 3 is a schematic structural view of the binding device of the present invention;

fig. 4 is a schematic structural view of a first upper connection ring according to the present invention;

fig. 5 is a schematic structural view of the fixing device of the present invention;

fig. 6 is a schematic structural view of the fixing ring of the present invention.

The drawings illustrate schematically: 1. a binding device; 11. a net body; 111. a reinforcing ring; 12. a first upper connecting ring; 13. a first lower connecting ring; 14. a second upper connecting ring; 15. a second lower connecting ring; 16. a first upper lead-out rope; 17. a first lower outgoing rope; 18. a second upper outgoing rope; 19. a second downward leading-out rope; 2. a fixing device; 21. a fixing ring; 22. a ground anchor; 23. a connecting belt; 24. a shackle; 25. and a length tightening unit.

Detailed Description

Referring to fig. 1 and fig. 2, fig. 1 is a first schematic view of a mounting structure of an aircraft tire mooring device of the present invention, and fig. 2 is a second schematic view of the mounting structure of the aircraft tire mooring device of the present invention.

The airplane tire mooring device provided by the embodiment comprises a binding device 1 and two fixing devices 2. The two fixing devices 2 are respectively arranged at two sides of the binding device 1. When the binding device 1 is used, the binding device is sleeved on the surface of an airplane tire and is fixed through the two fixing devices 2.

Please refer to fig. 3, fig. 3 is a schematic structural diagram of the binding device of the present invention.

The binding device 1 comprises a net body 11, a first upper connecting ring 12, a first lower connecting ring 13, a second upper connecting ring 14, a second lower connecting ring 15, a first upper leading rope 16, a first lower leading rope 17, a second upper leading rope 18 and a second lower leading rope 19, the first upper connecting ring 12 and the first lower connecting ring 13 are both located at one end of the mesh body 11, the second upper connecting ring 14 and the second lower connecting ring 15 are both positioned at the other end of the net body 11, the first upper draw string 16 is drawn from the first upper connection ring 12 and threaded through the second upper connection ring 14, the first lower drawing string 17 is drawn from the first lower connection ring 13 and is inserted through the second lower connection ring 15, the second upper withdrawal string 18 is drawn from the second upper coupling ring 14 and threaded through the first upper coupling ring 12, the second lower connection ring 13 is connected to the second lower connection ring 15 and the second lower connection rope 19.

The net body 11 comprises a plurality of warp ropes and a plurality of weft ropes, the warp ropes and the weft ropes are arranged in a staggered manner, and knots are formed at the joints of the warp ropes and the weft ropes, wherein the knots can be formed by weaving the warp ropes and the weft ropes or bonding the warp ropes and the weft ropes. Preferably, the net body 11 further comprises a plurality of reinforcing rings 111, the plurality of reinforcing rings 111 are arranged at knots at the edge of the net body 11, and the reinforcing rings 111 increase the firmness of the knots.

Referring to fig. 4, fig. 4 is a schematic structural view of a first upper connecting ring according to the present invention.

In this embodiment, the first upper connection ring 12, the first lower connection ring 13, the second upper connection ring 14 and the second lower connection ring 15 are each provided with two through holes. The first upper outgoing rope 16 and the second upper outgoing rope 18 are respectively located on two hole positions, the first lower outgoing rope 17 and the second lower outgoing rope 19 are respectively located on two hole positions, friction of the two outgoing ropes in the same hole position is prevented, and the service life is prolonged. In other embodiments, the first upper connecting ring 12, the first lower connecting ring 13, the second upper connecting ring 14 and the second lower connecting ring 15 are provided with a through hole, the first upper outgoing cord 16 and the second upper outgoing cord 18 are located at the same hole, and the first lower outgoing cord 17 and the second lower outgoing cord 19 are located at the same hole.

The first upper outgoing rope 16 and the first lower outgoing rope 17 are both connected to one of the fixing devices 2, and the second upper outgoing rope 18 and the second lower outgoing rope 19 are both connected to the other fixing device 2. The two fixing devices 2 fix the two ends of the binding device 1 in a crossed manner.

Please refer to fig. 5 and fig. 6, in which fig. 5 is a schematic structural diagram of the fixing device of the present invention, and fig. 6 is a schematic structural diagram of the fixing ring of the present invention.

Fixing device 2 is including solid fixed ring 21, earth anchor 22 and connecting band 23, draw rope 16 on the first with first rope 17 of drawing down all is connected with one of them solid fixed ring 21, draw rope 18 on the second with second rope 19 of drawing down all with another gu fixed ring 21 is connected, the one end of connecting band 23 with gu fixed ring 21 is connected, the other end of connecting band 23 with earth anchor 22 is connected. The fixing ring 21 concentrates the force applied to the first upper lead-out string 16 and the first lower lead-out string 17, and concentrates the force applied to the second upper lead-out string 18 and the second lower lead-out string 19. The ground anchor 22 is fixedly disposed with the ground or other mounting surface.

Preferably, both ends of the connecting band 23 are respectively connected with the ground anchor 22 and the fixing ring 21 through a shackle 24, and the shackle 24 facilitates manual operation. The connection band 23 is provided with a length-tightening unit 25, and a user can adjust the length of the connection band 23 by adjusting the length-tightening unit 25. The connecting band 23 is a braided band, and the braided band is low in manufacturing cost and high in toughness.

The present invention is not limited to the above embodiment, and if various modifications or variations of the present invention do not depart from the spirit and scope of the present invention, they are intended to be covered if they fall within the scope of the claims and the equivalent technology of the present invention.

Claims

1. An aircraft tire tie-down apparatus, comprising:

2. An aircraft tire tie down apparatus as in claim 1, wherein:

the net body comprises a plurality of warp ropes and a plurality of weft ropes, the warp ropes and the weft ropes are arranged in a staggered mode, and rope knots are formed at the joints of the warp ropes and the weft ropes.

3. An aircraft tire tie down apparatus as in claim 2, wherein:

the net body further comprises a plurality of reinforcing rings, and the reinforcing rings are arranged at knot positions on the edge of the net body.

4. An aircraft tire tie down apparatus as in claim 3, wherein:

the first upper connecting ring, the first lower connecting ring, the second upper connecting ring and the second lower connecting ring are provided with two through holes.

5. An aircraft tire mooring device according to any one of claims 1 to 4, wherein:

fixing device is including solid fixed ring, earth anchor and connecting band, first go up to draw out the rope with first draw out the rope all is connected with one of them solid fixed ring, draw out the rope on the second with the second is drawn out the rope all with another down gu fixed ring connects, the one end of connecting band with gu fixed ring connects, the other end of connecting band with the earth anchor is connected.

6. An aircraft tire tie down apparatus as in claim 5, wherein:

the two ends of the connecting band are respectively connected with the ground anchor and the fixing ring through shackles.

7. An aircraft tire tie down apparatus as in claim 6, wherein:

the connecting band is provided with a length tightening unit.

8. An aircraft tire tie down apparatus as in claim 6, further comprising:

the connecting band is a braided band.