An airport runway non-stop construction vertical surface quick elimination installation structure

CN224858689UActive Publication Date: 2026-10-16SHANXI MECHANIZATION CONSTRUCTION GROUP CO LTD
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Patent Information

Application Number
CN202522503210.9
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2025-11-26
Publication Date
2026-10-16
Estimated Expiration
2035-11-26

AI Technical Summary

Technical Problem

该直立面会导致飞机滑行时轮胎与跑道边缘产生冲击,不仅影响轮胎使用寿命,还可能引发飞机滑行姿态不稳定,存在安全隐患

Benefits of technology

[0014] This type of rapid vertical surface elimination installation structure for airport runway construction without interrupting flight operations eliminates the vertical surface at the runway edge by using a 5°-15° angle between the side runway and the horizontal plane, with the top flush with the continuous runway. This avoids impact on aircraft tires and ensures taxiing safety. The side runway is formed by welding I-beams and I-beams to the base plate, combined with load-bearing steel plates, resulting in high load-bearing strength. It is suitable for the high-frequency load-bearing requirements of airport runways. Through the cooperation of lifting rings and traction components, the side runway can be quickly positioned and connected to the continuous runway without the need for complex hoisting equipment, significantly improving installation efficiency.

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Abstract

The utility model discloses an airport runway non-stop construction vertical surface quick elimination installation structure relates to the technical field of aircraft road surface, including the through paving runway and side vertical surface runway, the top surface of through paving runway is with the horizontal setting of airport runway sliding surface, and the side vertical surface runway sets up in the both sides of through paving runway or airport runway, the highest place of side vertical surface runway road surface is consistent with the top surface of through paving runway. The utility model discloses through the included angle of 5 degree-15 degree of side vertical surface runway and horizontal plane, and the top is flush with through paving runway, can quickly eliminate the vertical surface of runway edge, avoids the impact of aircraft tire, guarantees the sliding safety, and side vertical surface runway adopts I -shaped steel no.
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Description

Technical Field

[0001] This utility model relates to the field of aircraft pavement technology, specifically to a rapid removal and installation structure for vertical surfaces during airport runway construction without interrupting operations. Background Technology

[0002] During airport runway construction or maintenance, vertical surfaces often form at the runway edges due to construction splicing, settlement differences, and other reasons. These vertical surfaces cause impacts between the aircraft tires and the runway edge during taxiing, affecting tire lifespan and potentially leading to unstable aircraft taxiing attitudes, posing safety hazards. Current methods for eliminating these vertical surfaces primarily involve on-site concrete pouring or laying single, inclined slabs. The former suffers from long construction periods and difficult on-site operations, while the latter, due to the large size and weight of the slabs, is difficult to precisely align with the runway surface during installation and lacks convenient traction and positioning structures, resulting in low installation efficiency and difficulty in ensuring overall flatness. Therefore, there is an urgent need for an airport runway structure that can quickly eliminate vertical surfaces, is easy to install, and allows for precise alignment. Utility Model Content

[0003] The purpose of this invention is to provide a rapid removal and installation structure for vertical surfaces during airport runway construction without interrupting operations, in order to solve the problems mentioned in the background art.

[0004] To achieve the above objectives, this utility model provides the following technical solution: a rapid removal and installation structure for vertical surfaces during airport runway construction without interrupting operations, comprising:

[0005] The continuous running track and the side running track;

[0006] The top surface of the continuous runway is set at the same level as the airport runway taxiway, and the side runways are set on both sides of the continuous runway or the airport runway.

[0007] The highest point of the side facade track surface is consistent with the top surface of the continuous track, and the side facade track has an angle of 5°-45° with the horizontal plane.

[0008] Further, the side runway includes two rows of vertically erected I-beams, the tops of which are connected by I-beams, and the bottoms of which are connected by a base plate. The I-beams, I-beams, and the base plate are all welded together.

[0009] Further, the two I-beams have load-bearing steel plates welded to their top surfaces, and the top surface of the continuous runway uses the same steel plates as the side runway.

[0010] Furthermore, the plan includes threaded holes at the four corners of the top surface of both the continuous running track and the side running track, with lifting rings screwed into the threaded holes.

[0011] Further, the traction component includes a steel cable with a hook fixed at one end and a threaded connector fixed at the end of the steel cable away from the hook, with a baffle screwed onto the threaded connector.

[0012] Further, when the side facade track connects with the continuous track, the traction component passes through from the same side. The diameter of the baffle is larger than the diameter of the hanging ring. A traction cable is used on one side of the continuous track to pull the side facade track to align with the continuous track.

[0013] Compared with the prior art, the beneficial effects of this utility model are:

[0014] This type of rapid vertical surface elimination installation structure for airport runway construction without interrupting flight operations eliminates the vertical surface at the runway edge by using a 5°-15° angle between the side runway and the horizontal plane, with the top flush with the continuous runway. This avoids impact on aircraft tires and ensures taxiing safety. The side runway is formed by welding I-beams and I-beams to the base plate, combined with load-bearing steel plates, resulting in high load-bearing strength. It is suitable for the high-frequency load-bearing requirements of airport runways. Through the cooperation of lifting rings and traction components, the side runway can be quickly positioned and connected to the continuous runway without the need for complex hoisting equipment, significantly improving installation efficiency. Attached Figure Description

[0015] Figure 1 This is a front structural diagram of the present invention;

[0016] Figure 2 This is a schematic diagram of the side elevation of the runway structure of this utility model;

[0017] Figure 3 This is a schematic diagram of the traction component structure of this utility model.

[0018] In the diagram: 1. Continuous running track; 2. Side running track; 201. Load-bearing steel plate; 202. I-beam one; 203. I-beam two; 204. Base plate; 205. Threaded hole; 206. Lifting ring; 3. Traction component; 301. Steel cable; 302. Threaded joint; 303. Baffle plate; 304. Hook. Detailed Implementation

[0019] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0020] like Figures 1 to 3As shown, this utility model provides a technical solution: a rapid removal and installation structure for the vertical surface of an airport runway during non-stop construction, including a continuous runway 1, a side runway 2, and a traction component 3.

[0021] The top surface of the continuous runway 1 is level with the airport runway taxiway surface to ensure the flatness requirements when aircraft taxi. The side runways 2 are selectively set on both sides of the continuous runway 1 or on both sides of the airport runway to eliminate the vertical surfaces at the runway edges.

[0022] like Figure 1 and Figure 2 As shown, the highest point of the side runway 2 is flush with the top surface of the continuous runway 1, and the angle between the side runway 2 and the horizontal plane is controlled within the range of 5°-45°. This angle range can effectively prevent the formation of a vertical surface at the edge of the runway, while avoiding the impact hazards caused by too small an angle or the space occupation problem caused by too large an angle.

[0023] The side facade running track 2 includes two rows of vertically installed I-beams 203. The tops of the two rows of I-beams 203 are fixedly connected by I-beams 202, and the bottoms of the I-beams 203 are fixedly connected by a base plate 204. The I-beams 202, I-beams 203 and the base plate 204 are all welded together to form a stable frame structure and ensure the load-bearing strength of the side facade running track 2.

[0024] The top surfaces of the two I-beams 202 are welded and fixed with load-bearing steel plates 201. The top surface of the continuous runway 1 and the load-bearing steel plates 201 of the side runway 2 are made of the same material and specifications to ensure that the flatness of the two after they are joined is consistent and meets the use standards of airport runways.

[0025] Threaded holes 205 are provided at the four corners of the top surface of the continuous running track 1 and the side running track 2. A lifting ring 206 is screwed into the threaded hole 205. The lifting ring 206 is used to cooperate with the traction component 3 to achieve docking and positioning of the two.

[0026] like Figure 3 As shown, the traction component 3 includes a steel cable 301. One end of the steel cable 301 is fixed with a hook 304, and the other end is fixed with a screw connector 302. A baffle 303 is screwed onto the screw connector 302. The diameter of the baffle 303 is larger than the inner diameter of the lifting ring 206 to prevent the screw connector 302 from coming out of the lifting ring 206 during the traction process.

[0027] When the side facade track 2 is connected to the continuous track 1, the traction component 3 is passed through the same side of both. First, the hook 304 is attached to the lifting ring 206 of the side facade track 2. Then, the end of the steel cable 301 away from the hook 304 is passed through the lifting ring 206 on the same side of the continuous track 1. The baffle 303 is tightened through the screw connector 302. Then, the steel cable 301 is pulled on one side of the continuous track 1 to adjust the position of the side facade track 2 until its top surface is flush with the top surface of the continuous track 1, thus completing the precise connection. After the continuous track 1 or the side facade track 2 is installed, the top surface can be kept flat simply by unscrewing the replacement 206.

[0028] Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the present invention, the scope of which is defined by the appended embodiments and their equivalents.

Claims

1. A rapid removal and installation structure for vertical surfaces during airport runway construction without interrupting flight operations, characterized in that... include: The continuous running track (1) and the side running track (2); The top surface of the continuous runway (1) is set at the same level as the airport runway taxiway, and the side runway (2) is set on both sides of the continuous runway (1) or the airport runway. The highest point of the side runway (2) is consistent with the top surface of the continuous runway (1), and the side runway (2) has an angle of 5°-45° with the horizontal plane.

2. The rapid removal and installation structure for vertical surfaces during airport runway construction without interrupting flight operations, as described in claim 1, is characterized in that: The side runway (2) includes two rows of I-beams (203) erected vertically. The tops of the two rows of I-beams (203) are connected by I-beams (202), and the bottoms of the I-beams (203) are connected by a base plate (204). The I-beams (202), I-beams (203) and the base plate (204) are all welded together.

3. The rapid removal and installation structure for vertical surfaces during airport runway construction without interrupting flight operations, as described in claim 2, is characterized in that: The top surfaces of the two I-beams (202) are welded with load-bearing steel plates (201), and the top surface of the continuous runway (1) and the side runway (2) use the same steel plates.

4. The rapid removal and installation structure for vertical surfaces during airport runway construction without interrupting flight operations, as described in claim 1, is characterized in that: The top surface of the continuous running track (1) and the side running track (2) are provided with threaded holes (205) at the four corners, and a hanging ring (206) is screwed into the threaded hole (205).

5. The rapid removal and installation structure for vertical surfaces during airport runway construction without interrupting flight operations, as described in claim 1, is characterized in that: The traction component includes a steel cable (301), one end of which is fixed with a hook (304), and the other end of the steel cable (301) away from the hook (304) is fixed with a screw connector (302), and a baffle (303) is screwed onto the screw connector (302).

6. The rapid removal and installation structure for vertical surfaces during airport runway construction without interrupting flight operations, as described in claim 5, is characterized in that: When the side facade track (2) is connected to the continuous track (1), the traction member (3) passes through from the same side. The diameter of the baffle (303) is larger than the diameter of the hanging ring (206). The traction cable (301) on one side of the continuous track (1) pulls the side facade track (2) to be aligned with the continuous track (1).