A pluggable roller connector for aircraft landing gear that avoids the effects of harsh environments

Abstract

This utility model discloses a pluggable roller connector for aircraft landing gear that avoids the impact of harsh environments. It includes a connector with a roller inserted at its lower end. The outer sides of the bolts and nuts are respectively provided with spiral grooves on the connector, and protective covers are spirally wound within each spiral groove. Each protective cover has a rubber plate on its outer wall. The protective covers of this pluggable roller connector for aircraft landing gear, which avoids the impact of harsh environments, form a spiral locking structure with the connector through the spiral grooves. This spirally installed protective cover protects the bolts and related components, thus preventing the connecting parts between the connectors from being affected by harsh external environments. The rubber pads of this device, through locking blocks and spiral blocks, form a spiral locking structure with the protective covers. This spirally installed rubber pad further limits the movement of the bolts and nuts and provides shock absorption protection, thereby increasing the stability of the connector connecting parts.

Description

Technical Field

[0001] This utility model relates to the field of aviation technology, specifically to a pluggable roller connector for aircraft landing gear that avoids the effects of harsh environments. Background Technology

[0002] Aviation specifically refers to human flight activities and related technological fields conducted within the atmosphere using mechanical devices. Its flight range is limited to the airspace below the 100-kilometer karman line above the Earth's surface, primarily relying on air-breathing engines and aviation fuel as its power source. During aviation, to facilitate quick installation of the rollers for normal flight operation, pluggable roller connectors are used for assembly.

[0003] In the use of pluggable roller connectors, the connector and rollers are assembled using multiple sets of bolts to ensure the device can operate normally during flight. However, existing pluggable roller connectors are susceptible to low-temperature vibration damage to the bolts and other connecting components in harsh environments, thus reducing their operational stability. Therefore, a pluggable roller connector for aircraft landing gear that avoids the effects of harsh environments is proposed to solve the above problems. Utility Model Content

[0004] The purpose of this invention is to provide a pluggable roller connector for aircraft landing gear that avoids the influence of harsh environments, in order to solve the problem mentioned in the background art that existing pluggable roller connectors are prone to low-temperature vibration affecting the bolts and other connecting components on the connector during use when the external environment is relatively harsh, thereby reducing their working stability.

[0005] To achieve the above objectives, this utility model provides the following technical solution: a pluggable roller connector for aircraft landing gear that avoids the influence of harsh environments, comprising a connector, wherein a roller is inserted through the lower end of the connector, and multiple sets of bolts are inserted through the connector, and the other end of the bolts is screwed with a nut, and the outer sides of the bolts and nuts are respectively provided with spiral grooves on the connector, and protective covers are respectively screwed in the spiral grooves, and the protective covers are provided with rubber plates on their outer walls;

[0006] The protective cover has a rubber pad inside, and the rubber pad has a locking block. The locking block is inserted into the through hole on the protective cover, and a spiral block is spiraled inside the locking block.

[0007] The protective cover has multiple sets of limiting frames inside, and an insulation board is placed between the limiting frames and the protective cover. One end of the rubber pad is inserted between the insulation boards.

[0008] Preferably, the connectors are connected by bolts and nuts to form a spiral locking structure.

[0009] Preferably, the protective cover is configured with a spiral locking structure by means of a spiral groove and a connector.

[0010] Preferably, the rubber pad forms a spiral locking structure with the locking block, the spiral block, and the protective cover.

[0011] Preferably, the insulation board has an arc-shaped structure, and the insulation board and the protective cover form a spiral locking structure through the limiting frame.

[0012] Compared with the prior art, the beneficial effects of this utility model are as follows: The protective cover of the pluggable roller connector for aircraft landing gear, which avoids the influence of harsh environments, forms a spiral locking structure with the connector through spiral grooves. Thus, the spirally installed protective cover can protect the bolts and related components, thereby preventing the connecting parts between the connectors from being affected by harsh external environments. The rubber pad of this device forms a spiral locking structure with the protective cover through locking blocks and spiral blocks. Thus, the spirally installed rubber pad can further limit the bolts and nuts and provide shock absorption protection, thereby increasing the stability of the connector connecting parts. The insulation board of this device has an arc-shaped structure, and the insulation board forms a spiral locking structure with the protective cover through a limiting bracket. Thus, when the external ambient temperature is low, the insulation board can protect the bolts and related components. Attached Figure Description

[0013] Figure 1 This is a schematic diagram of a pluggable roller connector for aircraft landing gear that avoids the effects of harsh environments according to this utility model.

[0014] Figure 2 This is a schematic diagram of the structure of a pluggable roller connector protective cover assembly for aircraft landing gear to avoid the effects of harsh environments according to this utility model.

[0015] Figure 3 This is a schematic diagram of the rubber plate assembly structure of a pluggable roller connector for aircraft landing gear to avoid the effects of harsh environments according to this utility model.

[0016] Figure 4 This is a schematic diagram of the structure of a pluggable roller connector limit bracket assembly for aircraft landing gear that avoids the effects of harsh environments according to this utility model;

[0017] Figure 5 This is a schematic diagram of the insulation board assembly for a pluggable roller connector for aircraft landing gear that avoids the effects of harsh environments.

[0018] In the diagram: 1. Connector, 2. Roller, 3. Bolt, 4. Nut, 5. Protective cover, 6. Rubber plate, 7. Rubber pad, 8. Clamping block, 9. Spiral block, 10. Limiting frame, 11. Insulation board. 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] Please see Figure 1-5 This utility model provides a technical solution: a pluggable roller connector for aircraft landing gear that avoids the influence of harsh environments, including a connector 1, a roller 2 inserted at the lower end of the connector 1, multiple sets of bolts 3 inserted on the connector 1, and a nut 4 screwed on the other end of the bolt 3.

[0021] Furthermore, the connectors 1 are connected by bolts 3 and nuts 4 to form a spiral locking structure, thereby facilitating the assembly and use of the connectors 1 through the bolts 3 and nuts 4 assembly.

[0022] The outer sides of the bolts 3 and nuts 4 are respectively provided with spiral grooves on the connector 1, and protective covers 5 are spirally spiraled in the spiral grooves. The protective covers 5 are provided with rubber plates 6 on their outer walls. It should be noted that the protective covers 5 are made of high-strength materials such as stainless steel and aluminum alloy, so as to effectively ensure their own protective effect.

[0023] Furthermore, the protective cover 5 forms a spiral locking structure with the connector 1 through spiral grooves, thereby facilitating the protection of the bolt 3 and its related connecting parts through the spirally installed protective cover 5 assembly.

[0024] The protective cover 5 has a rubber pad 7 inside, and the rubber pad 7 has a locking block 8. The locking block 8 is inserted into the through hole on the protective cover 5, and a spiral block 9 is spiraled inside the locking block 8.

[0025] Furthermore, the rubber pad 7 forms a spiral locking structure with the protective cover 5 through the locking block 8, the spiral block 9, and the corresponding rubber pad 7 can be installed inside the protective cover 5 through the spiral block 9, so as to limit the bolt 3 and the nut 4 and provide shock absorption protection through the corresponding rubber pad 7.

[0026] The protective cover 5 has multiple sets of limiting brackets 10 inside, and an insulation board 11 is placed between the limiting brackets 10 and the protective cover 5. One end of the rubber pad 7 is inserted between the insulation boards 11. It should be noted that this utility model is a pluggable roller connector for aircraft landing gear that avoids the influence of harsh environments. All components are standard parts or components known to those skilled in the art. Its structure and principle can be learned by those skilled in the art through technical manuals or conventional experimental methods.

[0027] Furthermore, the insulation board 11 has an arc-shaped structure, and the insulation board 11 forms a spiral locking structure with the protective cover 5 through the limiting frame 10, so that the insulation board 11 placed in a limiting position can avoid the impact of the low external environment on the bolt 3 and its related components.

[0028] Working Principle: When using a pluggable roller connector for aircraft landing gear designed to withstand harsh environments, the connector 1 and roller 2 are first assembled using multiple sets of bolts 3 and nuts 4 via a spiral connection. This allows the roller 2 to function properly in the aircraft. After the bolts 3 and nuts 4 are installed, they are spirally mounted onto the connector 1 via the threads on the outer wall of the protective cover 5. The protective cover 5 protects the bolts 3 and nuts 4, while the rubber plate 6 further protects the spiral groove and related components, thus preventing the connection from being affected by harsh external environments. Before using the protective cover 5, the appropriate rubber pad 7 can be selected based on the bolts 3 and nuts 4, and the locking block 8 is used to secure the connection. The connector is placed inside the protective cover 5 and screwed on by the bolt block 9. The screw-mounted rubber pad 7 can limit and dampen the bolt 3 and nut 3, further ensuring the working stability of the connecting components on the connector 1. If the aircraft needs to pass through a low-temperature environment during operation, the insulation plate 11 is limited by the limiting frame 10. At the same time, the rubber pad 7 inserted in the limiting plate 11 provides auxiliary limiting for the insulation plate 11. Thus, the insulation plate 11 prevents the low temperature environment from affecting the connecting components of the connector 1. This is the usage process of the plug-in roller connector for aircraft landing gear that avoids the influence of harsh environments.

[0029] Although the present invention has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions described in the foregoing embodiments or make equivalent substitutions for some of the technical features. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of the present invention should be included within the protection scope of the present invention.

Claims

1. A pluggable roller connector for aircraft landing gear to avoid the effects of harsh environments, comprising a connector (1), wherein a roller (2) is inserted through the lower end of the connector (1), and a plurality of bolts (3) are respectively inserted through the connector (1), and a nut (4) is screwed onto the other end of the bolts (3), characterized in that: The outer sides of the bolt (3) and nut (4) are respectively provided with spiral grooves on the connector (1), and protective covers (5) are spirally spiraled in the spiral grooves respectively. The protective cover (5) is provided with a rubber plate (6) on its outer wall. The protective cover (5) has a rubber pad (7) inside, and the rubber pad (7) has a locking block (8). The locking block (8) is inserted into the through hole on the protective cover (5), and a spiral block (9) is spiraled inside the locking block (8). The protective cover (5) has multiple sets of limiting frames (10) inside, and a heat insulation board (11) is placed between the limiting frames (10) and the protective cover (5). One end of the rubber pad (7) is inserted between the heat insulation boards (11).

2. A plug-in roller connector for an aircraft landing gear to avoid the influence of harsh environments according to claim 1, characterized in that: The connectors (1) are connected by bolts (3) and nuts (4) to form a spiral locking structure.

3. A plug-in roller connector for an aircraft landing gear to avoid the influence of harsh environments according to claim 1, characterized in that: The protective cover (5) forms a spiral locking structure with the connector (1) through a spiral groove.

4. The plug-in roller connector for an aircraft landing gear to avoid the influence of harsh environments according to claim 1, characterized in that: The rubber pad (7) forms a spiral locking structure with the locking block (8), the spiral block (9) and the protective cover (5).

5. The plug-in roller connector for an aircraft landing gear to avoid the influence of harsh environments according to claim 1, characterized in that: The insulation board (11) has an arc-shaped structure, and the insulation board (11) and the protective cover (5) form a spiral locking structure through the limiting frame (10).

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