Airplane mooring rope take-up machine
By designing an aircraft tether rope take-up machine, a DC motor is used to drive the take-up fixture for automatic winding. Combined with a limit plate and rope guide groove, the problem of low efficiency in traditional manual take-up is solved, and a highly efficient and automated take-up process is achieved.
Patent Information
- Application Number
- CN202520153481.3
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-01-23
- Publication Date
- 2026-01-23
- Estimated Expiration
- 2035-01-23
AI Technical Summary
The traditional aircraft tether cable retrieval process is inefficient, requiring manual rolling on the ground to retrieve the cable, which is both inefficient and inconvenient to handle.
Design an aircraft tether rope take-up machine, including a base, take-up fixture, rope guide mechanism and drive mechanism. The take-up fixture is driven by a DC motor to automatically take up the rope. The machine is guided and limited by a limit plate and rope guide groove, eliminating the need for manual squatting to take up the rope.
It improves the efficiency and uniformity of aircraft mooring rope winding, makes it easier for users to handle the wound ropes, and enhances operational efficiency and convenience.
Smart Images
Figure CN223823090U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to the field of airport equipment, especially an aircraft mooring rope winding machine. BACKGROUND
[0002] When a large number of aircrafts on the parking apron encounter strong wind, they are generally handled in three ways, i.e., mooring, transposition and entering the hangar, to avoid damage to the aircraft. Because of the inherent flight characteristics of the aircraft, when the wind speed is greater than a certain degree, the aircraft is prone to move. At this time, the aircraft maintenance personnel need to connect and fix the connection point between the ground anchor on the ground of the parking apron and the landing gear of the aircraft through a mooring cable, so that the aircraft body can be kept stable under the action of the ground anchor and the mooring rope lock to prevent the aircraft from being blown away by the wind. However, the mooring cable must be untied before takeoff, and then the aircraft maintenance personnel need to collect the cable. SUMMARY
[0003] The technical problem to be solved by the embodiment of the utility model is to provide an aircraft mooring rope winding machine to improve the winding efficiency.
[0004] To solve the above technical problem, the embodiment of the utility model provides an aircraft mooring rope winding machine, which comprises a base, a winding tool, a rope guide mechanism and a driving mechanism. The base is provided with a plurality of casters at the bottom, the driving mechanism is arranged on the base, the winding tool is arranged on the driving mechanism, and the rope guide mechanism is correspondingly arranged on the base.
[0005] Further, the base is provided with a table top, and the winding tool is provided with a limiting plate.
[0006] Further, the driving mechanism adopts a DC motor, the DC motor is vertically arranged, and the winding tool is arranged on the main shaft of the DC motor.
[0007] Further, the limiting plate is parallel to the table top.
[0008] Further, the limiting plate is provided with a through groove.
[0009] Further, the rope guide mechanism comprises a body, and the body is provided with a rope guide groove with openings at both ends.
[0010] Further, the base is provided with a handle.
[0011] The utility model has the advantages that the rope guide mechanism is used for guiding, the winding tool is driven by the driving mechanism for winding, the manual squatting action for collecting the rope is saved, the efficiency and uniformity are greatly improved, and the user can conveniently carry the wound aircraft mooring rope. BRIEF DESCRIPTION OF DRAWINGS
[0012] Fig. 1It is the stereogram of the aircraft mooring rope take-up machine of the utility model embodiment.
[0013] Fig. 2 It is the side view of the aircraft mooring rope take-up machine of the utility model embodiment.
[0014] Fig. 3 It is the partial structure view of the aircraft mooring rope take-up machine of the utility model embodiment.
[0015] Explanation of reference numerals
[0016] Base 1, take-up tool 2, table top 3, limiting plate 4, DC motor 5, through slot 6, body 7, rope belt guide slot 8, handle 9, caster 10, main shaft 11. Specific implementation mode
[0017] It should be noted that the embodiments in the present application and the features in the embodiments can be combined with each other without conflict, and the utility model will be further explained in detail in combination with the drawings and specific embodiments.
[0018] In the embodiment of the utility model, if there is a directional indication (such as up, down, left, right, front, back, …), it is only used to explain the relative position relationship, movement condition, etc. between components in a certain specific posture (as shown in the drawings), if the specific posture changes, the directional indication also changes accordingly.
[0019] In addition, in the utility model, if the description of "first", "second" and the like is only for the purpose of description, and cannot be understood as indicating or implying the relative importance or implicitly indicating the number of the indicated technical features. Therefore, the features limited by "first", "second" can explicitly or implicitly include at least one feature.
[0020] Please refer to Figs. 1-3 The aircraft mooring rope take-up machine of the embodiment of the utility model comprises a base, a take-up tool, a rope belt guide mechanism and a driving mechanism.
[0021] The base bottom is provided with a plurality of casters, which facilitates the movement of the aircraft mooring rope take-up machine and the carrying of the aircraft mooring rope for the maintenance personnel in the airport. The driving mechanism is arranged on the base. The take-up tool is arranged on the main shaft of the driving mechanism, and the driving mechanism drives the take-up tool to wind. The take-up tool usually adopts a winding reel. The rope belt guide mechanism is correspondingly arranged on the base, and the rope belt guide mechanism is used to guide the scattered aircraft mooring rope on the bottom surface, so as to prevent the aircraft mooring rope from folding, tape sticking and the like during winding.
[0022] As an implementation mode, the base is provided with a table top, and the take-up tool is provided with a limiting plate. When the take-up tool winds the aircraft mooring rope, the upper and lower sides are limited by the limiting plate and the table top.
[0023] In one implementation, the drive mechanism includes a DC motor, a lithium battery, and a control circuit. The DC motor is controlled by the control circuit and powered by the lithium battery (this part is in the prior art). The DC motor is vertically mounted, and the winding fixture is mounted on the main shaft of the DC motor. Preferably, the limiting plate is parallel to the table surface.
[0024] As one implementation method, the limiting plate is provided with a through groove, which allows users to easily check the winding status of the aircraft mooring rope.
[0025] In one embodiment, the rope guiding mechanism includes a body with rope guiding grooves open at both the front and rear ends. Preferably, the rope guiding grooves are flush with the rope take-up fixture. Preferably, the two side edges at both the front and rear ends of the rope guiding grooves are curved surfaces to facilitate the insertion of aircraft mooring lines.
[0026] As one implementation, the base is equipped with a handle. The handle allows users to push it by hand, making it convenient for maintenance personnel to move the aircraft tether retractor and the aircraft tether rope.
[0027] The working principle of this utility model is as follows: the aircraft tether rope is manually placed into the rope tooling, the aircraft tether rope is guided into the rope guide groove of the rope guide mechanism, and the drive mechanism is started to realize automatic rope winding.
[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 claims and their equivalents.
Claims
1. An aircraft tether rope take-up machine, characterized in that, It includes a base, a winding fixture, a rope guide mechanism, and a drive mechanism. The base has several casters at the bottom, the drive mechanism is located on the base, the winding fixture is mounted on the drive mechanism, and the rope guide mechanism is located on the base.
2. The aircraft tether rope take-up machine as described in claim 1, characterized in that, The base is equipped with a platform, and the conveyor belt fixture is equipped with a limit plate.
3. The aircraft tether rope take-up machine as described in claim 2, characterized in that, The drive mechanism uses a DC motor, which is vertically mounted, and the winding fixture is mounted on the main shaft of the DC motor.
4. The aircraft tether rope take-up machine as described in claim 2, characterized in that, The limiting plate is parallel to the table surface.
5. The aircraft tether rope take-up machine as described in claim 2, characterized in that, The limiting plate is provided with a through groove.
6. The aircraft tether rope take-up machine as described in claim 1, characterized in that, The rope guide mechanism includes a body, on which a rope guide groove with openings at both the front and rear ends is provided.
7. The aircraft tether rope take-up machine as described in claim 1, characterized in that, The base is equipped with a handle.