Mounting and handling tool for an aircraft engine

Abstract

The utility model discloses an installation and carrying tool for airplane engine relates to AGV technical field, including the car body, its bottom symmetry is provided with mobile module, mobile module includes the wheel of being driven rotation by servo motor, the both sides of car body top are equipped with hydraulic pressure top telescopic rod group respectively, hydraulic pressure top telescopic rod group is by two symmetrical rotation setting parallel distribution and is composed of main hydraulic pressure top telescopic rod, the end of main hydraulic pressure top telescopic rod telescopic end is fixedly installed with the plug connector, the car body is hinged with additional hydraulic pressure top telescopic rod, additional hydraulic pressure top telescopic rod with main hydraulic pressure top telescopic rod shell rotation is connected, and two additional hydraulic pressure top telescopic rods on hydraulic pressure top telescopic rod group are adjacent distribution. The utility model discloses through its innovation self -adaptation hydraulic pressure jacking mechanism and high reliability, the mobile chassis of redundancy design, has successfully solved the technical problem of heavy -duty engine in the factory area automation, safety, stable, high -efficient transfer.

Description

Technical Field

[0001] This utility model relates to AGV technology, specifically an installation and handling tool for aircraft engines. Background Technology

[0002] Currently, the transportation of engines relies on manual crane operation for handling and loading / unloading, which involves a large amount of manpower, low work efficiency, low automation, and high safety risks. Therefore, this solution is designed based on the current situation to create a transport vehicle and a manual handling and loading / unloading system, in order to significantly improve work efficiency, reduce manpower, and lower operational safety risks. Utility Model Content

[0003] The purpose of this invention is to provide an installation and handling tool for aircraft engines to address the aforementioned shortcomings in the prior art.

[0004] To achieve the above objectives, this utility model provides the following technical solution: an installation and handling tool for an aircraft engine, comprising a vehicle body with symmetrically arranged movable modules at its bottom, the movable modules including wheels driven to rotate by servo motors;

[0005] Hydraulic jacking rod assemblies are respectively installed on both sides of the top of the vehicle body. Each hydraulic jacking rod assembly consists of two main hydraulic jacking rods that are symmetrically rotated and parallel to each other. A connector is fixedly installed at the end of the telescopic end of each main hydraulic jacking rod.

[0006] The vehicle body is hinged with an auxiliary hydraulic jacking rod, which is rotatably connected to the housing of the main hydraulic jacking rod, and the two auxiliary hydraulic jacking rods on the hydraulic jacking rod assembly are distributed adjacent to each other.

[0007] Preferably, the system also includes a side wing accommodating shell fixedly installed on the top of the vehicle body, the side wing accommodating shell having perforated slots for the main hydraulic extension rod and the auxiliary hydraulic extension rod to extend out.

[0008] Preferably, a groove is formed between the two side wing cavities, and a plurality of inclined trapezoidal plates with side wall contact are installed on the fixing plate between the side wing cavities and the top of the vehicle body.

[0009] Preferably, the vehicle body has a window in the center, and a ventilation grille is fixedly installed inside the window.

[0010] Preferably, the number of mobile modules is at least six, and each mobile module includes at least a control compartment.

[0011] Preferably, the mobile module includes a base, and wheels are rotatably mounted on opposite sides of the base;

[0012] The servo motor includes a first servo motor and a second servo motor, and the first servo motor and the second servo motor are connected to the two wheels via chain drive.

[0013] Preferably, the first servo motor and the second servo motor are relatively distributed.

[0014] In the above technical solution, the aircraft engine installation and handling tool provided by this utility model has the following beneficial effects: It consists of two sets of symmetrically arranged, rotatable main hydraulic jacking rods and hinged auxiliary hydraulic jacking rods. Through coordinated action, the connectors at the ends of the jacking rods can accurately and stably lift the engine. The bottom of the vehicle is equipped with multiple sets of moving modules driven by independent servo motors, ensuring the flexibility and load-bearing capacity of the AGV. Attached Figure Description

[0015] To more clearly illustrate the technical solutions in the embodiments of this application or the prior art, the drawings used in the embodiments will be briefly introduced below. Obviously, the drawings described below are only some embodiments recorded in this utility model. For those skilled in the art, other drawings can be obtained based on these drawings.

[0016] Figure 1 A schematic diagram of the overall structure provided for an embodiment of this utility model;

[0017] Figure 2 A schematic diagram of the main hydraulic jacking rod and the auxiliary hydraulic jacking rod provided for an embodiment of this utility model;

[0018] Figure 3 This is a schematic diagram of the structure of the mobile module provided in an embodiment of the present utility model.

[0019] Explanation of reference numerals in the attached figures:

[0020] 1. Vehicle body; 2. Mobile module; 21. Wheels; 22. Control compartment; 23. Base; 241. First servo motor; 242. Second servo motor; 3. Main hydraulic jacking rod; 4. Connector; 5. Attached hydraulic jacking rod; 6. Side wing trough shell; 61. Sloping trapezoidal plate; 7. Ventilation grille; 100. Groove. Detailed Implementation

[0021] To enable those skilled in the art to better understand the technical solution of this utility model, the present utility model will be further described in detail below with reference to the accompanying drawings.

[0022] Please see Figure 1-3The present invention provides a technical solution: an installation and handling tool for an aircraft engine, including a vehicle body 1, with a movable module 2 symmetrically arranged at its bottom, the movable module 2 including wheels 21 driven to rotate by a servo motor;

[0023] Hydraulic jacking rod assemblies are respectively installed on both sides of the top of the vehicle body 1. The hydraulic jacking rod assembly consists of two main hydraulic jacking rods 3 that are symmetrically rotated and parallel to each other; a connector 4 is fixedly installed at the end of the telescopic end of the main hydraulic jacking rod 3.

[0024] A secondary hydraulic jacking rod 5 is hinged to the vehicle body 1. The secondary hydraulic jacking rod 5 is rotatably connected to the housing of the main hydraulic jacking rod 3, and the two secondary hydraulic jacking rods 5 on the hydraulic jacking rod assembly are distributed adjacent to each other.

[0025] Specifically, through symmetrically arranged hydraulic jacking rod assemblies and a unique hinged structure—that is, the main hydraulic jacking rod 3 and the auxiliary hydraulic jacking rod 5 are rotatably connected—stable support and flexible extension / retraction of the jacking mechanism are achieved. This allows the equipment to accurately insert the connector 4 (with a T-shaped cross-section) into the engine lifting hole, completing fully automated gripping and lifting, significantly improving the transfer efficiency and automation level of the engine assembly line.

[0026] As a further embodiment of this utility model, it also includes a side wing accommodating shell 6 fixedly installed on the top of the vehicle body 1, and the side wing accommodating shell 6 is provided with a through groove for the main hydraulic extension rod 3 and the auxiliary hydraulic extension rod 5 to extend out.

[0027] By setting the side wing accommodating shell 6 and the perforated slot, a safe housing space is provided for the hydraulic jacking rod assembly, effectively preventing dust, oil and other pollutants in the workshop environment from entering the hinge point and piston rod surface, reducing the failure rate, extending the equipment life, and making the equipment shape more regular, thus reducing safety hazards.

[0028] As a further embodiment of this utility model, a groove 100 is formed between the two side wing cavities 6, and multiple inclined trapezoidal plates 61 with sidewall contact are installed on the fixing plate between the side wing cavities 6 and the top of the vehicle body 1. The groove 100 structure achieves lightweight design while ensuring overall strength, which helps to reduce the energy consumption of AGV operation. The multiple inclined trapezoidal plates 61 act as reinforcing ribs, significantly enhancing the rigidity and torsional resistance at the connection between the side wing cavities 6 and the top of the vehicle body 1, ensuring that the equipment can effectively resist deformation when bearing a heavy engine, and ensuring the smooth and safe operation and lifting process.

[0029] As a further embodiment of this utility model, a window is centrally located on the vehicle body 1, and a ventilation grille 7 is fixedly installed inside the window. This provides an effective air convection channel, which can dissipate the heat generated by internal components such as the electrical control cabinet and hydraulic pump station in a timely manner, preventing overheating damage to the components and ensuring the continuous and reliable operation of the equipment under high-intensity work.

[0030] As a further embodiment of this utility model, the number of mobile modules 2 is at least six, and each mobile module 2 includes at least a control compartment 22. Furthermore, the mobile module 2 includes a base 23, with wheels 21 rotatably mounted on opposite sides of the base 23; the servo motors include a first servo motor 241 and a second servo motor 242, both connected to the two wheels 21 via chain drive. The first servo motor 241 and the second servo motor 242 are relatively distributed. Differential rotation is achieved by driving the two wheels 21 through the first servo motor 241 and the second servo motor 242.

[0031] Specifically, the distributed design of each module's built-in control compartment allows each module to function as an independent control unit, achieving standardized and modular design and ensuring ease of maintenance. A first servo motor 241 and a second servo motor 242 drive two relatively distributed wheels 21 respectively, connected by chain transmission, giving the AGV stronger driving force and more precise control performance, enabling it to move forward, backward, and turn flexibly, adapting to narrow workshop environments. The aforementioned mobile module 2 has an adjustment accuracy of ±2mm and a maximum driving speed of 30m / min. Furthermore, the aforementioned mobile module 2 can realize control functions such as driving at a leftward tilt of 45°±15°, a rightward tilt of 45°±15°, lateral movement, and 360° turning on the spot.

[0032] The above description only illustrates certain exemplary embodiments of the present invention. Undoubtedly, those skilled in the art can modify the described embodiments in various ways without departing from the spirit and scope of the present invention. Therefore, the above drawings and descriptions are illustrative in nature and should not be construed as limiting the scope of protection of the claims of the present invention.

Claims

1. An installation and handling tool for an aircraft engine, characterized in that, It includes a vehicle body (1), and a moving module (2) is symmetrically arranged at its bottom. The moving module (2) includes wheels (21) that are driven to rotate by a servo motor. Hydraulic jacking rod assemblies are respectively installed on both sides of the top of the vehicle body (1). The hydraulic jacking rod assembly consists of two main hydraulic jacking rods (3) that are symmetrically rotated and parallel to each other. A connector (4) is fixedly installed at the end of the telescopic end of the main hydraulic jacking rod (3). The vehicle body (1) is hinged with an auxiliary hydraulic jacking rod (5), which is rotatably connected to the housing of the main hydraulic jacking rod (3), and the two auxiliary hydraulic jacking rods (5) on the hydraulic jacking rod assembly are distributed adjacent to each other.

2. The installation and handling tool for aircraft engines according to claim 1, characterized in that, It also includes a side wing caving shell (6) fixedly installed on the top of the vehicle body (1), and the side wing caving shell (6) has a perforated slot for the main hydraulic extension rod (3) and the auxiliary hydraulic extension rod (5) to extend out.

3. The installation and handling tool for aircraft engines according to claim 2, characterized in that, A groove (100) is formed between the two side wing cavities (6), and a plurality of inclined trapezoidal plates (61) with side wall contact are installed on the fixing plate between the side wing cavities (6) and the top of the vehicle body (1).

4. The installation and handling tool for aircraft engines according to claim 1, characterized in that, The vehicle body (1) has a window in the center, and a ventilation grille (7) is fixedly installed inside the window.

5. The installation and handling tool for an aircraft engine according to claim 1, characterized in that, The number of the mobile modules (2) is at least six, and each mobile module (2) includes at least a control compartment (22).

6. The installation and handling tool for an aircraft engine according to claim 5, characterized in that, The mobile module (2) includes a base (23), and wheels (21) are rotatably mounted on opposite sides of the base (23); The servo motor includes a first servo motor (241) and a second servo motor (242), and the first servo motor (241) and the second servo motor (242) are connected to the two wheels (21) via chain drive.

7. The installation and handling tool for an aircraft engine according to claim 6, characterized in that, The first servo motor (241) and the second servo motor (242) are relatively distributed.

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