Low-altitude aircraft micro-combustion power module with structure convenient to quickly disassemble and assemble

Abstract

The utility model belongs to the technical field of low-altitude aircrafts, and discloses a low-altitude aircraft micro-combustion power module with a structure convenient to quickly disassemble and assemble, which comprises a lower supporting shell, a positioning groove is arranged on the lower supporting shell, a positioning hole and a first threaded hole are arranged in the positioning groove, and a power module body is arranged in the lower supporting shell. A base is fixedly connected to the outer surface of the power module body, a positioning plate is fixedly connected to the outer surface of the power module body, a positioning block is fixedly connected to the lower surface of the positioning plate, a first bolt is arranged on the positioning plate, and an upper supporting shell is installed on the lower supporting shell. Through cooperation of a positioning groove, a positioning hole, a first threaded hole, a positioning block, a first bolt, a base and a positioning plate and cooperation of a positioning structure, hole alignment time can be shortened, rapid positioning can be achieved only by aligning positioning features during assembly, time for aligning or hole alignment one by one is shortened, shutdown time is saved through rapid disassembly and assembly, and working efficiency is improved; and the position consistency during each assembly is ensured, and the mounting accuracy is improved.

Description

Technical Field

[0001] This utility model belongs to the field of low-altitude aircraft technology, specifically a micro-fuel power module for low-altitude aircraft with a structure that is easy to assemble and disassemble. Background Technology

[0002] With the widespread application of short-endurance, low-altitude unmanned platforms in reconnaissance, mapping, logistics, and emergency response missions, there is a growing demand for power systems that are small in size, have high power-to-weight ratio, fast response, and are easy to maintain. Micro-fuel propulsion modules, with their compact structure and high energy density, have become one of the mainstream options. Meanwhile, diverse operational and civilian maintenance environments often require rapid replacement and repair in the field or under limited conditions, necessitating modularity, replaceability, and ease of rapid on-site assembly and disassembly of the power modules.

[0003] A hybrid electric vehicle module for unmanned aerial vehicles (UAVs) with application number CN201921431188.X includes an engine, a motor, and a mounting plate. The stator of the motor is fixed to the crankcase of the engine, and the rotor of the motor is driven to the crankshaft of the engine. The output end of the engine is driven to the power output shaft through a transmission system. The transmission system includes small multi-wedge pulleys, multi-wedge belts, and large multi-wedge pulleys. The output end of the engine is fixed with small multi-wedge pulleys, and the power output shaft is fixed with large multi-wedge pulleys. The small multi-wedge pulleys and the large multi-wedge pulleys are driven to each other through a multi-wedge belt.

[0004] However, the following problems were found in the implementation of the relevant technology: during installation, it requires multiple alignments and positioning and fixing with bolts or pins one by one. The disassembly and assembly process is cumbersome and highly dependent on professional tools and fixtures. On-site maintenance time is long, which affects the continuity of the task. At the same time, when parts need to be replaced, the whole thing needs to be replaced, and individual parts cannot be removed and replaced, resulting in high maintenance costs in the later stage.

[0005] To address this, we propose a micro-fuel propulsion module for low-altitude aircraft with a structure that is easy to assemble and disassemble quickly. Utility Model Content

[0006] To address the problems mentioned in the background art, this utility model provides a low-altitude aircraft micro-fuel power module with a structure that facilitates quick assembly and disassembly. It features a positioning structure that reduces the time spent on hole alignment, improving work efficiency and installation accuracy. Furthermore, it adopts a segmented installation method, which allows for maintenance by removing only the affected modules without requiring complete disassembly.

[0007] To achieve the above objectives, this utility model provides the following technical solution: a low-altitude aircraft micro-fuel propulsion module with a structure that is easy to assemble and disassemble quickly, comprising a lower support shell, a positioning groove provided on the lower support shell, a positioning hole and a first threaded hole provided in the positioning groove, a power module body installed inside the lower support shell, a base fixedly connected to the outer surface of the power module body, a positioning plate fixedly connected to the outer surface of the power module body, a positioning block fixedly connected to the lower surface of the positioning plate, a first bolt provided on the positioning plate, an upper support shell installed on the lower support shell, second bolts installed on the lower and upper support shells, slots provided on both sides of the lower and upper support shells, clamp flanges installed on the slots, a second flange installed on the outer surface of the clamp flanges, and a connecting pipe fixedly connected to the other side of the second flange.

[0008] Preferably, the base is provided with a second threaded hole, and the lower support shell and the upper support shell are fixed to the base through the second threaded hole and the second bolt.

[0009] Preferably, the positioning plate, the lower support shell, and the upper support shell are provided with recessed holes, and the first bolt and the second bolt are located in the recessed holes.

[0010] Preferably, the positioning block is movably connected to the positioning hole, and the first bolt is threadedly connected to the first threaded hole.

[0011] Preferably, the positioning plate is movably connected to the positioning groove.

[0012] Preferably, the outer diameter of the base is equal to the inner diameter of the lower support shell, and the base is in contact with the lower support shell and the upper support shell.

[0013] Preferably, two mounting plates are fixedly connected to the outer surfaces of the lower support shell and the upper support shell, and a third bolt is provided on the mounting plate.

[0014] Compared with the prior art, the beneficial effects of this utility model are as follows:

[0015] 1. This utility model, through the cooperation of positioning groove, positioning hole, first threaded hole, positioning block, first bolt, base and positioning plate, can reduce the time for hole alignment. During assembly, it is only necessary to align the positioning features to quickly put it in place, reducing the time for alignment or hole alignment one by one. Quick disassembly and assembly save downtime, improve work efficiency, and ensure consistent position during each assembly, reduce human error and improve installation accuracy.

[0016] 2. This utility model, through the cooperation of the lower support shell, the slot, the clamp flange, the second flange, the connecting pipe and the upper support shell, allows the power module installation section and the connecting pipe to be installed in sections. The power module section is installed separately in sections and modularly. Only the affected modules need to be removed, without the need for overall disassembly, which significantly shortens downtime and improves efficiency. Furthermore, consumable parts or small modules can be replaced individually, avoiding the need for expensive replacement of large assemblies. Attached Figure Description

[0017] Figure 1 This is a schematic diagram of the overall side view structure of this utility model;

[0018] Figure 2 This is a schematic diagram of the lower support shell connection structure of this utility model;

[0019] Figure 3 This is a schematic diagram of the internal structure of the support shell of this utility model;

[0020] Figure 4 This is a top view of the overall structure of this utility model.

[0021] In the diagram: 1. Lower support shell; 2. Positioning groove; 3. Positioning hole; 4. First threaded hole; 5. Power module body; 6. Base; 7. Positioning plate; 8. Positioning block; 9. First bolt; 10. Second bolt; 11. Slot; 12. Clamp flange; 13. Second flange; 14. Connecting pipe; 15. Mounting plate; 16. Third bolt; 17. Upper support shell. Detailed Implementation

[0022] 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.

[0023] like Figures 1 to 4As shown, this utility model provides a low-altitude aircraft micro-fuel power module with a structure that is easy to assemble and disassemble quickly. It includes a lower support shell 1, a positioning groove 2 on the lower support shell 1, a positioning hole 3 and a first threaded hole 4 in the positioning groove 2, a power module body 5 installed in the lower support shell 1, a base 6 fixedly connected to the outer surface of the power module body 5, a positioning plate 7 fixedly connected to the outer surface of the power module body 5, a positioning block 8 fixedly connected to the lower surface of the positioning plate 7, a first bolt 9 on the positioning plate 7, an upper support shell 17 installed on the lower support shell 1, a second bolt 10 installed on the lower support shell 1 and the upper support shell 17, slots 11 on both sides of the lower support shell 1 and the upper support shell 17, clamp flanges 12 installed on the slots 11, a second flange 13 installed on the outer surface of the clamp flange 12, and a connecting pipe 14 fixedly connected to the other side of the second flange 13.

[0024] Specifically, the base 6 is provided with a second threaded hole, and the lower support shell 1 and the upper support shell 17 are fixed to the base 6 through the second threaded hole and the second bolt 10.

[0025] Furthermore, the positioning plate 7, the lower support shell 1, and the upper support shell 17 are provided with recessed holes, and the first bolt 9 and the second bolt 10 are located in the recessed holes.

[0026] Furthermore, the positioning block 8 is movably connected to the positioning hole 3, and the first bolt 9 is threadedly connected to the first threaded hole 4.

[0027] It is worth noting that the positioning plate 7 is movably connected to the positioning groove 2.

[0028] It is worth noting that the outer diameter of the base 6 is equal to the inner diameter of the lower support shell 1, and the base 6 is in contact with the lower support shell 1 and the upper support shell 17.

[0029] It is worth mentioning that two mounting plates 15 are fixedly connected to the outer surfaces of the lower support shell 1 and the upper support shell 17, and a third bolt 16 is provided on the mounting plate 15.

[0030] The power module body 5 is existing technology and will not be described in detail here. Additionally, this utility model also includes a power supply, controller, and switch, which are not the main technical points of this patent and will not be described in detail here. The "front, rear, left, and right" views of this device are... Figure 1 The direction shown in the diagram is the reference.

[0031] Working principle: During installation, first install the lower support shell 1, then align the power module body 5 with the positioning plate 7 and positioning groove 2 and install it inside the lower support shell 1. The positioning plate 7 is aligned and positioned with the positioning hole 3 via the positioning block 8. Thus, the power module body 5 can be installed simply by installing the positioning plate 7 in the positioning groove 2 without needing to be positioned. Then, tighten the first bolt 9 in the first threaded hole 4 to fix the position of the positioning plate 7, thereby fixing the power module body 5. Then, tighten the second bolt 10 in the second threaded hole on the base 6 to reinforce the installation of the power module body 5 and ensure the stability of the power module body 5. Finally, install the upper support shell 17. Install it on the lower support shell 1, and lock the mounting plate 15 on the lower support shell 1 and the upper support shell 17 with the third bolt 16 to fix the lower support shell 1 and the upper support shell 17, thus completing the installation of the lower support shell 1 and the upper support shell 17. Then, snap the clamp flange 12 into the groove 11 on the lower support shell 1 and the upper support shell 17 to ensure the tightness between the lower support shell 1 and the upper support shell 17. Then, install the connecting pipe 14 on the clamp flange 12 through the second flange 13, thereby connecting the connecting pipe 14 to the lower support shell 1 and the upper support shell 17, thus completing the installation of the connecting pipe 14. Note that all connections of this device are equipped with a sealing layer.

[0032] It should be noted that, in this document, relational terms such as "first" and "second" are used only to distinguish one entity or operation from another, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Furthermore, the terms "comprising," "including," or any other variations thereof are intended to cover non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements includes not only those elements but also other elements not expressly listed, or elements inherent to such process, method, article, or apparatus.

[0033] 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. A low-altitude aircraft micro-fuel propulsion module with a structure that is easy to assemble and disassemble quickly, comprising a lower support shell (1), characterized in that: The lower support shell (1) is provided with a positioning groove (2), the positioning groove (2) is provided with a positioning hole (3) and a first threaded hole (4), the power module body (5) is installed in the lower support shell (1), the base (6) is fixedly connected to the outer surface of the power module body (5), the positioning plate (7) is fixedly connected to the outer surface of the power module body (5), the positioning block (8) is fixedly connected to the lower surface of the positioning plate (7), the positioning plate (7) is provided with a first bolt (9), the upper support shell (17) is installed on the lower support shell (1), the lower support shell (1) and the upper support shell (17) are provided with a second bolt (10), the lower support shell (1) and the upper support shell (17) are provided with slots (11) on both sides, the slots (11) are provided with clamp flanges (12), the outer surface of the clamp flanges (12) is provided with a second flange (13), and the other side of the second flange (13) is fixedly connected with a connecting pipe (14).

2. The low-altitude aircraft micro-fuel propulsion module with a structure that is easy to assemble and disassemble according to claim 1, characterized in that: The base (6) is provided with a second threaded hole, and the lower support shell (1) and the upper support shell (17) are fixed to the base (6) through the second threaded hole and the second bolt (10).

3. The low-altitude aircraft micro-fuel propulsion module with a structure that is easy to assemble and disassemble according to claim 1, characterized in that: The positioning plate (7), the lower support shell (1), and the upper support shell (17) are provided with recessed holes, and the first bolt (9) and the second bolt (10) are located in the recessed holes.

4. The low-altitude aircraft micro-fuel propulsion module with a structure that is easy to assemble and disassemble according to claim 1, characterized in that: The positioning block (8) is movably connected to the positioning hole (3), and the first bolt (9) is threadedly connected to the first threaded hole (4).

5. The low-altitude aircraft micro-fuel propulsion module with a structure that is easy to assemble and disassemble according to claim 1, characterized in that: The positioning plate (7) is movably connected to the positioning groove (2).

6. The low-altitude aircraft micro-fuel propulsion module with a structure that is easy to assemble and disassemble according to claim 1, characterized in that: The outer diameter of the base (6) is equal to the inner diameter of the lower support shell (1), and the base (6) is in contact with the lower support shell (1) and the upper support shell (17).

7. The low-altitude aircraft micro-fuel propulsion module with a structure that is easy to assemble and disassemble according to claim 1, characterized in that: Two mounting plates (15) are fixedly connected to the outer surfaces of the lower support shell (1) and the upper support shell (17), and a third bolt (16) is provided on the mounting plate (15).

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