Modularized patrolling bomb

Abstract

The utility model discloses a modularization patrolling bomb which comprises a warhead, an electronic cabin, a battery cabin, a propeller cabin, a first wing and a second wing, and the warhead, the electronic cabin, the battery cabin and the propeller cabin are respectively provided with a modularization connection interface which is used for achieving fast disassembly and assembly of all cabin sections. And the first wing and the second wing are connected with the aircraft body through a quick-assembly and quick-disassembly structure. According to the utility model, all cabin sections of the patrolling bomb can be quickly disassembled and assembled conveniently.

Description

TECHNICAL FIELD

[0001] The utility model relates to unmanned plane technical field especially is related to a modularized cruise missile. BACKGROUND

[0002] At present, the unmanned plane technology has been widely applied in the military field, especially in the reconnaissance and strike tasks. The traditional cruise missile is usually designed in an integrated manner, and the components cannot be disassembled, which leads to inconvenience in maintenance and upgrading. With the increase of task diversity and complexity, the cruise missile designed in an integrated manner cannot meet the changing combat requirements, therefore, modular design has become a new development trend. The modular design can realize quick replacement of different functional modules, improve the flexibility and adaptability of the cruise missile, and thus better cope with various combat environments.

[0003] The existing cruise missile design has the following defects: the cruise missile designed in an integrated manner cannot be quickly replaced, leading to inconvenience in maintenance and upgrading, and cannot adapt to changing combat requirements; although the plug-in interface design can realize replacement of some modules, it has problems of complex installation and easy damage to the interface in actual use, affecting the reliability and service life of the cruise missile; although the quick disassembly and assembly design can realize quick replacement of some modules, it still has problems of error-proof assembly and damage prevention in actual application, which easily leads to damage of the interface and failure of the module. Therefore, how to design a modular connection method that is both quick and reliable has become a technical problem to be solved. UTILITY MODEL CONTENT

[0004] The application provides a modular cruise missile, which facilitates quick disassembly and assembly of each cabin section of the cruise missile.

[0005] The application provides a modular cruise missile, which adopts the following technical scheme:

[0006] A modular cruise missile comprises a warhead, an electronic cabin, a battery cabin, a propeller cabin, a first wing and a second wing, wherein the warhead, the electronic cabin, the battery cabin and the propeller cabin are each provided with a modular connection interface for realizing quick disassembly and assembly between the cabin sections, and the first wing and the second wing are connected to the body through a quick assembly and disassembly structure.

[0007] Through the above technical scheme, the modular cruise missile designed by the utility model can realize quick disassembly and assembly of each cabin section of the cruise missile through modular design and modular connection structure.

[0008] Preferably, the modular connection interface comprises an electrical connection interface and a mechanical connection interface, and the electrical connection interface is provided with an error-proof mechanism.

[0009] By adopting the above technical scheme, in use, the combination design of the electrical connection interface and the mechanical connection interface ensures the simultaneous completion of electrical connection and physical connection, simplifying the operation process. The introduction of the error-proof mechanism effectively avoids connection errors caused by misoperation, thereby damaging the electrical connection interface.

[0010] Preferably, the electrical connection interface comprises a plug and a socket, and the plug and the socket are respectively arranged on the abutting faces of adjacent cabin sections.

[0011] By adopting the above technical scheme, in use, the design of the plug and the socket can ensure the reliability and stability of electrical connection between cabin sections, while simplifying the connection process and improving assembly efficiency. Specifically, the arrangement of the plug and the socket can effectively avoid signal transmission problems caused by poor contact, ensuring the normal operation of the modular cruise missile in complex environments.

[0012] Preferably, the mechanical connection interface comprises a clamping block and a clamping groove arranged on adjacent cabin sections, and the clamping block and the clamping groove are mutually clamped to realize mechanical connection of adjacent cabin sections.

[0013] By adopting the above technical scheme, in use, the mutual clamping design of the clamping block and the clamping groove ensures the reliability and convenience of mechanical connection, reducing assembly time and operation difficulty.

[0014] Preferably, the error-proof mechanism comprises a sliding groove structure, the sliding groove structure is arranged on one side of the socket, and the plug passes through the sliding groove structure so that the modular connection interface can only be aligned and inserted in a predetermined direction during installation.

[0015] By adopting the above technical scheme, in use, the sliding groove structure ensures that the plug can only be aligned and inserted in the socket in a predetermined direction during installation, effectively preventing incorrect installation and improving the reliability and safety of the modular connection interface.

[0016] Preferably, the first wing and the second wing are fixed on both sides of the fuselage through a quick-mounting and quick-detaching mechanism, the quick-mounting and quick-detaching mechanism comprises a buckle and a groove matched with the buckle, and a guide slope is arranged in the groove for guiding the wing to align with the buckle position during installation.

[0017] By adopting the above technical scheme, in use, the quick-mounting and quick-detaching mechanism comprises a buckle and a groove matched with the buckle, and a guide slope is arranged in the groove, which can guide the wing to accurately align with the buckle position during installation, thereby significantly improving installation efficiency and reliability, reducing operation time, and reducing maintenance difficulty.

[0018] Preferably, the buckle is provided with an elastic locking member for automatic locking after the wing is installed in place.

[0019] By adopting the above technical scheme, the elastic locking member provided on the buckle can automatically lock after the wing is installed in place, effectively preventing the wing from loosening or falling off during flight, and improving the stability and safety of the cruise missile.

[0020] Preferably, the modular connection interfaces of the warhead, electronic cabin, battery cabin and propeller cabin have the same size and shape, facilitating standardized production and interchangeable use.

[0021] By adopting the above technical scheme, the modular connection interfaces of the warhead, electronic cabin, battery cabin and propeller cabin have the same size and shape, facilitating standardized production and interchangeable use, and improving production efficiency and maintenance convenience.

[0022] In summary, the present application has the following beneficial effects:

[0023] 1. The modular cruise missile designed by the utility model can be quickly disassembled and assembled between cabin sections, improving the maintainability and expandability of the cruise missile, reducing production cost and maintenance difficulty, and being particularly suitable for rapid replacement and maintenance on the battlefield.

[0024] 2. The modular cruise missile designed by the utility model introduces a quick mounting and dismounting structure, making the mounting process of the first wing and the second wing more convenient, improving the flexibility and adaptability of the cruise missile, and enabling quick replacement of wing assemblies of different shapes and sizes to adapt to different flight environments.

[0025] 3. The modular cruise missile designed by the utility model sets an error-proof mounting mechanism to effectively avoid the risk of incorrect mounting of the electrical connection interface, ensure correct connection between cabin sections, and enhance the stability and safety of the system. BRIEF DESCRIPTION OF DRAWINGS

[0026] Fig. 1 is a structural schematic view of an embodiment;

[0027] Fig. 2 is a structural schematic view of an embodiment showing an electronic cabin;

[0028] Fig. 3 is a structural schematic view of an embodiment showing a battery cabin;

[0029] Fig. 4 is a sectional view of an embodiment showing a quick mounting and dismounting structure;

[0030] Explanation of the accompanying symbols: 1. Warhead; 2. Electronic compartment; 3. Battery compartment; 4. Propeller compartment; 5. First wing; 6. Second wing; 7. Modular connection interface; 71. Electrical connection interface; 711. Plug; 712. Socket; 72. Mechanical connection interface; 721. Block; 722. Slot; 8. Quick assembly and disassembly structure; 81. Buckle; 82. Groove; 9. Anti-misassembly mechanism; 91. Slide structure; 10. Elastic locking part. DETAILED DESCRIPTION

[0031] The present invention will be described in further detail below with reference to the accompanying drawings. Like components are denoted by like reference numerals. It should be noted that the terms "front," "rear," "left," "right," "upper," "lower," "bottom," and "top" used in the following description refer to directions in the accompanying drawings, and the terms "inner" and "outer" refer to directions toward or away from the geometric center of a particular component, respectively.

[0032] The utility model discloses a modular loitering bomb, such as Figs. 1 to 4 As shown, it includes a warhead 1, an electronic compartment 2, a battery compartment 3, a propeller compartment 4, a first wing 5, and a second wing 6. The warhead 1, the electronic compartment 2, the battery compartment 3, and the propeller compartment 4 are all provided with a modular connection interface 7 for realizing rapid disassembly and assembly between the compartments. The first wing 5 and the second wing 6 are connected to the fuselage through a quick assembly and disassembly structure 8.

[0033] The modular connection interface 7 includes an electrical connection interface 71 and a mechanical connection interface 72. The electrical connection interface 71 includes a plug 711 and a socket 712, respectively located on the mating surfaces of adjacent compartments. The plug 711 can be made of a copper alloy, while the socket 712 can be a gold-plated plastic shell, ensuring good conductivity and corrosion resistance. The electrical connection interface 71 is equipped with an anti-misinstallation mechanism 9. This anti-misinstallation mechanism 9 includes a slide structure 91, which is located on one side of the socket 712. The slide structure 91 ensures that the plug 711 can be aligned and inserted only in a predetermined direction during installation. The slide structure 91 can be a groove 82 with a guide bar. The plug 711 is provided with a ridge that matches the guide bar, ensuring that the plug 711 does not shift when inserted into the socket 712. The mechanical connection interface 72 includes a block 721 and a slot 722, located on the adjacent compartments. The block 721 and slot 722 engage with each other to achieve mechanical connection between the adjacent compartments.

[0034] The first wing 5 and the second wing 6 are fixed on both sides of the fuselage through quick-mounting and quick-detaching mechanisms, which include buckles 81 and recesses 82 matched with the buckles 81, the recesses 82 are provided with guide inclined surfaces for guiding the wings to align with the positions of the buckles 81 during the mounting process, the buckles 81 can be spring buckles 81 made of high-strength plastic, the recesses 82 can be rectangular recesses 82 formed on the fuselage, and the guide inclined surfaces can make the wings more easily align with the positions of the buckles 81 during the mounting process, the buckles 81 are provided with elastic locking pieces 10 for automatically locking after the wings are mounted in place, and the elastic locking pieces 10 can be spring steel sheets, which will automatically pop out to fix the wings on the fuselage when the wings are mounted in place, and the quick-mounting and quick-detaching mechanisms can also adopt magnetic connection, that is, strong magnets are arranged on the wings and magnetic materials are arranged on the fuselage, so that the wings are quickly fixed and separated through magnetic force, and this design can realize tool-free mounting and dismounting and is suitable for rapid response and emergency rescue missions.

[0035] The modular connection interfaces 7 of the warhead 1, the electronic cabin 2, the battery cabin 3 and the propeller cabin 4 have the same size and shape, so that standardized production and interchangeable use are facilitated, the production process is simplified, and the cost is reduced.

[0036] Working principle: The modularized patrol flying bomb designed by the utility model realizes quick dismounting between the cabin sections, improves the maintainability and expandability of the patrol flying bomb through the adoption of the modular connection interfaces 7 and the quick-mounting and quick-detaching structure 8, the design of the mechanical connection interfaces 72 and the electrical connection interfaces 71 ensures the firm connection between the cabin sections and the stable signal transmission, the mistake-proofing mechanism 9 avoids the occurrence of mistake mounting, and the quick-mounting and quick-detaching mechanism makes the mounting and dismounting of the wings more convenient.

[0037] The above are preferred embodiments of the present application, which do not limit the protection scope of the present application, therefore: all equivalent changes made according to the structure, shape and principle of the present application should be covered within the protection scope of the present application.

Claims

1. A modular loitering munition, characterized by: The invention comprises a warhead (1), an electronic compartment (2), a battery compartment (3), a propeller compartment (4), a first wing (5), and a second wing (6); the warhead (1), the electronic compartment (2), the battery compartment (3), and the propeller compartment (4) are all provided with a modular connection interface (7) for realizing rapid assembly and disassembly between the compartment sections; the first wing (5) and the second wing (6) are connected to the fuselage via a quick assembly and disassembly structure (8).

2. The modular loitering munition according to claim 1, characterized in that: The modular connection interface (7) comprises an electrical connection interface (71) and a mechanical connection interface (72), and the electrical connection interface (71) is provided with an anti-misinstallation mechanism (9).

3. The modular loitering munition according to claim 2, characterized in that: The electrical connection interface (71) comprises a plug (711) and a socket (712), and the plug (711) and the socket (712) are respectively arranged on the docking surfaces of adjacent compartments.

4. The modular loitering munition according to claim 2, characterized in that: The mechanical connection interface (72) comprises a clamping block (721) and a clamping slot (722) provided on adjacent compartments, and the clamping block (721) and the clamping slot (722) are mutually clamped to realize the mechanical connection of the adjacent compartments.

5. The modular loitering munition according to claim 2, characterized in that: The anti-misinstallation mechanism (9) includes a slide groove structure (91), which is arranged on one side of the socket (712). The plug (711) can only be aligned and inserted along a predetermined direction during the installation process through the slide groove structure (91).

6. The modular loitering munition according to claim 1, characterized in that: The first wing (5) and the second wing (6) are fixed to both sides of the fuselage via a quick-install and quick-release mechanism, wherein the quick-install and quick-release mechanism comprises a buckle (81) and a groove (82) cooperating therewith, wherein a guiding inclined surface is provided in the groove (82) for guiding the wings to align with the buckle (81) during the installation process.

7. The modular loitering munition according to claim 6, characterized in that: The buckle (81) is provided with an elastic locking piece (10) for automatically locking the wing after it is installed in place.

8. The modular loitering munition according to claim 1, characterized in that: The modular connection interfaces (7) of the warhead (1), the electronic compartment (2), the battery compartment (3), and the propeller compartment (4) have the same size and shape, facilitating standardized production and interchangeable use.

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