Aircraft propelling device

Abstract

The utility model discloses an aircraft propelling device, which relates to the technical field of aircraft propelling devices and comprises a connecting assembly, a main body assembly and an internal assembly. The collector is arranged on the outer surface wall of the aircraft propulsion main body and communicated with the wind energy collecting device in the aircraft propulsion main body, and the sensor is arranged on one side of the valve switch to sense and recognize wind flow and collect and process wind energy. The wind energy collecting device converts collected wind energy into kinetic energy of the aircraft propulsion main body for conversion and use, so that energy is effectively converted and used, resource waste is avoided, two convex grooves are formed in one side of the aircraft propulsion main body and used for containing baffles to be embedded in the convex grooves, and the two convex grooves are formed in the other side of the aircraft propulsion main body. The two connecting pieces are arranged on one side of the baffle to be fixedly connected with the aircraft propelling body, the three-way catalytic converter and the particle filter are arranged on one side of the baffle to filter exhausted tail gas, and environmental pollution caused by excessive tail gas emission is avoided.

Description

Technical Field

[0001] The utility model relates to the technical field of aircraft propulsion devices, in particular to an aircraft propulsion device. Background Art

[0002] Aircraft propulsion is a vital component in aviation and aerospace engineering. It provides the necessary power for the aircraft to take off, fly, maneuver and land. The working principle of the aircraft propulsion is based on Newton's third law.

[0003] For example, Chinese patent "201520708521.2" discloses a serial electric field force aircraft propulsion device, which can be applied to various occasions inside and outside the atmosphere. The propulsion device includes a positive and negative ion generator array layer frame, a positive and negative ion generator, a shell, positive and negative screen grids, positive and negative neutralization layers, positive and negative acceleration grids, and insulating fixing bolts. The utility model uses positive and negative ion generators to continuously ionize the air through alternating current to generate a large number of positive and negative ions. The ions will be immediately captured by oxygen molecules, nitrogen molecules, carbon dioxide molecules, etc. in the air, thereby forming weak positive ion wind and negative ion wind. After multi-stage ionization and multi-stage acceleration, what comes out of the accelerator is an ion wind with high speed and high flux, so that the propulsion device can provide high thrust, and has the advantages of stable operation, no noise, large specific impulse, large thrust, and wide application occasions.

[0004] However, in the prior art, the combustion of existing aircraft propulsion devices will produce a large amount of harmful gases such as carbon dioxide, which pollutes the atmosphere. At the same time, the aircraft propulsion device contains many precision parts, which are not convenient for maintenance and repair. Utility Model Content

[0005] The utility model aims to solve the problems existing in the above-mentioned prior art and proposes an aircraft propulsion device.

[0006] In order to achieve the above-mentioned purpose, the utility model adopts the following technical scheme: an aircraft propulsion device, comprising a connecting component, a main body component and an internal component; the connecting component comprises a convex block, a support frame is installed on one side of the convex block, a rotating motor is arranged inside the support frame, and a rotating fan is installed on the output end of the rotating motor; the main body component comprises an aircraft propulsion body, a collector is installed on the outer wall of the aircraft propulsion body, a valve switch is arranged on the outer wall of the collector, a sensor is arranged on one side of the valve switch, a baffle is arranged on one side of the aircraft propulsion body, two connecting members are installed on one side of the baffle, and two convex grooves are opened on one side of the aircraft propulsion body; the internal component comprises a built-in box, two grooves are opened on one side of the built-in box, a circular arc groove is opened on one side of the built-in box, two fasteners are arranged on one side of the built-in box, a wind energy collection device is arranged inside the built-in box, and a particle filter is arranged inside the built-in box.

[0007] Preferably, the rotating motor is sleeved and installed on the support frame, and the rotating fan is sleeved and installed on the convex block.

[0008] Preferably, the collector is communicated with the interior of the aircraft propulsion body, and the valve switch is movably connected to the collector.

[0009] Preferably, the two connecting members are movably mounted on the baffle, and the two convex grooves are embedded in the baffle.

[0010] Preferably, the two grooves are connected to the arc groove, the two fasteners are movably mounted on the built-in box, the built-in box is fixedly mounted on the wind energy collection device, and the particle filter is sleeved on the built-in box.

[0011] Preferably, the built-in box is sleeved and installed with the aircraft propulsion body, a three-way catalytic converter is arranged on one side of the baffle, and the three-way catalytic converter is fixedly connected to the particulate filter.

[0012] Preferably, the wind energy collection device is electrically connected to the aircraft propulsion body, the two connecting parts are movably installed with the three-way catalytic converter and the wind energy collection device, and the collector is connected to the interior of the wind energy collection device.

[0013] Compared with the prior art, the advantages and positive effects of the utility model are:

[0014] 1. In the utility model, a collector is arranged on the outer wall of the aircraft propulsion body and is connected with the internal wind energy collection device. A sensor is arranged on one side of the valve switch to sense and identify the wind flow and collect and process the wind energy. The wind energy collection device converts the collected wind energy into kinetic energy of the aircraft propulsion body for conversion and use, so that the energy is effectively converted and used to avoid waste of resources. Two convex grooves are opened on one side of the aircraft propulsion body for placing a baffle and embedding it therewith. Two connecting parts are arranged on one side of the baffle to be fixedly connected with the aircraft propulsion body. A three-way catalytic converter and a particulate filter are arranged on one side of the baffle to filter and process the exhaust gas to avoid excessive exhaust gas emissions causing pollution to the environment.

[0015] 2. In the utility model, two connecting pieces are used to fix the three-way catalytic converter and the particulate filter to the aircraft propulsion body, which is convenient for disassembly and installation, as well as for inspection and maintenance. Two grooves and arc grooves are provided on one side of the aircraft propulsion body to communicate with each other, and the convex block is rotatably connected to the aircraft propulsion body. Two fasteners are provided to fix the two convex blocks of the convex block, and the rotating fan can also be movably connected, so that it can be disassembled and assembled, which is conducive to inspecting the interior of the aircraft propulsion body. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] Figure 1 The utility model provides a schematic diagram of the overall structure of an aircraft propulsion device;

[0017] Figure 2 A structural schematic diagram of a connecting assembly of an aircraft propulsion device is proposed for the utility model;

[0018] Figure 3 A schematic diagram of the structure of a main component of an aircraft propulsion device is provided for the utility model;

[0019] Figure 4 The utility model provides a structural schematic diagram of the internal components of an aircraft propulsion device.

[0020] Legend: 1. Connecting assembly; 101. Convex block; 102. Support frame; 103. Rotating motor; 104. Rotating fan; 2. Main assembly; 201. Aircraft propulsion body; 202. Collector; 203. Valve switch; 204. Sensor; 205. Baffle; 206. Connector; 207. Convex groove; 3. Internal assembly; 301. Built-in box; 302. Groove; 303. Arc groove; 304. Fastener; 305. Wind energy collection device; 306. Particle filter. DETAILED DESCRIPTION

[0021] In order to more clearly understand the above-mentioned purpose, features and advantages of the utility model, the utility model is further described below in conjunction with the accompanying drawings and embodiments. It should be noted that the embodiments of the present application and the features in the embodiments can be combined with each other without conflict.

[0022] In the following description, many specific details are set forth to facilitate a full understanding of the present invention. However, the present invention may also be implemented in other ways than those described herein. Therefore, the present invention is not limited to the specific embodiments of the following disclosure.

[0023] Embodiment 1, as Figure 1-Figure 4 As shown, the utility model provides an aircraft propulsion device, including a connection component 1, a main component 2 and an internal component 3; the connection component 1 includes a convex block 101, a support frame 102 is installed on one side of the convex block 101, a rotating motor 103 is arranged inside the support frame 102, and a rotating fan 104 is installed at the output end of the rotating motor 103; the main component 2 includes an aircraft propulsion body 201, a collector 202 is installed on the outer wall of the aircraft propulsion body 201, a valve switch 203 is arranged on the outer wall of the collector 202, and one side of the valve switch 203 is arranged A sensor 204 is arranged, a baffle 205 is arranged on one side of the aircraft propulsion body 201, two connecting parts 206 are installed on one side of the baffle 205, and two convex grooves 207 are opened on one side of the aircraft propulsion body 201; the internal component 3 includes a built-in box 301, two grooves 302 are opened on one side of the built-in box 301, an arc groove 303 is opened on one side of the built-in box 301, two fasteners 304 are arranged on one side of the built-in box 301, a wind energy collection device 305 is arranged inside the built-in box 301, and a particle filter 306 is arranged inside the built-in box 301.

[0024] The effect achieved by the entire embodiment 1 is that a support frame 102 is installed on one side of the convex block 101, a rotating motor 103 is arranged inside the support frame 102, a rotating fan 104 is installed at the output end of the rotating motor 103, a collector 202 is installed on the outer wall of the aircraft propulsion body 201, a valve switch 203 is arranged on the outer wall of the collector 202, a sensor 204 is arranged on one side of the valve switch 203, a baffle 205 is arranged on one side of the aircraft propulsion body 201, two connecting members 206 are installed on one side of the baffle 205, two convex grooves 207 are opened on one side of the aircraft propulsion body 201, and two grooves 302 are opened on one side of the built-in box 301. A circular arc groove 303 is provided on one side of the built-in box 301, two fasteners 304 are arranged on one side of the built-in box 301, a wind energy collecting device 305 is arranged inside the built-in box 301, a particle filter 306 is arranged inside the built-in box 301, a collector 202 is arranged on the outer wall of the aircraft propulsion body 201 and is connected to the internal wind energy collecting device 305, a sensor 204 is arranged on one side of the valve switch 203 to sense and identify the wind flow, collect and process the wind energy, and the wind energy collecting device 305 converts the collected wind energy into kinetic energy of the aircraft propulsion body 201 for conversion and use, so that energy is effectively converted and used to avoid waste of resources.

[0025] Embodiment 2, as Figure 1-Figure 4 As shown, the rotating motor 103 is sleeved and installed with the support frame 102, the rotating fan 104 is sleeved and installed with the convex block 101, the collector 202 is connected to the interior of the aircraft propulsion body 201, the valve switch 203 is movably connected to the collector 202, the two connecting members 206 are movably installed with the baffle 205, the two convex grooves 207 are embedded and installed with the baffle 205, the two grooves 302 are connected with the arc groove 303, the two fasteners 304 are movably installed with the built-in box 301, and the built-in box 301 is connected to the wind energy collector The device 305 is fixedly installed, the particulate filter 306 is installed in a sleeve arrangement with the built-in box 301, the built-in box 301 is installed in a sleeve arrangement with the aircraft propulsion body 201, a three-way catalytic converter is arranged on one side of the baffle 205, the three-way catalytic converter is fixedly connected to the particulate filter 306, the wind energy collection device 305 is electrically connected to the aircraft propulsion body 201, two connecting parts 206 are movably installed with the three-way catalytic converter and the wind energy collection device 305, and the collector 202 is communicated with the interior of the wind energy collection device 305.

[0026] The effects achieved by the entire embodiment 2 are as follows: the rotating motor 103 is sleeved and installed with the support frame 102, the rotating fan 104 is sleeved and installed with the convex block 101, the collector 202 is connected to the interior of the aircraft propulsion body 201, the valve switch 203 is movably connected to the collector 202, the two connecting members 206 are movably installed with the baffle 205, the two convex grooves 207 are embedded and installed with the baffle 205, the two grooves 302 are connected with the arc groove 303, the two fasteners 304 are movably installed with the built-in box 301, the built-in box 301 is fixedly installed with the wind energy collection device 305, the particle filter 306 is sleeved and installed with the built-in box 301, the built-in box 301 is sleeved and installed with the aircraft propulsion body 201, a three-way catalytic converter is arranged on one side of the baffle 205, and the three-way catalytic converter is fixedly connected with the particle filter 306, The wind energy collection device 305 is electrically connected to the aircraft propulsion body 201, and two connecting pieces 206 are movably installed with the three-way catalytic converter and the wind energy collection device 305. The collector 202 is connected to the interior of the wind energy collection device 305. The two connecting pieces 206 fix the three-way catalytic converter and the particulate filter 306 to the aircraft propulsion body 201, which is convenient for disassembly and installation, and also convenient for inspection and maintenance. Two grooves 302 and arc grooves 303 are opened on one side of the aircraft propulsion body 201 to connect, and the convex block 101 is rotatably connected to the aircraft propulsion body 201. The two fasteners 304 are fixedly connected to the two convex blocks of the convex block 101, and the rotating fan 104 can also be movably connected, and can be disassembled and assembled, which is conducive to checking the interior of the aircraft propulsion body 201.

[0027] Working principle: a support frame 102 is installed on one side of the convex block 101, a rotating motor 103 is arranged inside the support frame 102, a rotating fan 104 is installed on the output end of the rotating motor 103, a collector 202 is installed on the outer wall of the aircraft propulsion body 201, a valve switch 203 is arranged on the outer wall of the collector 202, a sensor 204 is arranged on one side of the valve switch 203, a baffle 205 is arranged on one side of the aircraft propulsion body 201, two connecting members 206 are installed on one side of the baffle 205, two convex grooves 207 are opened on one side of the aircraft propulsion body 201, two grooves 302 are opened on one side of the built-in box 301, a circular arc groove 303 is opened on one side of the built-in box 301, and two fasteners 304 are arranged on one side of the built-in box 301. A wind energy collection device 305 is arranged inside the built-in box 301, a particle filter 306 is arranged inside the built-in box 301, a collector 202 is arranged on the outer wall of the aircraft propulsion body 201 and is connected to the internal wind energy collection device 305, a sensor 204 is arranged on one side of the valve switch 203 to sense and identify the wind flow, collect and process the wind energy, and the wind energy collection device 305 converts the collected wind energy into kinetic energy of the aircraft propulsion body 201 for conversion and use, so that energy is effectively converted and used, and waste of resources is avoided. Two convex grooves 207 are opened on one side of the aircraft propulsion body 201 for placing the baffle 205 and embedding it therewith, and two connectors 206 are arranged on one side of the baffle 205 to connect with the aircraft propulsion body 2 01 is fixedly connected, a three-way catalytic converter and a particle filter 306 are arranged on one side of the baffle 205 to filter the exhaust gas to avoid excessive exhaust gas emissions causing pollution to the environment, the rotating motor 103 is sleeved and installed on the support frame 102, the rotating fan 104 is sleeved and installed on the convex block 101, the collector 202 is connected to the inside of the aircraft propulsion body 201, the valve switch 203 is movably connected to the collector 202, the two connecting pieces 206 are movably installed on the baffle 205, the two convex grooves 207 are embedded and installed on the baffle 205, the two grooves 302 are connected to the arc groove 303, the two fasteners 304 are movably installed on the built-in box 301, the built-in box 301 is fixedly installed on the wind energy collection device 305, and the particle filter 3 06 is installed in a sleeve with the built-in box 301, the built-in box 301 is installed in a sleeve with the aircraft propulsion body 201, a three-way catalytic converter is arranged on one side of the baffle 205, the three-way catalytic converter is fixedly connected with the particle filter 306, the wind energy collection device 305 is electrically connected with the aircraft propulsion body 201, two connecting pieces 206 are movably installed with the three-way catalytic converter and the wind energy collection device 305, the collector 202 is connected with the inside of the wind energy collection device 305, the two connecting pieces 206 are fixedly connected with the three-way catalytic converter and the particle filter 306 and the aircraft propulsion body 201, it is convenient to disassemble and install, and it is also convenient to check and repair, two grooves 302 are opened on one side of the aircraft propulsion body 201 and are connected with the arc groove 303,The convex block 101 is rotatably connected to the aircraft propulsion body 201, and two fasteners 304 are provided to fix the two convex blocks of the convex block 101. The rotating fan 104 can also be movably connected and can be disassembled and assembled, which is conducive to viewing the interior of the aircraft propulsion body 201.

[0028] The above description is only a preferred embodiment of the present invention and does not limit the present invention in other forms. Any technician familiar with the profession may use the technical content disclosed above to change or modify it into an equivalent embodiment with equivalent changes and apply it to other fields. However, any simple modification, equivalent change and modification made to the above embodiment based on the technical essence of the present invention without departing from the content of the technical solution of the present invention still falls within the protection scope of the technical solution of the present invention.

Claims

1. An aircraft propulsion device, characterized in that: It comprises a connection component (1), a main body component (2) and an internal component (3); The connection assembly (1) comprises a convex block (101), a support frame (102) is installed on one side of the convex block (101), a rotating motor (103) is arranged inside the support frame (102), and a rotating fan (104) is installed at the output end of the rotating motor (103); The main body component (2) comprises an aircraft propulsion body (201), a collector (202) is installed on the outer wall of the aircraft propulsion body (201), a valve switch (203) is arranged on the outer wall of the collector (202), a sensor (204) is arranged on one side of the valve switch (203), a baffle (205) is arranged on one side of the aircraft propulsion body (201), two connecting members (206) are installed on one side of the baffle (205), and two convex grooves (207) are provided on one side of the aircraft propulsion body (201); The internal component (3) comprises a built-in box (301), two grooves (302) are provided on one side of the built-in box (301), a circular arc groove (303) is provided on one side of the built-in box (301), two fasteners (304) are provided on one side of the built-in box (301), a wind energy collection device (305) is provided inside the built-in box (301), and a particle filter (306) is provided inside the built-in box (301).

2. An aircraft propulsion device according to claim 1, characterized in that: The rotating motor (103) is sleeved and installed on the support frame (102), and the rotating fan (104) is sleeved and installed on the convex block (101).

3. An aircraft propulsion device according to claim 1, characterized in that: The collector (202) is connected to the interior of the aircraft propulsion body (201), and the valve switch (203) is movably connected to the collector (202).

4. An aircraft propulsion device according to claim 1, characterized in that: The two connecting members (206) are movably mounted on the baffle plate (205), and the two convex grooves (207) are embedded in the baffle plate (205).

5. The aircraft propulsion device according to claim 1, characterized in that: The two grooves (302) are connected to the arc groove (303), the two fasteners (304) are movably mounted on the built-in box (301), the built-in box (301) and the wind energy collection device (305) are fixedly mounted, and the particle filter (306) is sleeved and mounted on the built-in box (301).

6. An aircraft propulsion device according to claim 1, characterized in that: The built-in box (301) is sleeved and installed with the aircraft propulsion body (201); a three-way catalytic converter is arranged on one side of the baffle (205); and the three-way catalytic converter is fixedly connected to the particle filter (306).

7. An aircraft propulsion device according to claim 1, characterized in that: The wind energy collection device (305) is electrically connected to the aircraft propulsion body (201), the two connecting pieces (206) are movably mounted on the three-way catalytic converter and the wind energy collection device (305), and the collector (202) is in communication with the interior of the wind energy collection device (305).

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