Launching device and unmanned aerial vehicle cluster launcher
The launch device, which generates high-temperature and high-pressure gas through chemical reactions, solves the problems of complex structure and poor portability of existing folding UAV launch devices, and realizes efficient and portable continuous launch capabilities.
Patent Information
- Application Number
- CN202422953808.3
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-12-02
- Publication Date
- 2025-10-21
- Estimated Expiration
- 2034-12-02
AI Technical Summary
Existing folding drone launch devices have complex structures, large sizes, heavy weights, and cumbersome operations. They cannot achieve rapid and continuous launches, and their reliance on air pumps and air tanks limits their portability and efficiency.
Chemical reactions are used instead of air pumps and gas tanks to generate high-temperature and high-pressure gas. The chemical raw materials in the launching assembly react quickly after receiving energy, releasing high-temperature and high-pressure gas for launching, which simplifies the structure of the launching mechanism.
It improves launch efficiency and portability, enables rapid and continuous launch, reduces dependence on large air pumps and gas tanks, and adapts to complex and high-frequency launch requirements.
Smart Images
Figure CN223460924U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The present application relates to the field of unmanned aerial vehicle launching, in particular to a launching device and an unmanned aerial vehicle cluster launcher. BACKGROUND
[0002] With the continuous development of unmanned aerial vehicle technology, folding unmanned aerial vehicles are widely used in reconnaissance, monitoring and emergency rescue fields due to their compact structure, portability and rapid deployment. The foldable design enables the device to greatly reduce the volume in the non-working state, thereby facilitating single soldier carrying and rapid deployment in complex scenarios. In many task scenarios, the efficiency and portability of launching the folding unmanned aerial vehicle directly affect the success rate of executing the task, and therefore higher requirements are put forward for the performance of the launching device.
[0003] The current launching device of the folding unmanned aerial vehicle mainly adopts a compressed gas launching scheme, and its basic components include a launching barrel, a gas pump, a gas storage tank and an electric control valve. In use, the gas storage tank is pressurized by the gas pump, the unmanned aerial vehicle and the launching piston are loaded into the launching barrel when the gas pressure reaches the launching requirement, and the high-pressure gas is released to push the unmanned aerial vehicle to launch through the electromagnetic valve.
[0004] However, the current folding unmanned aerial vehicle launching device still has certain limitations. First, the launching device has a complex structure, multiple components are connected to each other, occupies a large volume and weight, and reduces portability; in addition, the operation steps are complicated, which is not conducive to rapid deployment. Second, a single set of launching device cannot realize rapid and continuous launching, and the gas storage tank needs to be pressurized by the gas pump after each launching, and the efficiency is limited by the power of the gas pump. Even if the power of the gas pump is improved to shorten the pressurization time, the weight and volume of the device will also increase, further affecting the mobility. CONTENT OF THE INVENTION
[0005] In view of the above problems, the purpose of the embodiments of the present application is to provide a launching device and an unmanned aerial vehicle cluster launcher, which generates high-temperature and high-pressure gas through chemical reaction instead of gas pump and gas storage tank, greatly simplifying the structure of the launching mechanism. The chemical reaction in the launching assembly can quickly release energy to realize instantaneous generation of gas, thereby improving the launching efficiency and better meeting the demand for continuous launching.
[0006] In a first aspect, the embodiments of the present application provide a launching device, which comprises a launching assembly and a launching shell with a launching control board; the launching control board is arranged at a first end of the launching shell to form a launching cavity; a second side of the launching control board is connected with an energy source, and a first side of the launching control board is configured to receive the launching assembly; the launching control board is configured to transmit launching energy generated by the energy source to the launching control board, and the launching assembly is configured to release high-temperature and high-pressure gas to fill the launching cavity under the condition of receiving the launching energy.
[0007] In the implementation process, the launching device provided by the embodiment of the present application comprises a launching shell and a launching assembly, wherein the launching assembly is added once for single launching of consumables. Compared with the traditional compressed gas launching device, the launching device provided by the embodiment of the present application generates high-temperature and high-pressure gas through chemical reaction instead of a gas pump and a gas tank, greatly simplifying the structure of the launching mechanism. The chemical reaction in the launching assembly can quickly release energy to achieve instantaneous generation of gas, thereby improving the launching efficiency and better meeting the demand for continuous launching. Therefore, the launching device provided by the embodiment of the present application has significant advantages in portability, launching efficiency and simplified structure.
[0008] Optionally, in the embodiment of the present application, the launching assembly comprises chemical raw materials, a consumable accommodating part and a trigger signal linker; the consumable accommodating part is connected with the trigger signal linker and is configured to accommodate the chemical raw materials for generating high-temperature and high-pressure gas; and the trigger signal linker is connected with the launching control board and is configured to transmit launching energy to the consumable accommodating part.
[0009] In the implementation process, compared with the traditional compressed gas launching device, the launching assembly provided by the embodiment of the present application has higher energy conversion efficiency, more concise structure design and higher portability, can adapt to more complex and high-frequency launching requirements, reduces the dependence on large gas pumps and gas tanks, and has higher portability; in addition, by replacing the traditional compressed gas with chemical reaction, a large amount of high-temperature and high-pressure gas can be generated in a short time, greatly improving the efficiency and response speed of launching.
[0010] Optionally, in the embodiment of the present application, the trigger signal linker comprises a positive electrode contact, a negative electrode contact, a positive electrode resistance wire and a negative electrode resistance wire; the positive electrode contact is connected with the positive electrode resistance wire, and the negative electrode contact is connected with the negative electrode resistance wire; the positive electrode resistance wire and the negative electrode resistance wire are connected with the consumable accommodating part and are configured to generate Joule heat when receiving launching energy; wherein the Joule heat is configured to ignite the chemical raw materials to occur chemical reaction.
[0011] In the implementation process, the Joule heat of the launching device provided by the embodiment of the present application is quickly generated by the resistance wire, directly ignites the chemical raw materials to occur reaction, eliminates the dependence on external complex gas pump systems, and significantly simplifies the structure of the launching device. The external connection seat and the internal connection seat of the launching control board not only improve the reliability of energy transmission, but also enhance the modularization characteristics of the device, facilitating maintenance and expansion.
[0012] Optionally, in the embodiment of the present application, the emission control board comprises an external connecting seat, and an internal connecting seat with a positive electrode connecting hole and a negative electrode connecting hole; the positive electrode connecting hole of the internal connecting seat is configured to pass through the positive electrode contact, and the negative electrode connecting hole of the internal connecting seat is configured to pass through the negative electrode contact; the positive electrode contact extends to the external connecting seat through the positive electrode connecting hole, and the negative electrode contact extends to the external connecting seat through the negative electrode connecting hole.
[0013] Optionally, in the embodiment of the present application, the trigger signal linker further comprises a receiving groove; the receiving groove is configured to accommodate the positive electrode contact and the negative electrode contact, and to receive the internal connecting seat.
[0014] In the above implementation process, the trigger signal linker of the emission device provided by the embodiment of the present application not only ensures the accurate docking of the positive and negative electrode contacts with the internal connecting seat, but also improves the working reliability and safety of the overall device through the physical support and protection structure.
[0015] Optionally, in the embodiment of the present application, the emission shell further comprises an emission barrel body, and a first end of the emission barrel body is welded to the emission control board.
[0016] Optionally, in the embodiment of the present application, the emission barrel body comprises an emission handle; the emission handle is arranged along the length direction of the emission barrel body.
[0017] Optionally, in the embodiment of the present application, a second end of the emission barrel body comprises an opening; the opening is configured to receive the emission assembly and the target emission object.
[0018] Optionally, in the embodiment of the present application, the target emission object comprises a UAV.
[0019] In the above implementation process, the emission barrel body of the embodiment of the present application is tightly connected to the emission control board through welding, which greatly enhances the structural strength and impact resistance. The design of the second end opening ensures the convenience and position accuracy of loading the emission assembly and the target emission object, and the emission handle arranged along the barrel body direction significantly improves the operation stability and portability of the device. The overall design ensures that the emission device can still operate stably in complex application scenarios such as high vibration and strong impact, thereby meeting the emission requirements in various environments.
[0020] In a second aspect, the present application provides a UAV cluster launcher, comprising an emission frame and a plurality of emission devices provided by the first aspect of the present application; the emission devices are arranged on the emission frame.
[0021] The emission device and the UAV cluster launcher provided by the embodiment of the present application have compact overall device structure and high stability, can quickly and reliably complete the emission task of the folded UAV in a complex environment, and have excellent adaptability and practical value.
[0022] In order to make the above objectives, characteristics and advantages of the present application more apparent, clear and easy to understand, the following specific examples are described in detail below, together with the accompanying drawings. BRIEF DESCRIPTION OF DRAWINGS
[0023] In order to more clearly illustrate the technical solutions of the embodiments of the present application, the following will briefly introduce the drawings needed to be used in the embodiments of the present application. It should be understood that the following drawings only show some embodiments of the present application, and therefore should not be regarded as a limitation on the scope. For those skilled in the art, other related drawings can also be obtained without creative labor on the basis of these drawings.
[0024] Figure 1 The first schematic diagram of the structure of the transmitting device provided by the embodiments of the present application;
[0025] Figure 2 The schematic diagram of the structure of the transmitting assembly provided by the embodiments of the present application;
[0026] Figure 3 The schematic diagram of the transmitting control board provided by the embodiments of the present application;
[0027] Figure 4 The second schematic diagram of the structure of the transmitting device provided by the embodiments of the present application;
[0028] Reference signs: transmitting device-1000; transmitting assembly-100; chemical raw material-110; consumable containing part-120; trigger signal linker-130; positive electrode contact-131; negative electrode contact-132; receiving groove-H; transmitting shell-200; transmitting tube body-220; transmitting handle-221; transmitting control board-210; external connecting seat-211; internal connecting seat-212; positive electrode connecting hole-2121; negative electrode connecting hole-2122; first end of the transmitting shell-A; second end of the transmitting shell-B; first side of the transmitting control board-a; second side of the transmitting control board-b. DETAILED DESCRIPTION
[0029] In order to make the above objectives, characteristics and advantages of the present application more apparent, clear and easy to understand, the following specific examples are described in detail below, together with the accompanying drawings.
[0030] Therefore, the following detailed description of the embodiments of the application provided in the drawings is not intended to limit the scope of the application claimed, but merely represents selected embodiments of the application. Based on the embodiments in the application, all other embodiments obtained by those of ordinary skill in the art without creative labor fall within the scope of the application.
[0031] It should be noted that: similar reference numbers and letters represent similar items in the following drawings, therefore, once an item is defined in one drawing, it does not need to be further defined and explained in subsequent drawings.
[0032] In the description of the application, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer" and the like indicate the orientation or positional relationship based on the orientation or positional relationship shown in the drawings, or the orientation or positional relationship commonly placed when the product of the application is used, and are only for the convenience of describing the application and simplifying the description, and therefore cannot be understood as indicating or implying that the device or element must have a particular orientation, be constructed and operated in a particular orientation, and therefore cannot be understood as limiting the application. In addition, the terms "first", "second", "third" and the like are only used to distinguish the description and cannot be understood as indicating or implying relative importance.
[0033] In addition, the terms "horizontal", "vertical" and the like do not mean that the components must be absolutely horizontal or hanging, but can be slightly inclined. For example, "horizontal" only means that its direction is more horizontal relative to "vertical", and does not mean that the structure must be completely horizontal, but can be slightly inclined.
[0034] In the description of the application, it should also be noted that unless otherwise explicitly specified and limited, the terms "provided", "mounted", "connected", "connected" should be broadly understood, for example, it can be fixedly connected, or it can be detachably connected, or integrally connected; it can be mechanically connected, or it can be electrically connected; it can be directly connected, or it can be indirectly connected through an intermediate medium, or it can be the communication between two elements. For those of ordinary skill in the art, the specific meaning of the above terms in the application can be understood according to the specific circumstances.
[0035] Applicant found in the process of research that at present, the folding unmanned aerial vehicle launching device generally adopts a compressed gas launching scheme, the core structure of which is composed of multiple key components, including a launching barrel, a gas pump, a gas storage tank and an electric control valve. In specific application, first, the gas storage tank is pressurized by the gas pump, so that the gas in the gas storage tank reaches a preset high pressure standard. When the pressure condition meets the launching requirement, the folding unmanned aerial vehicle and the matching launching piston are loaded into the launching barrel. When starting launching, the high-pressure gas in the gas storage tank is released by rapidly opening the control electromagnetic valve, the launching piston is pushed to drive the unmanned aerial vehicle to slide out of the launching barrel at high speed, and the launching function is realized.
[0036] Although the compressed gas launching device has been applied in some fields, its structure design and working mode still have significant limitations, which restrict the actual use effect. First of all, the volume and weight of the device are particularly prominent. The gas pump and the gas storage tank are core components and complement each other. In order to ensure sufficient gas pressure during launching, the volume of the gas storage tank and the power of the gas pump usually need to reach a high standard, which inevitably increases the volume and weight of the system, greatly reducing the portability of the equipment. In addition, the pipeline connection between multiple components is complex and depends on precise sealing, which not only increases the manufacturing cost, but also increases the maintenance difficulty of the device.
[0037] Secondly, the launching device performs poorly in the high-frequency continuous launching scene. The gas pump needs to re-pressurize the gas storage tank after each launch, and the length of this process mainly depends on the power of the gas pump. Even if a high-power gas pump is used to shorten the pressurization time and improve the launching efficiency, the volume and weight of the equipment will still be further increased, which contradicts the demand for portability. More importantly, the instantaneous power output of the high-pressure gas launching mode itself is difficult to adjust, which may not be adaptable when facing different launching distances or environmental requirements. The superposition of the above problems makes it difficult for the compressed gas launching device to meet the needs of rapid response, multiple launches and portable operation in complex task scenarios.
[0038] In summary, the existing compressed gas launching device is still difficult to balance reliability, portability and high efficiency.
[0039] Based on this, the embodiments of the present application provide a launching device and an unmanned aerial vehicle cluster launcher, the launching device is provided with a launching shell and a launching assembly, wherein the launching assembly is a consumable, single filling and single launching; based on a special structure design, the launching assembly can be quickly replaced after each launch to continue launching, the launching assembly provided by the embodiments of the present application not only has extremely high portability, but also has extremely high launching efficiency.
[0040] Please refer to Figure 1 , Figure 1A first schematic diagram of the structure of the transmitting device 1000 provided by the embodiments of the present application; the embodiments of the present application provide a transmitting device 1000, which comprises a transmitting assembly 100, and a transmitting shell 200 with a transmitting control board 210.
[0041] As shown in Figure 1 , the transmitting control board 210 is arranged at the first end A of the transmitting shell, constituting a transmitting cavity.
[0042] The second side b of the transmitting control board is connected with an energy source, and the first side a of the transmitting control board is configured to receive the transmitting assembly 100. The energy source can be a portable power source, which has a small volume and a light weight, and is helpful to improve the overall portability; optionally, a switch can be arranged at the second end of the energy source and the transmitting control board 210, and when the switch is closed, the energy source transmits the transmission energy to the transmitting control board 210.
[0043] The transmitting control board 210 is configured to transmit the transmission energy generated by the energy source to the transmitting control board 210, and the transmitting assembly 100 is configured to release high-temperature and high-pressure gas to fill the transmitting cavity in the case of receiving the transmission energy.
[0044] During launching, the transmitting assembly 100 and the target launching object (for example, a drone / foldable drone) are sent into the transmitting cavity from the opening of the second end of the transmitting shell 200 in turn. The transmitting assembly 100 can be in contact with the second end of the transmitting control board 210, and after the contact, the transmission energy can be transmitted from the energy source to the transmitting assembly 100. After the transmitting assembly 100 receives the transmission energy, the temperature rises rapidly, thereby igniting the chemical substances in the transmitting assembly 100 to cause a violent chemical reaction, thereby releasing a large amount of high-temperature and high-pressure gas. The high-temperature and high-pressure gas will fill the inside of the transmitting shell 200 instantly, and the inside and the outside of the transmitting shell 200 have a large pressure difference, forcing the drone to accelerate and be launched out of the transmitting shell 200.
[0045] It should be noted that the chemical substances capable of chemical reaction in the transmitting assembly 100 described above generally include sodium azide.
[0046] By Figure 1It can be known that the launching device 1000 provided in the embodiment of the present application comprises a launching shell 200 and a launching assembly 100, wherein the launching assembly 100 is single-time added for single-time launching of consumables. Compared with the traditional compressed gas launching device 1000, the launching device 1000 provided in the embodiment of the present application generates high-temperature and high-pressure gas through chemical reaction instead of gas pump and gas storage tank, greatly simplifying the structure of the launching mechanism. The chemical reaction in the launching assembly 100 can quickly release energy, realize instantaneous generation of gas, thereby improving the launching efficiency and better meeting the demand of continuous launching. Therefore, the launching device 1000 provided in the embodiment of the present application has significant advantages in portability, launching efficiency and simplified structure.
[0047] Please refer to Figure 2 , Figure 2 The structure schematic diagram of the launching assembly 100 provided in the embodiment of the present application; the launching assembly 100 provided in the embodiment of the present application comprises chemical raw materials 110, a consumable accommodating part 120 and a trigger signal linker 130.
[0048] The consumable accommodating part 120 is connected with the trigger signal linker 130 and is configured to accommodate the chemical raw materials 110 generating high-temperature and high-pressure gas. The trigger signal linker 130 is connected with the launching control board 210 and is configured to transmit launching energy to the consumable accommodating part 120.
[0049] The chemical raw materials 110, for example, sodium azide, will have a violent chemical reaction when heated or triggered, release a lot of heat and gas, and can quickly fill the launching cavity.
[0050] The trigger signal linker 130 is a control component of the launching assembly 100, which is connected with the launching control board 210 and is responsible for receiving the launching energy transmitted by the launching control board 210. When the energy source transmits energy through the launching control board 210, the trigger signal linker 130 transmits these energies to the consumable accommodating part 120 to activate the chemical raw materials 110 to react. The trigger signal linker 130 can be understood as a switch or a transmission channel, which releases high-temperature and high-pressure gas after the chemical reaction is started.
[0051] In the above implementation process, when the launching device 1000 is ready, the launching assembly 100 is in contact with the launching control board 210, and the launching control board 210 transmits the required launching energy to the consumable accommodating part 120 through the trigger signal linker 130. At this time, the chemical raw materials 110 have a violent chemical reaction after receiving the energy, for example, sodium azide rapidly decomposes under the action of heat, releasing a large amount of gas and heat. The generated high-temperature and high-pressure gas will quickly fill the launching cavity, and the pressure inside the launching cavity will quickly rise, forcing the target object to be launched at high speed from the opening of the launching shell 200.
[0052] ThroughFigure 2 It can be known that, compared with the conventional compressed gas launching device 1000, the launching device 1000 provided by the embodiment of the application has higher energy conversion efficiency, more concise structure design and stronger portability, can adapt to more complex and high-frequency launching requirements, reduces the dependence on large air pumps and gas storage tanks, and has higher portability; in addition, the chemical reaction is used to replace the conventional compressed gas, a large amount of high-temperature and high-pressure gas can be generated in a short time, and the efficiency and response speed of launching are greatly improved.
[0053] Please continue to see Figure 2 The trigger signal linker 130 includes a positive electrode contact 131, a negative electrode contact 132, a positive electrode resistance wire (not shown in the figure) and a negative electrode resistance wire (not shown in the figure).
[0054] The positive electrode contact 131 is connected with the positive electrode resistance wire, and the negative electrode contact 132 is connected with the negative electrode resistance wire. The positive electrode resistance wire and the negative electrode resistance wire are connected with the consumable accommodating part 120, and are configured to generate Joule heat in the case of receiving launching energy; wherein the Joule heat is configured to ignite the chemical raw material 110 to occur chemical reaction.
[0055] Please see Figure 3 , Figure 3 The schematic diagram of the launching control board provided by the embodiment of the application; the launching control board 210 includes an external connecting seat 211 and an internal connecting seat 212 with a positive electrode connecting hole 2121 and a negative electrode connecting hole 2122. The positive electrode connecting hole 2121 of the internal connecting seat 212 is configured to pass through the positive electrode contact 131, and the negative electrode connecting hole 2122 of the internal connecting seat 212 is configured to pass through the negative electrode contact 132. The positive electrode contact 131 extends to the external connecting seat 211 through the positive electrode connecting hole 2121, and the negative electrode contact 132 extends to the external connecting seat 211 through the negative electrode connecting hole 2122.
[0056] When the launching device 1000 works, the energy source transmits electric energy to the trigger signal linker 130 through the launching control board 210. After the current passes through the positive electrode contact 131 and the negative electrode contact 132, it is transmitted to the positive electrode resistance wire and the negative electrode resistance wire in turn. The resistance wire generates Joule heat due to the current passing through, and transmits heat to the chemical raw material 110 in the consumable accommodating part 120. At a high enough temperature, the chemical raw material 110 is ignited, and a violent chemical reaction occurs, releasing high-temperature and high-pressure gas. These gases will quickly fill the launching chamber, and under the action of pressure difference, the unmanned aerial vehicle is launched at high speed.
[0057] Therefore, the Joule heat of the launching device 1000 provided by the embodiment of the present application is generated quickly by the resistance wire, directly ignites the chemical raw material 110 to occur reaction, eliminates the dependence on the external complex air pump system, and significantly simplifies the structure of the launching device 1000. The external connecting seat 211 and the internal connecting seat 212 of the launching control board 210 are designed to not only improve the reliability of energy transmission, but also enhance the modularization characteristics of the device, facilitating maintenance and expansion.
[0058] Please continue to see Figure 2 and Figure 3 The trigger signal linker 130 also includes a receiving groove H. The receiving groove H is configured to accommodate the positive contact 131 and the negative contact 132, and to receive the internal connecting seat 212.
[0059] The receiving groove H can accommodate the internal connecting seat 212, fix it in the trigger signal linker 130, and form a nested section structure; thereby ensuring the precise docking of the internal connecting seat 212 with the positive and negative contacts 132, and simplifying the assembly process between the trigger signal linker 130 and the launching control board 210.
[0060] Therefore, the trigger signal linker 130 of the launching device 1000 provided by the embodiment of the present application not only ensures the precise docking of the positive and negative contacts 132 with the internal connecting seat 212, but also improves the working reliability and safety of the overall device through the physical support and protection structure.
[0061] Please see Figure 4 , Figure 4 The second schematic diagram of the structure of the launching device provided by the embodiment of the present application; as shown in Figure 4 The launching shell 200 also includes a launching barrel 220, and the first end of the launching barrel (i.e. the first end A of the launching shell) is welded with the launching control board 210. Therefore, it can withstand a larger impact force and ensure the stability of the structure.
[0062] Please continue to see Figure 4 The launching barrel 220 of the launching device 1000 provided by the embodiment of the present application includes a launching handle 221, which is arranged along the length direction of the launching barrel 220.
[0063] The second end (the second end B of the launching shell) of the launching barrel includes an opening, which is configured to receive the launching assembly 100 and the target launching object.
[0064] Therefore, the launching tube body 220 is tightly connected with the launching control panel 210 by welding, so that the structural strength and impact resistance are greatly enhanced. The design of the second end opening ensures the convenience and position accuracy of loading the launching assembly 100 and the target launching object, and the launching handle 221 arranged along the tube body direction significantly improves the operation stability and portability of the device. The overall design ensures that the launching device 1000 can still operate stably in complex application scenarios such as high vibration and strong impact, thereby meeting the launching requirements in various environments.
[0065] The application provides a UAV cluster launcher, which comprises a launching rack and a plurality of the launching devices.
[0066] In summary, the launching device provided by the application embodiment is provided with a launching shell and a launching assembly, wherein the launching assembly is consumable, and single filling is used for single launching; based on the special structural design, the launching assembly can be quickly replaced after each launching is completed to continue launching, and the launching assembly provided by the application embodiment is not only highly portable, but also has high launching efficiency.
[0067] The above is only an embodiment of the application and is not used to limit the protection scope of the application. For those skilled in the art, the application can have various modifications and changes. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the application shall be included in the protection scope of the application.
Claims
1. A transmitting device, characterized by The launching device includes: a launching assembly, and a launching shell having a launching control board; The launch control board is arranged at the first end of the launch shell to form a launch cavity; The second side of the launch control board is connected to the energy source, and the first side of the launch control board is configured to receive the launch assembly; The launch control board is configured to transmit the launch energy generated by the energy source to the launch control board, and the launch component is configured to release high-temperature and high-pressure gas to fill the launch cavity when receiving the launch energy.
2. The transmitting apparatus of claim 1, wherein The launch assembly includes chemical raw materials, consumable material receiving parts and a trigger signal linker; The consumable material receiving portion is connected to the trigger signal linker and is configured to receive chemical raw materials for generating the high-temperature and high-pressure gas; The trigger signal linker is connected to the emission control board and is configured to transmit the emission energy to the consumable material receiving portion.
3. The launch device of claim 2, wherein, The trigger signal linker includes a positive contact, a negative contact, a positive resistance wire and a negative resistance wire; The positive contact is connected to the positive resistance wire, and the negative contact is connected to the negative resistance wire; The positive resistance wire and the negative resistance wire are connected to the consumable material storage portion and are configured to generate Joule heat when receiving the emission energy; wherein the Joule heat is configured to ignite the chemical raw material to generate a chemical reaction.
4. The transmitting apparatus of claim 3, wherein The emission control board includes an external connection seat and an internal connection seat having a positive electrode connection hole and a negative electrode connection hole; The positive electrode connection hole of the internal connection base is configured to pass through the positive electrode contact, and the negative electrode connection hole of the internal connection base is configured to pass through the negative electrode contact; The positive contact extends to the external connection seat through the positive connection hole, and the negative contact extends to the external connection seat through the negative connection hole.
5. The transmitting apparatus of claim 4, wherein, The trigger signal linker also includes a receiving slot; The receiving slot is configured to accommodate the positive contact and the negative contact, and receive the internal connection base.
6. The transmitting apparatus of claim 1, wherein The launch shell further includes a launch tube body, and a first end of the launch tube body is welded to the launch control board.
7. The transmitting apparatus of claim 6, wherein, The launch tube body includes a launch handle; the launch handle is arranged along the length direction of the launch tube body.
8. The transmitting apparatus of claim 6, wherein, The second end of the launch tube body includes an opening; the opening is configured to receive the launch assembly and the target launch object.
9. The launch device of claim 1, wherein, in, The target launch object of the launch device includes a drone.
10. A drone swarm launcher, comprising: It comprises a launching rack and a plurality of launching devices as described in any one of claims 1 to 9; the launching devices are arranged on the launching rack.