Launching device
By designing a launch device consisting of a pallet assembly, a track assembly, and a power assembly, the problem of ammunition launch devices limiting aircraft mission efficiency and drone cluster launches was solved, and the continuous, rapid, and automatic delivery of drones and ammunition was achieved, thereby improving delivery efficiency.
Patent Information
- Application Number
- CN202423163383.2
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-12-20
- Publication Date
- 2025-10-21
- Estimated Expiration
- 2034-12-20
AI Technical Summary
In existing technologies, ammunition launchers limit the efficiency of aircraft mission execution, making it impossible to achieve rapid launch of drone clusters and direct air delivery of supplies.
A launching device including a tray assembly, a track assembly and a power assembly is designed. The tray assembly is used to carry the launched object, the track assembly is used to guide it, and the power assembly provides power to realize the movement of the tray assembly on the track, supporting the continuous, rapid and automatic delivery of drones and ammunition.
It realizes the continuous, rapid and automatic delivery of drones and ammunition, improves delivery efficiency, supports the intensive and continuous delivery of bare bombs/bare metals, and solves the problem that materials must be delivered with outer packaging/cargo platforms.
Smart Images

Figure CN223460926U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The application belongs to the technical field of air-throwing object launching, and particularly relates to a launching device. BACKGROUND
[0002] In the field of ammunition launching, ammunition launching in the air is usually completed by means of an aircraft rack, the number of ammunition that can be carried by the rack is small, if the ammunition has a problem after the aircraft takes off, the ammunition cannot be maintained, and usually needs to be disassembled for maintenance after the aircraft returns, which affects the efficiency of the aircraft in the current task. In addition, the subsequent types of ammunition must also be adapted to the existing rack system, which restricts the development of ammunition.
[0003] In the field of unmanned aerial vehicles, unmanned aerial vehicles usually take off from the ground by themselves, if facing the scene of using unmanned aerial vehicle clusters, batch unmanned aerial vehicles need to be transported to the ground of the use scene to continue to complete the subsequent tasks, for example, in wartime, this will be difficult to achieve, so the combat mode will be limited; at the same time, it also restricts the development of unmanned aerial vehicles, which requires unmanned aerial vehicles to be ground-launched type, and gives up the possibility of air launching.
[0004] In the field of air delivery, in the scene of batch automatic delivery of unmanned aerial vehicles, ammunition, disaster relief materials, etc., the current cannot complete the direct delivery of materials without external packaging / cargo deck form, which leads to the fact that the delivered objects cannot directly enter the use mode in the air.
[0005] Therefore, it is necessary to solve the problem of delivering materials with external packaging / cargo deck to support continuous, rapid and automatic delivery of unmanned aerial vehicles, and to support ammunition / unmanned aerial vehicles to get rid of the mode of hanging a small amount of ammunition, to achieve dense and continuous delivery of bare ammunition / bare machine, and greatly improve the delivery efficiency. CONTENT OF THE INVENTION
[0006] The purpose of the present application is to provide a launching device to solve or alleviate at least one problem in the background art.
[0007] The technical solution of the present application is: a launching device, the launching device comprises a tray assembly, a track assembly and a power assembly,
[0008] The tray assembly comprises a tray for carrying the launched object, the tray has an upper interface and a lower interface, the upper interface is used for locking and releasing the launched object, and the lower interface is used for connecting with the track assembly;
[0009] The track assembly is installed on a launching platform and is used for guiding the tray assembly;
[0010] The power assembly is arranged on the launching platform and is connected with the tray assembly, and is used for providing power to the tray assembly to realize the movement of the tray assembly on the track assembly.
[0011] Preferably, the track assembly is a double-rail structure.
[0012] Preferably, the power assembly provides power to the tray assembly through multiple power forms, including electromagnetic, pneumatic, battery, hydraulic.
[0013] Preferably, it also includes a launched object rack mounted on the launch platform for transporting launched objects to the tray assembly.
[0014] Preferably, the launched object rack is in the form of a frame structure.
[0015] The launch device provided by the present application can solve the problem of having to put out materials with external packaging / pallets, can support continuous, rapid and automatic delivery of unmanned aerial vehicles, and can support ammunition / unmanned aerial vehicles to get rid of the mode of hanging a small amount of delivery and achieve dense and continuous delivery of bare ammunition / bare machines, greatly improving the delivery efficiency. BRIEF DESCRIPTION OF DRAWINGS
[0016] In order to more clearly illustrate the technical solutions provided by the present application, the following will briefly introduce the drawings. Obviously, the drawings described below are only some embodiments of the present application.
[0017] Figure 1 The present application provides a launch device structure schematic diagram. DETAILED DESCRIPTION
[0018] In order to make the purpose, technical solutions and advantages of the present application clearer, the following will describe the technical solutions in the embodiments of the present application in more detail in combination with the drawings in the embodiments of the present application.
[0019] As Figure 1 shown, the present application provides a launch device, which comprises a tray assembly 1, a track assembly 2 and a power assembly 3.
[0020] The tray assembly 1 comprises a tray 101, and the upper and lower sides of the tray 101 are respectively provided with an upper interface 102 and a lower interface 103. The tray 101 is used to carry launched objects, the upper interface 102 is used to lock and release the launched objects 4, and the lower interface 103 is used to connect the track assembly 2.
[0021] The track assembly 2 can be installed and arranged on a launch platform 6 and is used to guide the tray assembly 1. In some embodiments of the present application, the track assembly 2 is a double-rail structure and is used to provide stability when guiding the tray assembly 1. The launch platform 6 can belong to the fields of aviation, aerospace, navigation and land.
[0022] The power assembly 3 can be arranged on the tray assembly 1, the track assembly 2, the launching platform 6 or other objects. The power assembly 3 is connected to the tray assembly 1 to provide power to the tray assembly 1, so as to realize the movement of the tray assembly 1 on the track assembly 2. The power provided by the power assembly 3 to the tray assembly 1 can be in the form of electromagnetism, gas pressure, battery, hydraulic pressure, manual operation and the like; the power control form can be controllable or free.
[0023] Further, the tray assembly 1, the track assembly 2 and the power assembly 3 can be collectively or individually managed by another electronic or electrical system, or not managed by another electronic or electrical system. The tray assembly 1, the track assembly 2 and the power assembly 3 can be connected to each other in the form of electronics, electricity or other forms, or not connected to each other in the form of electronics, electricity or other forms.
[0024] The launching platform 6 is arranged on the launching platform 6, and can transport the launched object 4 to the tray assembly 1. In some embodiments of the present application, the launching platform 5 is in the form of a frame structure.
[0025] The launching device provided by the present application drives the tray assembly 2 on the track assembly 1 by using the power assembly 3, so as to launch the ammunition, unmanned aerial vehicle and other launched objects 4 on the track assembly 2 arranged on the launching platform of aviation, aerospace, navigation and land. In the field of aerial delivery, in the scenes of batch and automatic delivery of unmanned aerial vehicles, ammunition and key disaster relief materials, the current cannot complete the direct delivery of materials without external packaging / truck form, so that the launched objects cannot directly enter the use mode in the air. The launching device of the present application can solve the problem of delivery of materials with external packaging / truck, can support continuous, rapid and automatic delivery of unmanned aerial vehicles, can support ammunition / unmanned aerial vehicles to get rid of the mode of hanging a small amount of ammunition / unmanned aerial vehicles, and can realize the intensive and continuous delivery of naked ammunition / naked machine, thereby greatly improving the delivery efficiency. In addition, the launching device of the present application also has the recycling capability, that is, the tray assembly runs in the recycling direction on the track assembly.
[0026] The launching process of the launching device of the present application is as follows:
[0027] The tray assembly 1, the track assembly 2 and the power assembly 3 are installed on the floor of the cargo compartment of the transport aircraft, the starting end of the track assembly 2 is towards the head of the aircraft, the ending end is towards the tail of the aircraft, and the door of the cargo compartment of the transport aircraft is opened. The UAV is placed on the tray assembly 1, and the upper interface 102 of the tray assembly 1 is used to lock the UAV. The tray assembly 1 is transported along the track assembly 2 to the ending end of the track assembly 2 by using the power assembly 3, and the power assembly 3 can make the tray assembly 1 and the UAV obtain the required initial speed when reaching the ending end of the track assembly 2. At this time, the upper interface 102 of the tray assembly 1 releases the UAV, and then the UAV can pass through the door hole of the cargo compartment of the transport aircraft and leave the transport aircraft. After that, the UAV continues to complete the subsequent task. In this embodiment, the way of placing the UAV on the tray assembly 1 can be manual or automatic; wherein the automatic mode can place the UAV on the tray assembly 1 in batches and in sequence by means of other mechanisms, that is, the UAV can be launched in batches.
[0028] The launching device of the present application is used as a recovery device, and the process is as follows:
[0029] The tray assembly 1, the track assembly 2 and the power assembly 3 are installed on the floor of the cargo compartment of the transport aircraft, the starting end of the track assembly 2 is towards the head of the aircraft, the ending end is towards the tail of the aircraft, and the door of the cargo compartment of the transport aircraft is opened. The UAV is placed on the tray assembly 1 of the launching device after being recovered from the air near the door of the cargo compartment of the transport aircraft by means of other mechanisms, and the upper interface 102 of the tray assembly 1 is used to lock the UAV. The tray assembly 1 and the UAV are transported along the track assembly from the ending end of the track assembly to the launching end of the track assembly 2 by using the power assembly 3, the upper interface 102 of the tray assembly 1 releases the UAV, and then the UAV is taken off by means of other mechanisms or manually, so as to realize the recovery of the UAV.
[0030] The above is only a specific embodiment of the present application, but the protection scope of the present application is not limited thereto, any changes or replacements that can be easily thought of by those skilled in the art within the technical range disclosed in the present application should be covered in the protection scope of the present application. Therefore, the protection scope of the present application should be subject to the protection scope of the claims.
Claims
1. A transmitting device, characterized by The launching device comprises a tray assembly, a track assembly and a power assembly, The tray assembly comprises a tray for carrying the launched object, the tray having an upper interface for locking and releasing the launched object and a lower interface for connecting with the track assembly; The track assembly is installed on a launching platform for guiding the tray assembly; The power assembly is installed on the launching platform and connected with the tray assembly for providing power to the tray assembly to realize the movement of the tray assembly on the track assembly.
2. The transmitting apparatus of claim 1, wherein, The track assembly is a double-rail structure.
3. The transmitting apparatus of claim 1, wherein, The power assembly provides power to the tray assembly through various power forms, including electromagnetic, air pressure, battery and hydraulic pressure.
4. The transmitting apparatus of claim 1, wherein, A launched object rack is further included, which is installed on the launching platform for transporting the launched object to the tray assembly.
5. The transmitting apparatus of claim 4, wherein, The launched object rack is in the form of a frame structure.