Fast-assembly structure and launching system of launcher and unmanned aerial vehicle

Abstract

The utility model relates to a launcher and unmanned aerial vehicle quick-assembly structure and launching system, which comprises a quick-assembly component for connecting the unmanned aerial vehicle and the launcher, the quick-assembly component comprises a first connecting piece and a second connecting piece, and the first connecting piece and the second connecting piece are respectively provided with a first joint and a second joint. When the first connecting piece and the second connecting piece are mounted in place, the first joint is communicated with the second joint; the first connector is connected with a quick plug which is used for being connected with an unmanned aerial vehicle. According to the utility model, the unmanned aerial vehicle and the transmitter are quickly connected through the quick assembly component, so that the efficiency of the unmanned aerial vehicle and the transmitter in the disassembly and assembly process is improved.

Description

TECHNICAL FIELD

[0001] The utility model relates to unmanned plane equipment technical field, concretely relates to a quick -wearing structure of launcher and unmanned plane and launch system. BACKGROUND

[0002] Unmanned plane has been widely used in military and civilian fields. In the military field, unmanned plane can realize electronic reconnaissance, radar detection, electronic countermeasure, unmanned combat and other functions. When a fire breaks out in a high-rise building, the fire fighting water gun attacks from outside, often blocked by glass curtain wall, fire extinguishing agent cannot be punched into the high-rise building, and the fire ladder and the high ladder cannot approach the curtain wall glass of the dangerous area to break. With the development of science and technology, unmanned plane is widely used in fire fighting and rescue, and the unmanned plane is mounted with a glass breaking launcher, which can break the glass of the high-rise curtain wall.

[0003] Because the number of glass breaking bullets in the launcher is limited, the new launcher needs to be quickly replaced and put into use immediately after launching, and the unmanned plane needs to be quickly assembled when in use. However, the existing launcher is usually installed on the unmanned plane by threaded butt joint, and the unmanned plane and the launcher also need to be controlled and powered by a conductive part. After the unmanned plane and the launcher are installed, wiring is needed again, which has the technical problem of low installation efficiency. UTILITY MODEL CONTENTS

[0004] The utility model discloses a quick -wearing structure of launcher and unmanned plane, can set up quick -wearing structure at the connecting position of unmanned plane and launcher, so that the efficiency of the launcher installed on the unmanned plane is higher, and the main idea is that:

[0005] A quick -wearing structure of launcher and unmanned plane, including quick -wearing subassembly for connecting unmanned plane and launcher, the quick -wearing subassembly includes first connecting piece and second connecting piece, first connecting piece and second connecting piece are provided with first joint and second joint respectively, when first connecting piece and second connecting piece are installed in place, first joint and second joint are communicated;The first joint connects the quick -wearing plug, and the quick -wearing plug is used for connecting the unmanned plane. The utility model discloses that the unmanned plane and the launcher are connected quickly by the quick -wearing subassembly, and the installation efficiency is higher due to the setting of the sliding assembly. The first joint and the second joint for realizing electrical connection between the unmanned plane and the launcher are respectively arranged on the first connecting piece and the second connecting piece, and the first joint and the second joint are communicated after abutting by contact after the first connecting piece and the second connecting piece are installed in place. The electrical connection efficiency between the unmanned plane and the launcher is further improved on the basis of improving the installation efficiency.

[0006] Preferably, the first connecting piece is provided with a sliding cavity accommodating the second connecting piece, one side of the sliding cavity is provided with a guide opening for passing through the second connecting piece, and the opposite side of the guide opening is provided with a closed limiting portion.

[0007] Preferably, the second connecting piece comprises a positioning portion, and when the second connecting piece is installed in place in the sliding cavity of the first connecting piece, the positioning portion is in contact with the limiting portion of the first connecting piece.

[0008] The second aspect of the utility model aims at solving the technical problem of poor power connection efficiency between the unmanned aerial vehicle and the launcher.

[0009] Preferably, the first connecting piece is provided with a sliding cavity accommodating the second connecting piece, one side of the sliding cavity is provided with a guide opening for passing through the second connecting piece, and the opposite side of the guide opening is provided with a closed limiting portion.

[0010] Preferably, the second connecting piece comprises an installation cavity, the installation cavity is provided with a control module, the control module is used for connecting the launcher through a wire, a hollow portion for passing through the wire is formed in the bottom of the installation cavity, and a second connecting portion is arranged at the bottom of the second connecting piece.

[0011] Preferably, the second connecting portion comprises a supporting hook, and the supporting hook is provided with an elastic pad.

[0012] Preferably, the quick-mounting assembly further comprises a fastener, the fastener being used to lock the first connecting member and the second connecting member.

[0013] Preferably, a launching system comprises a launcher and a quick-mounting structure of a UAV, the launching system further comprising the UAV and the launcher, the UAV being connected to the first connecting member and the launcher being connected to the second connecting member.

[0014] Preferably, the launcher comprises a mounting portion, the mounting portion being provided with a mounting opening, the second connecting member extending into the mounting portion through the mounting opening, the mounting opening having a width smaller than that of the second connecting portion, the mounting opening being used to restrict the movement of the support hook in the direction away from the mounting portion, and the support hook being in abutting engagement with the mounting portion.

[0015] The present application has the advantages that the UAV and the launcher are quickly connected through the quick-mounting assembly, and the efficiency of disassembly and assembly of the UAV and the launcher is improved. BRIEF DESCRIPTION OF DRAWINGS

[0016] Figure 1 FIG. 1 is a structural schematic view of the present application.

[0017] Figure 2 FIG. 2 is a structural cross section of the present application. Figure 1 .

[0018] Figure 3 FIG. 3 is a structural cross section of the present application. Figure 2 .

[0019] Figure 4 FIG. 4 is a structural schematic view of the first connecting member of the present application.

[0020] Figure 5 FIG. 5 is a structural side view of the first connecting member of the present application.

[0021] Figure 6 FIG. 6 is a structural schematic view of the second connecting member of the present application.

[0022] Figure 7 FIG. 7 is a structural side view of the second connecting member of the present application.

[0023] Figure 8 FIG. 8 is a structural mounting view of the launcher of the present application.

[0024] Figure 9 FIG. 9 is a structural schematic view of the fastener of the present application.

[0025] The reference signs include 1, first connecting piece; 11, guide opening; 12, sliding cavity; 13, first connecting part; 14, limiting part; 15, first mounting hole; 2, second connecting piece; 21, mounting cavity; 22, second connecting part; 221, elastic pad; 222, supporting hook; 23, positioning part; 24, second mounting hole; 3, first connector; 31, quick connector; 4, second connector; 41, control module; 5, fastener; 51, rotating part; 511, guide channel; 512, limiting hole; 52, pushing part; 521, bolt; 522, pull rod; 523, compression spring; 524, pulling head; 6, mounting part. DETAILED DESCRIPTION

[0026] In order to make the purpose, technical scheme and advantages of the embodiments clearer, the utility model will be further described in detail below in combination with the drawings and embodiments. When the following description relates to the drawings, the same numbers in different drawings represent the same or similar elements unless otherwise indicated. The implementation manners described in the following exemplary embodiments do not represent all the implementation manners consistent with the present disclosure. Instead, they are merely examples of devices and methods consistent with some aspects of the present disclosure as detailed in the appended claims.

[0027] It should be noted that all actions of acquiring signals, information or data in the present application are carried out in compliance with the corresponding data protection regulations and policies of the country where the device is located, and with the authorization given by the owner of the corresponding device.

[0028] In the present disclosure, the orientation words such as "inner" and "outer" are defined according to the contour of the corresponding parts themselves unless otherwise stated. The terms such as "first" and "second" used in the present disclosure are used to distinguish one element from another element, and do not have sequentiality and importance.

[0029] Embodiment 1

[0030] As shown in the accompanying drawings, the utility model discloses a quick mounting assembly for connecting a unmanned aerial vehicle and a launcher, the quick mounting assembly comprises a first connecting piece 1 and a second connecting piece 2, the first connecting piece 1 and the second connecting piece 2 are slidably connected, the first connecting piece 1 and the second connecting piece 2 are respectively provided with a first connector 3 and a second connector 4, and the first connector 3 and the second connector 4 are communicated when the first connecting piece 1 and the second connecting piece 2 are installed in place. Figures 1-8

[0031] ​The unmanned aerial vehicle and the transmitter are connected through the quick-mounting assembly in this embodiment, and the installation efficiency is further improved through the sliding assembly. The first joint and the second joint for realizing electrical connection between the unmanned aerial vehicle and the transmitter are arranged on the first connecting piece 1 and the second connecting piece 2 respectively, and the first joint 3 and the second joint 4 are connected through the contact after the first connecting piece 1 and the second connecting piece 2 are installed in place through the sliding fit, so that the electrical connection efficiency between the unmanned aerial vehicle and the transmitter is further improved on the basis of improving the installation efficiency.

[0032] The first connecting piece 1 and the second connecting piece 2 are slidably fitted, the first connecting piece 1 comprises a first sliding part, and the second connecting piece 2 comprises a second sliding part. The first connecting piece 1 and the second connecting piece 2 can be quickly installed through the sliding fit through the first sliding part and the second sliding part. The unmanned aerial vehicle and the transmitter are quickly connected through the quick-mounting assembly, so that the efficiency of the unmanned aerial vehicle and the transmitter in the disassembly and assembly process is improved. The sliding fit mode guides the path of the quick-mounting assembly installation and improves the accuracy of the cooperation of the quick-mounting.

[0033] Embodiment 2

[0034] As shown in Figures 4-5 , the first connecting piece 1 of this embodiment is provided with a sliding cavity 12 for accommodating the second connecting piece 2. The sliding cavity 12 is provided with a guide opening 11 on one side for passing through the second connecting piece 2. The opposite side of the sliding cavity 12 is provided with a closed limiting part 14.

[0035] The second connecting piece 2 is slid through the guide opening 11 on one side of the first connecting piece 1 into the sliding cavity 12 of the first connecting piece 1, and the sliding distance of the second connecting piece 2 is limited by the limiting part 14 on the other side of the first connecting piece 1, so that the second connecting piece 2 can be stably and efficiently installed in the first connecting piece 1.

[0036] The second connecting piece 2 comprises a positioning part 23. When the second connecting piece 2 is installed in place in the sliding cavity 12 of the first connecting piece 1, the positioning part 23 is in contact with the limiting part 14 of the first connecting piece 1.

[0037] When the positioning part 23 is slid into the sliding cavity 12, the positioning part 23 arranged on the side edge of the second connecting piece 2 is in contact with the limiting part 14 of the sealing end of the sliding cavity 12, which can limit the sliding position of the second connecting piece 2, and the contact between the positioning part 23 and the limiting part 14 can make the first connecting piece 1 and the second connecting piece 2 installed in place.

[0038] Embodiment 3

[0039] As shown in Figure 4 , Figure 6As shown, the inner wall of the limiting part 14 is provided with a mounting groove one 141, the first connector 3 is mounted in the mounting groove one 141, the outer wall of the positioning part 23 is provided with a mounting groove two 231, and the second connector 4 is mounted in the mounting groove two 231. When the first connecting piece 1 and the second connecting piece 2 are installed in place, the first connector 3 and the second connector 4 mounted in the limiting part 14 and the positioning part 23 are quickly connected through abutting connection.

[0040] As shown in the figure, Figure 6 As shown, the mounting groove one 141 is also provided with a quick connector 31, the quick connector 31 is mounted between the first connector 3 and the mounting groove 141, and the mounting groove one 141 is provided with a wiring opening 142.

[0041] The quick connector 31 and the first connector 3 are both mounted in the mounting groove one 141 of the limiting part 14, the first connector 3 is arranged outside to be connected with the second connector 4 and communicate with the transmitter, and the quick connector 31 is arranged inside and provided with the wiring opening 142 to facilitate wiring of the unmanned aerial vehicle. When the unmanned aerial vehicle is running, the wiring opening 142 faces downward, which can further avoid water and water accumulation.

[0042] Embodiment 4

[0043] As shown in the figure, Figures 1-7 In this embodiment, the top of the sliding cavity 12 is provided with a first connecting part 13, the first connecting part 13 is provided with a plurality of threaded holes for connecting with the unmanned aerial vehicle, and the first connecting part 13 is detachably connected with the unmanned aerial vehicle, so that the unmanned aerial vehicle can be adapted to various types of quick-mount assemblies.

[0044] In this embodiment, the two sides of the sliding cavity 12 are L-shaped support structures, which include side plates and guide constraint plates. The side plates are perpendicular to the first connecting part 13, and the guide constraint plates are parallel to the first connecting part 13. The guide constraint plates on the two sides of the L-shaped support structure are oppositely arranged, so that the guide constraint plates on the two sides can support the second connecting piece 2.

[0045] The second connecting piece 2 of this embodiment is a T-shaped structure, which includes an upper matching part and a lower matching part. The upper matching part of the second connecting piece 2 is guided and matched with the side plate of the first connecting piece 1 and is supported by the guide constraint plate. The lower matching part of the second connecting piece 2 extends from the gap between the guide constraint plates. In this embodiment, the second connecting part 22 is installed below the second connecting piece 2 in the lower matching part, so that the second connecting part 22 for connecting the transmitter is located outside the quick-mount assembly.

[0046] Embodiment 5

[0047] The second connecting piece 22 comprises a mounting cavity 21, a control module 41 is arranged in the mounting cavity 21, a top plate is arranged on the top of the mounting cavity 21, the control module 41 is used for being connected with the transmitter through a wire, a hollow part for the wire is arranged on the bottom of the mounting cavity 21, and the second connecting part 22 is arranged on the bottom of the second connecting piece 22. The hollow part facilitates the wire of the control module 41 to be connected into the transmitter.

[0048] As shown in the drawings, Figure 6 In the embodiment, the mounting cavity 21 in the second connecting piece 2 is provided with a plurality of positioning mounting tables, the control module 41 is stably arranged in the mounting cavity 21 through the positioning mounting tables, and the control module 41 is connected with the second joint 4 through a wire.

[0049] As shown in the drawings, Figure 7 The second connecting part 22 comprises a supporting hook 222, and the supporting hook 222 is provided with an elastic pad 221. In the scheme, the transmitter is connected with the quick-mounting assembly through the supporting hook 222 of the second connecting part, and the supporting hook 222 is provided with the elastic pad 221, so that when the unmanned aerial vehicle vibrates or collides in the flight process, the elastic pad 221 can absorb the acting force of the vibration or the collision, and the launching projectile in the transmitter is prevented from being launched out in the vibration or the collision.

[0050] Embodiment 6

[0051] As shown in the drawings, Figures 1-8 The quick-mounting assembly of the embodiment further comprises a fastener 5, the fastener 5 is used for fastening and connecting the first connecting piece 1 and the second connecting piece 2, the first connecting piece 1 is provided with a first mounting hole 15, the second connecting piece 2 is provided with a second mounting hole 24, and the first mounting hole 15 and the second mounting hole 24 are inserted into the fastener 5.

[0052] As shown in the drawings, Figure 2 The fastener 5 comprises a rotating part 51 and a pushing part 52, the rotating part 51 is externally provided with an external thread matched with the first mounting hole 15, the rotating part 51 is internally provided with a stepped guide channel, and the pushing part 52 penetrates through the stepped guide channel and is inserted into the second mounting hole 24.

[0053] The fastener 5 is connected with the first connecting piece 1 and the second connecting piece 2 through the rotating part 51 and the pushing part 52 respectively. The rotating part 51 is externally provided with an external thread, and the first mounting hole 15 is a threaded hole. After the fastener 5 is threadedly connected with the first mounting hole 15 through the rotating part 51, the whole fastener 5 is arranged on the outside of the first connecting piece 1. Even if the pushing part 52 is pulled, the fastener 5 can be always arranged on the first connecting piece 1 in the use process, the fastener 5 does not need to be completely removed, and the locking between the first connecting piece 1 and the second connecting piece 2 can be unlocked.

[0054] As shown in the drawings, Figure 9As shown, the stepped guide channel inside the rotating part 51 of the embodiment extends through both ends, and the pushing part 52 can be inserted into the center of the rotating part 51 and extended from the end of the rotating part 51. The stepped guide channel includes a guide channel 511 and a limiting hole 512, the inner diameter of the limiting hole 512 is smaller than the inner diameter of the guide channel 511, and the connecting position of the limiting hole 512 and the guide channel 511 forms a limiting surface.

[0055] The pushing part 52 includes a pull rod 522 and a plug 521, the outer diameter of the pull rod 522 is smaller than the outer diameter of the plug 511, and the connecting position of the pull rod 522 and the plug 521 forms a stepped surface; the pull rod is externally sleeved with a compression spring 523, and the two ends of the compression spring 523 abut against the limiting surface and the stepped surface respectively.

[0056] A pulling head 524 is installed at the end of the pull rod 522 away from the plug 521, which is used to facilitate the operator to pull the pushing part 52.

[0057] The fastener 5 of the embodiment can prevent axial displacement between the first connecting piece 1 and the second connecting piece 2 after connecting them, and after the first connecting piece 1 and the second connecting piece 2 are fitted in place, the compression spring 523 provides sufficient compression force to ensure that the plug is firmly fixed in the second mounting hole 24, and the stable connection of the first connecting piece 1 and the second connecting piece 2 is ensured.

[0058] In addition, when disassembling, the pushing part 52 is pulled outwards by overcoming the elastic force of the compression spring 523 through the pulling head 524, so that the plug 521 can quickly disengage from the second mounting hole 24 to achieve quick disassembly.

[0059] Embodiment 7

[0060] As Figures 1-8 shown, the embodiment of the present application is a kind of launch system including launcher and quick-mount structure of unmanned aerial vehicle, also including unmanned aerial vehicle and launcher, unmanned aerial vehicle connects first connecting piece 1, launcher connects second connecting piece 2.

[0061] The launcher includes a mounting part 6, which is provided with a mounting opening, and the second connecting piece 2 extends into the mounting part 6 through the mounting opening, and the support hook 222 of the second connecting part 22 is in abutting fit with the mounting opening. The mounting part 6 of the embodiment is arranged above the launcher, and the mounting part 6 is a two-lipped mounting shell, and the width of the mounting opening arranged above the mounting part 6 is smaller than the width of the support hook 222 of the second connecting part 22. When the second connecting part 22 of the second connecting piece 2 extends into the launcher, the support hook 222 cannot disengage from the launcher under the constraint of the mounting opening formed after the mounting part 6 is mounted and closed, so that the launcher and the second connecting piece 2 are stably connected.

[0062] Since the second connecting part 22 extends into the interior of the mounting part 6, the bottom of the second connecting part 2 is a hollow structure, so that the wires of the control module 41 arranged in the second connecting part 2 can pass through the hollow structure and the mounting opening of the transmitter to extend into the interior of the transmitter for wiring.

[0063] The above is only the embodiment of the present application, and the well-known specific structure and characteristics and other common knowledge in the scheme are not described in detail. It should be pointed out that for those skilled in the art, without departing from the structure of the present application, a number of modifications and improvements can be made, which should also be considered as the protection scope of the present application, which will not affect the effect and practicability of the present application. The protection scope of the present application should be subject to the content of its claims, and the specific implementation mode and the like in the specification can be used to explain the content of the claims.

Claims

1. A quick-release structure for a launcher and a drone, characterized in that: The device includes a quick-connect assembly for connecting a drone and a transmitter. The quick-connect assembly includes a first connector (1) and a second connector (2). The first connector (1) and the second connector (2) are slidably connected. The first connector (1) and the second connector (2) are respectively provided with a first connector (3) and a second connector (4). When the first connector (1) and the second connector (2) are installed in place, the first connector (3) and the second connector (4) are connected. The first connector (3) is connected to a quick-connect plug (31), which is used for wiring the drone.

2. The quick-release structure for a launcher and a drone according to claim 1, characterized in that: The first connector (1) is provided with a sliding cavity (12) for accommodating the second connector (2). One side of the sliding cavity (12) is provided with a guide opening (11) for the second connector (2) to pass through. The sliding cavity (12) is provided with a closed limiting part (14) on the opposite side of the guide opening (11). The second connector (2) includes a positioning part (23). When the second connector (2) is installed in the sliding cavity (12) of the first connector (1), the positioning part (23) contacts the limiting part (14) of the first connector (1).

3. The quick-release structure for a launcher and a drone according to claim 2, characterized in that: The inner wall of the limiting part (14) is provided with a first mounting groove (141), and a first connector (3) is installed in the first mounting groove (141). The outer wall of the positioning part (23) is provided with a second mounting groove (231), and a second connector (4) is installed in the second mounting groove (231).

4. The quick-release structure for a launcher and a drone according to claim 3, characterized in that: A quick-connect plug (31) is also installed in the first mounting slot (141). The quick-connect plug (31) is installed between the first connector (3) and the first mounting slot (141). The first mounting slot (141) has a wiring opening (142) for wiring the quick-connect plug (31).

5. The quick-release structure for a launcher and a drone according to claim 1, characterized in that: The second connector (2) includes a mounting cavity (21), a control module (41) is provided in the mounting cavity (21), the control module (41) is used to connect the transmitter through a wire, the bottom of the mounting cavity (21) is provided with a hollow part for the wire to pass through, and the bottom of the second connector (2) is provided with a second connector (22).

6. The quick-release structure for a launcher and a drone according to claim 5, characterized in that: The second connecting part (22) includes a support hook (222), and the support hook (222) is provided with an elastic pad (221).

7. The quick-release structure for a launcher and a drone according to claim 1, characterized in that: The quick-release assembly also includes a fastener (5) for locking the first connector (1) and the second connector (2).

8. A launching system, characterized in that, The quick-release structure includes the transmitter and the drone as described in any one of claims 1-7, and also includes the drone and the transmitter, wherein the drone is mounted on the first connector (1) and the transmitter is mounted on the second connector (2).

9. A launching system according to claim 8, characterized in that: The transmitter includes a mounting part (6), which has a mounting opening. The second connector (2) extends into the mounting part (6) through the mounting opening. The width of the mounting opening is smaller than the width of the second connector (22). The mounting opening restricts the movement of the support hook (222) outward from the mounting part (6). The support hook (222) abuts against the mounting part (6).

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