Unmanned aerial vehicle flying platform and adaptive unmanned aerial vehicle thereof

Abstract

The utility model belongs to the technical field of unmanned aerial vehicles, and particularly relates to an unmanned aerial vehicle flying platform and an adaptive unmanned aerial vehicle thereof.The unmanned aerial vehicle flying platform comprises a shell, two flange seats are fixed to the bottom of the interior of the shell, a first bottom plate is fixed between the two flange seats, and a supporting plate is assembled in the shell and located at the upper ends of the flange seats; the four end corners of the top of the shell are provided with first quick-mounting pieces, and the four end corners of the bottom of the shell are each fixedly provided with a second quick-mounting piece. The first fast-assembly sleeve and the second fast-assembly sleeve are arranged at the top and the bottom of the shell respectively, and the first fast-assembly sleeve and the second fast-assembly sleeve are matched, so that the multiple shells can be stacked, the number of the shells can be conveniently adjusted according to the use number of unmanned aerial vehicles, the occupied area of the shells cannot be increased, and the unmanned aerial vehicles can be conveniently and rapidly assembled. And the device can flexibly and conveniently adjust the number of the shells according to the use number of the unmanned aerial vehicles, the use requirements of different scenes can be met, and the applicability of the device is improved.

Description

TECHNICAL FIELD

[0001] The utility model belongs to unmanned plane technical field, concretely relates to an unmanned plane flight platform and the unmanned plane of adaptation thereof. BACKGROUND

[0002] The rapid development of unmanned plane technology promotes its wide application in many fields such as logistics transportation, inspection and monitoring, emergency rescue, and the unmanned plane flight platform as the core supporting equipment for storing, scheduling and assisting unmanned plane to complete the landing operation has also become an indispensable part of the unmanned plane system. This kind of platform usually needs to have stable supporting structure and basic function module to meet the safe storage and preparation needs of unmanned plane before operation, and its performance and design rationality directly affect the overall operation efficiency of unmanned plane system.

[0003] The unmanned plane flight platform in the prior art is designed with fixed storage structure, that is, the number of unmanned planes that a single platform can accommodate is pre-set at the factory, and the common fixed number specifications are one or more. This fixed design has obvious limitations in actual application: for example, the unmanned plane airport, flight lifesaving system, method and use of the public number CN115610690A, the multi-station type platform can park and take off multiple unmanned planes, but it is an integral structure. For users who purchase a small amount, the cost of purchasing and subsequent use of the entire hangar is high. When the use demand of unmanned planes increases, for example, more unmanned planes are needed for cooperative operation in large-scale inspection tasks or multi-region logistics distribution scenarios, the existing platform cannot flexibly adjust its storage capacity according to the actual number of unmanned planes. To meet the storage needs of new unmanned planes, users can only add unmanned plane flight platforms of the same specification, and each new platform needs to occupy independent ground space, resulting in a significant increase in overall floor area, especially in scenarios where space resources are limited (such as indoor hangars and small operation sites). The superposition of floor area will further exacerbate the tension of space utilization.

[0004] In summary, the existing unmanned plane flight platform lacks flexibility in capacity adjustment due to fixed storage quantity, and when faced with the demand for dynamic changes in the number of unmanned planes, it can only increase the number of platforms to cope with the problem of increasing floor area. This situation not only limits the adaptability of the unmanned plane system in different scale operation scenarios, but also increases the user's use cost due to excessive occupation of space resources, which is difficult to meet the demand for flexibility and space economy of unmanned plane platform in actual application. UTILITY MODEL CONTENTS

[0005] The purpose of this utility model is to provide a drone flight platform and a drone adapted thereto. By setting a first quick-release sleeve and a second quick-release sleeve at the top and bottom of the shell respectively, the cooperation of the first quick-release sleeve and the second quick-release sleeve allows multiple shells to be stacked, making it easy to adjust the number of shells according to the number of drones used, without increasing the footprint of the shells. This allows the device to flexibly and conveniently adjust the number of shells according to the number of drones used, meeting the needs of different scenarios and improving the applicability of the device.

[0006] The specific technical solution adopted by this utility model is as follows:

[0007] A drone flight platform includes at least one shell. Two flange seats are fixed to the bottom inside the shell, and a first base plate is fixed between the two flange seats. A support plate is assembled inside the shell and above the flange seats. First quick-release components are provided at the four corners of the top of the shell, and second quick-release components are fixed at the four corners of the bottom of the shell. The first and second quick-release components are compatible with each other. When multiple shells are stacked vertically, the first and second quick-release components cooperate to form a stacking structure between adjacent shells. The first and second quick-release components are connected end to end to form a square layout.

[0008] Furthermore, a drive assembly is assembled between the two flange seats and at the upper end of the first base plate. The drive assembly includes two first guide rails and two first sliders. The two first guide rails are respectively fixed to the two flange seats on their respective adjacent sides. The two first sliders are respectively slidably connected to the two first guide rails on their respective adjacent sides. A second guide rail is fixed to the adjacent side of each of the two first sliders. A first crossbeam and a second crossbeam are respectively fixed to the two ends of the bottom of the two second guide rails. The second guide rails, the first crossbeams, and the second crossbeams form a rectangular structure. A motor is fixed to the upper end of the first crossbeam. A drive wheel is fixed to the output end of the motor. A driven wheel is rotatably connected to the upper end of the second crossbeam. A transmission belt is assembled on the outer side of the drive wheel and the driven wheel. A first linkage plate is fixed to the lower end of the outer side of the transmission belt. A second linkage plate is fixed to the upper end of the outer side of the transmission belt. A second slider is slidably connected to the adjacent side of each of the two second guide rails. The first linkage plate and the first base plate, the second linkage plate and the support plate, and the second slider and the support plate are all fixedly connected.

[0009] Furthermore, distance sensors are fixed at both ends of the top of the first base plate, a first sensing plate is fixed at the top of the first crossbeam, and a second sensing plate is fixed at the top of the second crossbeam. The distance sensors and the first sensing plate, as well as the distance sensors and the second sensing plate, are adapted to each other.

[0010] Further, the first quick mounting piece is a quick mounting groove (104a) arranged above the shell, the second quick mounting piece is a support (105a) arranged below the shell, and the outer layer of the support (105a) is covered with corrosion-resistant rubber, and the support (105a) is in interference fit with the quick mounting groove through the corrosion-resistant rubber.

[0011] Further, the first quick mounting piece is a first quick mounting sleeve (104b), the second quick mounting piece is a second quick mounting sleeve (105b), the upper end of the outer side of the first quick mounting sleeve (104b) is provided with external threads, the outer side of the second quick mounting sleeve (105b) is rotationally connected with a locking sleeve, the lower end of the inner wall of the locking sleeve is provided with internal threads, the external threads and the internal threads are matched, and the first quick mounting sleeve (104b) and the second quick mounting sleeve (105b) are fixedly connected through the locking sleeve.

[0012] Further, a plurality of anti-skid lines are uniformly formed on the outer side of the locking sleeve.

[0013] Further, a dust cover is threadedly connected to the top of the first quick mounting sleeve (104b).

[0014] Further, one end of the shell is provided with a hatch, the top of the shell is provided with a dustproof heat dissipation element, and the two sides of the shell are rotationally connected with access doors, wherein the hatch and the shell and the access doors and the shell are mutually attached, and a closed space is formed in the shell.

[0015] Further, at least one first quick mounting sleeve (104b) is internally fixed with a quick coupling female head, a second quick mounting sleeve (105b) matched with the first quick mounting sleeve (104b) is internally fixed with a quick coupling male head, and the quick coupling female head and the quick coupling male head are matched.

[0016] A UAV uses any one of the UAV flight platforms, and the UAV is matched with the support plate.

[0017] The utility model discloses technical effects are obtained:

[0018] The first quick mounting piece and the second quick mounting piece are arranged on the top and the bottom of the shell respectively, the first quick mounting piece and the second quick mounting piece are matched, a plurality of shells can be stacked and placed to form a stacking structure, the number of shells can be adjusted according to the number of UAVs, the floor area of the shells is not increased, the number of shells can be flexibly and conveniently adjusted according to the number of UAVs, different scene use demands can be met, and the applicability of the device is improved.

[0019] The utility model discloses a first fast -assembling piece and second fast -assembling piece of square distribution can conveniently adjust the installation direction of shell, when the installation direction of two adjacent shells is staggered, can simultaneously carry out start -stop operation to multiple unmanned planes, improves operating efficiency;

[0020] The utility model discloses a drive assembly runs through the starting motor, drives the pallet to move in the horizontal direction, and carries out start -stop operation to the unmanned plane through the side operation mode, compared with the upper start -stop operation mode in the prior art, can reduce the rainwater, dust that the device upper accumulation or residual enters the shell inside, and then effectively maintains the cleanliness of shell inside. BRIEF DESCRIPTION OF DRAWINGS

[0021] Figure 1 It is the structure schematic diagram of the whole in the utility model embodiment one;

[0022] Figure 2 It is the utility model Figure 1 It is the partial close -up schematic diagram of A place in the utility model embodiment one;

[0023] Figure 3 It is the structure bottom view of the whole in the utility model embodiment one;

[0024] Figure 4 It is the sectional view of the whole structure in the utility model embodiment one;

[0025] Figure 5 It is the assembly schematic diagram of first fast -assembling sleeve and second fast -assembling sleeve in the utility model embodiment one;

[0026] Figure 6 It is the structure sectional view of first fast -assembling sleeve and second fast -assembling sleeve in the utility model embodiment one;

[0027] Figure 7 It is the structure schematic diagram of drive assembly in the utility model embodiment one;

[0028] Figure 8 It is the structure explosion drawing of drive assembly in the utility model embodiment one;

[0029] Figure 9 It is the schematic diagram of rectangular structure in the utility model embodiment one;

[0030] Figure 10 It is the assembly schematic diagram of first linkage plate and second linkage plate in the utility model embodiment one;

[0031] Figure 11 It is the structure schematic diagram of drive assembly when the pallet is located in the shell in the utility model embodiment one;

[0032] Figure 12The structure sectional view of the first quick mounting sleeve and the second quick mounting sleeve in the second embodiment of the utility model;

[0033] Figure 13 The state schematic view of four unmanned aerial vehicles simultaneously taking off in the stacked state of the plurality of shells of the utility model;

[0034] Figure 14 The state schematic view of four unmanned aerial vehicles simultaneously taking off in the stacked state of the plurality of shells of the utility model;

[0035] Figure 15 The structure schematic view of the whole in the third embodiment of the utility model;

[0036] Figure 16 The structure bottom view of the whole in the third embodiment of the utility model.

[0037] In the drawings, the component list represented by each sign is as follows:

[0038] 100, shell; 101, flange seat; 102, first bottom plate; 103, supporting plate; 104a, quick mounting groove; 104b, first quick mounting sleeve; 105a, supporting piece; 105b, second quick mounting sleeve; 106, locking sleeve; 107, dustproof cover; 108, hatch; 109, dustproof heat dissipation element; 110, maintenance door; 111, quick connection female head; 112, quick connection male head;

[0039] 200, driving assembly;

[0040] 201, first guide rail; 202, first sliding block; 203, second guide rail; 204, first cross beam; 205, second cross beam; 206, motor; 207, driving wheel; 208, driven wheel; 209, transmission belt; 210, first linkage plate; 211, second linkage plate; 212, second sliding block; 213, distance sensor; 214, first induction plate; 215, second induction plate. DETAILED DESCRIPTION

[0041] In order to make the purpose and the advantage of the utility model more clear and obvious, the following is specifically explained to the utility model in combination with the embodiment. It should be understood that the following text is only used to describe one or several specific implementation manners of the utility model, and does not strictly limit the protection scope specifically requested by the utility model.

[0042] The unmanned aerial vehicle flight platform comprises at least a shell 100, two flange seats 101 are fixed at the bottom of the interior of the shell 100, a first bottom plate 102 is fixed between the two flange seats 101, a supporting plate 103 is assembled at the upper end of the flange seat 101 in the interior of the shell 100, first quick-mounting pieces are arranged at the four end corners of the top of the shell 100, second quick-mounting pieces are fixed at the four end corners of the bottom of the shell 100, and the first quick-mounting pieces and the second quick-mounting pieces are matched with each other, wherein, after a plurality of shells 100 are stacked in the vertical direction in sequence, the first quick-mounting pieces and the second quick-mounting pieces are matched with each other, so that a stacking structure is formed between the two adjacent shells 100, and the first quick-mounting pieces and the second quick-mounting pieces are sequentially connected in a head-tail mode to form a square layout.

[0043] Through the above arrangement, the unmanned aerial vehicle flight platform is changed from a traditional fixed position to an adjustable position, the flexibility of purchase of the user is improved, and the usability in the use process is considered. In addition, since the flight platform generally has a charging function, that is, whether it is a single machine or multiple positions, there is a charging circuit. In actual combination, the circuit can be selected to be connected to the grid, or each position can be used independently. If the circuit is selected to be connected to the grid, the specific mode can refer to the grid connection mode in the prior art, and according to the needs, a plug-in port can be reserved above and below each shell 100 in the structure. Here, no specific details are given. The unmanned aerial vehicle flight platform will be discussed in more detail below. Embodiment one

[0044] As shown in Figures 1 to 6 An unmanned aerial vehicle flight platform comprises at least one shell 100, two flange seats 101 are fixed on the two sides of the bottom of the interior of the shell 100 through bolts, a first bottom plate 102 is fixed between the two flange seats 101 through bolts, a supporting plate 103 is assembled at the upper end of the flange seat 101 in the interior of the shell 100, first quick-mounting sleeves 104b are fixed at the four end corners of the top of the shell 100 through bolts, second quick-mounting sleeves 105b are fixed at the four end corners of the bottom of the shell 100 through bolts, and the first quick-mounting sleeves 104b and the second quick-mounting sleeves 105b are matched with each other, wherein, after a plurality of shells 100 are stacked in the vertical direction in sequence, the first quick-mounting sleeves 104b and the second quick-mounting sleeves 105b are matched with each other, so that the two adjacent shells 100 can be fixed.

[0045] Here, a control circuit board, a power supply and other related elements are also fixed in the interior of the shell 100. The control circuit board can control the start and stop of various electrical elements in the interior of the shell 100 and process related data. The power supply can charge the unmanned aerial vehicle. The related elements in the interior of the shell 100 that ensure stable operation of the device can refer to the prior art, and no further details are given here. The device can be adaptively adjusted according to the use requirements of the device.

[0046] It should be noted that, Figure 5The diagram shows the engagement of the first quick-release sleeve 104b and the second quick-release sleeve 105b on two adjacent housings 100 when they are stacked. Figure 5 In the middle, the first quick-release sleeve 104b is fixed to the top of the housing 100 located at the lower end, and the second quick-release sleeve 105b is fixed to the bottom of the housing 100 located at the upper end.

[0047] Specifically, multiple shells 100 stacked in the vertical direction refers to the state in which at least two shells 100 are stacked in the vertical direction, such as... Figure 13 and Figure 14 As shown in the illustration, in this embodiment, four shells 100 are stacked. The specific number of shells 100 stacked can be adjusted according to the usage requirements and safety standards of the drone, and does not constitute a specific limitation.

[0048] In a preferred embodiment, such as Figures 7 to 11 As shown, a drive assembly 200 is assembled between the two flange seats 101 and at the upper end of the first base plate 102. The drive assembly 200 includes two first guide rails 201 and two first sliders 202. The two first guide rails 201 are respectively fixed to the two flange seats 101 on their adjacent sides by bolts. The two first sliders 202 are respectively slidably connected to the two first guide rails 201 on their adjacent sides. A second guide rail 203 is fixed to the adjacent sides of the two first sliders 202 by bolts. A first crossbeam 204 and a second crossbeam 205 are respectively fixed to the two ends of the bottom of the two second guide rails 203. The two second guide rails 203, the first crossbeam 204, and the second crossbeam 205 form a rectangular structure. A motor 206 is fixed to the upper end of the first crossbeam 204 by bolts. The output end of the motor 206 is fixed with a drive wheel 207. The upper end of the second crossbeam 205 is fixed with two flange blocks. The two flange blocks are rotatably connected with a driven wheel 208 through a ball bearing. The second crossbeam 205 and the driven wheel 208 are rotatably connected through the cooperation of the flange blocks and the ball bearing. The drive wheel 207 and the driven wheel 208 are equipped with a transmission belt 209. The lower end of the outer side of the transmission belt 209 is fixed with a first linkage plate 210. The upper end of the outer side of the transmission belt 209 is fixed with a second linkage plate 211. The two second guide rails 203 are slidably connected with second sliders 212 on the side that are close to each other. The first linkage plate 210 and the first base plate 102, the second linkage plate 211 and the support plate 103, and the second slider 212 and the support plate 103 are all fixedly connected by bolts.

[0049] In the embodiment, the inner wall of the transmission belt 209 is uniformly provided with a plurality of teeth, the first linkage plate 210 and the second linkage plate 211 are both internally provided with a tooth groove, and the teeth and the tooth groove are matched with each other, and the transmission belt 209 and the first linkage plate 210 and the transmission belt 209 and the second linkage plate 211 are both relatively limited through the matching of the tooth groove and the teeth.

[0050] Specifically, the driving assembly 200 can drive the supporting plate 103 to move in the horizontal direction, and when the supporting plate 103 moves to the outside of the shell 100, the unmanned aerial vehicle is started and stopped through the side operation mode, which can greatly reduce or avoid the rainwater and dust accumulated or remaining on the device from entering the inside of the shell 100, thereby effectively maintaining the cleanliness of the inside of the shell 100.

[0051] Here, a control terminal is also used with the circuit control board, and the control terminal and the circuit control board are connected through circuit connection or wireless connection, and the start and stop of the motor 206 can be controlled through the control terminal. Of course, the overall operation of the device can also be controlled through an automatic control system, and the specific working mechanism and specific structure can refer to the prior art, and will not be described further here.

[0052] In a preferred embodiment, as shown in Figures 7 to 8 The two ends of the top of the first bottom plate 102 are both fixed with a distance sensor 213 through bolts, the top of the first cross beam 204 is fixed with a first induction plate 214 through bolts, the top of the second cross beam 205 is fixed with a second induction plate 215 through bolts, the distance sensor 213 and the first induction plate 214 and the distance sensor 213 and the second induction plate 215 are matched one by one, and the distance sensor 213 and the control circuit board are electrically connected through wires.

[0053] Here, since the first bottom plate 102 and the shell 100, the first induction plate 214 and the first cross beam 204, and the second induction plate 215 and the second cross beam 205 are all fixedly connected, and the position of the first bottom plate 102 remains unchanged relative to the shell 100, the distance between the first bottom plate 102 and the first cross beam 204 and the distance between the first bottom plate 102 and the second cross beam 205 can be obtained in real time through the cooperation of the distance sensor 213 and the first induction plate 214 and the distance sensor 213 and the second induction plate 215.

[0054] In a preferred embodiment, as shown in Figure 1 and Figure 3As shown, the center points of the plurality of first quick-mount sleeves 104b are connected to form a first square, the center points of the plurality of second quick-mount sleeves 105b are connected to form a second square, the midpoint of the first square, the midpoint of the second square, and the center of the housing 100 are collinear in the vertical direction, and the projections of the first square and the second square on the horizontal plane coincide with each other.

[0055] In the present embodiment, the horizontal cross-sectional shape of the housing 100 is a square.

[0056] It should be noted that, as shown in Figure 13 and Figure 14 , by the above scheme, two adjacent housings 100 can adjust the installation direction so that the moving directions of the pallets 103 are staggered, and when a plurality of housings 100 are used simultaneously, the staggered pallets 103 can simultaneously perform the take-off / landing operation of the unmanned aerial vehicle, as shown in Figure 13 , the included angle between two adjacent pallets 103 is 180° (at this time, a maximum of two unmanned aerial vehicles can simultaneously perform the take-off / landing operation), as shown in Figure 14 , the included angle between two adjacent pallets 103 is 90° (at this time, a maximum of four unmanned aerial vehicles can simultaneously perform the take-off / landing operation), of course, the included angle between two adjacent pallets 103 can be adjusted according to actual use requirements, which is not specifically limited here.

[0057] Further, in the present embodiment, the housing 100 adjusts different installation directions, which can adjust the moving direction of the pallet 103.

[0058] In a preferred embodiment, an outer thread is formed on the upper end of the outer side of the first quick-mount sleeve 104b, a lock sleeve 106 is slidably and rotatably connected to the outer side of the second quick-mount sleeve 105b, an inner thread is formed on the lower end of the inner wall of the lock sleeve 106, the outer thread and the inner thread are matched, and the first quick-mount sleeve 104b and the second quick-mount sleeve 105b are fixedly connected through the lock sleeve 106.

[0059] It should be noted that a guide groove is formed in the first quick-mount sleeve 104b, a guide column is formed on the lower end of the outer side of the lock sleeve 106, and the guide groove and the guide column are matched, an annular groove is formed on the upper end of the outer side of the second quick-mount sleeve 105b, the lock sleeve 106 is slidably and rotatably connected to the inside of the annular groove, and the outer diameter of the annular groove is smaller than the outer diameter of the guide column, so as to avoid the lock sleeve 106 from sliding off the outer side of the second quick-mount sleeve 105b.

[0060] In a preferred embodiment, the outer side of the locking sleeve 106 is uniformly provided with a plurality of anti-skid lines. The anti-skid lines can increase the friction between the hands of the workers and the locking sleeve 106, thereby facilitating the workers to rotate the locking sleeve 106.

[0061] In a preferred embodiment, the top of the first quick-mounting sleeve 104b is detachably screwed with a dust cover 107. The dust cover 107 can block the inside of the first quick-mounting sleeve 104b.

[0062] It should be noted that when the plurality of housings 100 are stacked for use, the one at the lowermost end needs to be fixed to the ground or other base by bolts or other reliable fixing means. The first quick-mounting sleeve 104b at the top of the one at the uppermost end needs to be screwed with the dust cover 107, which covers the first quick-mounting sleeve 104b at the uppermost end to prevent rain, dust or other substances from falling into the first quick-mounting sleeve 104b, so as to ensure that the first quick-mounting sleeve 104b and the second quick-mounting sleeve 105b can be stably connected.

[0063] In a preferred embodiment, one end of the housing 100 is provided with a hatch 108, the top of the housing 100 is provided with a dustproof and heat dissipation element 109, and the two sides of the housing 100 are rotatably connected with an access door 110. When the hatch 108 and the housing 100 and the access door 110 and the housing 100 are in close contact with each other, a closed space is formed in the housing 100. The dustproof and heat dissipation element 109 is configured to prevent dust from entering the housing 100 and to dissipate heat in the housing 100. The specific structure can refer to the prior art. The access door 110 is configured to allow the structure elements in the housing 100 to be repaired and maintained.

[0064] In a specific embodiment, the hatch 108 is fixed to one end of the supporting plate 103 by bolts or angle irons or other reliable fixing means. When the driving assembly 200 drives the supporting plate 103 to move, the supporting plate 103 can drive the hatch 108 to move synchronously.

[0065] In another specific embodiment, the lower end of the shell 100 near one end of the hatch 108 is bolted with a plurality of self-closing hinges, which have the characteristic of automatic closing, and in the free state, the self-closing hinges are in the normally closed state, when the drive assembly 200 drives the tray 103 to move outward from the shell 100, the tray 103 can extrude and drive the hatch 108 to rotate, so that the hatch 108 is rotated to the lower end of the tray 103, when the drive assembly 200 drives the tray 103 to move inward from the shell 100, the tray 103 no longer extrudes the hatch 108, and the tray 103 can be attached to the shell 100 under the drive of the self-closing hinge, wherein the specific installation method in this embodiment is not shown in the figure, and the tray 103, the hatch 108 and the drive assembly 200 do not interfere with each other during operation. Embodiment two

[0066] Please refer to Figure 12 The embodiment is further optimized on the basis of embodiment one, specifically:

[0067] The inside of at least one first quick-mounting sleeve 104b is fixed with a quick-connect female head 111, and the inside of the second quick-mounting sleeve 105b compatible with the first quick-mounting sleeve 104b is fixed with a quick-connect male head 112, and the quick-connect female head 111 and the quick-connect male head 112 are compatible.

[0068] In this embodiment, the inside of each of the plurality of first quick-mounting sleeves 104b is fixed with a quick-connect female head 111, and the inside of each of the plurality of second quick-mounting sleeves 105b is fixed with a quick-connect male head 112, so that when adjusting the installation direction of the shell 100, the quick-connect female head 111 can be compatible with the quick-connect male head 112.

[0069] It should be noted that, Figure 12 The first quick-mounting sleeve 104b and the second quick-mounting sleeve 105b shown in the figure are in a stacked state, and the cooperation between the first quick-mounting sleeve 104b and the second quick-mounting sleeve 105b on two adjacent shells 100 is shown in the figure, Figure 12 In the figure, the first quick-mounting sleeve 104b is fixed to the top of the shell 100 at the lower end, and the second quick-mounting sleeve 105b is fixed to the bottom of the shell 100 at the upper end, and the quick-connect female head 111 inside the first quick-mounting sleeve 104b and the circuit control board inside the shell 100 at the lower end, and the quick-connect male head 112 inside the second quick-mounting sleeve 105b and the circuit control board inside the shell 100 at the upper end are all electrically connected through wires.

[0070] Through the above scheme setting, the control circuit boards in the mutually stacked multiple housings 100 can form a series circuit structure, thereby facilitating unified control and cooperative operation through a matching control program, wherein the control program can be developed and programmed by professionals according to actual use requirements, as long as the purpose of unified control and cooperative operation of the multiple housings 100 can be achieved, and further description is not made here. Embodiment three

[0071] Please refer to Figure 15 and Figure 16 The difference between the present embodiment and embodiment one is that the first quick mounting part and the second quick mounting part are different, specifically, the first quick mounting part is a quick mounting groove 104a arranged above the housing 100, and the second quick mounting part is a support 105a arranged below the housing 100, and the outer layer of the support 105a is covered with corrosion-resistant rubber, and the support 105a is in interference fit with the quick mounting groove 104a through the corrosion-resistant rubber.

[0072] In the present embodiment, the overall layout of the top of the housing 100 is considered to avoid the protrusion of the top of the housing 100, but the setting of the top dustproof and heat dissipation element 109 is sacrificed accordingly, which can be set to the side of the housing 100 to avoid normal heat dissipation use. In actual use process, the support 105a can be used as a bottom support, and when stacking, the support 105a is placed in the quick mounting groove 104a (both are cylindrical or circular truncated cone), and the interference fit state between the two is realized by the deformability of the corrosion-resistant rubber, and the corrosion-resistant rubber has good resistance effect, thereby ensuring the connection strength between the two. The advantage of this design is that the overall contact area of the housing 100 is larger when stacked, has better support, and the whole is more neat and beautiful. In addition, in order to avoid outdoor use, the quick mounting groove 104a should be provided with a waterproof rubber cover in the non-stacked state, which ensures waterproof and dustproof and improves the overall appearance. Embodiment four

[0073] A UAV suitable for the UAV flight platform of any one of embodiments one or two, specifically, the UAV is matched with the support plate 103.

[0074] The working principle of the utility model is:

[0075] According to the number of unmanned aerial vehicle demand, the shell 100 at the lower end is fixed on the ground or base by bolts or other reliable fixing mode, the other shells 100 are stacked on the upper end of the shell 100 on the ground, and the guide column of the lower end of the second quick-assembly sleeve 105b is inserted into the guide groove in the inside of the first quick-assembly sleeve 104b (and the quick-assembly male head 112 and the quick-assembly female head 111 are electrically connected), the locking sleeve 106 is rotated to make the locking sleeve 106 and the first quick-assembly sleeve 104b threadedly connected, thereby forming a stable connection between the two adjacent shells 100, until the number of stacked shells 100 is consistent with the number of unmanned aerial vehicles, at this time, the unmanned aerial vehicle and the shell 100 are one-to-one corresponding, thereby ensuring that the number of shells 100 can be flexibly and conveniently adjusted according to the number of unmanned aerial vehicles, and the floor area of the shell 100 is not substantially increased, after the plurality of shells 100 are stacked, when the unmanned aerial vehicle is started or stopped, the motor 206 is started to rotate the output end of the motor 206, through the fixed connection of the motor 206 and the driving wheel 207, the motor 206 drives the driving wheel 207 to rotate, the driving wheel 207 drives the transmission belt 209 to rotate, since the first linkage plate 210 and the shell 100 are fixedly connected through the flange seat 101 and the first bottom plate 102, the first linkage plate 210 remains stationary relative to the shell 100 during the rotation of the transmission belt 209, the transmission belt 209 transmits driving force to the rectangular structure (composed of the two second guide rails 203, the first cross beam 204 and the second cross beam 205), the rectangular structure moves relative to the shell 100 and the first linkage plate 210 driven by the transmission belt 209, and the motor 206 and the second linkage plate 211 are synchronously moved by the rectangular structure, since the second linkage plate 211 and the supporting plate 103 are fixedly connected, the second linkage plate 211 drives the supporting plate 103 to move synchronously, when the supporting plate 103 moves to the outside of the shell 100, the unmanned aerial vehicle can take off or land on the upper end of the supporting plate 103, when the included angle between the two adjacent supporting plates 103 is 90° or 180°, multiple unmanned aerial vehicles can take off or land simultaneously.

[0076] The above is only the preferred embodiment of the present application, it should be pointed out that, for those skilled in the art, without departing from the principle of the present application, a number of improvements and refinements can be made, these improvements and refinements should also be considered as the protection scope of the present application. The structures, devices and operation methods not specifically described and explained in the present application are implemented according to the conventional means in the art, unless otherwise specified and limited.

Claims

1. An unmanned aerial vehicle flight platform, characterized by: The utility model provides a quick -assembling type shell, including the shell (100), the bottom fixed with two flange seat (101) inside the shell (100), the first bottom plate (102) is fixed between two flange seat (101), the inside of shell (100) and be located flange seat (101) upper end assembly has the supporting plate (103), the top of shell (100) four end angle is provided with first quick -assembling spare, the bottom of shell (100) four end angle all are fixed with second quick -assembling spare, and first quick -assembling spare and second quick -assembling spare are adapted, wherein, a plurality of shell (100) is stacked in vertical direction in proper order after, through the cooperation of first quick -assembling spare and second quick -assembling spare, forms the stacking structure between adjacent two shell, wherein, the first quick -assembling spare and second quick -assembling spare head -to -tail are connected in proper order and form square layout.

2. The unmanned aerial vehicle flight platform of claim 1, wherein: Two flange seat (101) between and be located first bottom plate (102) upper end assembly has drive assembly (200), drive assembly (200) includes two first guide rail (201) and two first sliding block (202), two first guide rail (201) is fixed respectively in two flange seat (101) one side close to each other, two first sliding block (202) are connected respectively in two first guide rail (201) one side close to each other, two first sliding block (202) one side close to each other all are fixed with second guide rail (203), two second guide rail (203) bottom two ends are fixed with first crossbeam (204) and second crossbeam (205) respectively, and second guide rail (203), first crossbeam (204) and second crossbeam (205) constitute rectangular structure, first crossbeam (204) upper end is fixed with motor (206), motor (206) output is fixed with driving wheel (207), second crossbeam (205) upper end rotationally connected with driven wheel (208), driving wheel (207) and driven wheel (208) outside assembly has transmission belt (209), transmission belt (209) outside lower end is fixed with first linkage plate (210), transmission belt (209) outside upper end is fixed with second linkage plate (211), two second guide rail (203) one side close to each other all are connected with second sliding block (212), and first linkage plate (210) and first bottom plate (102), second linkage plate (211) and supporting plate (103) and second sliding block (212) and supporting plate (103) between are fixedly connected.

3. The unmanned aerial vehicle flight platform of claim 2, wherein: First bottom plate (102) top both ends are fixed with distance sensor (213), first crossbeam (204) top is fixed with first induction plate (214), second crossbeam (205) top is fixed with second induction plate (215), distance sensor (213) and first induction plate (214) and distance sensor (213) and second induction plate (215) between one -to -one adaptation.

4. The unmanned aerial vehicle flight platform of any one of claims 1 to 3, wherein: The first quick mounting piece is a quick mounting groove (104a) arranged above the shell (100), the second quick mounting piece is a support piece (105a) arranged below the shell (100), and the outer layer of the support piece (105a) is coated with corrosion-resistant rubber, and the support piece (105a) is in interference fit with the quick mounting groove through the corrosion-resistant rubber.

5. The unmanned aerial vehicle flight platform of any one of claims 1 to 3, wherein: The first quick mounting piece is a first quick mounting sleeve (104b), the second quick mounting piece is a second quick mounting sleeve (105b), an outer side of the upper end of the first quick mounting sleeve (104b) is provided with external threads, the second quick mounting sleeve (105b) is rotatably connected with a locking sleeve (106) on the outer side, the inner wall of the locking sleeve (106) is provided with internal threads at the lower end, the external threads and the internal threads are matched, and the first quick mounting sleeve (104b) and the second quick mounting sleeve (105b) are fixedly connected through the locking sleeve (106).

6. The unmanned aerial vehicle flight platform of claim 5, wherein: The outer side of the locking sleeve (106) is uniformly provided with a plurality of anti-skid lines.

7. The unmanned aerial vehicle flight platform of claim 5, wherein: The top of the first quick mounting sleeve (104b) is threadedly connected with a dust cover (107).

8. The unmanned aerial vehicle flight platform of claim 5, wherein: One end of the shell (100) is provided with a hatch (108), the top of the shell (100) is provided with a dustproof and heat dissipation element (109), and both sides of the shell (100) are rotatably connected with an access door (110), wherein the hatch (108), the shell (100) and the access door (110) and the shell (100) are mutually attached, and a closed space is formed in the shell (100).

9. The unmanned aerial vehicle flight platform of claim 5, wherein: The inside of at least one first quick mounting sleeve (104b) is fixedly provided with a quick connector female head (111), the inside of the second quick mounting sleeve (105b) matched with the first quick mounting sleeve (104b) is fixedly provided with a quick connector male head (112), and the quick connector female head (111) and the quick connector male head (112) are matched.

10. A UAV using the UAV flight platform according to any one of claims 1 to 9. The unmanned aerial vehicle is matched with the supporting plate (103).

Images