CN210316752U - Unmanned aerial vehicle multimachine hangar - Google Patents
Unmanned aerial vehicle multimachine hangar Download PDFInfo
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- CN210316752U CN210316752U CN201920984470.4U CN201920984470U CN210316752U CN 210316752 U CN210316752 U CN 210316752U CN 201920984470 U CN201920984470 U CN 201920984470U CN 210316752 U CN210316752 U CN 210316752U
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Abstract
The utility model belongs to the technical field of unmanned aerial vehicle equips, a unmanned aerial vehicle multimachine hangar is disclosed, including the cabin body, still include: the platforms are arranged in the cabin body in a lifting manner and used for parking the unmanned aerial vehicle; the unmanned aerial vehicle fixing mechanism is arranged on the platform and used for fixing the unmanned aerial vehicle; and the positioning mechanism is arranged on the cabin body and used for adjusting the position of the unmanned aerial vehicle on the platform to the fixed position of the unmanned aerial vehicle fixing mechanism. The utility model discloses a set up the platform of a plurality of liftable, can realize the storage, the parking of many unmanned aerial vehicles, can realize the continuous incessant operation of many unmanned aerial vehicles and simultaneous working simultaneously. Can pinpoint the unmanned aerial vehicle that descends on the platform through positioning mechanism for unmanned aerial vehicle arranges unmanned aerial vehicle fixed position of unmanned aerial vehicle fixed establishment in, and by it fixed.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle equips technical field, especially relates to an unmanned aerial vehicle multimachine hangar.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by radio remote control devices and program control devices, or is operated autonomously, either completely or intermittently, by an onboard computer. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle is matched with the industry for application, and is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.
The problem of continuation of the journey and charging in the unmanned aerial vehicle use of considering, can be equipped with the unmanned aerial vehicle hangar usually, current unmanned aerial vehicle hangar is the stand-alone hangar mostly, can only be used for charging, the storage of an unmanned aerial vehicle promptly, and an unmanned aerial vehicle's charge time is longer, can't be suitable for the occasion of continuous incessant operation. In addition, an unmanned aerial vehicle that the stand-alone hangar stored can only carry out an operation simultaneously, and when many unmanned aerial vehicles of needs were worked simultaneously, the stand-alone hangar can't satisfy above-mentioned requirement.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle multimachine hangar can realize parking, the storage of many unmanned aerial vehicles, and can realize multimachine continuous incessant operation or simultaneous operation.
To achieve the purpose, the utility model adopts the following technical proposal:
the utility model provides an unmanned aerial vehicle multimachine hangar, includes the cabin body, still includes:
the platforms are arranged in the cabin body in a lifting manner and used for parking the unmanned aerial vehicle;
the unmanned aerial vehicle fixing mechanism is arranged on the platform and used for fixing the unmanned aerial vehicle;
and the positioning mechanism is arranged on the cabin body and used for adjusting the position of the unmanned aerial vehicle on the platform to the fixed position of the unmanned aerial vehicle fixing mechanism.
Preferably, the platform comprises a bottom plate fixedly arranged on the cabin body, a guide seat arranged on the bottom plate, a guide column capable of axially moving relative to the guide seat, a platform table surface fixedly connected to the guide column, and a lifting cylinder for driving the platform table surface to lift.
Preferably, a two-dimensional code identification plate is fixed at the middle position of the platform, and the two-dimensional code identification plate is configured to be used for the unmanned aerial vehicle to scan codes and locate.
Preferably, the unmanned aerial vehicle fixed establishment including be fixed in mounting panel on the platform sets firmly in the first motor of mounting panel, by first motor drive is in opposite directions or two sets of holders that move from each other, and is two sets of the holder is used for the centre gripping to be fixed unmanned aerial vehicle.
Preferably, the clamping piece comprises clamping plates which are respectively arranged on two sides of the mounting plate, and the clamping plates penetrate through the platform.
Preferably, the clamping plate is provided with a V-shaped clamping opening, and the V-shaped clamping openings of the two clamping plates located on the same side of the mounting plate are arranged oppositely.
As preferred, unmanned aerial vehicle fixed establishment still include by first motor drive pivoted positive and negative lead screw, threaded connection in two nuts of positive and negative lead screw, the rigid coupling in the slider of nut, and locate the guide rail under the mounting panel, the slider for guide rail slidable, and every a set of is installed to the slider the holder.
Preferably, the positioning mechanism comprises two groups of X-direction linear modules and two groups of Y-direction linear modules, the two groups of X-direction linear modules are mounted on the cabin body, the X-direction linear modules are in driving connection with one ends of the X-direction positioning rods, the other ends of the X-direction positioning rods are in sliding connection with the X-direction guide rails, the Y-direction linear modules are in driving connection with one ends of the Y-direction positioning rods, and the other ends of the Y-direction positioning rods are in sliding connection with the Y-direction.
Preferably, still include cloud platform fixed establishment, cloud platform fixed establishment including set firmly in the mounting bracket of platform below, the rigid coupling in the driving piece of mounting bracket, by the fixed block that the vertical direction removed is followed in the driving piece drive, the fixed block can pass the platform.
Preferably, the cabin further comprises a movable cabin door, and the movable cabin door is arranged at the top of the cabin body in a sliding mode.
Preferably, a temperature and humidity adjusting device, a monitoring device, a lighting device and a charging device are arranged in the cabin body.
The utility model has the advantages that: through setting up the platform of a plurality of liftable, can realize many unmanned aerial vehicle's storage, parking, can realize many unmanned aerial vehicle continuous uninterrupted duty and simultaneous operation simultaneously. Can pinpoint the unmanned aerial vehicle that descends on the platform through positioning mechanism for unmanned aerial vehicle arranges unmanned aerial vehicle fixed position of unmanned aerial vehicle fixed establishment in, and by it fixed.
Drawings
Fig. 1 is a schematic view of a three-dimensional structure of the unmanned aerial vehicle multi-machine hangar of the present invention;
fig. 2 is a schematic structural view of the platform of the unmanned aerial vehicle multi-machine hangar of the present invention;
fig. 3 is a schematic structural view of the fixing mechanism of the unmanned aerial vehicle multi-machine hangar of the present invention;
fig. 4 is an assembly schematic diagram of the platform of the unmanned aerial vehicle multi-machine hangar and the unmanned aerial vehicle fixing mechanism of the utility model;
fig. 5 is a schematic structural view of the positioning mechanism of the multi-machine hangar of the unmanned aerial vehicle of the present invention;
fig. 6 is the utility model discloses the cloud platform fixed establishment's of unmanned aerial vehicle multimachine hangar structure schematic diagram.
In the figure:
1. a cabin body; 11. ground feet;
2. a platform; 21. a base plate; 22. a guide seat; 23. a guide post; 24. a platform surface; 25. a lifting cylinder; 26. a two-dimensional code identification plate; 241. a rectangular hole;
3. an unmanned aerial vehicle fixing mechanism; 31. mounting a plate; 32. a first motor; 33. a clamping plate; 34. a positive and negative screw rod; 35. a nut; 36. a slider; 331. a V-shaped nip;
4. a positioning mechanism; 41. an X-direction linear module; 42. a Y-direction linear module; 43. an X-direction positioning rod; 44. a Y-direction positioning rod; 45. an X-direction guide rail; 46. a Y-direction guide rail;
5. a holder fixing mechanism; 51. a mounting frame; 52. a fixed block; 53. a second motor; 54. a sliding sleeve; 541. a pin hole; 511. a long hole;
6. a mobile hatch; 7. unmanned aerial vehicle.
Detailed Description
The present invention will be described in further detail with reference to the accompanying drawings and examples. It is to be understood that the specific embodiments described herein are merely illustrative of the invention and are not limiting of the invention. It should be further noted that, for the convenience of description, only some of the structures related to the present invention are shown in the drawings, not all of the structures.
In the description of the present invention, unless expressly stated or limited otherwise, the terms "connected," "connected," and "fixed" are to be construed broadly, e.g., as meaning permanently connected, detachably connected, or integral to one another; can be mechanically or electrically connected; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
In the present disclosure, unless expressly stated or limited otherwise, the first feature "on" or "under" the second feature may comprise direct contact between the first and second features, or may comprise contact between the first and second features not directly. Also, the first feature being "on," "above" and "over" the second feature includes the first feature being directly on and obliquely above the second feature, or merely indicating that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature includes the first feature being directly under and obliquely below the second feature, or simply meaning that the first feature is at a lesser elevation than the second feature.
In the description of the present embodiment, the terms "upper", "lower", "right", etc. are used in an orientation or positional relationship based on that shown in the drawings only for convenience of description and simplicity of operation, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used only for descriptive purposes and are not intended to have a special meaning.
The utility model provides an unmanned aerial vehicle multimachine hangar for realize the storage of many unmanned aerial vehicle 7, park, can refer to figure 1, this unmanned aerial vehicle multimachine hangar includes cabin body 1, a plurality of platform 2, unmanned aerial vehicle fixed establishment 3 and positioning mechanism 4, wherein:
above-mentioned cabin body 1 becomes rectangle form box structure, and its open-top sets up for supply unmanned aerial vehicle 7 business turn over cabin body 1. And a movable cabin door 6 is also arranged at the top of the cabin body 1, and the movable cabin door 6 is arranged in a sliding manner so as to realize the closing and opening of the top of the cabin body 1. In particular, the mobile hatch 6 can be driven by means of a motor, pulleys and toothed belts to slide relative to the cabin 1. And the sliding of the mobile hatch 6 is achieved by means of linear guide sliders. In order to reduce the footprint of the mobile hatch 6 when opened, the mobile hatch 6 is of double-decker retractable construction (shown in figure 1). In this embodiment, the structure of the movable cabin door 6 is a common structure in the prior art, and is not described in detail.
Four corners at the bottom of the cabin body 1 are provided with height-adjustable anchor feet 11 so as to ensure the levelness and stability of the cabin body 1 when placed.
Preferably, the outer surface of the cabin 1 of the present embodiment is treated with rust and corrosion prevention, and a sand-proof and rain-proof coating or cover may be further disposed on the outer surface of the cabin 1.
Optionally, a temperature and humidity adjusting device (for example, an air conditioning heat pump system) may be further disposed inside the cabin 1, and the temperature and humidity inside the cabin 1 can be adjusted by cooperating with a temperature and humidity detecting device (for example, a temperature and humidity sensor) and/or an exhaust fan. Monitoring devices can be further arranged in the cabin body 1, and the landing position and the angle deviation of the unmanned aerial vehicle 7 and the storage condition of the unmanned aerial vehicle 7 in the cabin can be monitored in real time through the monitoring devices. Lighting lamps and charging devices may also be provided in the cabin 1.
Further, a human-computer interaction system can be arranged outside the cabin 1 and used for displaying and controlling the unmanned aerial vehicle 7 in the cabin 1.
In this embodiment, above-mentioned platform 2 is installed in cabin body 1, and above-mentioned platform 2 is liftable platform, when unmanned aerial vehicle 7 just descends, platform 2 rises certain distance (if exceed 1 top plane in cabin body or portable hatch door 6), and 2 positions of platform are higher this moment, and unmanned aerial vehicle 7's wing is higher than the height of spare part around the cabin body 1, has reduced the risk that unmanned aerial vehicle 7's wing and 1 peripheral spare part of cabin body interfere when descending like this. And when the unmanned aerial vehicle 7 is fixed, the unmanned aerial vehicle 7 is placed in the cabin 1 (for example, is landed to a position for charging or replacing a battery) by descending the platform 2. But also the closing of the mobile hatch 6 can be facilitated by the lowering of the platform 2.
Specifically, as shown in fig. 2, the platform 2 includes a bottom plate 21, a guide seat 22, a guide post 23, a platform surface 24, a lifting cylinder 25, and a two-dimensional code identification plate 26, wherein:
the bottom plate 21 is fixedly installed in the cabin 1, the guide seat 22 is installed on the bottom plate 21, the guide seat 22 is of a columnar structure and is vertically arranged, the guide column 23 capable of moving axially relative to the guide seat 22 is arranged in the guide seat 22 in a penetrating mode, the top of the guide column 23 is fixedly connected to the platform table top 24, the shell of the lifting cylinder 25 is fixed to the bottom plate 21, and the output end of the lifting cylinder is fixed to the bottom of the platform table top 24. Through the flexible of lift cylinder 25, can drive platform mesa 24 lift, in this process, guide post 23 can realize the direction when support and platform mesa 24 removal to platform mesa 24.
In this embodiment, the guide bases 22 and the guide posts 23 are preferably arranged in groups, and at least two groups are arranged, so as to stably support the platform top 24. As shown in fig. 2, the guide bases 22 and the guide posts 23 are provided in two sets, and the two sets of guide bases 22 and the guide posts 23 are provided diagonally. It will be understood that three or more sets of guide seats 22 and guide posts 23 may be provided.
The two-dimensional code identification plate 26 is arranged on the platform surface 24 and used for scanning and positioning the code by the unmanned aerial vehicle. Because the positions of a plurality of platforms 2 are different, the two-dimensional code of the corresponding two-dimensional code identification plate 26 that is located on different platforms 2 is also different, so that the unmanned aerial vehicle 7 lands on different platforms 2 according to different two-dimensional codes. In this embodiment, the two-dimensional code identification plate 26 is preferably disposed at the middle position of the platform 2, so that the unmanned aerial vehicle 7 initially lands at the middle position of the platform 2, and collision between the unmanned aerial vehicle 7 and other structures is avoided.
When the two-dimensional code identification plate 26 of the embodiment is used, the two-dimensional code image is identified by the unmanned aerial vehicle 7, specifically, when the height of the unmanned aerial vehicle 7 from the platform 2 is greater than 5m, the target position is determined by continuously detecting and photographing, a kernel for corrosion or expansion operation is manufactured, the kernel is rectangular, an anchor point is defaulted as a central point, and the image is expanded according to the established kernel; converting an image from an RGB color space to a grayscale space; and binarizing the image information. When the height of the unmanned aerial vehicle 7 from the platform 2 is less than 5m, the corresponding aircraft landing position is obtained by identifying the two-dimensional code, four vertexes and corresponding coordinates of the two-dimensional code are identified clockwise, and then the coordinates of the center point of the two-dimensional code are obtained.
By finding out the pixel position of the target central point in the image, the pixel distances in the x direction and the y direction between the pixel position of the target central point and the pixel position of the image center are calculated, then the pixel distances are converted into an unmanned aerial vehicle coordinate system from the image coordinate system, the pixel distances are converted into actual horizontal distances by combining with actual heights, the actual horizontal distances are transmitted to the unmanned aerial vehicle 7, and the unmanned aerial vehicle 7 is controlled to horizontally align to the target central position in real time to land.
Above-mentioned unmanned aerial vehicle fixed establishment 3 is used for 7 fixed to the unmanned aerial vehicle that descends on platform 2 to when the transportation, prevent that 7 drunkenness of unmanned aerial vehicle from causing the damage. Every platform 2 all corresponds and is provided with an unmanned aerial vehicle fixed establishment 3. Referring to fig. 3, the fixing mechanism 3 of the unmanned aerial vehicle includes a mounting plate 31, a first motor 32 and two sets of clamping members, wherein:
above-mentioned mounting panel 31 is fixed in the bottom of above-mentioned platform mesa 24, and fixed mounting has above-mentioned first motor 32 on this mounting panel 31, and this first motor 32 can drive the removal that two sets of holders deviate from in opposite directions or mutually through transmission structure, when two sets of holders move in opposite directions, can realize fixed to unmanned aerial vehicle 7's centre gripping, when two sets of holders move away from mutually, can remove fixed to unmanned aerial vehicle 7's centre gripping.
Specifically, the transmission structure may be a positive and negative lead screw 34, the first motor 32 drives the positive and negative lead screw 34 to rotate through belts or gears, etc., and meanwhile, the positive and negative lead screw 34 is connected to two nuts 35 through threads, the two nuts 35 are respectively fixed with a sliding block 36, the sliding block 36 can slide on a guide rail, and the guide rail is installed at the bottom of the mounting plate 31. Each of the two sets of gripping members is mounted on a slider 36 and is capable of moving with the slider 36. Drive positive and negative lead screw 34 through first motor 32 and rotate for two nuts 35 are along positive and negative lead screw 34 and move in opposite directions or back of the body away from each other, and then drive slider 36 and holder by nut 35 and move, finally make two sets of holders move in opposite directions or back of the body away from each other, realize fixed or release fixedly to the unmanned aerial vehicle 7 centre gripping.
In this embodiment, the clamping member includes two clamping plates 33 respectively disposed on two sides of the mounting plate 31, and the two clamping plates 33 are respectively fixed on two sides of the sliding block 36 and move along with the sliding block 36. Referring to fig. 4, in this embodiment, a rectangular hole 241 for the clamping plate 33 to move is formed in the platform surface 24, and the clamping portion of the clamping plate 33 penetrates through the rectangular hole 241 to clamp and fix the unmanned aerial vehicle 7.
Further, as shown in fig. 3, a V-shaped clamping opening 331 is formed in the clamping plate 33, and the V-shaped clamping opening 331 is used for clamping the unmanned aerial vehicle 7. Wherein the V-shaped clamp openings 331 of the two clamp plates 33 on the same side of the mounting plate 31 are arranged oppositely, so that a space for placing the legs of the unmanned aerial vehicle 7 is formed between the two V-shaped clamp openings 331, and then under the movement of the clamp plates 33, the two opposite V-shaped clamp openings 331 can clamp the unmanned aerial vehicle 7.
Above-mentioned positioning mechanism 4 is used for the adjustment to descend the position of unmanned aerial vehicle 7 on platform 2 to make unmanned aerial vehicle 7 accurate clamping position department of arranging above-mentioned unmanned aerial vehicle fixed establishment 3 in, in order to avoid 7 positions of unmanned aerial vehicle not to lead to the centre gripping unstability or the clamping position mistake leads to unmanned aerial vehicle 7 impaired. And also can prevent 7 wings of unmanned aerial vehicle from touchhing cabin 1 when platform 2 descends, because 7 positions of unmanned aerial vehicle and angle are not accurate, can't carry out if trade operations such as battery, charging.
Specifically, as shown in fig. 5, the positioning mechanism 4 includes two sets of X-direction linear modules 41 and two sets of Y-direction linear modules 42 mounted on the cabin 1, wherein the X-direction linear modules 41 are connected with X-direction positioning rods 43 in a driving manner, the other ends of the X-direction positioning rods 43 are connected with X-direction guide rails 45 in a sliding manner, and the X-direction positioning rods 43 can be driven by the X-direction linear modules 41 to slide along the X-direction guide rails 45. Accordingly, the Y-direction linear module 42 is connected to a Y-direction positioning rod 44 in a driving manner, and the other end of the Y-direction positioning rod 44 is connected to a Y-direction rail 46 in a sliding manner.
It should be noted that, when the unmanned aerial vehicle 7 does not land on the platform 2, by moving the X-direction positioning rod 43 and the Y-direction positioning rod 44, two X-direction positioning rods 43 are located on two sides of the platform 2, and the Y-direction positioning rod 44 is located on the other two sides of the platform 2, after the unmanned aerial vehicle 7 lands on the platform 2, because of the existing position and angle deviation, the landing position and angle deviation of the unmanned aerial vehicle 7 can be obtained by the monitoring device at this time, and then, by moving one or two of the X-direction positioning rods 43 and one or two of the Y-direction positioning rods 44, the unmanned aerial vehicle 7 is moved to a desired position, that is, to the holding and fixing position of the unmanned aerial vehicle.
Above-mentioned X all includes high accuracy step motor or servo motor to linear module 41 and Y to linear module 42, and step motor or servo motor all integrate and have position encoder to realize accurate position control, and then make unmanned aerial vehicle 7's position adjustment more accurate.
It should be noted that, in cooperation with the lifting of the platform 2, when the platform 2 descends with the drone 7, the X-direction positioning rod 43 and the Y-direction positioning rod 44 need to be away from the platform 2 to prevent interference caused by the descending of the drone 7. In addition, after this platform 2 drove unmanned aerial vehicle 7 and descends, X is to locating lever 43 and Y to locating lever 44 when carrying out position adjustment to unmanned aerial vehicle 7 on other platforms 2, also can not receive unmanned aerial vehicle 7's on this platform 2 interference.
In this embodiment, when the unmanned aerial vehicle multimachine hangar is installed on the moving vehicle, above-mentioned unmanned aerial vehicle multimachine hangar can also include cloud platform fixed establishment 5, and this cloud platform fixed establishment 5 can realize the fixed of the cloud platform that loads to unmanned aerial vehicle 7 to the damage is rocked to the cloud platform when avoiding transporting.
Referring to fig. 6, the holder fixing mechanism 5 includes a mounting frame 51 fixedly disposed below the platform 2, a driving member fixedly connected to the mounting frame 51, and a fixing block 52 driven by the driving member to move in a vertical direction, and a hole is formed in the platform 2, and the fixing block 52 can pass through the hole and be fixed to the holder.
In this embodiment, the driving member includes a second motor 53, a screw (not shown) driven by the second motor 53, a nut (not shown) screwed to the screw, and a sliding sleeve 54 fixedly connected to the nut, wherein the sliding sleeve 54 is fixedly connected to the fixing block 52. The sliding sleeve 54 is provided with a pin hole 541, the mounting frame 51 is provided with a long hole 511 along the vertical direction, and the sliding sleeve 54 cannot rotate by a pin shaft passing through the long hole 511 and the pin hole 541. When the cradle head needs to be fixed, the second motor 53 drives the screw rod to rotate, at this time, due to the action of the pin shaft, the sliding sleeve 54 and the nut can move along the screw rod, and then the sliding sleeve 54 drives the fixing block 52 to penetrate through the platform 2 and be fixed on the cradle head.
It is understood that the driving member may be a linear motor, and may be a structure such as an air cylinder, which can realize the linear displacement of the fixed block 52. The driving member can directly drive the fixing block 52 to pass through the platform 2 and be fixed on the pan/tilt head.
Above-mentioned unmanned aerial vehicle multimachine hangar of this embodiment, when initial condition, portable hatch door 6 is in the closed condition, and 7 platforms 2 of unmanned aerial vehicle are in the decline position this moment, and unmanned aerial vehicle fixed establishment 3 and cloud platform fixed establishment 5 close, and the X of positioning mechanism 4 is in the biggest open position to locating lever 43 and Y to locating lever 44.
When unmanned aerial vehicle 7 need take off, portable hatch door 6 is opened, and the platform 2 of parking this unmanned aerial vehicle 7 rises, and unmanned aerial vehicle fixed establishment 3 is opened (if there is cloud platform fixed establishment 5, then cloud platform fixed establishment 5 also opens), controls unmanned aerial vehicle 7 to take off afterwards. In this process, if 7 electric quantities of a certain unmanned aerial vehicle are not enough and can not be used, then can directly control 7 take off of second unmanned aerial vehicle, continue to carry out corresponding operation. In addition, if the multiple unmanned aerial vehicles 7 are required to operate simultaneously, the multiple unmanned aerial vehicles 7 are controlled to take off simultaneously, and corresponding operation is executed.
When 7 descends of unmanned aerial vehicle, portable hatch door 6 is opened, platform 2 rises, and unmanned aerial vehicle fixed establishment 3 is in the open mode (if there is cloud platform fixed establishment 5, then cloud platform fixed establishment 5 also is in the open mode), control unmanned aerial vehicle 7 afterwards through two-dimensional code sign board 26, preliminary descending is on the intermediate position of this platform 2, X through positioning mechanism 4 afterwards is to the removal of locating lever 43 and Y to locating lever 44, with 7 accurate movements of unmanned aerial vehicle to unmanned aerial vehicle fixed establishment 3 departments, 7 centre gripping of unmanned aerial vehicle is fixed by unmanned aerial vehicle fixed establishment 3 afterwards, this platform 2 is kept away from to later positioning mechanism 4, platform 2 drives unmanned aerial vehicle 7 and descends, close portable hatch door 6 afterwards.
Above-mentioned unmanned aerial vehicle multimachine hangar of this embodiment through the platform 2 that sets up a plurality of liftable, can realize the storage of many unmanned aerial vehicle 7, park, can realize many unmanned aerial vehicle 7 continuous uninterrupted duty and simultaneous operation simultaneously.
It is obvious that the above embodiments of the present invention are only examples for clearly illustrating the present invention, and are not intended to limit the embodiments of the present invention. Numerous obvious variations, rearrangements and substitutions will now occur to those skilled in the art without departing from the scope of the invention. And are neither required nor exhaustive of all embodiments. Any modification, equivalent replacement, and improvement made within the spirit and principle of the present invention should be included in the protection scope of the claims of the present invention.
Claims (10)
1. The utility model provides an unmanned aerial vehicle multimachine hangar, includes cabin body (1), its characterized in that still includes:
the platforms (2) are arranged in the cabin body (1) in a lifting manner and are used for parking the unmanned aerial vehicle (7);
the unmanned aerial vehicle fixing mechanism (3) is mounted on the platform (2) and used for fixing the unmanned aerial vehicle (7);
positioning mechanism (4), install in on the cabin body (1), be used for the adjustment the position of unmanned aerial vehicle (7) on platform (2) extremely the fixed position of unmanned aerial vehicle fixed establishment (3).
2. The unmanned aerial vehicle multi-aircraft hangar of claim 1, wherein the platform (2) comprises a bottom plate (21) fixedly arranged on the cabin (1), a guide seat (22) mounted on the bottom plate (21), a guide post (23) axially movable relative to the guide seat (22), a platform table top (24) fixedly connected to the guide post (23), and a lifting cylinder (25) driving the platform table top (24) to lift.
3. The unmanned aerial vehicle multi-aircraft hangar of claim 1 or 2, wherein a two-dimensional code identification plate (26) is fixed at an intermediate position of the platform (2), and the two-dimensional code identification plate (26) is configured to be positioned by scanning a code of the unmanned aerial vehicle.
4. The unmanned aerial vehicle multi-machine hangar as claimed in claim 1, wherein the unmanned aerial vehicle fixing mechanism (3) comprises a mounting plate (31) fixed on the platform (2), a first motor (32) fixed on the mounting plate (31), and two sets of clamping members driven by the first motor (32) to move towards or away from each other, and used for clamping and fixing the unmanned aerial vehicle (7).
5. Unmanned aerial vehicle multi-airframe garage according to claim 4, wherein said clamps comprise clamping plates (33) provided on both sides of said mounting plate (31), said clamping plates (33) being arranged through said platform (2).
6. The unmanned aerial vehicle multi-aircraft hangar of claim 5, wherein the clamping plates (33) are provided with V-shaped clamping openings (331), and the V-shaped clamping openings (331) of the two clamping plates (33) positioned on the same side of the mounting plate (31) are arranged oppositely.
7. The unmanned aerial vehicle multi-aircraft hangar of any one of claims 4 to 6, wherein the unmanned aerial vehicle fixing mechanism (3) further comprises a positive and negative lead screw (34) driven by the first motor (32) to rotate, two nuts (35) screwed on the positive and negative lead screw (34), a sliding block (36) fixedly connected to the nuts (35), and a guide rail arranged below the mounting plate (31), wherein the sliding block (36) is slidable relative to the guide rail, and each sliding block (36) is provided with a group of clamping pieces.
8. The unmanned aerial vehicle multi-machine hangar as claimed in claim 1, wherein the positioning mechanism (4) comprises two sets of X-direction linear modules (41) and two sets of Y-direction linear modules (42) mounted on the cabin (1), the X-direction linear modules (41) are connected to one end of an X-direction positioning rod (43) in a driving manner, the other end of the X-direction positioning rod (43) is connected to an X-direction guide rail (45) in a sliding manner, the Y-direction linear modules (42) are connected to one end of a Y-direction positioning rod (44) in a driving manner, and the other end of the Y-direction positioning rod (44) is connected to a Y-direction guide rail (46) in a sliding.
9. The unmanned aerial vehicle multi-aircraft hangar of claim 1, further comprising a pan-tilt fixing mechanism (5), wherein the pan-tilt fixing mechanism (5) comprises a mounting frame (51) fixedly arranged below the platform (2), a driving member fixedly connected to the mounting frame (51), and a fixing block (52) driven by the driving member to move in a vertical direction, and the fixing block (52) can penetrate through the platform (2).
10. The unmanned aerial vehicle multi-airplane hangar of claim 1, further comprising a mobile hatch (6), wherein the mobile hatch (6) is slidably disposed on the top of the cabin (1).
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| Application Number | Priority Date | Filing Date | Title |
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| CN201920984470.4U CN210316752U (en) | 2019-06-27 | 2019-06-27 | Unmanned aerial vehicle multimachine hangar |
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| CN201920984470.4U CN210316752U (en) | 2019-06-27 | 2019-06-27 | Unmanned aerial vehicle multimachine hangar |
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN111874250A (en) * | 2020-07-31 | 2020-11-03 | 复亚智能科技(太仓)有限公司 | Unmanned aerial vehicle outdoor operations equipment |
| CN111942266A (en) * | 2020-09-11 | 2020-11-17 | 中国人民解放军陆军炮兵防空兵学院 | Unmanned aerial vehicle take-off and landing platform |
| CN112026560A (en) * | 2020-08-03 | 2020-12-04 | 广西大学 | Comb-tooth type parking garage for unmanned aerial vehicle parking charging |
| CN112144937A (en) * | 2019-06-27 | 2020-12-29 | 上海复亚智能科技有限公司 | Unmanned aerial vehicle multimachine hangar |
| CN112623248A (en) * | 2020-12-29 | 2021-04-09 | 上海比茵沃汽车电子有限公司 | Trunk unmanned aerial vehicle undercarriage |
| CN114313037A (en) * | 2021-12-24 | 2022-04-12 | 中国兵器工业计算机应用技术研究所 | Ground-air cooperative unmanned automatic equipment |
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2019
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| CN112144937A (en) * | 2019-06-27 | 2020-12-29 | 上海复亚智能科技有限公司 | Unmanned aerial vehicle multimachine hangar |
| CN111874250A (en) * | 2020-07-31 | 2020-11-03 | 复亚智能科技(太仓)有限公司 | Unmanned aerial vehicle outdoor operations equipment |
| CN112026560A (en) * | 2020-08-03 | 2020-12-04 | 广西大学 | Comb-tooth type parking garage for unmanned aerial vehicle parking charging |
| CN111942266A (en) * | 2020-09-11 | 2020-11-17 | 中国人民解放军陆军炮兵防空兵学院 | Unmanned aerial vehicle take-off and landing platform |
| CN112623248A (en) * | 2020-12-29 | 2021-04-09 | 上海比茵沃汽车电子有限公司 | Trunk unmanned aerial vehicle undercarriage |
| CN112623248B (en) * | 2020-12-29 | 2024-06-04 | 上海比茵沃汽车电子有限公司 | Trunk unmanned aerial vehicle undercarriage |
| CN114313037A (en) * | 2021-12-24 | 2022-04-12 | 中国兵器工业计算机应用技术研究所 | Ground-air cooperative unmanned automatic equipment |
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