CN210653683U - Take unmanned aerial vehicle platform of taking off and land of dustcoat - Google Patents
Take unmanned aerial vehicle platform of taking off and land of dustcoat Download PDFInfo
- Publication number
- CN210653683U CN210653683U CN201921229040.8U CN201921229040U CN210653683U CN 210653683 U CN210653683 U CN 210653683U CN 201921229040 U CN201921229040 U CN 201921229040U CN 210653683 U CN210653683 U CN 210653683U
- Authority
- CN
- China
- Prior art keywords
- unmanned aerial
- aerial vehicle
- cover
- platform
- spherical
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Images
Abstract
The utility model discloses an unmanned aerial vehicle taking-off and landing platform with an outer cover, which comprises a fixed frame, a hemispherical protective cover and a shutdown platform arranged in the protective cover; the bottom of the protective cover is arranged on the fixed frame, the shutdown platform is arranged in the middle of the fixed frame, the protective cover comprises a plurality of petal-shaped spherical covers, and the plurality of petal-shaped spherical covers are combined together to form the hemispherical protective cover in a closed state; the first driving mechanism is used for driving at least one spherical mask to move so that the hemispherical protective cover is opened to expose the shutdown platform. The utility model discloses an unmanned aerial vehicle take off and land platform of outband cover is pleasing to the eye, can save space to be convenient for unmanned aerial vehicle's maintenance charge and take off and land.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle equipment of taking off and land, concretely relates to take unmanned aerial vehicle platform of taking off and land of dustcoat.
Background
With the progress of technology, unmanned aerial vehicle technology has become more mature, and has been widely applied to the fields of military affairs, agriculture, aerial photography and the like. However, due to the problem of battery endurance in the prior art, the unmanned aerial vehicle needs to land on a base station platform for charging after flying for a period of time, so as to ensure normal flying operation of the unmanned aerial vehicle; in addition, the unmanned aerial vehicle who accomplishes outdoor flight operation need return to appointed place, shuts down and waits for relevant personnel's maintenance. After unmanned aerial vehicle navigates back to charge basic station or maintenance point, under the outdoor environment of complicacy, suffer damage of equidimension easily, especially to agricultural plant protection unmanned aerial vehicle, directly expose and park in the abominable open-air area of condition, be not convenient for unmanned aerial vehicle charge and overhaul, cause serious damage to unmanned aerial vehicle easily. A specific unmanned aerial vehicle take off and land platform in market is through the removal of platform, transports unmanned aerial vehicle from the open air to indoor to accomplish protection and the charging to unmanned aerial vehicle. However, above-mentioned unmanned aerial vehicle take-off and landing platform need shift out the platform outdoor, just can realize stopping and landing and taking off of unmanned aerial vehicle, leads to whole device to occupy too much space to when unmanned aerial vehicle need descend and take off, need flexible platform get into or shift out indoor, just can realize the transportation to unmanned aerial vehicle, complex operation, and inefficiency.
SUMMERY OF THE UTILITY MODEL
The utility model discloses aim at overcomes prior art's is not enough, provides an unmanned aerial vehicle platform of taking off and land of dustcoat, and this platform of taking off and land saves space, and unmanned aerial vehicle's of being convenient for descending and take off to play the guard action to unmanned aerial vehicle.
The purpose of the utility model is realized through the following technical scheme:
an unmanned aerial vehicle taking-off and landing platform with an outer cover is characterized by comprising a fixed frame, a hemispherical protective cover and a stopping platform arranged in the protective cover; the bottom of the protective cover is arranged on the fixed frame, the shutdown platform is arranged in the middle of the fixed frame, the protective cover comprises a plurality of petal-shaped spherical covers, and the plurality of petal-shaped spherical covers are combined together to form the hemispherical protective cover in a closed state; the first driving mechanism is used for driving at least one spherical mask to move so that the hemispherical protective cover is opened to expose the shutdown platform.
The operating principle of the unmanned aerial vehicle take-off and landing platform with the outer cover is as follows:
when unmanned aerial vehicle need return to the journey to descend, at least one spherical cover of a actuating mechanism drive rotates for the safety cover is opened, thereby makes and shuts down the platform and expose, thereby forms a flight passageway in the open position department of safety cover, shuts down the platform and exposes under the sky. The unmanned aerial vehicle vertically descends on the shutdown platform through a flight channel formed after the spherical cover is opened according to a planned air route, and the unmanned aerial vehicle descends. Accomplish unmanned aerial vehicle's descending back, the spherical cover that first actuating mechanism drive corresponds rotates back to seal whole shut down platform and protect in whole safety cover. When the unmanned aerial vehicle takes off, the first driving mechanism continues to drive the at least one spherical cover to rotate to form a flight channel, and the unmanned aerial vehicle takes off through the flight channel.
Preferably, the protective cover comprises two spherical covers, and one of the spherical covers rotates to one side of the other spherical cover around the vertical central line of the protective cover under the driving of the first driving mechanism so as to open the protective cover or the two spherical covers rotate in opposite directions around the vertical central line of the protective cover so as to open the protective cover. Through setting up two ball face guards, be convenient for the opening and the closing of safety cover to simple structure.
In a preferred embodiment of the present invention, the fixing frame comprises a base and a connecting seat disposed on the base; the connecting seat is annular and is provided with a guide groove; among two ball face guards of safety cover, one of them is the movable cover, and another is fixed cover, the movable cover slides and sets up in the guide way, fixed cover is fixed to be set up on the connecting seat, the movable cover is less than fixed cover, a actuating mechanism is connected with the movable cover. When the unmanned aerial vehicle needs to land, the first driving mechanism drives the movable cover to slide to one side of the fixed cover along the guide groove and is positioned in the fixed cover, so that the landing position of the shutdown platform is exposed to wait for the landing of the unmanned aerial vehicle; when the safety cover is closed to needs, first actuating mechanism drive safety cover resets and removes, forms a hemispherical safety cover with the concatenation of fixed cover, realizes unmanned aerial vehicle's protection. Through the setting of the base of mount for whole take-off and landing platform has certain distance with ground, ensures that unmanned aerial vehicle parks in the environment of airtight and dry, is favorable to depositing of unmanned aerial vehicle.
In a preferable scheme of the utility model, a second driving mechanism for driving the shutdown platform to rotate around the axis is arranged in the protective cover; the shutdown platform is circular, the bottom of the shutdown platform is rotatably connected to the fixing frame through the supporting shaft, and the second driving mechanism is connected with the supporting shaft. When a plurality of unmanned aerial vehicles land or take off, the second driving mechanism drives the stop platform to rotate, so that the vacancy of the stop platform rotates to one side corresponding to a flight channel formed after the protective cover is opened, and the next unmanned aerial vehicle lands on the stop platform; or the unmanned aerial vehicle which needs to take off moves to the corresponding position of the flight channel after the rotation of the stop platform, and the unmanned aerial vehicle takes off continuously in sequence. Set up the circular shape and shut down the platform, be convenient for rotate to be favorable to descending more unmanned aerial vehicles.
Preferably, the number of the shutdown platforms is multiple, and the shutdown platforms are arranged in a vertical direction; the number of the second driving mechanisms is multiple, and the multiple second driving mechanisms correspond to the multiple shutdown platforms one to one; wherein, all be equipped with the transition breach on a plurality of platforms of shutting down. A plurality of vertically arranged shutdown platforms are arranged to form a multi-layer shutdown platform, so that the whole take-off and landing platform can store more unmanned aerial vehicles; when needing take off and land unmanned aerial vehicle, all the transition breachs of shutting down the platform are aimed at, form unified take off and land passageway, and when the unmanned aerial vehicle on the platform of shutting down of certain layer took off or descended on this layer of shutting down the platform, the second actuating mechanism that corresponds with this layer of shutting down the platform drives the position of stopping and landing that should shut down the platform and rotate to the department that corresponds with transition passageway to the realization takes off or lands.
The utility model discloses a preferred scheme, still include the rotation actuating mechanism used for driving two ball masks to rotate at the same time; the connecting seat is rotatably connected to the base; the rotation driving mechanism is composed of a servo motor and a gear rack mechanism, the servo motor is fixedly arranged on the base, a rack of the gear rack mechanism is arranged on the connecting seat in a surrounding mode, and a gear of the gear rack mechanism is connected with a power shaft of the servo motor and is arranged in a matching mode with a rack of the gear rack mechanism. Through setting up rotation actuating mechanism, can drive two spherical covers simultaneously and rotate after the safety cover is opened to change the flight passageway's after the safety cover is opened position, and then realize shutting off the unmanned aerial vehicle's of the different positions on the platform takeoff.
In a preferred embodiment of the present invention, a charging mechanism is disposed at the bottom of the shutdown platform, the charging mechanism includes two charging buckles and a charging driving mechanism for driving the two charging buckles to approach or separate from each other, and the two charging buckles are respectively connected to the positive electrode and the negative electrode of the charging power supply; the charging driving mechanism consists of a charging motor and a bidirectional screw transmission mechanism, a bidirectional screw of the bidirectional screw transmission mechanism is connected with a main shaft of the charging motor, and the two charging buckles are respectively arranged on two screw sliders of the bidirectional screw transmission mechanism; and an avoiding groove for avoiding the movement of the two charging buckles is arranged on the stopping platform. Because the charging contact position of the unmanned aerial vehicle is arranged on the rack, when the unmanned aerial vehicle lands on the shutdown platform according to the reference identifier and the rack of the unmanned aerial vehicle is positioned between the two charging buckles; two charging buckles of charging motor drive are close to each other for two charging buckles respectively with the contact position contact that charges in the unmanned aerial vehicle frame, realize charging, after the completion of charging, two charging buckles of charging motor drive reverse migration each other, leave the unmanned aerial vehicle frame can, design benefit realizes automatic charging.
In a preferred embodiment of the present invention, the connecting seat of the fixing frame is provided with a first guide rail groove and a second guide rail groove, and the first guide rail groove and the second guide rail groove are internally tangent; the two spherical covers are respectively arranged in the first guide rail groove and the second guide rail groove; the first driving mechanism comprises a transmission motor, a screw rod transmission mechanism and a synchronous transmission mechanism, wherein the synchronous transmission mechanism comprises a synchronous moving rod and two guide sliders, the two guide sliders are arranged on the synchronous moving rod in a sliding mode and are respectively arranged in a first guide rail groove and a second guide rail groove, the two spherical covers are respectively and fixedly connected with the corresponding guide sliders, and an avoiding groove for avoiding the synchronous moving rod to move is formed in the bottom of the connecting seat; and a screw rod of the screw rod transmission mechanism is connected with a power output shaft of the transmission motor, and a screw rod nut of the screw rod transmission mechanism is fixedly connected with the synchronous moving rod. The during operation, driving motor drive screw drive mechanism operation, screw-nut rectilinear movement forward for synchronous mobile rod and slide set up two direction sliders on the synchronous mobile rod rectilinear movement forward simultaneously, at this moment, because two direction sliders receive the direction restraint in first guide rail groove and second guide rail groove respectively in rectilinear movement forward, consequently, two direction sliders are close to along first guide rail groove and second guide rail groove respectively gradually, thereby make two ball cover of being fixed connection respectively with two direction sliders and be close to the removal each other, open whole safety cover gradually, so that unmanned aerial vehicle takes off and descends.
According to a preferable scheme of the utility model, an arc-shaped fixing groove with an upward opening is arranged in the fixing frame, the two spherical masks are arranged on the fixing frame, the bottoms of the two spherical masks correspond to the opening parts of the fixing groove, and the radius of the fixing groove is the same as that of the two spherical masks; the first driving mechanisms are divided into two groups, each group of first driving mechanisms is composed of a gear rack transmission mechanism and a driving motor, gears of the gear rack transmission mechanisms are connected with a main shaft of the driving motor, and racks are arranged inside the spherical mask. Like this, when opening the safety cover, two spherical covers just can be in indentation fixed slots, bury inside the mount for whole shut down platform exposes completely, exposes under the sky, is favorable to unmanned aerial vehicle's the perpendicular take-off of going on smoothly and descends, and simultaneously, two spherical covers can bury in the fixed slot, save space more.
The utility model discloses a preferred scheme, the bottom of a plurality of ball face guards of safety cover is all rotated and is connected on the mount, and every ball face guard all is spherical triangle's petal form. All the spherical covers are driven by the first driving mechanism to rotate outwards or inwards at the same time, so that the protective covers are opened or closed.
Compared with the prior art, the utility model following beneficial effect has:
1. the utility model discloses a safety cover is opened or closed in the motion of spherical cover, thereby makes unmanned aerial vehicle take off smoothly and descend, easy operation to whole take off and land platform is little at during operation occupation space, and need not increase complementary unit, is particularly useful for in the outdoor environment in plant protection farmland.
2. Through hemispherical safety cover to leave unmanned aerial vehicle in confined indoor environment, be convenient for to unmanned aerial vehicle's maintenance, charge and take off and land, and aesthetic in appearance.
3. The utility model discloses a direct drive ball face guard motion just can realize opening or closing of safety cover to realize taking off and descending of unmanned aerial vehicle, control is simple.
Drawings
Fig. 1-3 are schematic structural diagrams of a first embodiment of the unmanned aerial vehicle take-off and landing platform with the enclosure of the present invention, wherein fig. 1 is a perspective view of the movable cover after being opened (not completely opened), fig. 2 is a perspective view of another viewing angle after the movable cover is opened (the transmission mode of the first driving mechanism is not shown), and fig. 3 is a perspective view of the movable cover after being closed.
Fig. 4 is a schematic diagram of a top view structure of the charging mechanism (a dotted circle is a schematic diagram of a landing range of the unmanned aerial vehicle).
Fig. 5 is a simplified structural diagram of a shutdown platform in a second embodiment of the unmanned aerial vehicle take-off and landing platform with an outer cover of the present invention.
Fig. 6-7 are schematic diagrams illustrating a top view of a fixed frame and a first driving mechanism in a third embodiment of the unmanned aerial vehicle take-off and landing platform with a housing, wherein fig. 6 is a schematic diagram illustrating a structure that the protection cover is in a closed state, and fig. 7 is a schematic diagram illustrating a structure that the protection cover is in an open state (not fully opened).
Fig. 8-9 are schematic front views of a fourth embodiment of the unmanned aerial vehicle take-off and landing platform with a cover, where fig. 8 is a schematic structural diagram of the protective cover in a closed state, and fig. 9 is a schematic structural diagram of the protective cover in an open state (not fully opened).
Fig. 10-12 are schematic structural diagrams of a fifth embodiment of the unmanned aerial vehicle take-off and landing platform with a cover, wherein fig. 10 is a schematic structural diagram of the protective cover in a closed state, fig. 11 is a schematic structural diagram of the protective cover in an open state, and fig. 12 is a schematic side view.
Fig. 13-15 are schematic structural diagrams of a sixth embodiment of the unmanned aerial vehicle take-off and landing platform with a cover, where fig. 13 is a schematic front-view structural diagram of the protective cover in a closed state, fig. 14 is a schematic front-view structural diagram of the protective cover in an open state, and fig. 15 is a schematic top-view structural diagram of the protective cover in a closed state.
Detailed Description
The present invention will be further described with reference to the following examples and drawings, but the embodiments of the present invention are not limited thereto.
Example 1
Referring to fig. 1 to 3, the unmanned aerial vehicle take-off and landing platform with the outer cover of the embodiment includes a fixing frame, a protective cover of a hemispherical outer cover, and a stopping platform 4 arranged in the protective cover; the bottom of the protective cover is arranged on the fixed frame, the shutdown platform 4 is arranged in the middle of the fixed frame, and the protective cover is composed of two spherical covers; the first driving mechanism 5 is used for driving one spherical cover to rotate around the vertical side of the protective cover to one side of the other spherical cover so as to open the protective cover; and a second driving mechanism for driving the shutdown platform 4 to rotate around the axis is arranged in the protective cover. In this embodiment, the safety cover is half spherical structure, two ball cover are quarter sphere, close when combining when two ball cover, form a hemispherical closed spherical structure, make unmanned aerial vehicle be in the confined indoor environment. In addition, it should be noted that "hemisphere" is not limited to strict half hemisphere, but may be greater than half or less than half incomplete spheroid, and the sphere of disappearance is located the bottom, and the purpose is convenient for be connected with the mount, and such safety cover can protect unmanned aerial vehicle equally, belong to the definition of "hemisphere" of the utility model.
Referring to fig. 1 to 3, the fixing frame includes a base 3 and a connecting seat 5 disposed on the base 3; the connecting seat 5 is annular, and a guide groove 10 is formed in the connecting seat 5; among two ball face guards of safety cover, one of them is movable cover 2, and another is fixed cover 1, movable cover 2 slides and sets up in guide way 10, fixed cover 1 is fixed to be set up on connecting seat 5, movable cover 2 is less than fixed cover 1, a actuating mechanism 5 is connected with movable cover 2. When the unmanned aerial vehicle needs to land, the first driving mechanism 5 drives the movable cover 2 to slide to one side of the fixed cover 1 along the guide groove 10, is positioned in the fixed cover 1 and is attached to the inner wall of the fixed cover, so that the landing position of the shutdown platform 4 is exposed to wait for the landing of the unmanned aerial vehicle; when the safety cover is closed to needs, the 5 drive safety covers of first actuating mechanism reset and remove, form a hemispherical safety cover with 1 concatenation of fixed cover, realize the protection to unmanned aerial vehicle. Through the setting of the base 3 of mount for whole take-off and landing platform has certain distance with ground, ensures that unmanned aerial vehicle parks in dry environment, is favorable to depositing of unmanned aerial vehicle.
Referring to fig. 2, the first driving mechanism 5 is composed of a motor and a toothed chain transmission mechanism, and the toothed chain transmission mechanism comprises a transmission gear 7 and a transmission rack 8; the motor is arranged in the protective cover, the transmission gear 7 is connected with a driving shaft of the motor, and the transmission rack 8 is arranged in the movable cover 2 in a surrounding mode and is connected with the transmission gear 7 in a matching mode. Through the matching of the gear and the rack, the movable cover 2 can be driven to rotate by a certain angle under the driving of the motor according to the taking-off and landing conditions of the field unmanned aerial vehicle, so that the size control of a flight channel is realized; in actual unmanned aerial vehicle's the in-process of taking off and land, if open whole movable cover 2 completely, half has just been opened in whole hemispherical safety cover in other words, nevertheless to specific unmanned aerial vehicle's descending, probably only need movable cover 2 open half, the quarter of whole safety cover promptly can, consequently, adopt tooth chain drive, just can adjust the size of flight passageway according to unmanned aerial vehicle's the circumstances of taking off and land, when certain unmanned aerial vehicle takes off or descends, still can provide best indoor protection to other unmanned aerial vehicles who park at the safety cover, especially in rainy day or other bad weather.
In this embodiment, the bottom of the movable cover 2 may be provided with a plurality of pulleys, the plurality of pulleys are connected with the movable cover 2 through a connecting block, the connecting block is rotatably connected with the bottom of the movable cover 2, and the pulleys are embedded in the guide groove 10 in a matching manner. Through the arrangement of the pulley, the movement of the movable hood 2 is smoother, and the friction between the movable hood 2 and the guide groove 10 can be reduced.
Referring to fig. 1 and 2, the stopping platform 4 is circular, the bottom of the stopping platform 4 is rotatably connected to the base 3 through a support shaft 9, and the second driving mechanism is connected to the support shaft 9. Set up circular shape and shut down platform 4, be favorable to descending more unmanned aerial vehicles.
The stop platform 4 is provided with a reference mark 22 so that the unmanned aerial vehicle can land. And the fixed frame and the shutdown platform 4 are provided with illuminating lamps. Can be convenient for unmanned aerial vehicle like this look for the position of shutting down platform 4 night, be favorable to accurate descending. In addition, because the safety cover is hemispherical, consequently, when unmanned aerial vehicle returned to navigate and descend, earlier hemispherical safety cover as the reference sign to look for whole unmanned aerial vehicle take off and land the specific position of platform fast, look for the discernment again to reference sign 22 on the platform of shutting down 4, carry out accurate descending.
In practical application, a rotation driving mechanism for driving the two spherical masks to rotate simultaneously can be arranged according to actual requirements; the connecting seat is rotatably connected to the base; the rotation driving mechanism is composed of a servo motor and a gear rack mechanism, the servo motor is fixedly arranged on the base, a rack of the gear rack mechanism is arranged on the connecting seat in a surrounding mode, and a gear of the gear rack mechanism is connected with a power shaft of the servo motor and is arranged in a matching mode with a rack of the gear rack mechanism. Through setting up rotation actuating mechanism, can drive two spherical covers simultaneously and rotate after the safety cover is opened to change the flight passageway's after the safety cover is opened position, and then realize shutting off the unmanned aerial vehicle's of the different positions on the platform takeoff.
Referring to fig. 4, two groups of charging mechanisms are provided in the embodiment, and are both disposed at the bottom of the shutdown platform 4, each charging mechanism includes two charging buckles 25 and a charging driving mechanism that drives the two charging buckles 25 to approach or separate from each other, and the two charging buckles 25 are respectively connected to the positive electrode and the negative electrode of the charging power supply; the charging driving mechanism consists of a charging motor 23 and a bidirectional screw transmission mechanism, a bidirectional screw 24 of the bidirectional screw transmission mechanism is connected with a main shaft of the charging motor 23, and the two charging buckles 25 are respectively arranged on two screw sliders 27 of the bidirectional screw transmission mechanism; and an avoiding groove 26 for avoiding the movement of the two charging buckles 25 is arranged on the stopping platform 4. Because the charging contact position of the unmanned aerial vehicle is arranged on the frame, when the unmanned aerial vehicle lands on the shutdown platform according to the reference mark 22 and the frame of the unmanned aerial vehicle is positioned between the two charging buckles 25; two buckles 25 that charge of charging motor 23 drive are close to each other for two buckles 25 that charge contact position contact with charging in the unmanned aerial vehicle frame respectively, realize charging, and after the completion of charging, two buckles 25 that charge of charging motor 23 drive reverse movement each other leave the unmanned aerial vehicle frame can, design benefit realizes automatic charging.
Referring to fig. 1-3, the working principle of the unmanned aerial vehicle take-off and landing platform with the outer cover of the embodiment is as follows:
when the unmanned aerial vehicle needs to return to the home and land, the first driving mechanism 5 drives one of the spherical masks to rotate, so that the protective cover is opened, a part of the shutdown platform 4 in the protective cover is exposed in the sky, and a flight channel for the unmanned aerial vehicle to take off and land vertically is formed; the unmanned aerial vehicle lands on the shutdown platform 4 through a flight channel formed after the spherical cover rotates according to the planned route, and the landing of the unmanned aerial vehicle is completed; subsequently, if other unmanned aerial vehicles need to continue to land, the second driving mechanism drives the stopping platform 4 to rotate, so that the vacant position of the stopping platform 4 rotates to one side corresponding to the flight channel, and the next unmanned aerial vehicle lands on the stopping platform 4; or two spherical covers are driven to rotate simultaneously through the rotation driving mechanism, so that the flying channel corresponds to other vacant positions of the shutdown platform, and the unmanned aerial vehicle can fly conveniently. Accomplish unmanned aerial vehicle's descending back, the corresponding spherical cover of 5 drive of first actuating mechanism is back rotated to 4 closed protections of stopping the platform with whole in whole safety cover. When unmanned aerial vehicle takes off, ball face guard of 5 continuous drive of first actuating mechanism rotates, forms the flight passageway, in addition, can shut down platform 4 through the drive of second actuating mechanism and rotate (or rotate two ball face guards of actuating mechanism drive and rotate) according to unmanned aerial vehicle's the order of taking off to the unmanned aerial vehicle that will take off rotates the department that corresponds with the flight passageway, so that unmanned aerial vehicle takes off.
Example 2
Referring to fig. 5, the present embodiment is different from embodiment 1 in that: the number of the shutdown platforms 4 is multiple, the shutdown platforms 4 are arranged in a vertical direction, the number of the second driving mechanisms is multiple, and the second driving mechanisms correspond to the shutdown platforms 4 one by one; each shutdown platform 4 is provided with two groups of charging mechanisms; wherein, all be equipped with transition breach 21 on a plurality of platforms 4 of shutting down, the platform 4 of shutting down that is located the lowest layer can not set up transition breach 21 to park more unmanned aerial vehicles. Each shutdown platform 4 is provided with a plurality of reference marks 22, in this embodiment, the lowest shutdown platform 4 is provided with four reference marks 22, and the rest shutdown platforms are provided with three reference marks 22. A plurality of shutdown platforms 4 are arranged, so that the whole take-off and landing platform can store more unmanned aerial vehicles; when needing take off and land unmanned aerial vehicle, all transition breach 21 of shutting down platform 4 are aimed at, form unified take off and land passageway, when the unmanned aerial vehicle on the platform 4 of shutting down of certain layer takes off or lands on this layer of shutting down platform 4, and the second actuating mechanism that is corresponding with this layer of shutting down platform 4 drives the position of shutting down and falls and rotate to the department that corresponds with transition passageway to the realization takes off or lands.
Example 3
Referring to fig. 6 and 7, the present embodiment is different from embodiment 1 in that: a first guide rail groove 15 and a second guide rail groove 16 are formed in the connecting seat 5 of the fixing frame, and the first guide rail groove 15 and the second guide rail groove 16 are arranged in an inscribed mode; the two ball masks 11 are respectively arranged in a first guide rail groove 15 and a second guide rail groove 16; the first driving mechanism comprises a transmission motor 13, a screw rod transmission mechanism and a synchronous transmission mechanism, wherein the synchronous transmission mechanism comprises a synchronous moving rod 12 and two guide sliders 18, the two guide sliders 18 are slidably arranged on the synchronous moving rod 12 and are respectively arranged in a first guide rail groove 15 and a second guide rail groove 16, the two spherical masks 11 are respectively and fixedly connected with the corresponding guide sliders 18, and the bottom of the connecting seat 5 is provided with an avoiding groove for avoiding the movement of the synchronous moving rod 12; the screw 14 of the screw transmission mechanism is connected with the power output shaft of the transmission motor 13, and the screw nut 17 of the screw transmission mechanism is fixedly connected with the synchronous moving rod 12. The during operation, the operation of drive motor 13 drive screw drive mechanism, screw-nut 17 rectilinear movement forward for synchronous mobile rod 12 and slide set up two guide slider 18 on the synchronous mobile rod 12 rectilinear movement forward simultaneously, at this moment, because two guide slider 18 when rectilinear movement forward, receive the direction restraint of first guide rail groove 15 and second guide rail groove 16 respectively, consequently, two guide slider 18 are close to along first guide rail groove 15 and second guide rail groove 16 respectively gradually, thereby make two ball cover 11 of two guide slider 18 difference fixed connection be close to each other and remove, open whole safety cover gradually, so that unmanned aerial vehicle takes off and descends.
Example 4
Referring to fig. 8 and 9, the present embodiment is different from embodiment 1 in that: an arc-shaped fixing groove 19 with an upward opening is formed in the fixing frame, the two spherical masks 11 are arranged on the fixing frame, the bottoms of the two spherical masks 11 correspond to the opening parts of the fixing groove 19, and the fixing groove 19 and the two spherical masks 11 have the same radius; the first driving mechanisms are divided into two groups, each group of the first driving mechanisms is composed of a gear rack transmission mechanism and a driving motor, a gear 20 of the gear rack transmission mechanism is connected with a main shaft of the driving motor, and the racks are arranged inside the spherical mask 11. Like this, when opening the safety cover, driving motor passes through gear drive rack motion for ball face guard 11 is to fixed slot 19 internal motion, and two final ball face guards 11 just can be in indentation fixed slot 19, bury inside the mount, make whole shut down platform 4 completely expose, are favorable to unmanned aerial vehicle's taking off smoothly and descending, and simultaneously, two ball face guards 11 can bury in fixed slot 19, save space more.
Example 5
Referring to fig. 10 to 12, the present embodiment is different from embodiment 1 in that the protective cover is composed of a plurality of spherical masks 11, the spherical masks 11 are divided into two groups symmetrically arranged, each group includes a plurality of spherical masks 11, the radii of the plurality of spherical masks 11 in each group increase sequentially from inside to outside, both ends of the plurality of spherical masks 11 are rotatably connected to the base 3, and the axes of the rotating shafts at the rotating connection portions are horizontally arranged. In an initial state, the protective cover is in a closed state, each group of spherical covers forms a half of the protective cover, and a plurality of spherical covers in each group of spherical covers are sequentially arranged from bottom to top; when the unmanned aerial vehicle takeoff device is opened, the first driving mechanism drives the spherical masks 11 to rotate downwards around the rotating shafts rotationally connected with the base 3 (the spherical masks 11 positioned at the lowest part can also be kept still), the rotating directions of the spherical masks 11 in the two groups of spherical masks are opposite, the postures of respectively rotating and opening from the middle to the two sides are formed, after the spherical masks 11 are opened, the spherical masks 11 with larger radius cover the spherical masks 11 with smaller radius adjacent to the spherical masks, and finally, the spherical masks 11 are overlapped from inside to outside according to the radius, so that the shutdown platform 4 is fully exposed, and the unmanned aerial vehicle takeoff is facilitated. Like this open the back at the guard shield, whole shut down platform 4 accomplishes to expose for all stop and land unmanned aerial vehicle on shutting down platform 4 can take off or descend in proper order fast, are favorable to improving unmanned aerial vehicle's taking off or landing speed. In addition, when the protective cover is closed, the first driving mechanism drives the plurality of ball masks 11 to rotate along the direction opposite to the opening direction, so that the protective cover can be closed.
Example 6
Referring to fig. 13 to 15, the present embodiment is different from embodiment 1 in that the bottoms of the plurality of spherical masks 11 of the protective cover are rotatably connected to the fixing frame, and each spherical mask 11 has a petal shape of a spherical triangle. All ball face guards 11 are driven to rotate outwards or rotate inwards simultaneously through a first driving mechanism, the opening or closing of the protective cover is realized, the opening and closing processes of the protective cover are similar to the opening and closing of petals, and a flight channel formed during opening is positioned right above the center of the protective cover, so that the unmanned aerial vehicle can take off and land conveniently. The ball mask 11 is typically three or four.
The above is the preferred embodiment of the present invention, but the embodiment of the present invention is not limited by the above, and any other changes, modifications, substitutions, combinations, and simplifications which do not depart from the spirit and principle of the present invention should be equivalent replacement modes, and all are included in the scope of the present invention.
Claims (10)
1. An unmanned aerial vehicle taking-off and landing platform with an outer cover is characterized by comprising a fixed frame, a hemispherical protective cover and a stopping platform arranged in the protective cover; the bottom of the protective cover is arranged on the fixed frame, the shutdown platform is arranged in the middle of the fixed frame, the protective cover comprises a plurality of petal-shaped spherical covers, and the plurality of petal-shaped spherical covers are combined together to form the hemispherical protective cover in a closed state; the first driving mechanism is used for driving at least one spherical mask to move so that the hemispherical protective cover is opened to expose the shutdown platform.
2. An unmanned aerial vehicle take-off and landing platform with a cover according to claim 1, wherein the protective cover comprises two spherical covers, and one of the spherical covers rotates around a vertical center line of the protective cover to one side of the other spherical cover to open the protective cover or both spherical covers rotate around the vertical center line of the protective cover in opposite directions to open the protective cover under the drive of the first driving mechanism.
3. The unmanned aerial vehicle take-off and landing platform with an enclosure of claim 2, wherein the fixing frame comprises a base and a connecting seat arranged on the base; the connecting seat is annular and is provided with a guide groove; among two ball face guards of safety cover, one of them is the movable cover, and another is fixed cover, the movable cover slides and sets up in the guide way, fixed cover is fixed to be set up on the connecting seat, the movable cover is less than fixed cover, a actuating mechanism is connected with the movable cover.
4. An unmanned aerial vehicle take-off and landing platform with a cover according to any one of claims 1-3, wherein a second driving mechanism for driving the shutdown platform to rotate around the axis is arranged in the cover; the shutdown platform is circular, the bottom of the shutdown platform is rotatably connected to the fixing frame through the supporting shaft, and the second driving mechanism is connected with the supporting shaft.
5. An unmanned aerial vehicle take-off and landing platform with a housing according to claim 4, wherein the number of the shutdown platforms is multiple, and the multiple shutdown platforms are arranged in a vertical direction; the number of the second driving mechanisms is multiple, and the multiple second driving mechanisms correspond to the multiple shutdown platforms one to one; wherein, all be equipped with the transition breach on a plurality of platforms of shutting down.
6. An unmanned aerial vehicle take-off and landing platform with a housing as claimed in claim 3, further comprising a rotation driving mechanism for driving two spherical masks to rotate simultaneously; the connecting seat is rotatably connected to the base; the rotation driving mechanism is composed of a servo motor and a gear rack mechanism, the servo motor is fixedly arranged on the base, and a rack of the gear rack mechanism is arranged on the connecting seat in a surrounding mode; and a gear of the gear rack mechanism is connected with a power shaft of the servo motor and is matched with a rack of the gear rack mechanism.
7. The unmanned aerial vehicle take-off and landing platform with the outer cover according to claim 1, wherein a charging mechanism is arranged at the bottom of the parking platform, and comprises two charging buckles and a charging driving mechanism for driving the two charging buckles to approach or separate from each other, and the two charging buckles are respectively connected with the positive electrode and the negative electrode of a charging power supply; the charging driving mechanism consists of a charging motor and a bidirectional screw transmission mechanism, a bidirectional screw of the bidirectional screw transmission mechanism is connected with a main shaft of the charging motor, and the two charging buckles are respectively arranged on two screw sliders of the bidirectional screw transmission mechanism; and an avoiding groove for avoiding the movement of the two charging buckles is arranged on the stopping platform.
8. An unmanned aerial vehicle take-off and landing platform with a housing according to claim 3, wherein a first guide rail groove and a second guide rail groove are formed in the connecting base of the fixing frame, and the first guide rail groove and the second guide rail groove are arranged in an inscribed mode; the two spherical covers are respectively arranged in the first guide rail groove and the second guide rail groove; the first driving mechanism comprises a transmission motor, a screw rod transmission mechanism and a synchronous transmission mechanism, wherein the synchronous transmission mechanism comprises a synchronous moving rod and two guide sliders, the two guide sliders are arranged on the synchronous moving rod in a sliding mode and are respectively arranged in a first guide rail groove and a second guide rail groove, the two spherical covers are respectively and fixedly connected with the corresponding guide sliders, and an avoiding groove for avoiding the synchronous moving rod to move is formed in the bottom of the connecting seat; and a screw rod of the screw rod transmission mechanism is connected with a power output shaft of the transmission motor, and a screw rod nut of the screw rod transmission mechanism is fixedly connected with the synchronous moving rod.
9. The unmanned aerial vehicle take-off and landing platform with the outer cover according to claim 2 or 3, wherein an arc-shaped fixing groove with an upward opening is formed in the fixing frame, the two spherical masks are arranged on the fixing frame, the bottoms of the two spherical masks correspond to the opening parts of the fixing groove, and the fixing groove and the two spherical masks have the same radius; the first driving mechanisms are divided into two groups, each group of first driving mechanisms is composed of a gear rack transmission mechanism and a driving motor, gears of the gear rack transmission mechanisms are connected with a main shaft of the driving motor, and racks are arranged inside the spherical mask.
10. An unmanned aerial vehicle take-off and landing platform with a cover according to claim 1, wherein the bottom portions of the plurality of spherical masks of the protective cover are rotatably connected to the fixing frame, and each spherical mask is in a petal shape of a spherical triangle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921229040.8U CN210653683U (en) | 2019-07-31 | 2019-07-31 | Take unmanned aerial vehicle platform of taking off and land of dustcoat |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921229040.8U CN210653683U (en) | 2019-07-31 | 2019-07-31 | Take unmanned aerial vehicle platform of taking off and land of dustcoat |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210653683U true CN210653683U (en) | 2020-06-02 |
Family
ID=70842851
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921229040.8U Active CN210653683U (en) | 2019-07-31 | 2019-07-31 | Take unmanned aerial vehicle platform of taking off and land of dustcoat |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210653683U (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111717408A (en) * | 2020-06-29 | 2020-09-29 | 山东科技大学 | Marine launching platform capable of bearing multiple unmanned aerial vehicles |
| CN112109915A (en) * | 2020-09-23 | 2020-12-22 | 同济大学 | Carousel formula unmanned aerial vehicle system of accomodating |
| JP6902308B1 (en) * | 2021-03-02 | 2021-07-14 | 株式会社エアロネクスト | Port, mobile, multiple port installation method |
| CN113575386A (en) * | 2021-07-26 | 2021-11-02 | 李柯 | Gardens irrigation equipment based on thing networking |
| CN113605768A (en) * | 2021-09-14 | 2021-11-05 | 江苏功业互联科技有限公司 | Can hold three-dimensional hangar of intelligence of many sizes unmanned aerial vehicle |
| CN114160401A (en) * | 2021-11-29 | 2022-03-11 | 湖南康捷生物科技有限公司 | Lipase equipment that sieves with prevent flying dirt structure |
| CN117554927A (en) * | 2024-01-11 | 2024-02-13 | 中国航天三江集团有限公司 | Follow-up spherical protection system |
-
2019
- 2019-07-31 CN CN201921229040.8U patent/CN210653683U/en active Active
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111717408A (en) * | 2020-06-29 | 2020-09-29 | 山东科技大学 | Marine launching platform capable of bearing multiple unmanned aerial vehicles |
| CN112109915A (en) * | 2020-09-23 | 2020-12-22 | 同济大学 | Carousel formula unmanned aerial vehicle system of accomodating |
| CN112109915B (en) * | 2020-09-23 | 2022-06-14 | 同济大学 | Carousel formula unmanned aerial vehicle system of accomodating |
| JP6902308B1 (en) * | 2021-03-02 | 2021-07-14 | 株式会社エアロネクスト | Port, mobile, multiple port installation method |
| WO2022186026A1 (en) * | 2021-03-02 | 2022-09-09 | 株式会社エアロネクスト | Port, mobile object, and method for installing plurality of ports |
| JP2022133543A (en) * | 2021-03-02 | 2022-09-14 | 株式会社エアロネクスト | Port, mobile object, and method for installing multiple ports |
| CN113575386A (en) * | 2021-07-26 | 2021-11-02 | 李柯 | Gardens irrigation equipment based on thing networking |
| CN113605768A (en) * | 2021-09-14 | 2021-11-05 | 江苏功业互联科技有限公司 | Can hold three-dimensional hangar of intelligence of many sizes unmanned aerial vehicle |
| CN114160401A (en) * | 2021-11-29 | 2022-03-11 | 湖南康捷生物科技有限公司 | Lipase equipment that sieves with prevent flying dirt structure |
| CN117554927A (en) * | 2024-01-11 | 2024-02-13 | 中国航天三江集团有限公司 | Follow-up spherical protection system |
| CN117554927B (en) * | 2024-01-11 | 2024-04-09 | 中国航天三江集团有限公司 | Follow-up spherical protection system |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN210653683U (en) | Take unmanned aerial vehicle platform of taking off and land of dustcoat | |
| CN107444101B (en) | A kind of unmanned platform of all-wheel steering by In-wheel motor driving | |
| US20170158353A1 (en) | Remote Aerodrome for UAVs | |
| CN209617531U (en) | A kind of unmanned plane electric charging pool device | |
| CN111422369B (en) | Unmanned aerial vehicle automatic airport and control method | |
| CN209875003U (en) | Multipurpose sun-shading device | |
| CN113148205A (en) | Complicated topography mapping device convenient to unmanned aerial vehicle carries | |
| CN108556577B (en) | Air-ground dual-purpose spherical robot | |
| CN108629321A (en) | A kind of face recognition device that shooting effect is good | |
| CN210681182U (en) | Composite wing unmanned aerial vehicle shuts down strorage device | |
| CN114110328A (en) | Forest vegetation dynamic change monitoring devices based on remote sensing image technique | |
| CN101836560A (en) | Continuous production test device of fresh plant food under simulated space microgravity effect | |
| CN105526914B (en) | A kind of six degree of freedom aviation oblique photograph simulation system | |
| CN211422014U (en) | Unmanned aerial vehicle deposits charging device | |
| CN112173152A (en) | Composite wing unmanned aerial vehicle shuts down strorage device | |
| CN113815877A (en) | Unmanned aerial vehicle basic station | |
| CN114084365A (en) | Mechanism and method for centering aircraft nest of unmanned aerial vehicle | |
| CN216424767U (en) | Lighting device for unmanned aerial vehicle | |
| CN113619802A (en) | Four-rotor unmanned aerial vehicle under multi-constraint condition | |
| CN206734648U (en) | A kind of multi-angle VR takes photo by plane unmanned plane | |
| CN217811864U (en) | Suspension open-close type astronomical dome | |
| CN111776210A (en) | Unmanned aerial vehicle is with protection casing that has scalable regulation | |
| CN217185481U (en) | View facility based on 3D model show | |
| CN214165324U (en) | Unmanned aerial vehicle night measurement direction guide device | |
| CN114180062B (en) | Multifunctional surveying and mapping unmanned aerial vehicle for surveying and mapping geographic information |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |