CN117508703A - Intelligent landing platform and machine library thereof - Google Patents
Intelligent landing platform and machine library thereof Download PDFInfo
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- CN117508703A CN117508703A CN202311295688.6A CN202311295688A CN117508703A CN 117508703 A CN117508703 A CN 117508703A CN 202311295688 A CN202311295688 A CN 202311295688A CN 117508703 A CN117508703 A CN 117508703A
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- landing
- base plate
- pushing
- intelligent
- unmanned aerial
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- 239000000758 substrate Substances 0.000 claims abstract description 12
- 230000000712 assembly Effects 0.000 claims description 26
- 238000000429 assembly Methods 0.000 claims description 26
- 230000006698 induction Effects 0.000 claims description 4
- 230000005540 biological transmission Effects 0.000 claims description 3
- 238000009434 installation Methods 0.000 abstract description 2
- 238000011897 real-time detection Methods 0.000 abstract 1
- 230000009977 dual effect Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
- 238000012876 topography Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U70/00—Launching, take-off or landing arrangements
- B64U70/90—Launching from or landing on platforms
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U80/00—Transport or storage specially adapted for UAVs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U80/00—Transport or storage specially adapted for UAVs
- B64U80/20—Transport or storage specially adapted for UAVs with arrangements for servicing the UAV
- B64U80/25—Transport or storage specially adapted for UAVs with arrangements for servicing the UAV for recharging batteries; for refuelling
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Transportation (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The invention discloses an intelligent landing platform, which comprises a landing substrate, wherein the landing substrate is used for supporting an unmanned aerial vehicle; the centering mechanism is used for pushing the unmanned aerial vehicle to the center position of the landing base plate; the space adjusting mechanism is used for adjusting the height of the landing base plate and enabling the landing base plate to be in a horizontal state all the time. This intelligence platform that falls, not influenced by mounted position, when the hangar box installation skew, angle sensor detects that the machine base plate that falls is in non-horizontal state, then coordinates the work through a plurality of electric putter of PLC controller control annular plate below, angle sensor real-time detection to make the machine base plate that falls be in horizontal state all the time, fine assurance unmanned aerial vehicle's steady landing.
Description
Technical Field
The patent application relates to the technical field of machine libraries, in particular to an intelligent machine landing platform and a machine library thereof.
Background
Unmanned aerial vehicles ("unmanned aerial vehicles"), abbreviated "UAV," are unmanned aerial vehicles that are operated by radio remote control devices and programmed control devices, or are operated autonomously, either entirely or intermittently, by an on-board computer. Unmanned aerial vehicles can be classified into military and civilian applications according to the field of application. For military purposes, unmanned aerial vehicles are classified into reconnaissance and drones. In civil aspect, the unmanned aerial vehicle is matched with industry 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 shooting, express delivery transportation, disaster relief, wild animal observation, infectious disease monitoring, mapping, news reporting, electric power inspection, disaster relief, video shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and the developed countries are also actively expanding the application of industries and developing unmanned aerial vehicle technologies.
Considering the problem of endurance and charging in unmanned aerial vehicle use, can be equipped with unmanned aerial vehicle hangar generally, and because in the field ground unevenness, present unmanned aerial vehicle hangar can't automatically regulated landing platform's angle, this leads to present hangar to hardly guarantee unmanned aerial vehicle's safe landing outdoor, this is also an important reason that restricts present mobile machine nest and uses.
Disclosure of Invention
In view of the above drawbacks of the prior art, an object of the present application is to provide an intelligent landing platform and a library thereof, which solve the above problems of the prior art.
In order to achieve the above purpose, the present invention provides the following technical solutions:
an intelligent landing platform, comprising:
the landing base plate is used for supporting the unmanned aerial vehicle;
the centering mechanism is used for pushing the unmanned aerial vehicle to the center position of the landing base plate;
the space adjusting mechanism is used for adjusting the height of the landing base plate and enabling the landing base plate to be in a horizontal state all the time.
Preferably, the centering mechanism comprises:
the pushing assemblies are arranged above the landing base plate, and the two pushing assemblies are arranged horizontally and vertically in a non-intersecting manner;
the number of the driving assemblies is two, the driving assemblies are in one-to-one correspondence with the pushing assemblies, and the driving assemblies are started to drive the pushing assemblies to push the unmanned aerial vehicle to the central position of the landing base plate.
Preferably, each group of pushing components comprises two pushing rods which are parallel and located at the edge above the landing base plate, the two pushing rods on the same pushing component are driven by the driving component to move in opposite directions to push the unmanned aerial vehicle to move towards the center of the landing base plate, two ends of each pushing rod are connected with mounting brackets extending towards the lower side of the landing base plate, the lower ends of the two mounting brackets located on the same side are movably mounted on the same sliding component, and the sliding component is mounted at the edge of the lower end of the landing base plate.
Preferably, the sliding assembly comprises a guide rail fixed at the lower end of the landing base plate, and two sliding blocks fixedly connected with the corresponding mounting brackets are connected to the guide rail in a sliding manner.
Preferably, the driving assembly comprises a speed reduction double-output shaft motor arranged at the lower end of the falling machine substrate, two side output ends of the speed reduction double-output shaft motor are in transmission connection with screw rods which are adjacent to any one of the two opposite guide rails and are arranged in parallel, moving blocks which are in one-to-one correspondence with sliding blocks on the adjacent guide rails are sleeved on the screw rods in a threaded mode, the two screw directions on the screw rods are oppositely arranged so that the two moving blocks move in opposite directions, the moving blocks are fixedly connected with the corresponding sliding blocks, and bearing seats which are fixed at the lower end of the falling machine substrate are arranged at the end parts of the screw rods.
Preferably, an angle sensor for detecting the inclination angle of the landing base plate is installed at the center of the lower end of the landing base plate.
Preferably, the lower end of the landing base plate is also provided with a plurality of induction sensors for detecting the position of the pushing rod on the pushing assembly.
Preferably, the horizontal adjustment mechanism comprises a triangle and an annular plate, a plurality of electric push rods for adjusting the landing base plate when the angle sensor detects that the landing base plate is at a non-horizontal position are arranged between the triangle and the annular plate, and the annular plate is fixedly connected to the lower end face of the landing base plate.
Preferably, the two ends of the electric push rod are connected with universal joints, and the lower end of the annular plate and the upper end of the triangular plate are connected with articulated joints which are in articulated matching with the corresponding universal joints.
A hangar comprising an intelligent landing platform as claimed in any preceding claim.
Compared with the prior art, the invention has the beneficial effects that: the intelligent landing platform is not influenced by the installation position, when the box body of the hangar is installed in a deflection mode, the angle sensor detects that the landing base plate is in a non-horizontal state, then the PLC controls the electric push rods below the annular plate to work in a coordinated mode, the angle sensor detects in real time, so that the landing base plate is always in a horizontal state, stable landing of the unmanned aerial vehicle is well guaranteed, and the influence of topography is small;
this intelligence platform that falls, when unmanned aerial vehicle falls on the base plate that falls, through being located the speed reduction double output shaft motor start of base plate lower extreme that falls, the lead screw rotates and drives two movable blocks of same group and move in opposite directions to make slider synchronous movement, drive the installing support and promote the catch bar and remove, make unmanned aerial vehicle arrive the central point of base plate that falls, make things convenient for subsequent trading electricity or charging.
Drawings
FIG. 1 is a schematic perspective view of an intelligent landing platform of the present invention;
FIG. 2 is a schematic perspective view of the centering mechanism of the present invention;
FIG. 3 is a schematic perspective view of the present invention from another perspective of FIG. 2;
FIG. 4 is a schematic perspective view of a horizontal adjustment mechanism according to the present invention;
fig. 5 is a schematic side view of the fig. 4 structure of the present invention.
Reference numerals illustrate: the automatic falling machine comprises a falling machine base plate 1, an angle sensor 11, an induction sensor 12, a centering mechanism 2, a pushing assembly 21, a pushing rod 211, a mounting bracket 212, a sliding assembly 213, a guide rail 2131, a sliding block 2132, a driving assembly 22, a speed reduction double-output shaft motor 221, a screw rod 222, a moving block 223, a horizontal adjusting mechanism 3, a triangular plate 31, an annular plate 32 and an electric push rod 33.
Detailed Description
Other advantages and effects of the present application will be readily apparent to those skilled in the art from the present disclosure, by describing embodiments of the present application with specific examples. This application is also intended to cover any adaptations or uses of various embodiments and can be practiced in different but specific details of the subject matter within the scope of the description and from various points of view. It should be noted that, in the case of no conflict, the embodiments and features in the embodiments may be combined with each other.
Referring to fig. 1-5, the present invention provides a technical solution:
an intelligent landing platform is shown in fig. 1, and comprises a landing base plate 1, a centering mechanism 2 and a space adjusting mechanism 3, wherein the landing base plate 1 is used for supporting an unmanned aerial vehicle; the centering mechanism 2 is used for pushing the unmanned aerial vehicle to the center position of the landing base plate 1; the space adjusting mechanism 3 is used for adjusting the height of the landing base plate 1 and keeping the landing base plate 1 in a horizontal state all the time.
Referring to fig. 2 and 3, the centering mechanism 2 includes two pushing assemblies 21 and a driving assembly 22, the number of the pushing assemblies 21 is two, the pushing assemblies 21 are located above the landing base plate 1, and the two pushing assemblies 21 are arranged horizontally and vertically in a non-intersecting manner; the number of the driving assemblies 22 is two, the driving assemblies 22 are in one-to-one correspondence with the pushing assemblies 21, and the driving assemblies 22 are started to drive the pushing assemblies 21 to push the unmanned aerial vehicle to the central position of the landing base plate 1.
As a preferred embodiment of the present disclosure, each group of pushing assemblies 21 includes two parallel pushing rods 211 located at the edge above the landing base plate 1, the two pushing rods 211 on the same pushing assembly 21 are driven by the driving assembly 22 to move in opposite directions to push the unmanned aerial vehicle to move towards the center of the landing base plate 1, two ends of the pushing rods 211 are connected with mounting brackets 212 extending towards the lower side of the landing base plate 1, the lower ends of the two mounting brackets 212 located on the same side are movably mounted on the same sliding assembly 213, and the sliding assembly 213 is mounted at the edge of the lower end of the landing base plate 1.
The sliding assembly 213 includes a guide rail 2131 fixed at the lower end of the landing base plate 1, and two sliding blocks 2132 respectively fixedly connected with the corresponding mounting brackets 212 are slidably connected to the guide rail 2131.
The driving assembly 22 includes a speed-reducing dual output shaft motor 221 installed at the lower end of the landing base plate 1, two side output ends of the speed-reducing dual output shaft motor 221 are in transmission connection with screw rods 222 adjacent to any one of two opposite guide rails 2231 and arranged in parallel, moving blocks 223 corresponding to the sliding blocks 2132 on the adjacent guide rails 2131 one by one are sleeved on the screw rods 222 in a threaded manner, spiral directions on the two screw rods 222 are oppositely arranged so that the two moving blocks 223 move in opposite directions, the moving blocks 223 are fixedly connected with the corresponding sliding blocks 2132, and bearing seats fixed at the lower end of the landing base plate 1 are installed at the end parts of the screw rods 222.
When the unmanned aerial vehicle falls on the landing base plate 1, the speed-reducing double-output shaft motor 221 positioned at the lower end of the landing base plate 1 is started, the screw rod 222 rotates to drive the two moving blocks 223 in the same group to move in opposite directions, so that the sliding blocks 2132 move synchronously, the mounting bracket 212 is driven to push the pushing rod 211 to move, the unmanned aerial vehicle reaches the central position of the landing base plate 1, subsequent power exchange or charging is facilitated, various devices are arranged on the lower end face of the landing base plate 1, the landing of the unmanned aerial vehicle is not influenced, and the space is saved.
As a preferred embodiment, an angle sensor 11 for detecting the inclination angle of the landing base plate 1 is installed at the center of the lower end of the landing base plate 1, and a plurality of induction sensors 12 for detecting the position of the push rod 211 on the push assembly 21 are also installed at the lower end of the landing base plate 1.
As a preferred embodiment, as shown in fig. 4, the horizontal adjustment mechanism 3 includes a triangle 31 and an annular plate 32, a plurality of electric push rods 33 are installed between the triangle 31 and the annular plate 32 to adjust the landing base plate 1 when the angle sensor 11 detects that the landing base plate 1 is at a non-horizontal position, and the annular plate 32 is fixedly connected to the lower end surface of the landing base plate 1. The electric putter 33 both ends all are connected with the universal joint, and the lower extreme of annular plate 32 and the upper end of set square 31 all are connected with the articulated joint that matches with corresponding universal joint is articulated. When the hangar box body is installed in a deflection mode, the angle sensor 11 detects that the landing base plate 1 is in a non-horizontal state, then the PLC controls the electric push rods 33 below the annular plate 32 to work in a coordinated mode, the angle sensor 11 detects in real time, so that the landing base plate 1 is always in a horizontal state, stable landing of the unmanned aerial vehicle is well guaranteed, and the influence of terrain is small.
Another embodiment of the present invention further provides a hangar, as shown in fig. 5, where the hangar includes the intelligent landing platform according to any one of the foregoing.
It should be noted that, the machine base is internally provided with a PLC controller, the PLC controller is a control device known to those skilled in the art, the PLC controller is installed inside the machine base, and the PLC controller controls the operation of each device by receiving the signals of the sensors, and further includes a server for performing cloud platform arrangement for issuing tasks, which are not described in detail herein.
The above-described embodiments are merely illustrative of the principles of the present application and their effectiveness, and are not intended to limit the present application. Modifications and variations may be made to the above-described embodiments by those skilled in the art without departing from the spirit and scope of the present application. Accordingly, it is intended that all equivalent modifications and variations which a person having ordinary skill in the art would accomplish without departing from the spirit and technical spirit disclosed in the present patent application shall be covered by the claims of the present patent application.
Claims (10)
1. An intelligent landing platform, which is characterized by comprising:
the landing machine comprises a landing machine substrate (1), wherein the landing machine substrate (1) is used for supporting an unmanned aerial vehicle;
the centering mechanism (2) is used for pushing the unmanned aerial vehicle to the center position of the landing base plate (1);
and the space adjusting mechanism (3) is used for adjusting the height of the landing base plate (1) and enabling the landing base plate (1) to be in a horizontal state all the time.
2. An intelligent landing platform according to claim 1, characterized in that the centering mechanism (2) comprises:
the pushing assemblies (21) are arranged in two groups, the pushing assemblies (21) are positioned above the landing base plate (1), and the two groups of pushing assemblies (21) are arranged in a horizontal and vertical disjoint mode;
the number of the driving assemblies (22) is two, the driving assemblies (22) are in one-to-one correspondence with the pushing assemblies (21), and the driving assemblies (22) are started to drive the pushing assemblies (21) to push the unmanned aerial vehicle to the center position of the landing base plate (1).
3. An intelligent landing platform according to claim 2, wherein each group of pushing assemblies (21) comprises two pushing rods (211) which are parallel and located at the edge above the landing base plate (1), the two pushing rods (211) on the same pushing assembly (21) are driven by the driving assembly (22) to move oppositely to push the unmanned aerial vehicle to move towards the central position of the landing base plate (1), two ends of each pushing rod (211) are connected with mounting brackets (212) extending towards the lower side of the landing base plate (1), the lower ends of the two mounting brackets (212) located on the same side are movably mounted on the same sliding assembly (213), and the sliding assembly (213) is mounted at the lower end edge of the landing base plate (1).
4. An intelligent landing platform according to claim 3, wherein the sliding assembly (213) comprises a guide rail (2131) fixed at the lower end of the landing base plate (1), and two sliding blocks (2132) fixedly connected with the corresponding mounting brackets (212) are slidably connected to the guide rail (2131).
5. The intelligent landing platform according to claim 4, wherein the driving assembly (22) comprises a speed-reducing double-output-shaft motor (221) installed at the lower end of the landing base plate (1), two side output ends of the speed-reducing double-output-shaft motor (221) are in transmission connection with screw rods (222) which are adjacent to any one of the two opposite guide rails (2231) and are arranged in parallel, moving blocks (223) which are in one-to-one correspondence with sliding blocks (2132) on the adjacent guide rails (2131) are sleeved on the screw rods (222) in a threaded manner, spiral directions on the two screw rods (222) are oppositely arranged so that the two moving blocks (223) move in opposite directions, the moving blocks (223) are fixedly connected with the corresponding sliding blocks (2132), and bearing seats which are fixed at the lower end of the landing base plate (1) are installed at the end parts of the screw rods (222).
6. The intelligent landing platform according to claim 5, wherein an angle sensor (11) for detecting the inclination angle of the landing substrate (1) is installed at the center of the lower end of the landing substrate (1).
7. The intelligent landing platform according to claim 5, wherein a plurality of induction sensors (12) for detecting the position of the pushing rod (211) on the pushing assembly (21) are further installed at the lower end of the landing substrate (1).
8. The intelligent landing platform according to claim 6, wherein the horizontal adjustment mechanism (3) comprises a triangular plate (31) and an annular plate (32), a plurality of electric push rods (33) for adjusting the landing substrate (1) when the angle sensor (11) detects that the landing substrate (1) is in a non-horizontal position are arranged between the triangular plate (31) and the annular plate (32), and the annular plate (32) is fixedly connected to the lower end face of the landing substrate (1).
9. The intelligent landing platform according to claim 8, wherein the two ends of the electric push rod (33) are connected with universal joints, and the lower end of the annular plate (32) and the upper end of the triangular plate (31) are connected with articulated joints which are in articulated matching with the corresponding universal joints.
10. A hangar comprising an intelligent landing platform according to any one of claims 1 to 9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202311295688.6A CN117508703A (en) | 2023-10-07 | 2023-10-07 | Intelligent landing platform and machine library thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202311295688.6A CN117508703A (en) | 2023-10-07 | 2023-10-07 | Intelligent landing platform and machine library thereof |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN117508703A true CN117508703A (en) | 2024-02-06 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202311295688.6A Pending CN117508703A (en) | 2023-10-07 | 2023-10-07 | Intelligent landing platform and machine library thereof |
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| Country | Link |
|---|---|
| CN (1) | CN117508703A (en) |
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2023
- 2023-10-07 CN CN202311295688.6A patent/CN117508703A/en active Pending
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