CN110654538B - Weather detection unmanned aerial vehicle - Google Patents
Weather detection unmanned aerial vehicle Download PDFInfo
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- CN110654538B CN110654538B CN201910815706.6A CN201910815706A CN110654538B CN 110654538 B CN110654538 B CN 110654538B CN 201910815706 A CN201910815706 A CN 201910815706A CN 110654538 B CN110654538 B CN 110654538B
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- 238000001514 detection method Methods 0.000 title claims abstract description 46
- 230000007246 mechanism Effects 0.000 claims abstract description 23
- 230000035939 shock Effects 0.000 claims description 20
- 230000005540 biological transmission Effects 0.000 claims description 8
- 238000010521 absorption reaction Methods 0.000 claims description 7
- 238000009434 installation Methods 0.000 abstract description 9
- 238000012423 maintenance Methods 0.000 abstract description 4
- 238000013016 damping Methods 0.000 description 14
- 238000010586 diagram Methods 0.000 description 5
- 230000000694 effects Effects 0.000 description 5
- 239000000725 suspension Substances 0.000 description 5
- 238000012544 monitoring process Methods 0.000 description 4
- 230000009471 action Effects 0.000 description 3
- 230000007547 defect Effects 0.000 description 3
- 238000013461 design Methods 0.000 description 3
- 238000003780 insertion Methods 0.000 description 3
- 230000037431 insertion Effects 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000008859 change Effects 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 238000012271 agricultural production Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
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- 230000002035 prolonged effect Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
- B64C27/14—Direct drive between power plant and rotor hub
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01W—METEOROLOGY
- G01W1/00—Meteorology
- G01W1/02—Instruments for indicating weather conditions by measuring two or more variables, e.g. humidity, pressure, temperature, cloud cover or wind speed
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01W—METEOROLOGY
- G01W1/00—Meteorology
- G01W1/14—Rainfall or precipitation gauges
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/35—UAVs specially adapted for particular uses or applications for science, e.g. meteorology
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Abstract
The invention discloses a meteorological detection unmanned aerial vehicle, which relates to the technical field of meteorological detection and comprises a machine body, wherein a mounting plate is fixedly arranged on the upper surface of the machine body, a battery bin is fixedly arranged on the lower surface of the machine body, four wings are equidistantly distributed on the outer side of the machine body in a circular array, a meteorological detector is fixedly arranged at the top of the mounting plate, a fixing plate is fixedly arranged at the bottom of the meteorological detector, and a fixing mechanism is arranged at the joint of the fixing plate and the mounting plate. The automatic opening and closing device is reasonable in structure and simple in operation, can realize automatic opening and closing of the bin cover, is convenient for installation of the battery, saves labor, effectively improves working efficiency, is high in practicability, can realize quick installation and disassembly of the meteorological detector through the arranged fixing mechanism, is convenient for maintenance and replacement of the meteorological detector, and can dismantle the meteorological detector when not in use to realize independent work of the unmanned aerial vehicle.
Description
Technical Field
The invention relates to the technical field of meteorological detection, in particular to a meteorological detection unmanned aerial vehicle.
Background
Weather has important influence on human life and agricultural production, a weather station is a main device for monitoring weather conditions, most of the weather stations are fixed on the ground at present, only some weather data near the ground can be monitored, and the weather data of high-altitude positions cannot be monitored, and manned fixed-wing aircrafts can acquire high-altitude weather data, but have the defects of high cost, short acquisition time, difficult flight path planning, few types of acquired data, high danger to aircrews in severe weather and the like.
In recent years, unmanned aerial vehicles are receiving more and more attention because of their advantages of being convenient and efficient, and unmanned aerial vehicles can carry on multiple platform and carry out various different operations, adopt unmanned aerial vehicle to carry out meteorological monitoring and are becoming a research focus. However in practical application, meteorological detection unmanned aerial vehicle is not only complicated in structure, and the function is comparatively single moreover, meteorological station and unmanned aerial vehicle have more passed through bolt fixed connection, the installation is dismantled and is wasted time and energy, bring inconvenience for its follow-up maintenance work, simultaneously, traditional meteorological detection unmanned aerial vehicle battery cang gai needs artifical manual opening, it is comparatively inconvenient to change the battery, work efficiency is lower, and the current meteorological detection unmanned aerial vehicle descending in-process easily produces vibrations phenomenon, its whole shock attenuation effect is relatively poor, unmanned aerial vehicle's life has been reduced. Therefore, the technical personnel in the field provide a meteorological detection unmanned aerial vehicle to solve the problems in the background art.
Disclosure of Invention
The invention aims to provide a meteorological detection unmanned aerial vehicle to solve the problems in the background technology.
In order to achieve the purpose, the invention provides the following technical scheme: the meteorological detection unmanned aerial vehicle comprises a machine body, wherein a mounting plate is fixedly mounted on the upper surface of the machine body, a battery bin is fixedly mounted on the lower surface of the machine body, four wings are equidistantly distributed on the outer side of the machine body in a circular array, a meteorological detector is fixedly mounted at the top of the mounting plate, a fixing plate is fixedly mounted at the bottom of the meteorological detector, a fixing mechanism is mounted at the joint of the fixing plate and the mounting plate, a driving motor is arranged at one end of each wing, a damping support leg is connected to the bottom end of each wing, and a propeller is mounted at the upper end of the driving; the fixing mechanism comprises a bottom plate, an inserting rod is installed in the lower end of the bottom plate in an embedded mode, a reset spring is arranged at the upper end of the inserting rod, a fixed rod is fixedly installed at the position, located at the upper surface of the bottom plate, of one side of the inserting rod, end covers are installed at the two ends of the reset spring, a limiting rod is fixedly installed at the top of the reset spring, a limiting groove is formed in one side of the limiting rod, a handle is connected to the outer side of the fixed rod in a rotating mode, and a bolt is arranged at the connecting position of the bottom plate.
As a further scheme of the invention: the meteorological detector and the fixed plate are of an integrally formed structure, and the fixed plate is fixedly connected with the mounting plate through a fixing mechanism.
As a still further scheme of the invention: the lower extreme of meteorological detector installs the connecting block, the upper end of connecting block is provided with the detection portion, the internally mounted of detection portion has the sensor, and the top of detection portion installs the rainfall detector.
As a still further scheme of the invention: the sensor is any one or more of a temperature sensor, a humidity sensor, an air pressure sensor and an PM. sensor, and a wind speed and direction sensor is arranged at the joint of the detection part and the rainfall detector.
As a still further scheme of the invention: the fixing mechanisms are four in number and are distributed at four corners of the fixing plate in a rectangular shape.
As a still further scheme of the invention: the fixing mechanism is fixedly connected with the fixing plate through a bolt, the inserted bar is fixedly connected with the limiting rod through a reset spring, and the fixing rod is connected with the limiting rod through a handle and a limiting groove in a clamping mode.
As a still further scheme of the invention: the front side of battery compartment is provided with the cang gai, and the dwang is installed with the junction of cang gai to the battery compartment, the inside of battery compartment is provided with the sliding plate, and the bottom of battery compartment has seted up the spout, one side fixed mounting of battery compartment has micro motor, the lower surface mounting of sliding plate has the slider, and the top of sliding plate is provided with the standing groove, the both sides of dwang all are provided with first gear, the inboard position department that micro motor's one end is located the battery compartment is connected with the pivot, the outside cover of pivot is equipped with the second gear, driving belt is installed with the junction of first gear to the second gear, and one side of second gear is provided with the third gear, the below fixed mounting of third gear has the rack.
As a still further scheme of the invention: the bin cover is rotatably connected with the battery bin through a rotating rod, the sliding plate is slidably connected with the battery bin through a sliding groove and a sliding block, the micro motor is rotatably connected with the second gear through a rotating shaft, the second gear is in transmission connection with the first gear through a transmission belt, and the rotating shaft is in meshing connection with the rack through a third gear.
As a still further scheme of the invention: the lower extreme of shock attenuation landing leg is provided with the bottom suspension strut, the shock attenuation pole is installed in the upper end embedding of bottom suspension strut, the top fixed mounting of shock attenuation pole has last supporting part, and the outside cover of shock attenuation pole is equipped with damping spring, go up supporting part and bottom suspension strut and pass through damping spring fixed connection.
Compared with the prior art, the invention has the beneficial effects that:
1. according to the automatic opening and closing device, the rotating shaft drives the second gear to rotate through the operation of the arranged micro motor, and then the transmission belt drives the first gear to rotate, so that the rotating rod drives the bin cover to rotate, meanwhile, the rotating shaft drives the third gear to rotate, and then the battery bin is driven to move outwards along the sliding groove through the rack, so that the bin cover is opened and closed automatically, the defects that the traditional unmanned aerial vehicle battery is time-consuming and labor-consuming in manual installation are overcome, the battery installation work is convenient to carry out, the design structure is simple, the operation is convenient, the manpower is saved, the working efficiency is effectively improved, and the practicability is high.
2. According to the invention, through the arranged fixing mechanism, the rapid mounting and dismounting work of the weather detector can be realized, the maintenance and replacement processing of the weather detector can be conveniently carried out, the weather detector can be dismounted when not in use, the independent work of the unmanned aerial vehicle is realized, when the weather detector needs to be fixed, the inserted link is inserted into the through hole on the surface of the mounting plate, pressure is applied to the limiting link, the reset spring is in a compressed state, then the handle is rotated to be clamped into the limiting groove, the fixing of the weather detector is realized, when the weather detector needs to be dismounted, the handle is rotated to be separated from the limiting groove, and under the elastic action of the reset spring, the inserted link is driven to pop out of the through hole on the surface of the mounting plate, so that the dismounting of the weather detector.
3. According to the invention, through the damping support legs, a certain damping effect can be achieved by using the damping springs, the vibration phenomenon of the unmanned aerial vehicle during landing is reduced, the stability of the unmanned aerial vehicle during landing is ensured, meanwhile, the damage of internal devices caused by vibration is prevented, and the service life of the unmanned aerial vehicle is prolonged.
Drawings
FIG. 1 is a schematic structural diagram of a weather detecting unmanned aerial vehicle;
FIG. 2 is an exploded view of a weather detecting drone;
FIG. 3 is a schematic diagram of a configuration of a meteorological detector in a meteorological detection drone;
FIG. 4 is a schematic structural diagram of a fixing mechanism in a weather detecting unmanned aerial vehicle;
FIG. 5 is a schematic structural diagram of a battery compartment of a weather detection unmanned aerial vehicle;
FIG. 6 is an enlarged view of a portion of A of a weather detecting drone;
fig. 7 is a schematic structural diagram of a shock absorption leg in a meteorological detection unmanned aerial vehicle.
In the figure: 1. a body; 2. mounting a plate; 3. a battery compartment; 31. a bin cover; 32. rotating the rod; 33. a sliding plate; 34. a chute; 35. a micro motor; 36. a slider; 37. a placement groove; 38. a first gear; 39. a rotating shaft; 310. a second gear; 311. a drive belt; 312. a third gear; 313. a rack; 4. an airfoil; 5. a weather detector; 51. connecting blocks; 52. a detection unit; 53. a sensor; 54. a rainfall detector; 6. a fixing plate; 7. a fixing mechanism; 701. a base plate; 702. inserting a rod; 703. a return spring; 704. fixing the rod; 705. an end cap; 706. a limiting rod; 707. a limiting groove; 708. a handle; 709. a bolt; 8. a drive motor; 9. a shock-absorbing leg; 91. a lower support section; 92. a shock-absorbing lever; 93. an upper support section; 94. a damping spring; 10. a propeller.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1 to 7, in the embodiment of the present invention, a weather detection unmanned aerial vehicle includes a machine body 1, a mounting plate 2 is fixedly installed on an upper surface of the machine body 1, a battery compartment 3 is fixedly installed on a lower surface of the machine body 1, a compartment cover 31 is installed on a front side of the battery compartment 3, a rotating rod 32 is installed at a connection position of the battery compartment 3 and the compartment cover 31, a sliding plate 33 is installed inside the battery compartment 3, a sliding groove 34 is opened at a bottom of the battery compartment 3, a micro motor 35 is fixedly installed on one side of the battery compartment 3, a sliding block 36 is installed on a lower surface of the sliding plate 33, a placing groove 37 is installed at a top of the sliding plate 33, first gears 38 are installed on two sides of the rotating rod 32, a rotating shaft 39 is connected at a position of one end of the micro motor 35, a second gear 310 is sleeved on an outer side of the rotating shaft 39, a, a third gear 312 is arranged on one side of the second gear 310, a rack 313 is fixedly arranged below the third gear 312, the bin cover 31 is rotatably connected with the battery bin 3 through a rotating rod 32, the sliding plate 33 is slidably connected with the battery bin 3 through a sliding chute 34 and a sliding block 36, the micro motor 35 is rotatably connected with the second gear 310 through a rotating shaft 39, the second gear 310 is rotatably connected with the first gear 38 through a transmission belt 311, the rotating shaft 39 is in meshed connection with the rack 313 through the third gear 312, the rotating shaft 39 drives the second gear 310 to rotate through the operation of the arranged micro motor 35, and then the first gear 38 is driven to rotate through the transmission belt 311, so that the rotating rod 32 drives the bin cover 31 to rotate, meanwhile, the rotating shaft 39 drives the third gear 312 to rotate, and then the battery bin 3 is driven to move outwards along the sliding chute 34 through the rack 313, thereby realizing the automatic opening and closing of the bin cover 31, and overcoming the defects of time and labor waste in the manual installation of, the installation work of battery is convenient for carry on, this design simple structure, the operation is convenient, not only uses manpower sparingly, effectively improves work efficiency moreover, and the practicality is stronger.
Further, the outside of organism 1 is that circular array equidistance distributes and has four wings 4, the top fixed mounting of mounting panel 2 has meteorological detector 5, connecting block 51 is installed to meteorological detector 5's lower extreme, the upper end of connecting block 51 is provided with detection portion 52, the internally mounted of detection portion 52 has sensor 53, and rainfall detector 54 is installed at detection portion 52's top, sensor 53 is temperature sensor, humidity transducer, baroceptor, arbitrary one or more in the PM2.5 sensor, detection portion 52 is provided with wind speed and direction sensor with rainfall detector 54's junction, meteorological detector 5 through the setting can utilize sensor 53 and rainfall detector 54 directly to realize the detection work of high altitude weather, realize the effective combination of unmanned aerial vehicle and meteorological detection, be convenient for going on of meteorological monitoring work.
Still further, a fixing plate 6 is fixedly installed at the bottom of the weather detecting instrument 5, fixing mechanisms 7 are installed at the joints of the fixing plate 6 and the mounting plate 2, the weather detecting instrument 5 and the fixing plate 6 are of an integrally formed structure, the fixing plate 6 and the mounting plate 2 are fixedly connected through the fixing mechanisms 7, the fixing mechanisms 7 are totally provided with four fixing mechanisms 7 which are distributed at four corners of the fixing plate 6 in a rectangular shape, through holes are formed in the surface of the mounting plate 2, the fixing mechanism 7 comprises a bottom plate 701, an insertion rod 702 is embedded and installed at the lower end of the bottom plate 701, a return spring 703 is arranged at the upper end of the insertion rod 702, a fixing rod 704 is fixedly installed at the position, located at the upper surface of the bottom plate 701, of one side of the insertion rod 702, end covers 705 are installed at both ends of the return spring 703, a limiting rod 706 is fixedly installed at the top of the return spring, the connecting part of the bottom plate 701 and the fixing plate 6 is provided with a bolt 709, the fixing mechanism 7 is fixedly connected with the fixing plate 6 through the bolt 709, the inserted link 702 is fixedly connected with the limit rod 706 through a reset spring 703, the fixing link 704 is connected with the limit rod 706 through a handle 708 and a limit groove 707 in a clamping way, the rapid installation and disassembly work of the weather detector 5 can be realized through the arranged fixing mechanism 7, the maintenance and replacement processing of the weather detector 5 are convenient, the weather detector 5 can be disassembled when not in use, the unmanned aerial vehicle can work independently, when the weather detector 5 needs to be fixed, the inserted link 702 is inserted into a through hole on the surface of the mounting plate 2, pressure is applied to the limit rod 706, the reset spring 703 is in a compression state, then the handle 708 is rotated to be clamped into the limit groove 707, the fixing of the weather detector 5 is realized, when the dismounting of the weather detector 5 needs to, the handle 708 is rotated to be separated from the limiting groove 707, and under the elastic action of the return spring 703, the inserted link 702 is driven to pop out of the through hole on the surface of the mounting plate 2, so that the weather detector 5 is removed.
Still further, the one end of wing 4 is provided with driving motor 8, and the bottom of wing 4 is connected with shock attenuation landing leg 9, screw 10 is installed to driving motor 8's upper end, shock attenuation landing leg 9's lower extreme is provided with bottom suspension strut 91, shock attenuation pole 92 is installed in bottom strut 91's upper end embedding, shock attenuation pole 92's top fixed mounting has last supporting part 93, and shock attenuation pole 92's outside cover is equipped with damping spring 94, go up supporting part 93 and bottom suspension strut 91 through damping spring 94 fixed connection, shock attenuation landing leg 9 through the setting can utilize damping spring 94 to reach certain shock attenuation effect, the vibrations phenomenon when reducing unmanned aerial vehicle descends, guarantee the stationarity of unmanned aerial vehicle descending in-process, prevent simultaneously to cause the damage of its inside device because of vibrations, extension unmanned aerial vehicle's life.
The working principle of the invention is as follows: firstly, fix the weather detecting instrument 5 above the machine body 1, insert the inserted link 702 into the through hole on the surface of the mounting plate 2, apply pressure to the limit rod 706, make the reset spring 703 in the compression state, then rotate the handle 708, make it block into the limit groove 707, that is, realize the fixing of the weather detecting instrument 5, then, start the work of the unmanned aerial vehicle through the remote controller, utilize the sensor 53 and the rainfall detector 54 in the weather detecting instrument 5, carry out the detection work of high altitude weather, realize the effective combination of the unmanned aerial vehicle and the weather detection, facilitate the weather monitoring work, furthermore, when the weather detection work is completed, when the unmanned aerial vehicle needs to land, can reach certain damping effect through the damping support leg 9 that is set up, utilize the damping spring 94 to reach certain damping effect, reduce the vibration phenomenon when the unmanned aerial vehicle lands, guarantee the stationarity of the unmanned aerial vehicle in the landing process, simultaneously prevent the, prolong unmanned aerial vehicle's life, it is further again, demolish meteorological detection instrument 5, twist grip 708 makes it break away from spacing groove 707, under reset spring 703's elastic action, it can to drive the through-hole that inserted bar 702 popped out mounting panel 2 surface, finally, when needing to carry out the change of battery, start micro motor 35 work, make pivot 39 drive second gear 310 rotate, and then drive first gear 38 through driving belt 311 and rotate, make dwang 32 drive cang gai 31 and rotate, and simultaneously, pivot 39 drives third gear 312 and rotates, and then drive battery compartment 3 through rack 313 and move to the outside along spout 34, thereby realize the automation of cangai 31 and open and shut, be convenient for carry out the installation work of battery, this design simple structure, and convenient for operation, not only use manpower sparingly, and effectively improve work efficiency, the practicality is stronger.
It will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, and that the present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.
Claims (9)
1. The utility model provides a meteorological detection unmanned aerial vehicle, includes organism (1), its characterized in that, the last fixed surface of organism (1) installs mounting panel (2), and the lower fixed surface of organism (1) installs battery compartment (3), the outside of organism (1) is circular array equidistance and distributes and have four wings (4), the top fixed mounting of mounting panel (2) has meteorological detection instrument (5), the bottom fixed mounting of meteorological detection instrument (5) has fixed plate (6), fixed mechanism (7) are installed to the junction of fixed plate (6) and mounting panel (2), the one end of wing (4) is provided with driving motor (8), and the bottom of wing (4) is connected with shock attenuation landing leg (9), screw (10) are installed to the upper end of driving motor (8);
fixing mechanism (7) include bottom plate (701), inserted bar (702) is installed in the lower extreme embedding of bottom plate (701), the upper end of inserted bar (702) is provided with reset spring (703), and the one side of inserted bar (702) is located the upper surface position department fixed mounting of bottom plate (701) has dead lever (704), end cover (705) are all installed at the both ends of reset spring (703), and the top fixed mounting of reset spring (703) has gag lever post (706), spacing groove (707) have been seted up to one side of gag lever post (706), the outside of dead lever (704) is rotated and is connected with handle (708), the junction of bottom plate (701) and fixed plate (6) is provided with bolt (709).
2. The weather detection unmanned aerial vehicle of claim 1, wherein the weather detector (5) and the fixing plate (6) are of an integrally formed structure, and the fixing plate (6) is fixedly connected with the mounting plate (2) through a fixing mechanism (7).
3. The weather detection unmanned aerial vehicle of claim 1, wherein a connecting block (51) is mounted at the lower end of the weather detector (5), a detection part (52) is arranged at the upper end of the connecting block (51), a sensor (53) is mounted inside the detection part (52), and a rainfall detector (54) is mounted at the top of the detection part (52).
4. Weather detection unmanned aerial vehicle of claim 3, wherein the sensor (53) is any one or more of a temperature sensor, a humidity sensor, an air pressure sensor and a PM2.5 sensor, and a wind speed and direction sensor is arranged at the connection position of the detection part (52) and the rainfall detector (54).
5. Weather detection unmanned aerial vehicle of claim 1, wherein the number of the fixing mechanisms (7) is four, and the four fixing mechanisms (7) are distributed at four corners of the fixing plate (6) in a rectangular shape.
6. The weather detection unmanned aerial vehicle of claim 1, wherein the fixing mechanism (7) is fixedly connected with the fixing plate (6) through a bolt (709), the inserting rod (702) is fixedly connected with the limiting rod (706) through a return spring (703), and the fixing rod (704) is connected with the limiting rod (706) through a handle (708) and a limiting groove (707) in a clamping manner.
7. The weather detection unmanned aerial vehicle according to claim 1, wherein a bin cover (31) is arranged on the front side of the battery bin (3), a rotating rod (32) is installed at the joint of the battery bin (3) and the bin cover (31), a sliding plate (33) is arranged inside the battery bin (3), a sliding groove (34) is formed in the bottom of the battery bin (3), a micro motor (35) is fixedly installed on one side of the battery bin (3), a sliding block (36) is installed on the lower surface of the sliding plate (33), a placing groove (37) is formed in the top of the sliding plate (33), first gears (38) are arranged on two sides of the rotating rod (32), a rotating shaft (39) is connected to the position, located on the inner side of the battery bin (3), of one end of the micro motor (35), and a second gear (310) is sleeved on the outer side of the rotating shaft (39), a transmission belt (311) is installed at the joint of the second gear (310) and the first gear (38), a third gear (312) is arranged on one side of the second gear (310), and a rack (313) is fixedly installed below the third gear (312).
8. The weather detection unmanned aerial vehicle of claim 7, wherein the cover (31) is rotatably connected with the battery compartment (3) through a rotating rod (32), the sliding plate (33) is slidably connected with the battery compartment (3) through a sliding groove (34) and a sliding block (36), the micro motor (35) is rotatably connected with a second gear (310) through a rotating shaft (39), the second gear (310) is in transmission connection with a first gear (38) through a transmission belt (311), and the rotating shaft (39) is in meshing connection with the rack (313) through a third gear (312).
9. The weather detection unmanned aerial vehicle of claim 1, wherein the lower end of the shock absorption leg (9) is provided with a lower support part (91), the shock absorption rod (92) is embedded in the upper end of the lower support part (91), the upper support part (93) is fixedly mounted at the top of the shock absorption rod (92), the shock absorption spring (94) is sleeved on the outer side of the shock absorption rod (92), and the upper support part (93) is fixedly connected with the lower support part (91) through the shock absorption spring (94).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
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| CN201910815706.6A CN110654538B (en) | 2019-08-30 | 2019-08-30 | Weather detection unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201910815706.6A CN110654538B (en) | 2019-08-30 | 2019-08-30 | Weather detection unmanned aerial vehicle |
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| CN110654538A CN110654538A (en) | 2020-01-07 |
| CN110654538B true CN110654538B (en) | 2021-02-12 |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN207208465U (en) * | 2017-06-30 | 2018-04-10 | 林沛义 | A kind of foldable aircraft |
| CN208915444U (en) * | 2018-09-30 | 2019-05-31 | 杭州市气象局 | Meteorological detection unmanned plane |
| CN109911184A (en) * | 2019-03-29 | 2019-06-21 | 芜湖市极星航空科技有限公司 | A kind of unmanned plane damping undercarriage |
| KR20190080713A (en) * | 2017-12-28 | 2019-07-08 | 주식회사 심지소프트 | Sensor mounting device of unmanned aerial vehicle for meteorological observation, unmanned aerial vehicle for meteorological observation and meteorological observation method thereof and sensor mounting device of unmanned aerial vehicle for meteorological observation |
| CN209274888U (en) * | 2018-12-29 | 2019-08-20 | 成都航空职业技术学院 | A kind of unmanned plane undercarriage |
-
2019
- 2019-08-30 CN CN201910815706.6A patent/CN110654538B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN207208465U (en) * | 2017-06-30 | 2018-04-10 | 林沛义 | A kind of foldable aircraft |
| KR20190080713A (en) * | 2017-12-28 | 2019-07-08 | 주식회사 심지소프트 | Sensor mounting device of unmanned aerial vehicle for meteorological observation, unmanned aerial vehicle for meteorological observation and meteorological observation method thereof and sensor mounting device of unmanned aerial vehicle for meteorological observation |
| CN208915444U (en) * | 2018-09-30 | 2019-05-31 | 杭州市气象局 | Meteorological detection unmanned plane |
| CN209274888U (en) * | 2018-12-29 | 2019-08-20 | 成都航空职业技术学院 | A kind of unmanned plane undercarriage |
| CN109911184A (en) * | 2019-03-29 | 2019-06-21 | 芜湖市极星航空科技有限公司 | A kind of unmanned plane damping undercarriage |
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| CN110654538A (en) | 2020-01-07 |
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