CN113250516A - Movable unmanned aerial vehicle hangar - Google Patents
Movable unmanned aerial vehicle hangar Download PDFInfo
- Publication number
- CN113250516A CN113250516A CN202110655386.XA CN202110655386A CN113250516A CN 113250516 A CN113250516 A CN 113250516A CN 202110655386 A CN202110655386 A CN 202110655386A CN 113250516 A CN113250516 A CN 113250516A
- Authority
- CN
- China
- Prior art keywords
- unmanned aerial
- aerial vehicle
- frame
- hangar
- screw rod
- 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.)
- Pending
Links
- 238000001514 detection method Methods 0.000 claims abstract description 8
- 230000008859 change Effects 0.000 claims description 7
- 230000001105 regulatory effect Effects 0.000 claims description 6
- 230000000712 assembly Effects 0.000 abstract description 2
- 238000000429 assembly Methods 0.000 abstract description 2
- 238000012876 topography Methods 0.000 abstract 1
- 230000008901 benefit Effects 0.000 description 6
- 230000001276 controlling effect Effects 0.000 description 5
- 230000000694 effects Effects 0.000 description 5
- 238000000034 method Methods 0.000 description 4
- 238000004378 air conditioning Methods 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000035899 viability Effects 0.000 description 1
Images
Classifications
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
- E04H6/00—Buildings for parking cars, rolling-stock, aircraft, vessels or like vehicles, e.g. garages
- E04H6/44—Buildings for parking cars, rolling-stock, aircraft, vessels or like vehicles, e.g. garages for storing aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
- B60L53/80—Exchanging energy storage elements, e.g. removable batteries
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
- E04B1/00—Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
- E04B1/343—Structures characterised by movable, separable, or collapsible parts, e.g. for transport
- E04B1/34336—Structures movable as a whole, e.g. mobile home structures
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
- E04B1/00—Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
- E04B1/343—Structures characterised by movable, separable, or collapsible parts, e.g. for transport
- E04B1/34336—Structures movable as a whole, e.g. mobile home structures
- E04B1/34352—Base structures or supporting means therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L2200/00—Type of vehicles
- B60L2200/10—Air crafts
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
Landscapes
- Engineering & Computer Science (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Power Engineering (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The invention relates to the technical field of unmanned aerial vehicle storehouses, and discloses a movable unmanned aerial vehicle storehouse which comprises a rack and a cabin door, wherein the outer side wall of the rack is provided with an outer shell, the bottom of the rack is provided with four groups of adjusting assemblies, a cabin door switch assembly is arranged above the inner side of the rack, the cabin door switch assembly is provided with the cabin door, the inner bottom surface of the rack is provided with a horizontal detection device and a lifting assembly, the top of the lifting assembly is provided with a lifting platform, the lifting platform is provided with an unmanned aerial vehicle, and the inner side of the rack is provided with a centering assembly; the hangar bottom sets up adjusting device, realizes can quick adjustment unmanned aerial vehicle hangar realization working plane level under complicated topography with simple structure, simultaneously, can realize that the unmanned aerial vehicle hangar is convenient removal in handling, after confirming position and height, can realize the location through adjusting device, ensures that the skew can not appear in the unmanned aerial vehicle hangar in the use.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicle hangars, in particular to a movable unmanned aerial vehicle hangar.
Background
An unmanned aerial vehicle, abbreviated as "unmanned aerial vehicle" ("UAV"), is an unmanned aerial vehicle that is operated using a radio remote control device and a self-contained program control device. Unmanned aerial vehicles are in fact a general term for unmanned aerial vehicles, and can be defined from a technical perspective as follows: unmanned fixed wing aircraft, unmanned VTOL aircraft, unmanned dirigible airship, unmanned helicopter, unmanned many rotor crafts, unmanned parachute-wing aircraft etc. compare with manned aircraft, and it has small, the cost is low, convenient to use, require advantages such as low, battlefield viability stronger to the operational environment, and the unmanned aerial vehicle hangar is used for realizing that unmanned aerial vehicle takes off, descends and saves to and fill automatically/trade full-automatic hangar of functions such as electricity and constitute and include: the system comprises a hangar box body, a platform lifting and centering system, an electrical system, a battery replacing and charging system, a temperature control system, a UPS (optional), an industrial control system, video monitoring inside the hangar and the like.
The existing unmanned aerial vehicle hangar has certain requirements on working environment, and can not be used on the ground with certain unevenness or certain angle.
Disclosure of Invention
Technical problem to be solved
Aiming at the defects of the prior art, the invention provides a movable unmanned aerial vehicle hangar which has the advantage of leveling the whole equipment and solves the problem that the equipment cannot be used when the equipment is inclined.
(II) technical scheme
In order to achieve the purpose, the invention provides the following technical scheme: the utility model provides a movable unmanned aerial vehicle hangar, includes frame and hangar hatch door, the lateral wall of frame is provided with the shell body, the bottom of frame is provided with four group's adjusting part, the inboard top of frame is provided with hatch door switch module, be provided with the hangar hatch door on the hatch door switch module, the inside bottom surface of frame is provided with level detection device and lifting unit, lifting unit's top is provided with lift platform, the last unmanned aerial vehicle that is provided with of lift platform, the inboard of frame is provided with the subassembly of returning to the center, the last battery of connecting of hatch door switch module fills and changes the arm of a robot.
Preferably, the adjusting part includes universal wheel and top lift portion, the bottom of top lift portion is provided with the universal wheel, top lift portion and external power source electric connection, the universal wheel mainly comprises regulating part, universal wheel carrier, adjust knob and wheel, the output shaft of top lift portion is connected the regulating part, the bottom of regulating part is connected the universal wheel carrier, the universal wheel carrier with be connected between the regulating part adjust knob, rotate on the universal wheel carrier and connect the wheel.
By adopting the scheme, when the whole device is positioned at a pit or a position with uneven ground, the four horizontal detection devices are used for detecting the inclined position and the inclined angle, one or more of the four horizontal detection devices are used for controlling one or more jacking parts, and the output shaft of each jacking part is extended or shortened to change the height of one corner of the rack, so that the whole rack is in a horizontal state.
Preferably, the lifting assembly comprises a first cylinder and a second cylinder, the inner side wall of the first cylinder is connected with the second cylinder in a sliding mode, limiting blocks are symmetrically arranged on the outer side wall of the second cylinder, a second motor is arranged on the inner bottom surface of the first cylinder, an output shaft of the second motor is connected with the first screw rod, and the top of the second cylinder is connected with the lifting platform.
By adopting the scheme, when the user controls the height of the lifting platform, the second motor is controlled to work, the first screw rod starts to rotate, the first screw rod is in threaded connection with the second cylinder, and the second cylinder rises in the first cylinder under the limitation of the limiting block, so that the height of the lifting platform is changed.
Preferably, the top of the lifting platform is provided with a limiting assembly, the limiting assembly comprises a box body, the outer side wall of the first screw rod is provided with a first bevel gear, the inner side wall of the box body is rotatably connected with a second screw rod, one end of the second screw rod is connected with a second bevel gear, the other end of the second screw rod is in threaded connection with a second pipe body, one side of the box body is provided with the first pipe body, the first pipe body is in sliding connection with the second pipe body, one end of the second pipe body is connected with a pressing block, and the second bevel gear is in meshed connection with the first bevel gear.
Through adopting above-mentioned scheme, rotate at screw rod one to drive lift platform in-process that rises, bevel gear one is connected with the meshing of bevel gear two, makes screw rod two and two threaded connection of body, and body two slides in body one this moment, makes the briquetting carry on spacingly to unmanned aerial vehicle's bottom.
Preferably, the pressing block is of an arc-shaped sheet structure.
Through adopting above-mentioned scheme, the design of arc shape does benefit to and carries on spacingly to the unmanned aerial vehicle bottom.
Preferably, the cabin door switch assembly comprises a supporting plate, a first motor, a connecting plate and a first screw rod, the supporting plate is located on the inner side of the rack, the top of the supporting plate is provided with the first motor, an output shaft of the first motor is connected with the first screw rod, and the outer side wall of the first screw rod is connected with the connecting plate.
By adopting the scheme, when a user operates the cabin door switch of the cabin, the first motor is controlled to work, the first screw rod is rotated, the connecting plate is driven to do linear motion on the supporting plate, and the position of the cabin door of the cabin is changed by the supporting plate.
Preferably, the frame includes frame one, support column two and frame two, the four corners of frame one all is provided with support column one, the lateral wall symmetry of frame one is provided with support column two, the top of frame one is provided with four groups support column three, the top of support column three is provided with the plate body, the lateral wall of plate body is provided with frame two.
Through adopting above-mentioned scheme, by the setting of frame one, restricted the position of four support columns one, connect four adjusting part by four support columns one to adjust the horizontality of whole frame.
Preferably, the shell body is provided with an indicator lamp and an air conditioner control panel, the top of the frame II is provided with an electric cabinet and a battery box control box, and the bottom of the support plate is provided with a battery box.
Through adopting above-mentioned scheme, the setting of pilot lamp for learn unmanned aerial vehicle's the condition of charging, air conditioner control panel is used for controlling the shell internal temperature, guarantees that the charging environment is in normal condition, and battery box control box is used for the effect of changing arm control to the battery charge, and the battery box is used for saving the effect of unmanned aerial vehicle battery.
(III) advantageous effects
Compared with the prior art, the invention provides a movable unmanned aerial vehicle hangar, which has the following beneficial effects:
according to the movable unmanned aerial vehicle hangar, the bottom of the hangar is provided with the adjusting device, the unmanned aerial vehicle hangar can be quickly adjusted under complex terrains by using a simple structure to achieve the level of a working plane, meanwhile, the unmanned aerial vehicle hangar can be conveniently moved in the carrying process, after the position and the height are determined, the positioning can be achieved through the adjusting device, and the unmanned aerial vehicle hangar is ensured not to deviate in the using process; the unmanned aerial vehicle is centered after the unmanned aerial vehicle lands on the lifting platform through the centering assembly, then the unmanned aerial vehicle lands to the height of the mechanical arm for replacing the battery through the lifting assembly, the unmanned aerial vehicle is replaced with the battery through the mechanical arm, and the battery is placed back to the battery box for charging; the whole occupied area of unmanned aerial vehicle hangar is little to be suitable for multiple environment, thereby do benefit to unmanned aerial vehicle and can change the battery under multiple environment.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic diagram of the internal left view structure of the present invention;
FIG. 3 is a schematic diagram of an internal top view of the present invention;
FIG. 4 is a schematic view of an internal axis measurement configuration of the present invention;
FIG. 5 is a schematic view of a spacing assembly according to the present invention;
FIG. 6 is a schematic view of a centering assembly according to the present invention;
FIG. 7 is an enlarged view of a portion of the centering assembly of the present invention;
fig. 8 is a schematic structural view of an adjusting assembly according to the present invention.
In the figure:
1. an indicator light; 2. a cabin door; 3. an air-conditioning control panel; 4. an adjustment assembly; 41. a universal wheel; 42. a jacking portion; 43. an adjustment member; 44. a universal wheel carrier; 45. adjusting a knob; 46. a wheel; 5. a hatch door switch assembly; 51. a support plate; 52. a first motor; 53. a connecting plate; 54. a first screw rod; 6. a centering component; 61. a slider; 62. a slider connecting plate; 63. a nut; 64. a nut seat; 65. returning to the middle pole; 7. a frame; 71. a first frame; 72. a first supporting column; 73. a second supporting column; 74. a second frame; 75. a plate body; 76. a third support column; 8. a lifting platform; 9. a lifting assembly; 91. a first column body; 92. a second column body; 93. a limiting block; 94. a second motor; 95. a first screw rod; 10. a battery box control box; 11. a battery box; 12. a level detection device; 14. an electric cabinet; 15. a battery charging replacement mechanical arm; 16. an unmanned aerial vehicle; 17. a limiting component; 171. a box body; 172. a first bevel gear; 173. a second bevel gear; 174. a second screw; 175. a first pipe body; 176. a second pipe body; 177. and (4) pressing the blocks.
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.
Example one
A movable unmanned aerial vehicle hangar comprises a rack 7 and a hangar cabin door 2, wherein the outer side wall of the rack 7 is provided with an outer shell, the bottom of the rack 7 is provided with four groups of adjusting components 4, a cabin door switch component 5 is arranged above the inner side of the rack 7, a cabin door 2 is arranged on the cabin door switch component 5, the inner bottom surface of the rack 7 is provided with a level detection device 12 and a lifting component 9, the top of the lifting component 9 is provided with a lifting platform 8, an unmanned aerial vehicle 16 is arranged on the lifting platform 8, a centering component 6 is arranged on the inner side of the rack 7, a battery charging and exchanging mechanical arm 15 is connected on the cabin door switch component 5, the adjusting components 4 comprise universal wheels 41 and jacking portions 42, the bottom of the jacking portions 42 is provided with the universal wheels 41, the jacking portions 42 are electrically connected with an external power supply, the adjusting components 4 comprise the universal wheels 41 and the jacking portions 42, the universal wheel 41 is arranged at the bottom of the lifting part 42, the lifting part 42 is electrically connected with an external power supply, the universal wheel 41 mainly comprises an adjusting piece 43, a universal wheel frame 44, an adjusting knob 45 and a wheel 46, an output shaft of the lifting part 42 is connected with the adjusting piece 43, the bottom of the adjusting piece 43 is connected with the universal wheel frame 44, the adjusting knob 45 is connected between the universal wheel frame 44 and the adjusting piece 43, and the universal wheel frame 44 is rotatably connected with the wheel 46.
Referring to fig. 1-8, when the user uses the unmanned aerial vehicle, firstly, the door switch assembly 5 is controlled to open the door on the outer shell, the unmanned aerial vehicle 16 is guided to the lifting platform 8, the centering assembly 6 is controlled to move the unmanned aerial vehicle 16 to the middle position of the lifting platform 8, secondly, the lifting component 9 is controlled to move the height of the battery of the unmanned aerial vehicle 16 to be consistent with the height of the battery charging mechanical arm 15, the battery charging mechanical arm 15 is controlled to replace and charge the battery in the unmanned aerial vehicle 16, and finally, when the whole device is located at a position where a pit or a floor is not flat, the tilt position and the tilt angle are first detected by the four level detecting devices 12, secondly, one or more of the four level detection devices 12 control one or more jacking parts 42, and the output shaft of the jacking part 42 is extended or shortened to change the height of one corner of the machine frame 7, so that the whole machine frame 7 is in a horizontal state; the user can adjust the adjusting knob 45 to change the height of the wheel 46;
the model number of the level detecting device 12 is (AL 322);
the centering assembly 6 mainly comprises a sliding block 61, a sliding block connecting plate 62, a nut 63, a nut seat 64 and a centering rod 65, firstly, a switch is controlled to enable a motor to rotate so as to enable the nut 63 and the nut seat 64 to move, the sliding block connecting plate 62 is connected with the lower sliding block 61 and the centering rod 65 to move along with the nut, and therefore the centering rod 65 can push the unmanned aerial vehicle 16 to reach a specified position, wherein the motor is not marked in the attached drawings of the specification;
by adjusting part 4's setting, do benefit to the horizontal position that changes whole unmanned aerial vehicle hangar to the unmanned aerial vehicle hangar is suitable for multiple ground, makes unmanned aerial vehicle can change the battery under the multiple condition, and unmanned aerial vehicle hangar area of occupation is little, and the user of being convenient for removes.
Example two
The function of limiting the position of the foot seat of the unmanned aerial vehicle 16 is added on the basis of the first embodiment.
The lifting assembly 9 comprises a first cylinder 91 and a second cylinder 92, the inner side wall of the first cylinder 91 is connected with the second cylinder 92 in a sliding manner, the outer side wall of the second cylinder 92 is symmetrically provided with limit blocks 93, the inner bottom surface of the first cylinder 91 is provided with a second motor 94, an output shaft of the second motor 94 is connected with a first screw 95, and the top of the second cylinder 92 is connected with the lifting platform 8; the top of the lifting platform 8 is provided with a limiting assembly 17, the limiting assembly 17 comprises a box body 171, the outer side wall of the first screw 95 is provided with a first bevel gear 172, the inner side wall of the box body 171 is rotatably connected with a second screw 174, one end of the second screw 174 is connected with a second bevel gear 173, the other end of the second screw is in threaded connection with a second pipe 176, one side of the box body 171 is provided with a first pipe 175, the first pipe 175 is in sliding connection with the second pipe 176, one end of the second pipe 176 is connected with a pressing block 177, and the second bevel gear 173 is in meshed connection with the first bevel gear 172; the pressing block 177 has an arc-shaped sheet structure.
Referring to fig. 1-8, the user is when controlling lift platform 8's height, control motor two 94 works, screw rod 95 begins to rotate, screw rod 95 and two 92 threaded connection of cylinder, by the restriction of stopper 93, make cylinder two 92 rise in cylinder one 91, thereby change lift platform 8's height, rotate at screw rod 95, and drive lift platform 8 and rise the in-process, bevel gear one 172 and two 173 meshing connections of bevel gear, make two 174 of screw rods and two 176 threaded connection of body, body two 176 slides in body one 175 this moment, make pressure application piece 177 carry on spacingly to unmanned aerial vehicle 16's bottom, the design of arc shape, it is spacing to do benefit to the unmanned aerial vehicle 16 bottom.
EXAMPLE III
And the function of controlling the opening and closing of the hangar cabin door 2 is added on the basis of the second embodiment.
The hatch switch assembly 5 comprises a supporting plate 51, a first motor 52, a connecting plate 53 and a first screw 54, wherein the supporting plate 51 is positioned on the inner side of the rack 7, the top of the supporting plate 51 is provided with the two first motors 52, the output shaft of the first motor 52 is connected with the first screw 54, and the outer side wall of the first screw 54 is connected with the connecting plate 53; the rack 7 comprises a first frame 71, a first support column 72, a second support column 73 and a second frame 74, the first support column 72 is arranged at each of four corners of the first frame 71, the second support column 73 is symmetrically arranged on the outer side wall of the first frame 71, four groups of third support columns 76 are arranged on the top of the first frame 71, plate bodies 75 are arranged on the tops of the third support columns 76, and the second frame 74 is arranged on the outer side wall of the plate bodies 75; the outer shell is provided with an indicator lamp 1 and an air-conditioning control panel 3, the top of the second frame 74 is provided with an electric cabinet 14 and a battery box control box 10, and the bottom of the support plate 51 is provided with a battery box 11;
referring to fig. 1-8, when a user operates the switch of the hangar door 2, the first motor 52 is controlled to work, so that the first screw rod 54 rotates, the connecting plate 53 is driven to do linear motion on the supporting plate 51, and the position of the hangar door 2 is changed by the supporting plate 51; the positions of the four supporting columns one 72 are limited by the arrangement of the frame one 71, and the four adjusting assemblies 4 are connected by the four supporting columns one 72 so as to adjust the horizontal state of the whole rack 7; setting up of pilot lamp 1 for learn unmanned aerial vehicle 16's the condition of charging, air conditioner control panel 3 is used for controlling the shell internal temperature, guarantees that the charging environment is in normal condition, and battery box control box 10 is used for the effect of changing arm 15 control to the battery charge, and battery box 11 is used for saving the effect of unmanned aerial vehicle battery.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (8)
1. The utility model provides a movable unmanned aerial vehicle hangar which characterized in that: including frame (7) and hangar hatch door (2), the lateral wall of frame (7) is provided with the shell body, the bottom of frame (7) is provided with four group's adjusting part (4), the inboard top of frame (7) is provided with hatch door switch module (5), be provided with hangar hatch door (2) on hatch door switch module (5), the inside bottom surface of frame (7) is provided with level detection device (12) and lift subassembly (9), the top of lift subassembly (9) is provided with lift platform (8), be provided with unmanned aerial vehicle (16) on lift platform (8), the inboard of frame (7) is provided with in the middle of subassembly (6), connect battery on hatch door switch module (5) and fill and change mechanical arm (15).
2. The mobile unmanned aerial vehicle hangar of claim 1, wherein: adjusting part (4) include universal wheel (41) and jacking portion (42), the bottom of jacking portion (42) is provided with universal wheel (41), jacking portion (42) and external power source electric connection, universal wheel (41) mainly comprise regulating part (43), universal wheel carrier (44), adjust knob (45) and wheel (46), the output shaft of jacking portion (42) adjusting part (43), the bottom of regulating part (43) is connected universal wheel carrier (44), universal wheel carrier (44) with connect between adjusting part (43) adjust knob (45), rotate on universal wheel carrier (44) and connect wheel (46).
3. The mobile unmanned aerial vehicle hangar of claim 2, wherein: lifting unit (9) include cylinder one (91) and cylinder two (92), the inside wall sliding connection of cylinder one (91) has cylinder two (92), the lateral wall symmetry of cylinder two (92) is provided with stopper (93), the inside bottom surface of cylinder one (91) is provided with motor two (94), the output shaft screw rod one (95) of motor two (94), the top of cylinder two (92) is connected lift platform (8).
4. The mobile unmanned aerial vehicle hangar of claim 3, wherein: the top of lift platform (8) is provided with spacing subassembly (17), spacing subassembly (17) include box (171), the lateral wall of screw rod (95) is provided with bevel gear (172), the inside wall of box (171) rotates and connects screw rod two (174), bevel gear two (173) are connected to the one end of screw rod two (174), other end threaded connection body two (176), one side of box (171) is provided with body one (175), body one (175) with body two (176) sliding connection, forcing piece (177) is connected to the one end of body two (176), bevel gear two (173) with bevel gear (172) meshing connection.
5. The mobile unmanned aerial vehicle hangar of claim 4, wherein: the pressing block (177) is of an arc-shaped sheet structure.
6. The mobile unmanned aerial vehicle hangar of claim 4, wherein: the cabin door switch assembly (5) comprises a supporting plate (51), a first motor (52), a connecting plate (53) and a first screw rod (54), the supporting plate (51) is located on the inner side of the rack (7), the top of the supporting plate (51) is provided with the two first motors (52), an output shaft of the first motors (52) is connected with the first screw rod (54), and the outer side wall of the first screw rod (54) is connected with the connecting plate (53).
7. The mobile unmanned aerial vehicle hangar of any one of claim 6, wherein: frame (7) are including frame one (71), support column one (72), support column two (73) and frame two (74), the four corners of frame one (71) all is provided with support column one (72), the lateral wall symmetry of frame one (71) is provided with support column two (73), the top of frame one (71) is provided with four sets of support column three (76), the top of support column three (76) is provided with plate body (75), the lateral wall of plate body (75) is provided with frame two (74).
8. The mobile unmanned aerial vehicle hangar of claim 7, wherein: the air conditioner is characterized in that an indicator lamp (1) and an air conditioner control panel (3) are arranged on the outer shell, an electric cabinet (14) and a battery box control box (10) are arranged at the top of the second frame (74), and a battery box (11) is arranged at the bottom of the support plate (51).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110655386.XA CN113250516A (en) | 2021-06-11 | 2021-06-11 | Movable unmanned aerial vehicle hangar |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110655386.XA CN113250516A (en) | 2021-06-11 | 2021-06-11 | Movable unmanned aerial vehicle hangar |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN113250516A true CN113250516A (en) | 2021-08-13 |
Family
ID=77187698
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202110655386.XA Pending CN113250516A (en) | 2021-06-11 | 2021-06-11 | Movable unmanned aerial vehicle hangar |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN113250516A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN207704246U (en) * | 2018-03-30 | 2018-08-07 | 广州优飞智能设备有限公司 | Unattended UAV Intelligent airplane parking area system |
| WO2018219226A1 (en) * | 2017-05-27 | 2018-12-06 | 星逻智能科技(苏州)有限公司 | Unmanned-aerial-vehicle hangar |
| CN110937127A (en) * | 2019-12-25 | 2020-03-31 | 上海赛摩电气有限公司 | Automatic charging hangar of unmanned aerial vehicle |
| CN111532443A (en) * | 2020-05-22 | 2020-08-14 | 上海芝松航空科技有限公司 | Unmanned vehicles all-weather guarantee carrier |
| CN112290459A (en) * | 2020-11-10 | 2021-01-29 | 广东电网有限责任公司 | Cable tightener |
-
2021
- 2021-06-11 CN CN202110655386.XA patent/CN113250516A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018219226A1 (en) * | 2017-05-27 | 2018-12-06 | 星逻智能科技(苏州)有限公司 | Unmanned-aerial-vehicle hangar |
| CN207704246U (en) * | 2018-03-30 | 2018-08-07 | 广州优飞智能设备有限公司 | Unattended UAV Intelligent airplane parking area system |
| CN110937127A (en) * | 2019-12-25 | 2020-03-31 | 上海赛摩电气有限公司 | Automatic charging hangar of unmanned aerial vehicle |
| CN111532443A (en) * | 2020-05-22 | 2020-08-14 | 上海芝松航空科技有限公司 | Unmanned vehicles all-weather guarantee carrier |
| CN112290459A (en) * | 2020-11-10 | 2021-01-29 | 广东电网有限责任公司 | Cable tightener |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN212195869U (en) | Balance weight device convenient for balance adjustment for unmanned aerial vehicle | |
| CN113250516A (en) | Movable unmanned aerial vehicle hangar | |
| CN110775877A (en) | AGV intelligent trolley and control method thereof | |
| CN112780079B (en) | Shelter with automatic walking function | |
| CN113212235A (en) | Arm that unmanned aerial vehicle changed battery usefulness | |
| CN211731820U (en) | Multifunctional remote sensing surveying and mapping unmanned aerial vehicle | |
| CN219545079U (en) | Multi-station lifting platform | |
| CN109353536A (en) | Unmanned plane lifting gear and automobile | |
| CN211255111U (en) | A hold in palm car for supporting engine | |
| CN112622521B (en) | Traveling system for shelter | |
| CN115743665A (en) | Unmanned aerial vehicle hangar with mechanical battery replacement function | |
| CN212586539U (en) | Low-altitude unmanned detection radar device | |
| CN110712694B (en) | Six-freedom-degree parallel posture adjusting platform assembled based on four-leg low horizontal butt joint | |
| CN207565856U (en) | A kind of unmanned plane device for supplying | |
| CN220662305U (en) | Jacking and positioning device of power exchange station | |
| CN110626980A (en) | A hold in palm car for supporting engine | |
| CN220518575U (en) | Aircraft hanging beam mounting vehicle | |
| CN216299140U (en) | Battery quick replacement platform for model airplane | |
| CN220007795U (en) | Robot with voice function | |
| CN219154750U (en) | Top-mounted equipment capable of adapting to aircraft posture | |
| CN220391894U (en) | Unmanned aerial vehicle storage device based on mapping service | |
| CN218877599U (en) | Onboard photoelectric pod loader device | |
| CN216994317U (en) | Automatic handling system based on AGV | |
| CN217947570U (en) | Full-automatic electric lifting vehicle | |
| CN215402790U (en) | Jacking device for aircraft maintenance |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20210813 |