CN113665832A - Unmanned aerial vehicle intelligent airport ground system - Google Patents
Unmanned aerial vehicle intelligent airport ground system Download PDFInfo
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- CN113665832A CN113665832A CN202110930228.0A CN202110930228A CN113665832A CN 113665832 A CN113665832 A CN 113665832A CN 202110930228 A CN202110930228 A CN 202110930228A CN 113665832 A CN113665832 A CN 113665832A
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- 230000000903 blocking effect Effects 0.000 claims abstract description 31
- 238000013016 damping Methods 0.000 claims description 15
- 230000003014 reinforcing effect Effects 0.000 claims description 9
- 239000011347 resin Substances 0.000 claims description 9
- 229920005989 resin Polymers 0.000 claims description 9
- 238000004804 winding Methods 0.000 claims description 9
- 230000005484 gravity Effects 0.000 claims description 8
- 239000011247 coating layer Substances 0.000 claims description 6
- 229910000831 Steel Inorganic materials 0.000 claims description 5
- 238000010079 rubber tapping Methods 0.000 claims description 5
- 239000010959 steel Substances 0.000 claims description 5
- 241000252254 Catostomidae Species 0.000 claims description 4
- 238000007689 inspection Methods 0.000 abstract description 6
- 238000012423 maintenance Methods 0.000 abstract description 5
- 230000001681 protective effect Effects 0.000 abstract 2
- 239000011248 coating agent Substances 0.000 description 3
- 238000000576 coating method Methods 0.000 description 3
- 238000009434 installation Methods 0.000 description 3
- 238000013461 design Methods 0.000 description 2
- 238000005286 illumination Methods 0.000 description 2
- 230000002035 prolonged effect Effects 0.000 description 2
- 239000003381 stabilizer Substances 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 102000010970 Connexin Human genes 0.000 description 1
- 108050001175 Connexin Proteins 0.000 description 1
- 241000196324 Embryophyta Species 0.000 description 1
- 241001465754 Metazoa Species 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
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- 210000003976 gap junction Anatomy 0.000 description 1
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/02—Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables
- B64F1/029—Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables using a cable or tether
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/36—Other airport installations
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
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Abstract
The invention discloses an intelligent airport ground system of an unmanned aerial vehicle, which comprises an air park, a flying runway and a light system, wherein a blocking device is arranged on the flying runway and comprises a blocking seat and a blocking cable, an upper cable wheel and a lower cable wheel are arranged in the blocking seat, a protective component is arranged between the upper cable wheel and the lower cable wheel, a guide wheel which moves up and down through connection of a lifting device is arranged at the top of the blocking seat, one end of the blocking cable is fixed with the blocking seat, and the free end of the blocking cable respectively bypasses the lower cable wheel, the protective component, the upper cable wheel and the guide wheel and extends outwards; the lighting system comprises a movable emergency lighting device, the movable emergency lighting device comprises a movable base, a fixed base is arranged on the movable base, a lifting lamp post is hinged to the fixed base, a lamp panel is arranged at the end of the lifting lamp post, and a fixed lamp and a movable lamp are arranged on the lamp panel. The invention has the characteristics of large airport capacity, long service life of the blocking device and convenient maintenance and inspection of the unmanned aerial vehicle system by the lighting system.
Description
Technical Field
The invention relates to an unmanned aerial vehicle airport, in particular to an unmanned aerial vehicle intelligent airport ground system.
Background
An unmanned aircraft, referred to as "drone", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle is combined with industrial application and is really just needed by the unmanned aerial vehicle; the method is currently applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, movie and television shooting, romantic manufacturing and the like. Unmanned aerial vehicle all is equipped with the unmanned aerial vehicle airport, supplies unmanned aerial vehicle to park and go up and down.
For a long-distance unmanned aerial vehicle, the requirement on a runway is high, a longer runway is needed, the capacity of an airport of the unmanned aerial vehicle is required to be large, a large number of unmanned aerial vehicle airports are small in capacity, the runway with the length required by the landing of the unmanned aerial vehicle cannot be provided, and the landing requirement of the long-distance unmanned aerial vehicle cannot be met even if a runway blocking device is arranged; and the height of the arresting cable in the arresting device is fixed, and the arresting hook of some unmanned aerial vehicles cannot be accurately hooked with the arresting cable due to different installation positions of the arresting hook of the unmanned aerial vehicles due to different types, so that the arresting device is easily damaged due to larger impact force, and the service life of the arresting device is short.
Light system on the airport is fixed light generally, and fixed light illumination zone is limited, under the darker condition of light, can't be accurate, the condition to unmanned aerial vehicle is overhauld and is maintained pertinently.
Therefore, the existing unmanned aerial vehicle airport system has the defects of small capacity, short service life of the blocking device and inconvenience in maintenance and inspection of the unmanned aerial vehicle system by a lighting system.
Disclosure of Invention
The invention aims to provide an intelligent airport ground system of an unmanned aerial vehicle. The invention has the characteristics of large airport capacity, long service life of the blocking device and convenient maintenance and inspection of the unmanned aerial vehicle system by the lighting system.
The technical scheme of the invention is as follows: an intelligent airport ground system of an unmanned aerial vehicle comprises an air park, a flying runway and a light system, wherein a blocking device is arranged on the flying runway, the blocking device comprises blocking seats positioned on two sides of the runway and a blocking cable positioned between the two blocking seats, an upper cable wheel and a lower cable wheel are arranged in the blocking seats, a protection assembly is arranged between the upper cable wheel and the lower cable wheel, a guide wheel which moves up and down through connection of a lifting device is arranged at the top of the blocking seats, one end of the blocking cable is fixed with the blocking seats, and the free end of the blocking cable extends outwards by respectively bypassing the lower cable wheel, the protection assembly, the upper cable wheel and the guide wheel; the lighting system comprises a movable emergency lighting device, the movable emergency lighting device comprises a movable base, a fixed base is arranged on the movable base, a rotating arm is hinged to the fixed base, a lifting lamp pole is connected to the rotating arm in a rotating mode, the end portion of the lifting lamp pole is connected with a lamp panel in a rotating mode, and a fixed lamp and a movable lamp are arranged on the lamp panel.
Among the aforesaid unmanned aerial vehicle intelligent airport ground system, be equipped with coiling chamber and direction chamber in the fixing base, go up cable pulley and cable pulley down and all rotate through the drive shaft and connect in coiling chamber, the one end of drive shaft is equipped with the attenuator, and the other end of drive shaft is equipped with coiling motor and the clutch that cable pulley and lower cable pulley rotated in the drive, and the leading wheel is located the direction intracavity.
In the aforesaid intelligent airport ground system of unmanned aerial vehicle, the protection component is including being located the horizontal slide rail between cable pulley and the lower cable pulley, and sliding connection has the protection wheel on the horizontal slide rail, and the protection wheel is connected with the protection push rod through the mounting bracket, and the outside cover of protection push rod is equipped with the damping cover, and the protection push rod stretches into in the damping cover to be connected with the damping cover through the extension spring.
In the aforesaid intelligent airport ground system of unmanned aerial vehicle, elevating gear include with block seat sliding connection's rack, the leading wheel is installed at the top of rack, and the meshing has the gear through driving motor drive on the rack, and one side of gear is equipped with the mount of being connected with electric putter, is equipped with the fixed plate with gear cooperation meshing on the mount.
In the intelligent airport ground system of unmanned aerial vehicle, the arresting cable comprises four steel cables, the arresting cable comprises a middle main body section and connecting sections at two ends, a resin coating layer is arranged outside the main body section, a sleeve is movably connected to each connecting section, two sides of the sleeve are fixed through anti-slip rings, the sleeve is in threaded connection with the arresting seat, the end portions of the connecting sections penetrate through the sleeve and are respectively connected with four reinforcing rods, and self-tapping screws in cross connection with the arresting seat are arranged at the end portions of the four reinforcing rods.
In the aforesaid intelligent airport ground system of unmanned aerial vehicle, be equipped with the movable sleeve on the main part section, movable sleeve and resin coating layer gap junction, the bottom of movable sleeve is equipped with two bracing pieces that are "eight" font, and the tip of bracing piece rotates and is connected with the gravity ball.
In the above unmanned aerial vehicle intelligent airport ground system, the movable lamp includes a lamp body, two ends of the lamp body are provided with lamp covers, one side of each of the two lamp covers is provided with a fixed column, and a connecting rod is arranged between the two fixed columns; the lamp panel is provided with a mounting seat, a telescopic rod is hinged to the mounting seat, a buckle sleeve fastened with the connecting rod is arranged at the end of the telescopic rod, and a notch is formed in one side of the buckle sleeve.
In the aforesaid unmanned aerial vehicle intelligent airport ground system, the tip of fixed column is equipped with a plurality of magnetic chuck along the circumferencial direction, and magnetic chuck's one end is articulated with the fixed column to the realization draws in or expandes outward to the fixed column in to the fixed column, and the terminal surface of fixed column is equipped with the recess that supplies the magnetic chuck embedding that draws in.
In the aforesaid unmanned aerial vehicle intelligent airport ground system, the bottom one side of removing the base is equipped with the stabilizer blade, and the bottom opposite side of removing the base is equipped with removes the wheel, and the bottom of stabilizer blade is less than the bottom of removing the wheel, and the top of removing the base is equipped with the push-and-pull rod and supports the support frame that the lift lamp pole crouched down.
Compared with the prior art, the runway design is optimized, the airport capacity is improved, the height-adjustable blocking device is arranged, the runway distance can be effectively reduced, the taking-off and landing requirements of short-distance and long-distance unmanned aerial vehicles are met, the blocking device is arranged in a multi-damping buffer mode, the damage of impact force to the blocking device is reduced, the service life is prolonged, pedestrians cannot be interfered when the blocking device is not used, and the use is safer and more convenient; the arresting cable is high in strength and strong in bearing capacity, and the stable and balanced arresting state of the arresting cable is guaranteed by the matching of the support rod and the gravity ball when the arresting cable is used;
the movable emergency lighting device is arranged, the lighting device can be moved to a required position at will, the use is flexible, the lighting device can be lifted, turned and adjusted when in use, the lighting range is expanded, the detachable movable lamp is also arranged, the lighting device can be carried by hand or fixed on an unmanned aerial vehicle for lighting, and the unmanned aerial vehicle system is more targeted and convenient to maintain and inspect; when not in use, the folding chair can be folded and folded, and is convenient to move.
Therefore, the invention has the characteristics of large airport capacity, long service life of the arresting device and convenience for maintenance and inspection of the unmanned aerial vehicle system.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic view of the structure of the arresting means;
FIG. 3 is a schematic view of the connection of the arrester cord within the anchor block;
FIG. 4 is a schematic structural view of the lifting device;
FIG. 5 is a schematic view of the structure of the arrester cord;
FIG. 6 is a schematic view of the construction of the mobile emergency lighting device;
FIG. 7 is a schematic view of a lamp panel;
fig. 8 is a schematic view of the structure of the mobile lamp.
Reference numerals: 1. parking apron; 2. a flight runway; 3. a stopping device; 31. a blocking seat; 311. a winding chamber; 312. a guide cavity; 32. a stopper cable; 321. a resin coating layer; 322. a sleeve; 323. a slip-stopping ring; 324. a reinforcing bar; 325. a self-tapping screw; 326. a movable sleeve; 327. a support bar; 328. a gravity ball; 33. a cable feeding wheel; 34. a cable discharging wheel; 341. a damper; 35. a guide wheel; 36. a transverse slide rail; 37. a guard wheel; 38. protecting the push rod; 39. a damping sleeve; 4. a mobile emergency lighting device; 41. moving the base; 411. a support leg; 412. a moving wheel; 413. a push-pull rod; 414. a support frame; 42. a fixed seat; 43. a rotating arm; 44. lifting the lamp post; 45. a lamp panel; 46. fixing the lamp; 47. moving the lamp; 5. a lifting device; 51. a rack; 52. a gear; 53. a drive motor; 54. a fixed mount; 541. a fixing plate; 55. an electric push rod; 61. a lamp body; 62. a lamp cover; 63. fixing a column; 631. a magnetic chuck; 632. a groove; 64. a connecting rod; 65. a mounting seat; 66. a telescopic rod; 67. and (6) buckling and sleeving.
The invention is further described with reference to the following figures and detailed description.
Detailed Description
The embodiment of the invention comprises the following steps: as shown in fig. 1-3, the intelligent airport ground system for unmanned aerial vehicles comprises an air park 1, a flight runway 2 and a lighting system, wherein the flight runway 2 comprises a main runway area communicated with the air park 1, the main runway area is a cross runway, the runway capacity is increased, the length of the main runway area can be 600-800 m, a secondary runway area can be arranged at the main runway area according to requirements, and the length of the secondary runway area can be 600m so as to meet the functional requirements of the unmanned aerial vehicles in non-short take-off and landing states.
The crossing runway is provided with a stopping device 3, the stopping device 3 comprises stopping seats 31 positioned at two sides of the runway and a stopping cable 32 positioned between the two stopping seats 31, a winding cavity 311 and a guide cavity 312 are arranged in the stopping seats 31, an upper cable wheel 33 and a lower cable wheel 34 are rotatably connected in the winding cavity 311 through a driving shaft, one end of the driving shaft is provided with a damper 341, and the other end of the driving shaft is provided with a winding motor and a clutch (not shown) for driving the upper cable wheel 33 and the lower cable wheel 34 to rotate. A protection assembly is arranged between the upper cable pulley 33 and the lower cable pulley 34 and comprises a transverse slide rail 36 positioned between the upper cable pulley 33 and the lower cable pulley 34, a protection wheel 37 is connected onto the transverse slide rail 36 in a sliding manner, the protection wheel 37 is connected with a protection push rod 38 through an installation frame, a damping sleeve 39 is sleeved outside the protection push rod 38, the damping sleeve 39 is fixedly connected with the blocking seat 31, and the protection push rod 38 extends into the damping sleeve 39 and is connected with the damping sleeve 39 through a tension spring; a guide wheel 35 which is connected by a lifting device 5 and moves up and down is arranged in the guide cavity 312; one end of the arrester wire 32 is fixed to the arrester seat 31, and the free end of the arrester wire 32 passes around the lower wire wheel 34, the guard wheel 37, the upper wire wheel 33 and the guide wheel 35, respectively, and extends outward to the arrester seat 31 on the other side.
The set arresting device 3 can effectively reduce the runway distance, reduce the safety distance of the runway to 400m and realize the emergency braking of the airplane under the emergency condition. The arrester cord 32 is wound on the upper cord wheel 33 and the lower cord wheel 34, the length of the arrester cord 32 can be automatically adjusted by the winding of the winding motor, and the arrester cord 32 is guided by the guide wheel 35 which can move up and down, so that the height of the arrester cord 32 can be adjusted, when the arrester cord is not used, the length of the arrester cord 32 can be properly lengthened, the height of the arrester cord 32 can be reduced, and the interference to pedestrians can be avoided. When the unmanned aerial vehicle lands, the height of the arresting cable 32 is adjusted according to the model of the unmanned aerial vehicle and the position of the arresting hook, so that the arresting hook of the unmanned aerial vehicle can be smoothly hooked to the arresting cable 32, the arresting cable 32 is slowly released under the action of the damper 341, and the damping arresting of the arresting cable 32 on the unmanned aerial vehicle is realized; when the arresting cable 32 wound on the upper cable wheel 33 and the lower cable wheel 34 is nearly exhausted, the arresting cable 32 pulls the protection wheel 37, so that the protection wheel 37 slowly moves along the transverse slide rail 36 under the damping action of the damping sleeve 39 and the tension spring to relieve the impact force and better protect the arresting device 3.
As shown in fig. 4, the lifting device 5 includes a rack 51 slidably connected to the blocking seat 31, the guide wheel 35 is mounted on the top of the rack 51, a gear 52 driven by a driving motor 53 is engaged on the rack 51, a fixing frame 54 connected to an electric push rod 55 is disposed on one side of the gear 52, and a fixing plate 541 engaged with the gear 52 is disposed on the fixing frame 54. The driving motor 53 drives the gear 52 to rotate, so as to drive the rack 51 and the guide wheel 35 engaged therewith to move up and down, and when the proper position is adjusted, the electric push rod 55 pushes the fixing plate 541 to engage with the gear 52, so as to fix the rack 51 and maintain the height position of the blocking cable 32.
As shown in fig. 5, the arrester cord 32 is composed of four steel cables, the arrester cord 32 includes a middle main body section and two connecting sections, a resin coating 321 is disposed outside the main body section, a sleeve 322 is movably connected to the connecting sections, two sides of the sleeve 322 are fixed by a slip ring 323, the sleeve 322 is in threaded connection with the arrester seat 31, the end portions of the connecting sections penetrate through the sleeve 322 and are respectively connected with four reinforcing rods 324, and self-tapping screws 325 in cross connection with the arrester seat 31 are disposed at the end portions of the four reinforcing rods 324.
The arranged resin coating 321 is coated on the main body section of the arresting cable 32 formed by four steel cables, so that the strength and the fastening performance of the arresting cable 32 are improved, the arresting cable 32 is doubly fixed with the arresting seat 31 by using the sleeve 322 and the self-tapping screw 325, the fixing performance of the arresting cable 32 is greatly improved, the sleeve 322 is tightly combined with the steel cables by the arranged slip ring 323, the slip is not easy to slip, and the fixing stability is improved; the resin coating layer 321, the slip-preventing ring 323, the sleeve 322 and the reinforcing rod 324 are used for protecting and reinforcing the arresting cable 32, so that the strength of the arresting cable 32 is improved, the strength of the arresting seat 31 for bearing the arresting cable 32 is improved, and the service life is prolonged.
The main body section is provided with a movable sleeve 326, the movable sleeve 326 is in clearance connection with the resin coating 321, the bottom of the movable sleeve 326 is provided with two splayed support rods 327, and the end parts of the support rods 327 are rotatably connected with gravity balls 328. Under the action of gravity of the gravity ball 328, the support rod 327 is always kept in a downward state, and the gravity ball 328 is in rolling contact with the ground of the runway, so that the main body section is supported and balanced, the arresting cable 32 is kept in a stable arresting state under the guiding action of the guide wheel 35 and a certain height away from the ground, and the arresting cable 32 slides towards two sides under stress due to the sliding connection of the movable sleeve 326, so that the arresting hook of the unmanned aerial vehicle cannot be influenced to hook the arresting cable 32.
As shown in fig. 6, the lighting system includes a mobile emergency lighting device 4, facilitating maintenance and inspection of the drone system. The movable emergency lighting device 4 comprises a movable base 41, wherein one side of the bottom of the movable base 41 is provided with a support leg 411, the other side of the bottom of the movable base 41 is provided with a movable wheel 412, the bottom of the support leg 411 is lower than the bottom of the movable wheel 412, and a push-pull rod 413 and a support frame 414 for supporting the lifting lamp pole 44 to lie down are arranged above the movable base 41. The design of push-pull rod 413 is convenient for artifical manual removal or is connected with the vehicle, utilizes the vehicle to drive lighting device and removes, conveniently removes lighting device to required position, uses nimble motor-driven.
Be equipped with fixing base 42 on the removal base 41, articulated on the fixing base 42 have a rotor arm 43, rotate on the rotor arm 43 and be connected with lift lamp pole 44, the tip of lift lamp pole 44 rotates and is connected with lamp panel 45, is equipped with fixed lamp 46 and removal lamp 47 on the lamp panel 45. When the lighting device is used, the lifting lamp post 44 is erected, and the height of the lifting lamp post 44 is adjusted, so that the lighting range is adjusted, and the lifting lamp post 44 can be of a conventional multi-section pipeline structure and fixed through bolts or of an electric cylinder telescopic rod 66 structure; when the lifting lamp pole 44 is not used, the lifting lamp pole 44 is contracted, bent to be in a horizontal state and fixed by the support frame 414, and the lifting lamp pole is convenient to move.
As shown in fig. 7, the movable lamp 47 includes a lamp body 61, two ends of the lamp body 61 are provided with lamp covers 62, one side of each of the two lamp covers 62 is provided with a fixing post 63, and a connecting rod 64 is arranged between the two fixing posts 63; the lamp panel 45 is provided with a mounting seat 65, the mounting seat 65 is hinged with a telescopic rod 66, the end part of the telescopic rod 66 is provided with a buckle sleeve 67 buckled with the connecting rod 64, and one side of the buckle sleeve 67 is provided with a notch.
As shown in fig. 8, a plurality of magnetic suckers 631 are disposed at an end of the fixing column 63 along a circumferential direction, one end of each magnetic sucker 631 is hinged to the fixing column 63, so as to be retracted into the fixing column 63 or extended out of the fixing column 63, and a groove 632 for allowing the retracted magnetic sucker 631 to be inserted into is disposed on an end surface of the fixing column 63.
The removal lamp 47 that sets up on lamp panel 45 is through detaining cover 67 demountable installation on mount pad 65, and adjust the illumination position who removes lamp 47 through telescopic link 66 and connecting rod 64, it is nimble to use, can also take off removal lamp 47 from mount pad 65, through the rotatory expansion with magnetic chuck 631, adsorb and fix on unmanned aerial vehicle, improve fixed stability, be convenient for maintain and overhaul unmanned aerial vehicle, just draw in the recess 632 with the rotation of magnetic chuck 631 when not using in, reduce occupation space.
Claims (9)
1. Unmanned aerial vehicle intelligent airport ground system, its characterized in that: the device comprises an air park (1), a flight runway (2) and a light system, wherein a stopping device (3) is arranged on the flight runway (2), the stopping device (3) comprises stopping seats (31) positioned on two sides of the runway and stopping cables (32) positioned between the two stopping seats (31), an upper cable wheel (33) and a lower cable wheel (34) are arranged in the stopping seats (31), a protection assembly is arranged between the upper cable wheel (33) and the lower cable wheel (34), guide wheels (35) which are connected through a lifting device (5) and move up and down are arranged at the tops of the stopping seats (31), one ends of the stopping cables (32) are fixed with the stopping seats (31), and the free ends of the stopping cables (32) respectively bypass the lower cable wheel (34), the protection assembly, the upper cable wheel (33) and the guide wheels (35) and extend outwards; the lighting system comprises a movable emergency lighting device (4), the movable emergency lighting device (4) comprises a movable base (41), a fixed seat (42) is arranged on the movable base (41), a rotating arm (43) is hinged to the fixed seat (42), a lifting lamp pole (44) is connected to the rotating arm (43) in a rotating mode, a lamp panel (45) is arranged at the end portion of the lifting lamp pole (44), and a fixed lamp (46) and a movable lamp (47) are arranged on the lamp panel (45).
2. The unmanned aerial vehicle intelligent airport ground system of claim 1, wherein: a winding cavity (311) and a guide cavity (312) are arranged in the fixed seat (42), the upper cable pulley (33) and the lower cable pulley (34) are rotatably connected into the winding cavity (311) through a driving shaft, a damper (341) is arranged at one end of the driving shaft, a winding motor and a clutch for driving the upper cable pulley (33) and the lower cable pulley (34) to rotate are arranged at the other end of the driving shaft, and the guide pulley (35) is located in the guide cavity (312).
3. The unmanned aerial vehicle intelligent airport ground system of claim 1, wherein: the protection component is including being located horizontal slide rail (36) between cable pulley (33) and lower cable pulley (34), and sliding connection has protection wheel (37) on horizontal slide rail (36), and protection wheel (37) are connected with protection push rod (38) through the mounting bracket, and the outside cover of protection push rod (38) is equipped with damping cover (39), and protection push rod (38) are connected with damping cover (39) through the extension spring in stretching into damping cover (39).
4. The unmanned aerial vehicle intelligent airport ground system of claim 1, wherein: the lifting device (5) comprises a rack (51) which is in sliding connection with the blocking seat (31), the guide wheel (35) is fixedly connected with the rack (51), a gear (52) driven by a driving motor (53) is meshed on the rack (51), a fixing frame (54) connected with an electric push rod (55) is arranged on one side of the gear (52), and a fixing plate (541) which is in matched meshing with the gear (52) is arranged on the fixing frame (54).
5. The unmanned aerial vehicle intelligent airport ground system of claim 1, wherein: the arrester cord (32) is composed of four steel cables, the arrester cord (32) comprises a middle main body section and connecting sections at two ends, a resin coating layer (321) is arranged outside the main body section, a sleeve (322) is movably connected onto the connecting sections, two sides of the sleeve (322) are fixed through slip stopping rings (323), the sleeve (322) is in threaded connection with the arrester base (31), the end portions of the connecting sections penetrate through the sleeve (322) and are respectively connected with four reinforcing rods (324), and self-tapping screws (325) which are connected with the arrester base (31) in a cross shape are arranged at the end portions of the four reinforcing rods (324).
6. The unmanned aerial vehicle intelligent airport ground system of claim 5, wherein: the main body section is provided with a movable sleeve (326), the movable sleeve (326) is in clearance connection with the resin coating layer (321), the bottom of the movable sleeve (326) is provided with two splayed support rods (327), and the end parts of the support rods (327) are rotatably connected with gravity balls (328).
7. The unmanned aerial vehicle intelligent airport ground system of claim 1, wherein: the movable lamp (47) comprises a lamp body (61), lamp covers (62) are arranged at two ends of the lamp body (61), fixing columns (63) are arranged on one sides of the two lamp covers (62), and a connecting rod (64) is arranged between the two fixing columns (63); the lamp panel (45) is provided with a mounting seat (65), the mounting seat (65) is hinged with a telescopic rod (66), the end part of the telescopic rod (66) is provided with a buckle sleeve (67) buckled with the connecting rod (64), and one side of the buckle sleeve (67) is provided with a notch.
8. The unmanned aerial vehicle intelligent airport ground system of claim 7, wherein: the end part of the fixed column (63) is provided with a plurality of magnetic suckers (631) along the circumferential direction, one end of each magnetic sucker (631) is hinged to the fixed column (63), so that the magnetic suckers can be folded inwards to the fixed column (63) or unfolded outwards to the fixed column (63), and a groove (632) for embedding the magnetic suckers (631) to be folded is formed in the end face of the fixed column (63).
9. The unmanned aerial vehicle intelligent airport ground system of claim 1, wherein: one side of the bottom of the movable base (41) is provided with a support leg (411), the other side of the bottom of the movable base (41) is provided with a movable wheel (412), the bottom of the support leg (411) is lower than the bottom of the movable wheel (412), and a push-pull rod (413) and a support frame (414) for supporting the lifting lamp pole (44) to lie down are arranged above the movable base (41).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110930228.0A CN113665832B (en) | 2021-08-13 | 2021-08-13 | Unmanned aerial vehicle intelligent airport ground system |
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| Application Number | Priority Date | Filing Date | Title |
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| CN202110930228.0A CN113665832B (en) | 2021-08-13 | 2021-08-13 | Unmanned aerial vehicle intelligent airport ground system |
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| CN113665832A true CN113665832A (en) | 2021-11-19 |
| CN113665832B CN113665832B (en) | 2024-03-15 |
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Citations (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4679369A (en) * | 1985-03-15 | 1987-07-14 | Wickes Manufacturing Company | Anchoring system |
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| CN112678197A (en) * | 2021-01-19 | 2021-04-20 | 西安爱生技术集团公司 | Herringbone supporting structure of unmanned aerial vehicle arresting cable, arresting system and method |
| CN112678196A (en) * | 2021-01-19 | 2021-04-20 | 西安爱生技术集团公司 | Cross-shaped supporting structure of unmanned aerial vehicle arresting cable, arresting system and method |
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| US4679369A (en) * | 1985-03-15 | 1987-07-14 | Wickes Manufacturing Company | Anchoring system |
| US6779756B1 (en) * | 2003-05-19 | 2004-08-24 | Engineered Arresting Systems Corporation | Low-profile brake-in-spool aircraft arresting systems |
| US6981673B1 (en) * | 2004-11-05 | 2006-01-03 | The United States Of America As Represented By The Secretary Of The Navy | Wear resisting sleeve system for aircraft landing arresting cables |
| US20120067020A1 (en) * | 2009-02-25 | 2012-03-22 | Andrew Paddock | Composite cable |
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| CN104002980A (en) * | 2013-02-21 | 2014-08-27 | 上海市南洋模范中学 | Carrier-based aircraft landing assist device |
| CN108443696A (en) * | 2017-02-16 | 2018-08-24 | 林钜于 | Panel is with carrying drag-line in processing procedure |
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| CN112678196A (en) * | 2021-01-19 | 2021-04-20 | 西安爱生技术集团公司 | Cross-shaped supporting structure of unmanned aerial vehicle arresting cable, arresting system and method |
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| Publication number | Publication date |
|---|---|
| CN113665832B (en) | 2024-03-15 |
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