CN113431409A - Unmanned aerial vehicle hangar - Google Patents
Unmanned aerial vehicle hangar Download PDFInfo
- Publication number
- CN113431409A CN113431409A CN202110782716.1A CN202110782716A CN113431409A CN 113431409 A CN113431409 A CN 113431409A CN 202110782716 A CN202110782716 A CN 202110782716A CN 113431409 A CN113431409 A CN 113431409A
- Authority
- CN
- China
- Prior art keywords
- unmanned aerial
- aerial vehicle
- plate
- lifting
- displacement
- 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
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
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
An unmanned aerial vehicle hangar comprises a lifting device, a transverse moving device, an unmanned aerial vehicle stopping and conveying frame and an unmanned aerial vehicle foot lock device; the lifting device is composed of two lifting units which are correspondingly arranged on the left and right surfaces and can realize up-down displacement, and an unmanned aerial vehicle stopping conveying frame which is erected between the two lifting units and can realize up-down displacement, so that a main framework of the lifting device of the unmanned aerial vehicle is formed; the unmanned aerial vehicle stopping conveying frame located between the two groups of lifting unit assemblies correspondingly arranged on the left and right sides can realize the horizontal displacement of the unmanned aerial vehicle stopping conveying frame between the front and back adjacent lifting unit assemblies under the action of the transverse moving device through another group of lifting units with the same structure and arranged in the front or back adjacent positions of the two groups of lifting units and the transverse moving device clamped and fixed between the upper and lower positions of the front and back groups of lifting units; from this the general framework of unmanned aerial vehicle hangar that constitutes to have multilayer multiseriate structure.
Description
Technical Field
The invention relates to an unmanned aerial vehicle hangar, and belongs to the technical field of unmanned aerial vehicle storage application.
Background
In the present stage, since the unmanned aerial vehicle has many advantages, it is used not only in the military field but also gradually spread to the fields of entertainment industry, agriculture, industry, and commercial circulation, etc., and it is increasingly showing its wide prospective. However, the storage of the unmanned aerial vehicle, especially for small-sized unmanned aerial vehicles, is a troublesome problem, not only because the unmanned aerial vehicle equipment is a precise intelligent instrument and cannot be stored in an overlapping manner; but would take up a large amount of floor space if a floor-laid arrangement were used.
Therefore, how to solve the problem of storing the whole unmanned aerial vehicle after being assembled is a technical problem that needs to be solved urgently by users.
Disclosure of Invention
The purpose of the invention is to: the unmanned aerial vehicle hangar not only can enable an unmanned aerial vehicle to realize three-dimensional storage, but also can put the stored unmanned aerial vehicle out of the garage and put the unmanned aerial vehicle off the garage at any time to be put into use.
The above object is achieved by the following technical scheme:
the unmanned aerial vehicle hangar comprises a lifting device, a transverse moving device 2, an unmanned aerial vehicle stopping and conveying frame 3 and an unmanned aerial vehicle foot lock mechanism 4; the lifting device comprises a group of lifting units 1 which are correspondingly arranged on the left and right sides, and an unmanned aerial vehicle stopping and conveying frame 3 which is erected between the two lifting units 1 and can realize vertical displacement, so that a main framework of the lifting units 1 for storing the unmanned aerial vehicle is formed; meanwhile, through another group of lifting units 1 with the same structure arranged at the front or rear adjacent position of the two groups of lifting units 1 and a traversing device 2 clamped and fixed between the upper and lower positions of the front and rear groups of lifting units 1, the unmanned aerial vehicle stopping and conveying frame 3 positioned between the two groups of lifting unit assemblies correspondingly arranged on the left and right sides can realize the horizontal displacement of the unmanned aerial vehicle stopping and conveying frame 3 between the front and rear adjacent lifting unit assemblies under the action of the traversing device 2; from this the general framework of unmanned aerial vehicle hangar that constitutes to have multilayer multiseriate structure.
Furthermore, the lifting unit 1 comprises two H-shaped plate vertical columns 1.1 which are vertically arranged on the same vertical column bottom plate 1.7 in a parallel shape, an annular chain transmission mechanism arranged between the two H-shaped plate vertical columns 1.1 and a lifting motor 1.5 arranged at the upper part of one H-shaped plate vertical column 1.1; the annular chain transmission mechanism consists of an annular chain 1.4, a main transmission chain wheel 1.3 and a main transmission shaft 1.2 which are arranged at the upper parts of two H-shaped plate body upright columns, and an auxiliary transmission chain wheel 1.8 and an auxiliary transmission shaft 1.9 which are arranged at the lower parts of the two H-shaped plate body upright columns, wherein the main transmission chain wheel 1.3 on the main transmission shaft 1.2 which is driven by a gear of a gear transmission mechanism 1.51 meshed with the output shaft end of a lifting motor 1.5 realizes the up-and-down circulating transmission by the auxiliary transmission chain wheel 1.8 and the auxiliary transmission shaft 1.9 which are simultaneously arranged at the lower parts of the two H-shaped plate body upright columns 1.1 through the annular chain 1.4 which surrounds the main transmission chain wheel and the auxiliary transmission chain wheel, thereby; meanwhile, the inner side edge parts of the two H-shaped plate upright posts 1.1 are respectively provided with a guide groove 1.10 from top to bottom, and the outer chain body of the ring-shaped chain 1.4 is provided with a plurality of uniformly distributed transverse roller way assemblies 1.6 which circularly move along with the ring-shaped chain 1.4.
Further, the transverse moving roller way assembly mechanism 1.6 comprises a roller way assembly main mounting plate 1.61, two groups of nylon guide wheel sets 1.62 which are arranged on the outer plate surface of the roller way assembly main mounting plate 1.61 and can rotate by depending on a fixed shaft and are distributed in an up-and-down parallel manner, and two groups of guide rail anti-overturning pulleys 1.63 arranged at the left end and the right end of the plate surface of the roller way assembly main mounting plate 1.61; wherein: the back surface of the roller way component main mounting plate 1.61 is connected with a mounting chain plate 1.67 arranged in the ring-shaped chain 1.4 through a screw; the two groups of guide rail anti-overturning pulleys 1.63 are respectively arranged on two parallel anti-overturning pulley arrangement plates 1.64 which are perpendicular to the edge part of the back surface of the roller way assembly main arrangement plate 1.61, and the distance between the adjacent wheel edges of the upper and lower groups of guide rail anti-overturning pulleys 1.63 is matched with the thickness of the H-shaped plate body at the edge part of the H-shaped plate body upright post 1.1.
Further, still be equipped with the vertical guide pulley 1.65 of a set of unmanned aerial vehicle on the main mounting plate 1.61 of roller assembly, the vertical guide pulley 1.65 of unmanned aerial vehicle set up on the main mounting plate 1.61 back panel body of roller assembly between the two sets of nylon guide pulley group 1.62 that are upper and lower distribution to through setting up two unmanned aerial vehicle frame side guide wheel holes 1.68 on the main mounting plate 1.61 of roller assembly, be arranged in stopping the outside limit butt of the side grudging post 3.4 in the carriage 3 with unmanned aerial vehicle.
Furthermore, the upper and lower parts of the outer side plate surfaces of the two H-shaped plate vertical columns 1.1 are respectively provided with a bolt mechanism 7, and the outer side plate surface of the H-shaped plate vertical column 1.1 between the two bolt mechanisms 7 is also provided with a bulkhead connecting piece 6.
Furthermore, the traversing device 2 consists of a friction driving mechanism which is arranged on a displacement bracket assembly capable of moving back and forth and takes a traversing driving motor 2.1 as a power source, and a horizontal driving reset mechanism which takes a cylinder 2.6 and a pre-tightening spring assembly as power sources; the transverse moving driving motor 2.1 is vertically arranged on the motor base 2.3, and a friction driving mechanism in an isosceles triangle layout is formed by a motor output shaft end driving wheel 2.2 arranged at the output shaft end of the transverse moving driving motor 2.1 and two friction driving belt wheels 2.20 arranged on the upper plane of the same displacement bracket component; and a friction driving mechanism is formed by two friction driving wheels 2.17 arranged between the friction driving upper support plate 2.16 and the friction driving lower support plate 2.19 which form the displacement support assembly and at the lower output shaft ends of two friction driving belt wheels 2.20 arranged on the friction driving upper support plate 2.16; the horizontal driving reset mechanism consists of a pneumatic propulsion structure taking a cylinder 2.6 as power and a compression reset structure taking a pre-tightening spring 2.8 as power; the unmanned aerial vehicle stopping conveying frame 3 can be clamped from the left side and the right side and can be lifted along the guide grooves 1.10 in the lifting units 1, and meanwhile, the unmanned aerial vehicle stopping conveying frame 3 can be enabled to horizontally displace between the front and the rear adjacent lifting units outside the upper and lower notches of the guide grooves 1.10 in the front and the rear lifting units.
Furthermore, the displacement bracket assembly is composed of a friction driving upper support plate 2.16, a friction driving lower support plate 2.19, two vertically arranged guide rail sliding blocks 2.13 which are arranged on the friction driving upper support plate 2.16 and the front part of the friction driving lower support plate 2.19 in a left-right way, and two vertically arranged spring guide pillar fixing plates 2.10 which are arranged on the friction driving upper support plate 2.16 and the rear part of the friction driving lower support plate 2.19, so that an integral framework of the displacement bracket assembly capable of realizing front-back displacement on the base 2.14 is formed; the displacement support assembly is located on a translation mechanism which is arranged on the inner bottom surface of the base 2.14 and is composed of a slide rail 2.12 and a linear guide rail slide block 2.21, and a translation structure controlled by the cylinder 2.6 and a pre-tightening spring assembly is formed by a cylinder mounting plate 2.22 arranged on the surfaces of the two spring guide pillar fixing plates 2.10 and a spring guide pillar 2.9 arranged on the surfaces of the spring guide pillar fixing plates 2.10 positioned on the two sides of the cylinder mounting plate 2.22.
Furthermore, the left side and the right side of the base 2.14 are respectively provided with a mounting seat 2.11 vertical to the base surface, the plate surface at the rear part of the base 2.14 is respectively provided with two spring base plates 2.4 vertical to the base surface and a cylinder base 2.5 positioned between the two spring base plates, the cylinder base 2.5 is arranged at the middle position, the left side and the right side are respectively provided with the spring base plates 2.4, so that a placement space for the cylinder 2.6 and the pre-tightening spring 2.8 facing the rear part of the displacement bracket assembly is formed, a spring guide post 2.9 provided with the pre-tightening spring 2.8 is penetrated in a linear bearing 2.7 arranged in the central hole of the spring base plate 2.4, and the front end of the spring guide post 2.9 is fixed on a spring guide post fixing plate 2.10 at the rear part of the displacement bracket assembly, thereby forming the displacement bracket assembly reset assembly relying on the pre-tightening spring; meanwhile, the front end of a piston rod 2.23 extending outwards of an air cylinder 2.6 arranged at the position of an air cylinder base 2.5 is matched with an air cylinder front end mounting plate 2.22 fixed with a left spring guide post fixing plate 2.10 and a right spring guide post fixing plate 2.10 at the rear part of a displacement support assembly, so that a horizontal driving assembly of the displacement support assembly depending on the air cylinder is formed; meanwhile, a group of sliding mechanisms for arranging the displacement support assembly are arranged on the inner base surface of the base 2.14, each sliding mechanism consists of two sliding rails 2.12 arranged on the inner bottom surface of the base 2.14 and a linear guide rail sliding block 2.21 matched with the sliding rails, and the displacement support assembly is fixed on the linear guide rail sliding block 2.21.
Furthermore, the linear guide rail slide block 2.21 is abutted with a guide rail slide block 2.13, the front surface of which is provided with two groups of transverse moving pulleys 2.15 which are distributed in parallel up and down.
Further, unmanned aerial vehicle shut down carriage 3 be a U type framework of constituteing by chassis 3.1 and the side grudging post 3.4 that sets up at chassis 3.1 both ends, wherein side grudging post 3.4 upper portion respectively be equipped with two interval certain interval be furnished with pulley support 3.3 of pulley 3.2 to still be equipped with tool to lock fixed orifices 3.5 on chassis 3.1.
Further, unmanned aerial vehicle foot tool to lock mechanism 4 correspond by a set of left and right sides and set up L shape foot rest 4.1 on unmanned aerial vehicle shuts down carriage 3 and constitute, inboard bottom of foot rest 4.1 be equipped with be applied to with the unmanned aerial vehicle shut down the fixed orifice plate 4.10 that tool to lock fixed orifices 3.5 matches on carriage 3, be equipped with slide rail 4.2, slider 4.3, lock foot 4.4, connecting rod 4.5, extension spring 4.6, foot rest 4.7 on the inboard roller way subassembly owner mounting plate of foot rest 4.1 to the top of foot rest 4.1 that sets up is equipped with two draw-in grooves 4.9 that realize the joint with unmanned aerial vehicle bottom supporting legs 5 and the locking otic placode 4.8 of closed draw-in groove 4.9 at vertical form.
According to the unmanned aerial vehicle hangar provided by the technical scheme, the storage problem of various small unmanned aerial vehicles can be effectively solved, the unmanned aerial vehicles can be timely put into use as required, and an effective solution is provided for unmanned aerial vehicle manufacturers and users.
It is characterized in that:
1) a space capable of being stored and parked in a stereoscopic mode is provided for the unmanned aerial vehicle.
2) Any unmanned aerial vehicle in the hangar can be flexibly called to carry out the warehouse-out operation.
3) The system can be used as a vehicle-mounted machine warehouse and can also be used as a storage warehouse which is statically mounted on the ground.
Drawings
Fig. 1 is a schematic view of the overall structure of an unmanned aerial vehicle hangar according to the present invention;
FIG. 2 is a schematic structural view of the lifting unit;
FIG. 3 is a schematic front view of the traverse roller assembly;
FIG. 4 is a schematic view of a back structure of the traverse roller assembly;
FIG. 5 is a schematic view of the overall configuration of the traverse device;
FIG. 6 is an exploded view of the traversing apparatus;
FIG. 7 is a front plan view of the traversing device of FIG. 5;
FIG. 8 is a sectional view taken along line A-A of FIG. 7;
FIG. 9 is a right side view of FIG. 5;
fig. 10 is a schematic structural view of the unmanned aerial vehicle parking carriage;
FIG. 11 is a schematic structural view of the locking device in the locking state;
fig. 12 is a schematic structural view of the unmanned aerial vehicle foot lock in an unlocked state.
In the figure:
1-lifting Unit
1.1-H-shaped plate body upright posts; 1.2-main drive shaft; 1.3-main drive sprocket; 1.4-ring type chain; 1.5-lifting motor; 1.6-transverse moving roller way component; 1.61-roller way assembly main setting plate;
1.62-nylon guide wheel; 1.63-guide rail overturn-preventing pulley; 1.64-overturn preventing pulley placing plate; 1.65-unmanned frame side guide pulley; 1.66-pulley shaft; 1.67-installing a chain plate;
1.68-side guide wheel hole of unmanned frame; 1.69-side guide pulley mount; 1.7-column bottom plate; 1.8-auxiliary drive sprocket; 1.9-auxiliary transmission shaft; 1.10-guide groove;
2-traversing device
2.1-a transverse moving driving motor; 2.2-the output shaft of the motor drives the wheel; 2.3-motor base;
2.4-spring base plate; 2.5-cylinder base; 2.6-cylinder; 2.7-linear bearings;
2.8-pre-tightening the spring; 2.9-spring guide post; 2.10-spring guide post fixing plate; 2.11-mounting seat; 2.12-slide rail; 2.13-guide rail slide block; 2.14-base; 2.15-traversing rollers;
2.16-friction drive upper bracket plate; 2.17-friction drive wheel; 2.18-drive belt;
2.19-friction drive lower carriage plate; 2.20-friction drive pulley; 2.21-linear guide slider;
2.22-cylinder mounting plate; 2.23-piston rod;
3-unmanned aerial vehicle shuts down carriage
3.1-underframe; 3.2-pulley; 3.3-pulley support; 3.4-side stand; 3.5-lock fixing hole; 4-unmanned aerial vehicle foot tool to lock mechanism
4.1-foot seat; 4.2-sliding rail; 4.3-sliding block; 4.4-locking feet; 4.5-connecting rod;
4.6-tension spring; 4.7-foot seat; 4.8-locking ear plate; 4.9-card slot.
Detailed Description
The invention is further explained by combining the drawings in the specification and provides an embodiment of the invention.
The unmanned aerial vehicle hangar is characterized in that the core originality of the unmanned aerial vehicle hangar is as follows according to the attached drawings 1-12 of the specification: through the unmanned aerial vehicle hangar of multilayer frame-type design, both realized that the unmanned aerial vehicle can realize the stratiform and deposit on multiseriate shelf support body, can rise automatically and the displacement according to the requirement of in-service use again simultaneously, the automatic positioning of being convenient for is used.
Fig. 1 shows a schematic overall structure diagram of the unmanned aerial vehicle hangar related to the invention.
The unmanned aerial vehicle hangar comprises a lifting device, a transverse moving device 2, an unmanned aerial vehicle stopping and conveying frame 3 and an unmanned aerial vehicle foot lock mechanism 4; the lifting device comprises a group of lifting units 1 which are correspondingly arranged on the left and right sides, and an unmanned aerial vehicle stopping and conveying frame 3 which is erected between the two lifting units 1 and can realize vertical displacement, so that a main framework of the lifting units 1 for storing the unmanned aerial vehicle is formed; meanwhile, through another group of lifting units 1 with the same structure arranged at the front or rear adjacent position of the two groups of lifting units 1 and a traversing device 2 clamped and fixed between the upper and lower positions of the front and rear groups of lifting units 1, the unmanned aerial vehicle stopping and conveying frame 3 positioned between the two groups of lifting unit assemblies correspondingly arranged on the left and right sides can realize the horizontal displacement of the unmanned aerial vehicle stopping and conveying frame 3 between the front and rear adjacent lifting unit assemblies under the action of the traversing device 2; from this the general framework of unmanned aerial vehicle hangar that constitutes to have multilayer multiseriate structure.
Fig. 2-8 show schematic structural diagrams of the unmanned aerial vehicle hangar forming device related to the invention.
Wherein fig. 2 shows a schematic mechanism diagram of the lifting unit 1 of the unmanned hangar.
The lifting unit 1 comprises two H-shaped plate vertical columns 1.1 which are vertically arranged on the same vertical column bottom plate 1.7 in a parallel shape, an annular chain transmission mechanism arranged between the two H-shaped plate vertical columns 1.1 and a lifting motor 1.5 arranged at the upper part of one H-shaped plate vertical column 1.1; the annular chain transmission mechanism consists of an annular chain 1.4, a main transmission chain wheel 1.3 and a main transmission shaft 1.2 which are arranged at the upper parts of two H-shaped plate body upright columns, and an auxiliary transmission chain wheel 1.8 and an auxiliary transmission shaft 1.9 which are arranged at the lower parts of the two H-shaped plate body upright columns, wherein the main transmission chain wheel 1.3 on the main transmission shaft 1.2 driven by a gear box 1.51 meshed with the output shaft end of a lifting motor 1.5 enables the auxiliary transmission chain wheel 1.8 and the auxiliary transmission shaft 1.9 which are simultaneously arranged at the lower parts of the two H-shaped plate body upright columns 1.1 to realize the up-and-down circulating transmission through the annular chain 1.4 which is encircled on the main transmission chain wheel and the auxiliary transmission chain wheel; thereby constituting a driving structure of the lifting unit 1.
Meanwhile, the lifting motor 1.5 is arranged on the outer side of the top of the H-shaped plate body upright post 1.1, and the lower part of the output shaft end of the lifting motor and a main transmission shaft 1.2 which is horizontally arranged form a driving structure of the lifting unit 1 through a gear transmission mechanism 1.51.
In addition, the inner side edge parts of the two H-shaped plate upright posts 1.1 are respectively provided with a guide groove 1.10 from top to bottom, and the outer chain body of the annular chain 1.4 is provided with a plurality of uniformly distributed transverse roller way assemblies 1.6 which circularly move along with the annular chain 1.4.
The transverse moving roller way component mechanism 1.6 comprises a roller way component main mounting plate 1.61, two groups of nylon guide wheel groups 1.62 which are arranged on the outer plate surface of the roller way component main mounting plate 1.61 and can rotate by depending on a fixed shaft and are distributed in an up-and-down parallel manner, and two groups of guide rail overturn-preventing pulleys 1.63 arranged at the left end and the right end of the plate surface of the roller way component main mounting plate 1.61; wherein: the back surface of the roller way component main mounting plate 1.61 is connected with a mounting chain plate 1.67 arranged in the ring-shaped chain 1.4 through a screw; the two groups of guide rail anti-overturning pulleys 1.63 are respectively arranged on two parallel anti-overturning pulley arrangement plates 1.64 which are perpendicular to the edge part of the back surface of the roller way assembly main arrangement plate 1.61, and the distance between the adjacent wheel edges of the upper and lower groups of guide rail anti-overturning pulleys 1.63 is matched with the thickness of the H-shaped plate body at the edge part of the H-shaped plate body upright post 1.1.
In the in-service use, the number of this kind of sideslip roller way subassembly mechanism 1.6 of setting on the 1.4 outer lane chain body of loop type chain should match with the corresponding number of piles that unmanned aerial vehicle was placed to whole unmanned aerial vehicle strorage device. The unmanned aerial vehicle storage device shown in fig. 1 and 2 is characterized in that three layers of unmanned aerial vehicles are stopped by the conveying frame 3, and therefore three transverse moving roller way assembly mechanisms 1.6 distributed at a certain interval are arranged on outer rings of corresponding annular chains 1.4. When the transverse moving roller way assembly mechanism 1.6 in operation is positioned at the lower part of the lifting device 1, the unmanned aerial vehicle stopped conveying frame 3 clamped between two rows of rollers 1.62 on the surface of the roller way assembly main mounting plate 1.61 forming the transverse moving roller way assembly mechanism 1.6 ascends along the guide grooves 1.10 positioned on the two H-shaped plate upright posts 1.1 in the lifting device 1 correspondingly arranged left and right.
In order to ensure the stability of the roller way component mounting plate 1.61 arranged on the annular chain 1.4 rotating along with the annular chain, the transverse roller way component mechanism 1.6 of the invention uses two groups of guide rail anti-overturning pulleys 1.63 on two anti-overturning pulley mounting plates 1.64 at the left and right ends of the back surface of the roller way component main mounting plate 1.61 in the transverse roller way component mechanism 1.6, and uses two groups of guide rail anti-overturning pulleys 1.63 arranged in a staggered way to respectively clamp the two guide rail anti-overturning pulleys 1.63 at the upper and lower positions on the inner side and the outer side of the same side flanging of the H-shaped plate body upright post 1.1, thereby further improving the stability of the transverse roller way component 1.6 synchronously rotating along with the annular chain 1.4.
The working principle of the lifting device is as follows:
the ring-shaped chains 1.4 correspondingly arranged in the two lifting units 1 synchronously rotate from bottom to top along with the simultaneous starting of the lifting motors 1.5 correspondingly arranged on the top of the group of lifting units 1 in a face-to-face mode and arranged on the left and right sides. Along with the synchronous rotation of the annular chain, the unmanned aerial vehicle stopping conveying frames 3 originally arranged in the left lifting unit and the right lifting unit, distributed in the corresponding annular chain 1.4 in a layered manner and supported on the roller way assembly main mounting plate 1.61 fixed together with the annular chain in the annular chain can stably and synchronously move upwards from bottom to top along with the rotation of the annular chain 1.4.
When unmanned aerial vehicle shut down carriage 3 under the effect of sideslip roller way subassembly mechanism 1.6, along guide slot 1.10 rise to guide slot 1.10 terminal, until breaking away from the upper and lower notch of guide slot, can realize under the effect of the sideslip device 2 that sets up on elevating gear 1 upper portion that unmanned aerial vehicle shut down the front and back displacement of carriage 3.
The upper part and the lower part of the outer side plate surfaces of the two H-shaped plate body upright posts 1.1 are respectively provided with a bolt mechanism 7, and the outer side plate surface of the H-shaped plate body upright post 1.1 between the two bolt mechanisms 7 is also provided with a bulkhead connecting piece 6.
Fig. 5-9 are schematic diagrams showing detailed structures of the traverse device of the unmanned aerial vehicle according to the present invention.
Wherein fig. 5 and 6 show a schematic perspective view of the entire traverse device and an exploded view of the constituent structure thereof, respectively.
The traversing device 2 shown in the figure is composed of a friction driving mechanism which is arranged on a displacement bracket assembly capable of moving forwards and backwards and takes a traversing driving motor 2.1 as a power source, and a horizontal driving reset mechanism which takes a cylinder 2.6 and a pre-tightening spring assembly as power sources; the transverse moving driving motor 2.1 is vertically arranged on the motor base 2.3, and a friction driving mechanism in an isosceles triangle layout is formed by a motor output shaft end driving wheel 2.2 arranged at the output shaft end of the transverse moving driving motor 2.1 and two friction driving belt wheels 2.20 arranged on the upper plane of the same displacement bracket component; a friction driving mechanism is formed by two friction driving wheels 2.17 which are arranged between the friction driving upper support plate 2.16 and the friction driving lower support plate 2.19 which form the displacement support assembly and pass through the lower output shaft ends of two friction driving belt wheels 2.20 arranged on the friction driving upper support plate 2.16; the horizontal driving reset mechanism consists of a pneumatic propulsion structure taking a cylinder 2.6 as power and a compression reset structure taking a pre-tightening spring 2.8 as power; the unmanned aerial vehicle stopping conveying frame 3 can be clamped from the left side and the right side and can be lifted along the guide grooves 1.10 in the lifting units 1, and meanwhile, the unmanned aerial vehicle stopping conveying frame 3 can be enabled to horizontally displace between the front and the rear adjacent lifting units outside the upper and the lower notches of the guide grooves 1.10 in the front and the rear lifting units.
The displacement bracket assembly is composed of a friction driving upper support plate 2.16, a friction driving lower support plate 2.19, two vertically arranged guide rail sliding blocks 2.13 which are arranged on the friction driving upper support plate 2.16 and the front part of the friction driving lower support plate 2.19 in a left and right way, and two vertically arranged spring guide pillar fixing plates 2.10 which are arranged on the friction driving upper support plate 2.16 and the rear part of the friction driving lower support plate 2.19, and thus, an integral framework of the displacement bracket assembly which can realize the front and back displacement on the base 2.14 is formed; the displacement support assembly is located on a translation mechanism which is arranged on the inner bottom surface of the base 2.14 and is composed of a slide rail 2.12 and a linear guide rail slide block 2.21, and a translation structure controlled by an air cylinder 2.6 and a pre-tightening spring assembly is formed by an air cylinder mounting plate 2.22 arranged on the surface of the two spring guide pillar fixing plates 2.10 and a column 2.9 arranged on the surface of the spring guide pillar fixing plate 2.10 positioned on the two sides of the air cylinder mounting plate 2.22.
The left side and the right side of the base 2.14 are respectively provided with a mounting seat 2.11 which is vertical to the base surface, the plate surface at the rear part of the base 2.14 is respectively provided with two spring base plates 2.4 which are vertical to the base surface and a cylinder base 2.5 which is positioned between the two spring base plates, the cylinder base 2.5 is arranged at the middle position, the left side and the right side are respectively provided with the spring base plates 2.4, thereby forming a placing space for the cylinder 2.6 and the pre-tightening spring 2.8 which face the rear part of the displacement bracket assembly, a linear bearing 2.7 which is arranged in a central hole of the spring base plate 2.4 is penetrated by a spring guide pillar 2.9 which is provided with the pre-tightening spring 2.8, and the front end of the spring guide pillar 2.9 is fixed on a spring guide pillar fixing plate 2.10 at the rear part of the displacement bracket assembly, thereby forming a displacement bracket assembly resetting structure which depends on the pre-tightening spring; meanwhile, the front end of a piston rod 2.23 extending outwards of an air cylinder 2.6 arranged at the position of an air cylinder base 2.5 is matched with an air cylinder front end mounting plate 2.22 fixed with a left spring guide post fixing plate 2.10 and a right spring guide post fixing plate 2.10 at the rear part of a displacement support assembly, so that a horizontal driving structure of the displacement support assembly propelled by the air cylinder is formed; meanwhile, a group of sliding mechanisms for arranging the displacement support assembly are arranged on the inner base surface of the base 2.14, each sliding mechanism consists of two sliding rails 2.12 arranged on the inner bottom surface of the base 2.14 and a linear guide rail sliding block 2.21 matched with the sliding rails, and the displacement support assembly is fixed on the linear guide rail sliding block 2.21, so that a horizontal displacement structure of the whole displacement support assembly is formed.
The working principle of the traversing device is as follows:
when the unmanned aerial vehicle which is required to ascend or descend in place is stopped and the conveying frame 3 is translated between the front and rear groups of lifting unit combinations, only the transverse moving driving motor 2.1 in the transverse moving device 2 is started. With the rotation of the traverse driving motor, the traverse driving motor 2.1 will make two friction driving pulleys 2,20 arranged on the friction driving upper bracket plate 2.16 synchronously rotate through the motor output shaft end driving wheel 2.2 at the front end of the motor output shaft, through the driving belt 2.18 surrounding the motor output shaft end driving wheel, and make two friction driving pulleys 2.17 arranged coaxially with the two friction driving pulleys 2,20 between the friction driving upper bracket plate 2.16 and the friction driving lower bracket plate 2.19 synchronously rotate through the two friction driving pulleys 2, 20; the unmanned aerial vehicle stopping conveying frame 3 can move forwards and backwards in the horizontal direction through the friction force generated by the two friction driving wheels 2.17 which are in close contact with the two ends of the unmanned aerial vehicle stopping conveying frame 3 and run in the same direction.
Meanwhile, in order to ensure that the two friction driving wheels 2.17 and the unmanned aerial vehicle stop the enough friction driving force between the conveying frames 3, the cylinder propelling mechanism which is arranged at the rear part of the shifting bracket assembly in the traversing device 2 and consists of the cylinder 2.6, the piston rod 2.23 and the two spring guide pillar fixing plates 2.10 arranged on the vertical plane at the rear parts of the friction driving upper bracket plate 2.16 and the friction driving lower bracket plate 2.19 is required to be started simultaneously, and due to the propelling action of the cylinder, the close contact degree of the front part of the whole shifting bracket assembly and the left and right ends of the unmanned aerial vehicle stop the conveying frames 3 can be increased, obviously, the effect is very effective for ensuring that the friction driving wheels 2.17 obtain the enough friction driving force.
Once the front and back translation action of the unmanned aerial vehicle stopping conveying frame 3 is completed, along with the stop work of the air cylinder 2.6 and the transverse moving driving motor 2.1, the close contact state of the friction driving wheel 2.17 and the two ends of the unmanned aerial vehicle stopping conveying frame 3 is finished.
At this time, in order to make the whole displacement bracket assembly retreat, a pre-tightening spring reset mechanism arranged between two spring guide post fixing plates 2.10 and a spring base plate 24 on the vertical surfaces of the friction driving upper bracket plate 2.16 and the friction driving lower bracket plate 2.19 plays a role; due to the action of the pre-tightening spring 2.8 sleeved on the spring guide post 2.9, the whole displacement support assembly is pulled back, so that the friction driving wheel 2.17 and the unmanned aerial vehicle stop conveying frame 3 are separated from the original stop working state.
Of course, the whole horizontal displacement motion needs to be supported on the linear guide rail sliding block 2.21 and the sliding rail 2.12 arranged on the base 2.14 by means of the whole displacement support assembly.
Meanwhile, it is pointed out that: the transverse moving device 2 is respectively arranged at the upper part and the lower part between the front and the back adjacent two groups of lifting units, the transverse moving device 2 at the lower part is arranged at the lower notch position of the guide groove 1.10 in the lifting unit 1, and the transverse moving device 2 at the upper part is arranged at the upper notch position of the guide groove 1.10 in the lifting unit 1.
Fig. 10-12 show specific structural diagrams of the unmanned aerial vehicle parking carrier 3 and the unmanned aerial vehicle foot lock according to the present invention, wherein fig. 10 is a schematic diagram of an overall structure of the unmanned aerial vehicle parking carrier.
The unmanned aerial vehicle stopping and conveying frame 3 shown in fig. 10 is a U-shaped framework composed of an underframe 3.1 and side stands 3.4 arranged at two ends of the underframe 3.1, wherein the upper parts of the side stands 3.4 are respectively provided with two pulley supports 3.3 which are provided with pulleys 3.2 at certain intervals, and the underframe 3.1 is also provided with a lock fixing hole 3.5.
Through the pulley 3.2 on the pulley support 3.3 that sets up on side grudging post 3.4 upper portion and the cooperation of the guide slot 1.10 of setting on platelike stand 1.1, make whole unmanned aerial vehicle carriage 3 realize displacement from top to bottom in the guide slot of injecing. Meanwhile, two rows of nylon guide wheels 1.62 which are matched with the upper surface and the lower surface of the side vertical frame 3.4 and arranged on a panel of a roller way assembly main mounting plate 1.61 in the transverse roller way assembly mechanism 1.6, and two unmanned aerial vehicle frame side guide pulleys 1.65 which are matched with the outer side surface of the side vertical frame 3.4 and arranged on a panel of the same roller way assembly main mounting plate 1.61 are utilized; the whole unmanned aerial vehicle conveying frame 3 completes lifting and translation actions in an interval limited between the left lifting unit 1 and the right lifting unit 1.
This kind of unmanned aerial vehicle foot tool to lock mechanism 4 shown in fig. 11, fig. 12 corresponds the L shape foot stool 4.1 that sets up on unmanned aerial vehicle shuts down carriage 3 by a set of left and right sides and constitutes, the inboard bottom of foot stool 4.1 be equipped with be used for with the unmanned aerial vehicle shut down the fixed orifice plate 4.10 that tool to lock fixed orifices 3.5 matches on carriage 3, be equipped with slide rail 4.2, slider 4.3, lock foot 4.4, connecting rod 4.5, extension spring 4.6, foot stool 4.7 on the inboard roller assembly owner mounting plate of foot stool 4.1 to the top of foot stool 4.1 that sets up at vertical form is equipped with two and realizes draw-in groove 4.9 and the locking otic placode 4.8 of closed draw-in groove 4.9 of joint with unmanned aerial vehicle bottom supporting legs 5.
The working principle of the unmanned aerial vehicle foot lock mechanism 4 is as follows:
two unmanned aerial vehicle foot lock mechanisms 4 which are symmetrical left and right are respectively fixed in corresponding lock fixing holes 3.5 of an underframe 3.1 of an unmanned aerial vehicle stopping conveying frame 3; unmanned aerial vehicle (unmanned aerial vehicle bottom sprag foot 5) spanes on two footstands 4.1 upper portions through the bottom to in the draw-in groove 4.9 of locating on two footstands 4.1 upper portions, stabilize whole unmanned aerial vehicle at unmanned aerial vehicle foot tool to lock mechanism 4 through locking otic placode 4.8 simultaneously. In case need use when unmanned aerial vehicle, as long as open locking otic placode 4.8 and just can make whole unmanned aerial vehicle leave unmanned aerial vehicle foot tool to lock mechanism 4 and put into normal use.
Practical use shows that: the unmanned aerial vehicle hangar provided according to the technical scheme can effectively solve the storage problem of the small unmanned aerial vehicle and can be guaranteed to be put into use at any time.
The above description is only a preferred embodiment of the present invention, and is not intended to limit the present invention in any way, and although the present invention has been disclosed in the preferred embodiment, the present invention is not limited thereto, and in practical use, the level of the unmanned aerial vehicle hangar may be increased, and a plurality of parallel lifting unit combinations may be added in the front and rear direction as required, so as to increase the storage capacity of the whole unmanned aerial vehicle hangar.
It is obvious that any person skilled in the art can make many modifications and variations to the above-described embodiments without departing from the scope of the invention, and all simple modifications, equivalent variations and modifications of the above-described embodiments without departing from the technical spirit of the invention should be considered as falling within the scope of the invention.
Claims (12)
1. An unmanned aerial vehicle hangar which characterized in that: comprises a lifting device, a transverse moving device (2), an unmanned aerial vehicle stopping and conveying frame (3) and an unmanned aerial vehicle foot lock device (4); the lifting device comprises a group of lifting units (1) which are correspondingly arranged on the left and right sides, and an unmanned aerial vehicle stopping and conveying frame (3) which is erected between the two lifting units (1) and can realize vertical displacement, so that a main framework of the lifting units (1) for storing the unmanned aerial vehicle is formed; meanwhile, through another group of lifting units (1) with the same structure arranged at the front or rear adjacent position of the two groups of lifting units (1) and a transverse moving device (2) clamped and fixed between the upper and lower positions of the front and rear groups of lifting units (1), the unmanned aerial vehicle stop conveying frame (3) located between the two groups of lifting unit assemblies correspondingly arranged on the left and right sides can realize the horizontal displacement of the unmanned aerial vehicle stop conveying frame (3) between the front and rear adjacent lifting unit assemblies under the action of the transverse moving device (2); from this the general framework of unmanned aerial vehicle hangar that constitutes to have multilayer multiseriate structure.
2. The unmanned aerial vehicle hangar of claim 1, wherein: the lifting unit (1) comprises two H-shaped plate vertical columns (1.1) which are vertically arranged on the same vertical column bottom plate (1.7) in a parallel shape, an annular chain transmission mechanism arranged between the two H-shaped plate vertical columns (1.1) and a lifting motor (1.5) arranged at the upper part of one H-shaped plate vertical column (1.1); the lifting unit comprises a lifting unit and a chain transmission mechanism, wherein the lifting unit comprises an annular chain (1.4), a main transmission chain wheel (1.3) arranged at the upper parts of two H-shaped plate body stand columns, a main transmission shaft (1.2), an auxiliary transmission chain wheel (1.8) arranged at the lower parts of the two H-shaped plate body stand columns and an auxiliary transmission shaft (1.9), and the auxiliary transmission chain wheel (1.8) and the auxiliary transmission shaft (1.9) are simultaneously arranged at the lower parts of the two H-shaped plate body stand columns (1.1) through the main transmission chain wheel (1.3) on the main transmission shaft (1.2) driven by a gear at the output shaft end of a lifting motor (1.5) to realize vertical circulating transmission through the annular chain (1.4) surrounding the main transmission chain wheel and the auxiliary transmission chain wheel, so as to form; meanwhile, the inner side edge parts of the two H-shaped plate body upright columns (1.1) are respectively provided with a guide groove (1.10) from top to bottom, and the outer chain body of the annular chain (1.4) is provided with a plurality of uniformly distributed transverse moving roller way assemblies (1.6) which circularly move along with the annular chain (1.4).
3. The unmanned aerial vehicle hangar of claim 2, wherein: the lifting motor (1.5) is arranged on the outer side of the top of the H-shaped plate body upright post (1.1), and the lower part of the output shaft end of the lifting motor and a main transmission shaft (1.2) which is horizontally arranged form a driving structure of the lifting device (1) through a gear transmission mechanism.
4. The unmanned aerial vehicle hangar of claim 2, wherein: the transverse moving roller way component mechanism (1.6) comprises a roller way component main mounting plate (1.61), two groups of nylon guide wheel sets (1.62) which are arranged on the outer plate surface of the roller way component main mounting plate (1.61) and can rotate by depending on a fixed shaft and are distributed in an up-down parallel manner, and two groups of guide rail anti-overturning pulleys (1.63) arranged at the left end and the right end of the plate surface of the roller way component main mounting plate (1.61); wherein: the back surface of the roller way component main mounting plate (1.61) is connected with a mounting chain plate (1.67) arranged in the annular chain (1.4) through a screw; each group of guide rail overturn-preventing pulleys (1.63) are respectively arranged on two overturn-preventing pulley arrangement plates (1.64) which are vertically arranged with the back of the roller way assembly main arrangement plate and are parallel up and down; the horizontal distance between the adjacent wheel edges of the upper and lower groups of guide rail overturn-preventing pulleys (1.63) is matched with the thickness of the edge part of the groove-shaped plate body of the H-shaped plate body upright post (1.1).
5. The unmanned aerial vehicle hangar of claim 4, wherein: still be equipped with the vertical guide pulley of a set of unmanned aerial vehicle (1.65) on roller assembly owner mounting plate (1.61), the vertical guide pulley of unmanned aerial vehicle (1.65) set up on the back panel body of roller assembly owner mounting plate (1.61) between two sets of nylon guide pulley group (1.62) that are upper and lower distribution to through setting up unmanned aerial vehicle frame side guide wheel hole (1.68) on roller assembly owner mounting plate (1.61), make the vertical guide pulley of unmanned aerial vehicle (1.65) foreign steamer reason and roller assembly owner mounting plate be in the coplanar.
6. The unmanned aerial vehicle hangar of claim 2, wherein: the upper part and the lower part of the outer side plate surfaces of the two H-shaped plate body upright columns (1.1) are respectively provided with a bolt mechanism (7), and the outer side plate surface of the H-shaped plate body upright column (1.1) between the two bolt mechanisms (7) is also provided with a bulkhead connecting piece (6).
7. The unmanned aerial vehicle hangar of claim 1, wherein: the transverse moving device (2) is composed of a friction driving mechanism which is arranged on a displacement support assembly capable of moving back and forth and takes a transverse moving driving motor (2.1) as a power source, and a horizontal driving reset mechanism which takes a cylinder (2.6) and a pre-tightening spring assembly as power sources; the transverse moving driving motor (2.1) is vertically arranged on the motor base (2.3), and a friction driving mechanism in an isosceles triangle layout is formed by a motor output shaft end driving wheel (2.2) arranged at the output shaft end of the transverse moving driving motor (2.1) and two friction driving belt wheels (2.20) arranged on the upper plane of the same displacement bracket component; and a friction driving mechanism is formed by two friction driving wheels (2.17) arranged between a friction driving upper support plate (2.16) and a friction driving lower support plate (2.19) which form the displacement support assembly and arranged at the lower output shaft ends of two friction driving belt wheels (2.20) on the friction driving upper support plate (2.16); the horizontal driving reset mechanism consists of a pneumatic propulsion structure taking a cylinder (2.6) as power and a compression reset structure taking a pre-tightening spring (2.8) as power; the unmanned aerial vehicle stopping conveying frame (3) can be clamped from the left side and the right side and can be lifted along the guide grooves (1.10) in the lifting units (1), and meanwhile, the unmanned aerial vehicle stopping conveying frame (3) can be lifted along the upper and lower notches at the two ends of the guide grooves (1.10) in the lifting units (1) to achieve horizontal displacement between the front and rear adjacent lifting units through the upper and lower notches of the guide grooves (1.10) in the front and rear adjacent lifting units.
8. The unmanned aerial vehicle hangar of claim 6, wherein: the displacement bracket assembly is composed of a friction driving upper support plate (2.16) arranged horizontally, a friction driving lower support plate (2.19), two vertically arranged guide rail sliding blocks (2.13) arranged on the friction driving upper support plate (2.16) and the front part of the friction driving lower support plate (2.19) in a left-right manner, and two vertically arranged spring guide post fixing plates (2.10) arranged on the friction driving upper support plate (2.16) and the rear part of the friction driving lower support plate (2.19), and thus, an integral framework of the displacement bracket assembly capable of realizing front-back displacement on the base (2.14) is formed; the displacement support assembly is located on a translation mechanism which is arranged on the inner bottom surface of the base (2.14) and consists of a slide rail (2.12) and a linear guide rail slide block (2.21), and a translation structure controlled by an air cylinder (2.6) and a pre-tightening spring assembly is formed by an air cylinder mounting plate (2.22) arranged on the surfaces of the two spring guide pillar fixing plates (2.10) and a spring guide pillar (2.9) arranged on the surfaces of the spring guide pillar fixing plates (2.10) positioned on the two sides of the air cylinder mounting plate (2.22).
9. The unmanned aerial vehicle hangar of claim 7, wherein: the left side and the right side of the base (2.14) are respectively provided with a mounting seat (2.11) which is vertical to the base surface, the plate surface at the rear part of the base (2.14) is respectively provided with two spring base plates (2.4) which are vertical to the base surface and a cylinder base (2.5) which is positioned between the two spring base plates, the cylinder base (2.5) is arranged at the middle position, the left side and the right side are respectively provided with the spring base plates (2.4),
therefore, an arrangement space facing the rear part of the displacement support assembly and used for the air cylinder (2.6) and the pre-tightening spring (2.8) is formed, a spring guide pillar (2.9) matched with the pre-tightening spring (2.8) penetrates through a linear bearing (2.7) arranged in a central hole of a spring base plate (2.4), and the front end of the spring guide pillar (2.9) is fixed on a spring guide pillar fixing plate (2.10) at the rear part of the displacement support assembly, so that a displacement support assembly reset structure depending on the pre-tightening spring is formed; meanwhile, the front end of a piston rod (2.23) extending outwards of an air cylinder (2.6) arranged at the position of an air cylinder base (2.5) is provided with an air cylinder front end mounting plate (2.22) fixed with a left spring guide post fixing plate (2.10) and a right spring guide post fixing plate (2.10) at the rear part of the displacement support assembly, so that a horizontal driving structure of the displacement support assembly depending on the air cylinder is formed; meanwhile, a group of sliding mechanisms for arranging the displacement support assembly are arranged on the inner seat surface of the base (2.14), each sliding mechanism consists of two sliding rails (2.12) arranged on the inner bottom surface of the base (2.14) and a linear guide rail sliding block (2.21) matched with the sliding rails, and the displacement support assembly is fixed on the linear guide rail sliding block (2.21), so that a horizontal displacement structure of the whole displacement support assembly is formed.
10. The unmanned aerial vehicle hangar of claim 7, wherein: the linear guide rail sliding block (2.21) is abutted with a guide rail sliding block (2.13) of which the front surface is provided with two groups of transverse sliding pulleys (2.15) which are distributed in parallel up and down.
11. The unmanned aerial vehicle hangar of claim 1, wherein: unmanned aerial vehicle shut down carriage (3) for by chassis (3.1) and set up the U type framework of constituteing in side grudging post (3.4) at chassis (3.1) both ends, wherein side grudging post (3.4) upper portion respectively be equipped with two interval certain interval be furnished with pulley support (3.3) of pulley (3.2) to still be equipped with tool to lock fixed orifices (3.5) on chassis (3.1).
12. The unmanned aerial vehicle hangar of claim 1, wherein: unmanned aerial vehicle foot tool to lock mechanism (4) correspond L shape foot stool (4.1) that sets up on unmanned aerial vehicle shuts down carriage (3) by a set of left and right sides and constitute, the inboard bottom of foot stool (4.1) be equipped with be applied to with the unmanned aerial vehicle shut down fixed orifices (3.5) the fixed orifice plate (4.10) that match on carriage (3), be equipped with slide rail (4.2), slider (4.3), lock foot (4.4), connecting rod (4.5), extension spring (4.6), foot stool (4.7) on the inboard roll table subassembly main mounting plate of foot stool (4.1) to the top of foot stool (4.1) that sets up at vertical form is equipped with two draw-in grooves (4.9) and the locking otic placode (4.8) of closed draw-in groove (4.9) that realize the joint with unmanned aerial vehicle bottom supporting legs (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110782716.1A CN113431409A (en) | 2021-07-12 | 2021-07-12 | Unmanned aerial vehicle hangar |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110782716.1A CN113431409A (en) | 2021-07-12 | 2021-07-12 | Unmanned aerial vehicle hangar |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN113431409A true CN113431409A (en) | 2021-09-24 |
Family
ID=77759951
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202110782716.1A Pending CN113431409A (en) | 2021-07-12 | 2021-07-12 | Unmanned aerial vehicle hangar |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN113431409A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0228552A1 (en) * | 1985-11-27 | 1987-07-15 | Siegfried Silzle | Aircraft hangar |
| CN112537458A (en) * | 2020-12-29 | 2021-03-23 | 贵州航天南海科技有限责任公司 | A sideslip device for three-dimensional access arrangement of unmanned aerial vehicle |
| CN112623594A (en) * | 2020-12-29 | 2021-04-09 | 贵州航天南海科技有限责任公司 | Lifting device for be used for three-dimensional access arrangement of unmanned aerial vehicle |
| CN112696073A (en) * | 2020-12-29 | 2021-04-23 | 贵州航天南海科技有限责任公司 | Loading machine device |
| CN112727216A (en) * | 2020-12-29 | 2021-04-30 | 贵州航天南海科技有限责任公司 | Unmanned aerial vehicle access method and three-dimensional access equipment thereof |
-
2021
- 2021-07-12 CN CN202110782716.1A patent/CN113431409A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0228552A1 (en) * | 1985-11-27 | 1987-07-15 | Siegfried Silzle | Aircraft hangar |
| CN112537458A (en) * | 2020-12-29 | 2021-03-23 | 贵州航天南海科技有限责任公司 | A sideslip device for three-dimensional access arrangement of unmanned aerial vehicle |
| CN112623594A (en) * | 2020-12-29 | 2021-04-09 | 贵州航天南海科技有限责任公司 | Lifting device for be used for three-dimensional access arrangement of unmanned aerial vehicle |
| CN112696073A (en) * | 2020-12-29 | 2021-04-23 | 贵州航天南海科技有限责任公司 | Loading machine device |
| CN112727216A (en) * | 2020-12-29 | 2021-04-30 | 贵州航天南海科技有限责任公司 | Unmanned aerial vehicle access method and three-dimensional access equipment thereof |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN109607014B (en) | Wheel adjusting device and four-way carrier thereof | |
| WO2019114170A1 (en) | Vehicle lifting mechanism and automatic power conversion system | |
| CN112079023B (en) | Multifunctional high-position sorting vehicle and operation method thereof | |
| CN106956242B (en) | A kind of F1 racing car intelligent transport robot | |
| CN211997499U (en) | Flexible structure of getting of material | |
| CN113816308B (en) | Fork device for forklift | |
| CN213623124U (en) | Multifunctional high-order-picking truck | |
| CN104032989B (en) | A kind of two layers of circulation parking apparatus | |
| CN113431409A (en) | Unmanned aerial vehicle hangar | |
| CN209908048U (en) | Vertical circulation stereo garage with anti-shaking function | |
| CN112681848B (en) | Guiding device applied to outer clamping type carrier of large pneumatic tire and using method | |
| CN203361723U (en) | Grabbing and rotating mechanism for stereoscopic parking equipment | |
| CN113090086A (en) | Three-dimensional parking equipment suitable for lifting plate type robot parking | |
| CN201722958U (en) | Three-dimensional garage two-way car parking and picking-up device | |
| CN213898345U (en) | Combined lateral access type stereo garage | |
| CN211286858U (en) | Loading attachment and stereo garage | |
| CN218253817U (en) | Portable shelter end plate riser device | |
| CN220414998U (en) | Down-rotation avoidance-free parking equipment | |
| CN215926928U (en) | Guiding device applied to outer clamping type carrier of large inflated tire | |
| CN103352590A (en) | Catching swing mechanism for three-dimensional parking equipment | |
| CN219384715U (en) | Library manages with rising ladder | |
| CN220030534U (en) | Furniture board lamination equipment | |
| CN221002158U (en) | Roadway parking AGV | |
| CN217625535U (en) | Goods shelf shuttle transport vehicle | |
| CN211257972U (en) | Compound train carries car mechanism and tower stereo garage |
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 | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20210924 |