CN215155757U

CN215155757U - Mobile airport

Info

Publication number: CN215155757U
Application number: CN202121175257.2U
Authority: CN
Inventors: 吕殿斌; 蒋佳霖; 余文彬
Original assignee: Hangzhou Anti Gravity Intelligent Technology Co ltd
Current assignee: Hangzhou Anti Gravity Intelligent Technology Co ltd
Priority date: 2021-05-28
Filing date: 2021-05-28
Publication date: 2021-12-14
Anticipated expiration: 2031-05-28

Abstract

The utility model discloses a remove airport, including removing the carrier, and be located remove the last support body of carrier, the support body includes: the cabin cover is connected with the functional cabin and forms a hangar space when being positioned above the lifting platform; the functional cabin comprises a shell, a lifting structure and a functional component positioned on the lifting structure, and the lifting structure can move downwards into the shell when the cabin cover forms a cabin space; the lifting platform is positioned on the upper portion of the frame body and comprises a lifting plate, a centering structure longitudinally arranged on the upper portion of the lifting plate, and guide rail structures transversely arranged on two sides of the lifting plate, wherein two ends of the centering structure are respectively connected with the guide rail structures. The lifting structure of the utility model is telescopic relative to the shell according to the opening or closing of the hatch cover, the structural arrangement is reasonable and compact, and the hatch cover has the protection function on the functional components after being closed; in addition, the centering structure is longitudinally connected to the guide rail structures on the two sides, so that the movement is stable, and the structure is firm.

Description

Mobile airport

Technical Field

The utility model relates to an unmanned aerial vehicle application, concretely relates to remove airport.

Background

Along with the rapid development of unmanned aerial vehicle technology, the use amount of unmanned aerial vehicles in the fields of surveying and mapping, routing inspection, fire fighting, express delivery and the like is increased year by year. The existing unmanned aerial vehicle is generally powered by a lithium ion battery, but the endurance of the battery is weak and expensive, the application cost is high, the influence of intensive work tasks and the influence of the external environment are accompanied, a mobile airport is required to be selected for use to provide safety guarantee for the unmanned aerial vehicle and provide a good platform for taking off or landing, the mobile airport can charge the unmanned aerial vehicle constantly when the unmanned aerial vehicle is stored, and the endurance of the unmanned aerial vehicle is ensured.

The prior art discloses many rotor unmanned aerial vehicle descending device (chinese patent No. CN201910846242.5), including descending platform, elevating system, a frame, hatch door and antenna, descending platform includes unmanned aerial vehicle foot rest clamping mechanism and platform self rotary mechanism, unmanned aerial vehicle foot rest clamping mechanism includes positive and negative lead screw module, first servo electricity, infrared sensor and W type clamp plate, coupling joint is passed through with first servo motor's output to positive and negative lead screw module, infrared sensor fixed mounting is in one side of positive and negative lead screw module, W type clamp plate is fixed on the slider of positive and negative lead screw module, be provided with the joint that charges on the unmanned aerial vehicle foot rest clamping mechanism. According to the landing platform, the foot rest clamping mechanism is arranged to clamp the unmanned aerial vehicle firmly, and the charging connector is arranged, so that the unmanned aerial vehicle can be charged at the first time after landing. However, this W type clamp plate carries out gliding through middle positive and negative lead screw module, and the clamp plate does not receive the support, and is consequently little to unmanned aerial vehicle's clamping force in clamp plate both sides, and the atress is uneven, leads to unmanned aerial vehicle to park the deviation easily, and then influences unmanned aerial vehicle's charging, and in the motion process of clamp plate, the both sides of clamp plate are unsettled, receive the influence of factors such as gravity, and the clamp plate is unstable at the motion process, and the steadiness is poor.

Disclosure of Invention

The utility model provides a mobile airport aiming at the defects in the prior art, the lifting structure of the mobile airport can be extended and contracted relative to the shell according to the opening or closing of the hatch cover, the structural arrangement is reasonable and compact, and the hatch cover has the protection function on the functional components after being closed; in addition, the centering structure is longitudinally connected to the guide rail structures on the two sides, so that the movement is stable, and the structure is firm.

In order to solve the technical problem, the utility model discloses a following technical scheme can solve:

a mobile airport comprising a mobile carrier, and a rack positioned on the mobile carrier, the rack comprising: the cabin cover is connected with the functional cabin and forms a hangar space when being positioned above the lifting platform;

the functional cabin comprises a shell, a lifting structure and a functional component positioned on the lifting structure, and the lifting structure can move downwards into the shell when the cabin cover forms a cabin space;

the lifting platform is located on the upper portion of the frame body and comprises a lifting plate, a centering structure and a guide rail structure, wherein the centering structure is longitudinally arranged on the upper portion of the lifting plate, the guide rail structure is transversely arranged on two sides of the lifting plate, and two ends of the centering structure are respectively connected with the guide rail structure.

Preferably, the guide rail structure comprises slide rails positioned at two sides of the lifting plate, and a slide block capable of moving transversely relative to the slide rails;

the slide block, at least one, be equipped with protruding in the supporting seat of take-off and landing board, the upper end of supporting seat with the end connection of centering structure.

Preferably, the centering structure comprises at least two centering plates which are oppositely arranged, and each centering plate comprises a first connecting body and a second connecting body which is symmetrically arranged with the first connecting body;

the first connecting body comprises an outer connecting end I and an inner connecting end I, the outer connecting end I is connected with the supporting seat, and the first connecting body is inwards concave towards the longitudinal edge of the lifting plate to form a first clamping part;

the second connecting body comprises an outer connecting end II and an inner connecting end II, the outer connecting end II is connected with the supporting seat, the second connecting body is inwards concave towards the longitudinal edge of the lifting plate to form a clamping part II, and the clamping part I and the clamping part II are arranged in the same direction;

the first inner connecting end is connected with the second inner connecting end and protrudes to form a propping part, and the propping part is arranged in a reverse direction with the first clamping part and/or the second clamping part.

Preferably, the centering plate comprises a first side end portion which can be attached to or close to the longitudinal edge of the lifting plate, and a second side end portion which is opposite to the first side end portion, and the first clamping portion, the abutting portion and the second clamping portion are sequentially arranged on the second side end portion.

Preferably, an adjustable clamping area I is formed between the two opposite clamping parts I, an adjustable clamping area II is formed between the two opposite clamping parts II, and the clamping area I is communicated with the clamping area I or is separated by the abutting part;

and at least one charging seat is arranged on the first clamping part and/or the first clamping part.

Preferably, the rack body comprises a first frame for supporting the lifting platform and a second frame for partially or completely supporting the functional cabin;

the first frame comprises a first cross beam and a first upright post positioned on the ground or a plane;

the second frame comprises a second cross beam and a second upright post positioned at the front part of the lifting plate;

the second upright posts are at least two and penetrate through the functional bin from the bottom and are connected with the lifting structure, and the second cross beam is located in the shell and is abutted against the shell.

Preferably, the lifting structure comprises at least two guide rails located at the front parts of the two upright posts, a lifting block movably connected with the guide rails, and a lifting beam transversely arranged at the front parts of the lifting blocks, wherein two ends of the lifting beam are respectively connected with the lifting block and move along the height direction relative to the guide rails.

Preferably, the functional assembly comprises a plurality of fixed seats, a connecting rod positioned on the fixed seats and a plurality of functional pieces positioned above the connecting rod, and the height of the functional assembly is less than or equal to the movement stroke of the lifting beam;

the fixed seats are arranged at the front part of the lifting beam at intervals, and are provided with connecting channels for the connecting rods to pass through;

the connecting rod is arranged along the height direction, the lower end of the connecting rod is positioned in the connecting channel, and the upper end of the connecting rod is connected with the functional part;

the functional parts comprise a base station, a weather instrument, a wind direction instrument and/or a communication antenna.

Preferably, the shell comprises a front plate body, a rear plate body and an upper plate body which can be connected with the hatch cover;

the front plate body is provided with an exhaust channel for heat dissipation, the rear plate body is partially supported on the lifting plate and/or the first frame, and the upper plate body is provided with at least one installation channel for lifting the functional part and/or the connecting rod out to the outside.

Preferably, the hatch cover comprises a top cover structure, a driving structure positioned below the lifting plate, a connecting rod structure used for driving the top cover structure to change in position, and an auxiliary opening structure used for adjusting the connecting rod structure to move;

the top cover structure comprises a top plate which can be connected with the front plate body and a side plate which is positioned below the top plate, and the top plate and the side plate can surround to form the hangar space;

one end of the connecting rod structure is connected with the inner wall of the top plate and/or the side plate, the other end of the connecting rod structure is connected with the driving structure and the auxiliary opening structure, and the connecting rod structure is located between the first frame and the guide rail structure.

The utility model discloses the main beneficial effect who gains as follows:

this remove airport is including removing the carrier and being located the support body that removes on the carrier, and wherein the support body is including the hatch cover that can open or closed, be located support body upper portion and supply the take off and landing platform that unmanned aerial vehicle parked or take off, and be located the function storehouse before the support body, when the hatch cover is closed, the hatch cover links to each other with the function storehouse promptly and is located the take off and landing platform top and form the hangar space, and unmanned aerial vehicle can be located this hangar space. Consequently, this hatch cover is in the closure back, not only has the effect of holding and protecting unmanned aerial vehicle, and this hatch cover links to each other with the function storehouse, has the guard action to the function storehouse again, avoids abominable external environment to cause the damage to the function storehouse, the life in extension function storehouse greatly, compare in present some removal airports, the hatch cover is only used for closing or protecting unmanned aerial vehicle usually, the function storehouse is still independent individual, consequently the function storehouse exposes in the external world for a long time, short and easy functional failure of life. The functional cabin mainly comprises a shell, a lifting structure and a functional component positioned on the lifting structure, wherein the lifting structure can move downwards into the shell when the cabin cover forms a cabin space, so that the functional component is also positioned in the shell. Therefore, the utility model discloses a elevation structure makes the functional unit can stretch out to the external world, also can accomodate in the casing, in the practical application process, when the cabin cover was opened, the cabin cover kept away from function storehouse and platform of taking off and land, the elevation structure upward movement in the function storehouse at this moment stretches out the functional unit to the external world to the signal in the functional unit can transmit to unmanned aerial vehicle better, or the response piece in the functional unit can detect the change of external environment more promptly or accurately; when the hatch cover is closed, the hatch cover is close to the function bin and is positioned above the lifting platform, and the lifting structure in the function bin moves downwards to store the function component into the shell, so that the structural arrangement is reasonable and compact, the space for movement of the hatch cover is not occupied, the hatch cover also has the function of protecting the function component, and the influence of external damage or severe environment is avoided. Additionally, the utility model discloses a platform that takes off and land includes the board that takes off and land, along vertically setting up in the centering structure on board upper portion that takes off and land and along transversely setting up in the rail construction of the board both sides that takes off and land, the both ends of centering structure are connected with rail construction respectively. Therefore, the centering structure is driven by the guide rail structures positioned on the two sides of the lifting plate, the two ends of the centering structure are supported and not suspended, so that the centering structure is slightly influenced by factors such as gravity, inertia force and the like in the moving process, the structure is firm, the movement is stable, and the clamping force is uniform.

Additional aspects and advantages of the invention will be set forth in part in the description which follows and, in part, will be obvious from the description, or may be learned by practice of the invention.

Drawings

The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this application, illustrate embodiment(s) of the invention and together with the description serve to explain the invention without undue limitation to the invention. In the drawings:

fig. 1 is a schematic overall structure diagram of a closed state of a mobile airport according to an embodiment of the present invention;

fig. 2 is a schematic overall structure diagram of an open state of a mobile airport according to an embodiment of the present invention;

fig. 3-6 are schematic diagrams illustrating an internal structure of a mobile airport according to an embodiment of the present invention;

fig. 7 and 8 are schematic diagrams illustrating a guide rail structure of a mobile airport according to an embodiment of the present invention;

fig. 9 is a partial schematic view of a portion a of fig. 4 in accordance with an embodiment of the present invention;

fig. 10-13 are schematic diagrams illustrating a centering structure of a mobile airport according to an embodiment of the present invention;

fig. 14-18 are schematic diagrams illustrating a lifting structure of a mobile airport according to an embodiment of the present invention.

Detailed Description

In order to make the purpose, technical solution and advantages of the embodiments of the present invention clearer, the drawings of the embodiments of the present invention are combined below to clearly and completely describe the technical solution of the embodiments of the present invention. It is to be understood that the embodiments described are only some of the embodiments of the present invention, and not all of them. All other embodiments, which can be obtained by a person skilled in the art without any inventive work based on the described embodiments of the present invention, belong to the protection scope of the present invention.

In the description of the present invention, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.

In the present invention, unless otherwise expressly specified or limited, the terms "mounted," "connected," and "fixed" are to be construed broadly and may, for example, be fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.

In the present disclosure, unless expressly stated or limited otherwise, the first feature "on" or "under" the second feature may comprise direct contact between the first and second features, or may comprise contact between the first and second features not directly. Also, the first feature being "on," "above" and "over" the second feature includes the first feature being directly on and obliquely above the second feature, or merely indicating that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature includes the first feature being directly under and obliquely below the second feature, or simply meaning that the first feature is at a lesser elevation than the second feature.

Unless defined otherwise, technical or scientific terms used herein shall have the ordinary meaning as understood by one of ordinary skill in the art to which this invention belongs. The use of "first," "second," and similar terms in the description and in the claims does not indicate any order, quantity, or importance, but rather is used to distinguish one element from another. Also, the use of the terms "a" or "an" and the like do not denote a limitation of quantity, but rather denote the presence of at least one.

As shown in fig. 1-6 and 14, as the first embodiment of the present invention, a mobile airport is disclosed, which is mainly used as an airport for mobile devices such as an unmanned aerial vehicle, the mobile airport includes a mobile carrier and a frame body 100 located on the mobile carrier, the mobile carrier is generally a vehicle, the frame body 100 includes an openable or closed hatch cover 1, a landing platform 2 located on the upper portion of the frame body 100 for the unmanned aerial vehicle 101 to park or take off, and a functional cabin 3 located in front of the frame body 100, when the hatch cover 1 is closed, that is, the hatch cover 1 is connected with the functional cabin 3 and located above the landing platform 2, a hangar space 201 is formed, and the unmanned aerial vehicle 101 can be located in the hangar space 201. Consequently, this hatch cover 1 is in the closure back, not only has the effect of holding and protecting unmanned aerial vehicle 101, and this hatch cover 1 links to each other with function storehouse 3, has the guard action to function storehouse 3 again, avoid abominable external environment to cause the damage to function storehouse, prolong the life in function storehouse 3 greatly, compare in some present removal airports, the hatch cover is only used for closing or protecting unmanned aerial vehicle usually, the function storehouse is still independent individual again, consequently, the function storehouse is exposed in the external world for a long time, short service life and easy function failure. The functional cabin 3 mainly comprises a housing 31, a lifting structure 32 and a functional component 33 located on the lifting structure 32, and the lifting structure 32 can move downwards into the housing 31 when the cabin cover 1 forms the cabin space 201, so that the functional component 33 is also located inside the housing 31. Therefore, the utility model discloses a lifting structure 32 makes functional component 33 can stretch out to the external world, also can accomodate in casing 31, in the actual application process, when hatch 1 was opened, hatch 1 kept away from functional compartment 3 and take off and land platform 2, lifting structure 32 upward movement in the functional compartment 3 stretched out functional component 33 to the external world this moment to the signal in functional component 33 can transmit to unmanned aerial vehicle 101 better, or the response part in functional component 33 can more timely and accurately detect the change of external environment; when the hatch cover 1 is closed, the hatch cover 1 is close to the functional cabin 3 and is positioned above the lifting platform 2, and at the moment, the lifting structure 32 in the functional cabin 3 moves downwards to store the functional component 33 into the shell 31, so that the structural arrangement is reasonable and compact, the space for moving the hatch cover 1 is not occupied, the hatch cover 1 also has the function of protecting the functional component 33, and the influence of external damage or severe environment is avoided. Additionally, the utility model discloses a platform 2 takes off and land includes that board 21 takes off and land, along vertically set up in the centering structure 22 on board 21 upper portion takes off and land and along transversely setting up in the rail structure 23 of board 22 both sides takes off and land, centering structure 22's both ends are connected with rail structure 23 respectively. Therefore, the centering structure 22 is driven by the guide rail structures 23 located on the two sides of the lifting plate 21, and the two ends of the centering structure 22 are supported rather than suspended, so that the centering structure 22 is slightly influenced by factors such as gravity, inertia force and the like in the movement process, and is firm in structure, stable in movement and uniform in clamping force.

As shown in fig. 7 to 13, as another embodiment of the present invention, the rail structure 23 includes sliding rails 231 located at both sides of the lifting plate 21, and a sliding block 232 capable of moving laterally relative to the sliding rails 231. Specifically, in this embodiment, the slide rail 231 is disposed along the length direction of the lifting plate 21, and the slide rail 231 includes a slide rail seat 2311 connected to the frame body 100 and a slide bar 2312 located on the slide rail seat 2311, where the slide rail seat 2311 is outwardly provided with a groove, and a stopper 2313 is located at a middle position of the groove, and the stopper 2313 is used for restricting the movement of the slide blocks 232 so as to avoid collision of adjacent slide blocks 232. Specifically, the sliding blocks 232 are sleeved on the sliding bars 2312, in this embodiment, two sliding blocks 232 are disposed on each sliding bar and are respectively located at two sides of the limiting block 2313, in other embodiments, three, four or more sliding blocks 232 may be disposed, and it should be noted that in other embodiments, the guide rail structure 23 may also be a moving structure having a driving function, such as a hydraulic sliding rail, a pneumatic rod, or the like. In addition, the upper end of the sliding block 232 is provided with a supporting seat 2314 protruding from the lifting plate 21, the upper end of the supporting seat 2314 is connected with the end of the centering structure 22, namely the height from the horizontal plane to the supporting seat 2314 is greater than the height from the horizontal plane to the lifting plate 21, the supporting seat 2314 supports the centering structure 22, a certain gap is formed between the centering structure 22 and the lifting plate 21, mutual friction is avoided, and the movement of the centering structure 22 is smoother and more stable.

In other embodiments, the centering structure 22 is at least two oppositely disposed centering plates 2201, and the centering plates 2201 include a first connecting body 221 and a second connecting body 222 symmetrically disposed with respect to the first connecting body 221. Specifically, in this embodiment, the centering plates 2201 are disposed in two and are disposed oppositely, the centering plates 2201 are divided into a first connecting body 221 and a second connecting body 221 which are symmetrical, wherein the first connecting body 221 includes a first external connecting end 231 and a first internal connecting end 232, the first external connecting end 231 is embedded or fastened in the upper end of the supporting seat 2314 so that the first external connecting end and the first internal connecting end are fixed to each other, and the first connecting body 221 is recessed towards the longitudinal edge of the lifting plate 21 to form a first clamping portion 233 for stably and clamping the unmanned aerial vehicle. Similarly, the second connecting body 222 includes a second outer connecting end 241 and a second inner connecting end 242, the second outer connecting end 241 is embedded or engaged with the upper end of the supporting seat 2314 to fix the two, and the second connecting body 222 is recessed toward the longitudinal edge of the rising and falling plate 21 to form a second clamping portion 243, and the first clamping portion 233 and the second clamping portion 234 are disposed in the same direction. It should be noted that the concave shape of the first clamping portion 233 and the second clamping portion 234 may be a plurality of shapes such as an arc shape and a polygon, the concave degree may be concave at different degrees, and the concave shape and the concave degree of the first clamping portion 233 and the second clamping portion 234 are not required to be consistent, and do not affect the clamping of the centering plate 2201 to the unmanned aerial vehicle. In addition, the first inner connecting end 232 and the second inner connecting end 242 are connected and protrude to form an abutting portion 251, and the abutting portion 251 and the first clamping portion 233 and/or the second clamping portion 243 are arranged in a reverse direction, so that when the two centering plates 2201 move in the opposite direction, the two opposite abutting portions 251 can abut against each other to limit the minimum stroke between the two centering plates 2201, the phenomenon that the unmanned aerial vehicle is excessively clamped is avoided, and the unmanned aerial vehicle has a protection effect. In other embodiments, the centering plate 2201 may further be provided with a plurality of first clamping portions 233 and/or second clamping portions 243 and/or abutting portions 251, which also has the above-mentioned effects.

In other embodiments, the centering plate 2201 includes a first side end 261 that can be attached to or near a longitudinal edge of the take-off and landing plate 21, and a second side end 262 opposite the first side end 261. Specifically, in the present embodiment, the centering plate 2201 includes two side ends, and during the movement of the centering plate 2201, the side end portion 261 can abut against the longitudinal edge of the lifting plate 21, and a plane parallel to the longitudinal edge of the lifting plate 21 is disposed on the side end portion 261 of the present embodiment, and the side end portion 261 may have other shapes in other embodiments. In addition, in this embodiment, the first clamping portion 233, the abutting portion 251, and the second clamping portion 243 are sequentially disposed on the second side end portion 262, so that the second side end portion 262 has a clamping effect on the unmanned aerial vehicle 101, and can limit a minimum clamping stroke, the structural design is reasonable, and the first clamping portion 233 and the second clamping portion 243 are respectively located at two sides of the abutting portion 251, and are uniformly stressed and stable in structure.

In other embodiments, an adjustable clamping area one 271 is formed between the two opposite clamping portions one 233, and an adjustable clamping area two 272 is formed between the two opposite clamping portions two 243, wherein the clamping area one 271 and the clamping area two 272 are communicated or separated by the abutting portion 251. In this embodiment, a first clamping area 271 for clamping a stand of the drone 101 is formed between the first clamping portions 233, and the first clamping area 271 is adjustable by the movement of the centering plate 2201 and is adapted to stands of the drone 101 with different lengths; similarly, a second clamping area 272 for clamping the other foot stool of the unmanned aerial vehicle 101 is formed between the two opposite clamping portions 243, the second clamping area 272 can be adjusted by the movement of the centering plate 2201 to adapt to the foot stool of the unmanned aerial vehicle 101 with different lengths, and the adjustment ranges of the first clamping area 271 and the second clamping area 272 are the same step in the embodiment, so that the clamping force is uniform and stable. Furthermore, in this embodiment, all be equipped with a charging seat 281 on clamping part 233 and the clamping part 243, consequently when unmanned aerial vehicle 101 descends to the board 21 that takes off and land on, centering board 2201 slides towards unmanned aerial vehicle 101, press from both sides unmanned aerial vehicle 101's foot rest tightly, make charging seat 281 lean on with unmanned aerial vehicle 101 foot rest counterbalance, corresponding unmanned aerial vehicle 101 foot rest is equipped with the joint that charges with charging seat 281 assorted, charging seat 281 charges for unmanned aerial vehicle 101 this moment, thereby this centering board 2201 not only presss from both sides tightly unmanned aerial vehicle 101, avoid it to rock in storehouse space 201, and this centering board 2201 can provide the electric quantity support to unmanned aerial vehicle 101, maintain unmanned aerial vehicle 101's performance at optimum.

As shown in fig. 14-18, in other embodiments, the rack 100 includes a first frame 11 for supporting the landing platform 2, and a second frame 12 for partially or/and fully supporting the functional cartridge 3. Specifically, in the present embodiment, the first frame 11 includes a first cross beam 111 and a first upright 112 located on a ground or plane, and the second frame 12 includes a second cross beam 121 and a second upright 122 located at the front of the landing plate 21. The first cross beam 111 and the first vertical column 112 are vertically arranged to surround the periphery of the lifting plate 21 and have a certain supporting function on the lifting plate 21, the second frame 12 is located in the front of the frame body 100 and has a function of forming and supporting the functional cabin 3, wherein the second vertical column 122 is arranged in two in the embodiment, and of course, three or more vertical columns can be arranged in other embodiments, which is beneficial to structural stability, the second vertical column 122 penetrates through the functional cabin 3 from the bottom to be connected with the lifting structure 32 and is vertically arranged with the second cross beam 121, the second cross beam 121 is partially located in the shell 31, and the second cross beam 121 at the top abuts against the shell 31, so that the shell 31 is supported, and the deformation resistance of the functional cabin 3 is improved.

In other embodiments, the lifting structure 32 includes at least two guide rails 321 located in front of the second upright 112, a lifting block 322 movably connected to the guide rails 321, and a lifting beam 323 transversely disposed in front of the lifting block 322, wherein two ends of the lifting beam 323 are respectively connected to the lifting block 322 and move in a height direction relative to the guide rails 321. Specifically, in this embodiment, the guide rail 321 is longitudinally disposed at the front end of the second upright post 112, the lifting block 322 is disposed on the guide rail 321 and moves relative to the guide rail 321, the lifting beam 323 is transversely disposed, and two ends of the lifting beam 323 are respectively connected to the lifting block 322.

In other embodiments, the functional assembly 33 includes a plurality of fixing bases 331, a connecting rod 332 located on the fixing bases 331, and a plurality of functional pieces 333 located above the connecting rod 332. Specifically, in this embodiment, the lower end of the connecting rod 332 is set as the fixing seat 331, the lower end is set as the functional component 333, and the fixing seat 331 is connected to the lifting beam 323, so that in an actual operation process, the movement of the lifting beam 323 drives the functional component 33 to extend and retract relative to the housing 31, so that the functional component 33 extends to the outside or is accommodated into the housing 31, and in order to ensure that the functional component 33 is completely located in the housing when being accommodated, the height of the functional component 33 is less than or equal to the movement stroke of the lifting beam 323. Further, in some embodiments, the fixing base 331 is disposed at an interval in front of the lifting beam 323, and a connection channel 334 for the lower end of the connection rod 332 to pass through is disposed on the fixing base 331, and the function 333 includes a base station, a weather meter, a wind direction meter, and/or a communication antenna, and the like for monitoring, sensing, and transmitting functions serving the drone 101. Therefore, the functional component 33 moves upwards through the lifting structure 32 to extend the functional component 33 to the outside, so that signals in the functional component 33 can be better transmitted to the unmanned aerial vehicle 101, and the sensing component in the functional component 33 can detect changes of the external environment more timely and accurately; after the functional component 33 is stored by the downward movement of the lifting structure 32, the space of the hatch cover 1 is not occupied, and the hatch cover 1 also has the function of protecting the functional component 33.

In other embodiments, the housing 31 comprises a front plate 311, a rear plate 312 and an upper plate 313 that can be associated with the hatch 1. Specifically, in this embodiment, the front plate 311 is provided with an exhaust passage 314 for dissipating heat to prevent overheating inside the functional compartment 3, the rear plate 312 is partially supported on the lifting plate 21 and/or the first frame 11, so that the lifting plate 21 and/or the first frame 11 have a certain supporting function on the housing 31 to further enhance the stability of the structure, and the upper plate 313 is provided with at least one installation passage 315 for raising the functional component 333 and/or the connecting rod 332 to the outside, and the installation passage 315 corresponds to the functional component 33. Therefore, the housing 31 has a reasonable and compact structure design, and has the functions of ventilation and storage, but does not hinder the lifting of the functional component 33.

As shown in fig. 5, in some other embodiments, the hatch 1 includes a top cover structure 400, a driving structure 500 located below the landing plate 21, a link structure 700 for driving the top cover structure 400 to change its position, and an auxiliary opening structure 600 for adjusting the movement of the link structure 700. Wherein the roof structure 400 includes a top plate 41 connected to the front plate 311, and a side plate 42 located below the top plate 41, and the top plate 41 and the side plate 42 may surround to form the hangar space 201. Therefore, at the in-process of 1 motion in cabin cover, the utility model discloses an indirect drive of drive structure 500, rethread connecting rod structure 700 directly drives top cap structure 400, and connecting rod structure 700 receives drive power, and gravity itself in addition, factors such as motion inertia result in connecting rod structure 700 poor stability in the motion process for moving speed is uneven when top cap structure 400 switches, or top cap structure 400 is not the full closure, and the condition such as hangar space 201 is not sealed, consequently the utility model discloses open structure 400 again through setting up the assistance and adjust connecting rod structure 700, further ensure top cap structure 400's switching, moving speed is even, stable in structure and controllability are good. Further, the link structure 700 is connected to the inner wall of the top plate 41 and/or the side plate 42 at one end and connected to the driving structure 500 and the auxiliary opening structure 600 at the other end, and the link structure 700 is located between the first frame 11 and the rail structure 23. Therefore, when the hatch cover structure 2 is closed, the connecting rod structure 700 is partially or completely accommodated in the hangar space 201 instead of being exposed to the external environment, and in practical application, especially in a severe outdoor environment, such a structure can prevent the connecting rod structure 700 from being damaged by oxidation, rusting, corrosion and the like, prolong the service life of the connecting rod structure 700, improve flexibility and ensure structural stability.

Finally, it should be noted that: the above embodiments are only used to illustrate the technical solution of the present invention, and not to limit it; although the present invention has been described in detail with reference to the foregoing embodiments, it should be understood by those skilled in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some technical features may be equivalently replaced; such modifications and substitutions do not depart from the spirit and scope of the present invention.

In short, the above description is only a preferred embodiment of the present invention, and all the equivalent changes and modifications made in accordance with the claims of the present invention should be covered by the scope of the present invention.

Claims

1. A mobile airport comprising a mobile carrier and a shelf on said mobile carrier, said shelf comprising: the cabin cover is connected with the functional cabin and forms a hangar space when being positioned above the lifting platform;

2. The mobile airport of claim 1, wherein: the guide rail structure comprises slide rails positioned on two sides of the lifting plate and a slide block capable of moving transversely relative to the slide rails;

3. A mobile airport according to claim 2, wherein: the centering structure comprises at least two centering plates which are oppositely arranged, and each centering plate comprises a first connecting body and a second connecting body which is symmetrically arranged with the first connecting body;

4. A mobile airport according to claim 3, wherein: the centering plate comprises a first side end portion which can be attached to or close to the longitudinal edge of the lifting plate and a second side end portion which is opposite to the first side end portion, and the first clamping portion, the abutting portion and the second clamping portion are sequentially arranged on the second side end portion.

5. The mobile airport of claim 4, wherein: an adjustable clamping area I is formed between the two opposite clamping parts I, an adjustable clamping area II is formed between the two opposite clamping parts II, and the clamping area I is communicated with the clamping area I or is separated by the abutting part;

6. The mobile airport of any of claims 1-5, wherein: the frame body comprises a first frame for supporting the lifting platform and a second frame for partially or/and completely supporting the functional cabin;

7. The mobile airport of claim 6, wherein: the lifting structure comprises at least two guide rails which are positioned at the front parts of the two upright posts, a lifting block movably connected with the guide rails and a lifting beam which is transversely arranged at the front parts of the lifting blocks, wherein the two ends of the lifting beam are respectively connected with the lifting block and move along the height direction relative to the guide rails.

8. The mobile airport of claim 7, wherein: the functional assembly comprises a plurality of fixed seats, a connecting rod positioned on the fixed seats and a plurality of functional pieces positioned above the connecting rod, and the height of the functional assembly is less than or equal to the movement stroke of the lifting beam;

9. The mobile airport of claim 8, wherein: the shell comprises a front plate body, a rear plate body and an upper plate body which can be connected with the hatch cover;

10. The mobile airport of claim 9, wherein: the hatch cover comprises a top cover structure, a driving structure positioned below the lifting plate, a connecting rod structure used for driving the top cover structure to change in position, and an auxiliary opening structure used for adjusting the connecting rod structure to move;