Unmanned aerial vehicle hangar

Abstract

The utility model provides an unmanned aerial vehicle hangar which comprises a hangar body, the hangar body comprises a base and a sealing cover, the sealing cover is movably arranged on the base, and the sealing cover and the base form a closed bin used for containing an unmanned aerial vehicle; and the air blowing assembly is arranged on the sealing cover and used for blowing the outer surface of the sealing cover. By means of the scheme, the problems that in the prior art, snow melting is conducted on the sealing cover of the unmanned aerial vehicle hangar in an electric heating mode, water formed after melting can be frozen again on the surface or the edge of the hatch cover, and the hatch cover opening difficulty is increased can be solved.

Description

TECHNICAL FIELD

[0001] The utility model relates to an unmanned plane hangar technical field, specifically, an unmanned plane hangar. BACKGROUND

[0002] In cold regions or winter, the hatch cover of the outdoor unmanned plane hangar often accumulates a large amount of snow, which not only increases the load of the hatch cover, but also may cause the opening and closing of the hatch cover to become difficult, affecting the normal operation of the unmanned plane. In the prior art, hatch cover snow removal mainly relies on manual or electric heating methods.

[0003] Although the manual snow removal method is intuitive and effective, in the case of severe snow accumulation or inconvenient hangar location, the operator has difficulty in quickly and safely removing the snow, and the continuous manual maintenance cost is high and the efficiency is low. If the snow is completely melted by the electric heating method, the efficiency is low, and even if the snow is melted, the water generated by the melting may re-freeze on the surface or edge of the hatch cover, forming an ice layer, which increases the difficulty of opening the hatch cover. SUMMARY

[0004] The utility model provides a kind of unmanned plane hangar to solve the problem that the water formed after melting by the way of electric heating in prior art is re-frozen on the surface or edge of hatch cover, increases the difficulty of opening hatch cover.

[0005] The utility model provides an unmanned plane hangar, comprising: a hangar body, the hangar body includes a base and a cover, the cover is movably arranged on the base, and the cover and the base form a closed warehouse for accommodating the unmanned plane;Blowing assembly, arranged on the cover, the blowing assembly is used to blow the outer surface of the cover.

[0006] Further, the blowing assembly comprises: a flow guide mechanism provided with a through flow guide channel, the flow guide mechanism is arranged on the cover;Blowing part, arranged in the flow guide channel, the blowing part blows along the extension direction of the flow guide channel.

[0007] Further, the flow guide mechanism is rotatably arranged on the cover, when the cover is in the closed state, at least part of the cover forms the top plate of the hangar body, and the extension direction of the flow guide mechanism is parallel to the top plate, and the rotation axis direction of the flow guide mechanism is perpendicular to the top plate.

[0008] Further, the flow guide mechanism is rotatably arranged at the edge of the top plate, the flow guide mechanism has air inlet end and air outlet end oppositely arranged along the extension direction, the flow guide mechanism has first limit position and second limit position, and the air outlet end is directed to the outside of the cover in the first limit position and the second limit position.

[0009] Further, the blowing range of the air outlet end to the top plate is set to 210-230 degrees.

[0010] Further, the part of the cover forming the top plate is provided with an adapter seat, and the flow guide mechanism is rotatably arranged on the adapter seat; the unmanned aerial vehicle hangar further comprises a driving part arranged on the adapter seat, and the driving part is drivingly connected with the flow guide mechanism to drive the flow guide mechanism to rotate.

[0011] Further, the unmanned aerial vehicle hangar further comprises a weather monitoring assembly arranged on the hangar body, and the weather monitoring assembly is used to monitor weather information.

[0012] Further, the weather monitoring assembly comprises a supporting part arranged on the cover, the supporting part has a containing cavity, the side of the supporting part is provided with an air outlet hole, the air outlet hole is communicated with the containing cavity, a blowing assembly is arranged in the containing cavity, and the blowing assembly blows the outer surface of the cover through the air outlet hole; and a weather monitoring part is arranged on the supporting part.

[0013] Further, the air outlet hole is provided in multiple groups, the multiple groups of air outlet holes are distributed along the circumference of the supporting part, each group of air outlet holes is provided with multiple air outlet holes, and the multiple air outlet holes are distributed along the axis direction of the supporting part.

[0014] Further, the cover comprises a first hatch cover and a second hatch cover arranged symmetrically, the bottom ends of the first hatch cover and the second hatch cover are hingedly connected with the base respectively, the first hatch cover and the second hatch cover are buckled to form the cover with an open bottom, and the blowing assembly is arranged on one of the first hatch cover and the second hatch cover.

[0015] The technical scheme of the utility model can avoid the situation that the snow on the cover is possibly frozen after the cover is heated by the heating assembly in the traditional technical scheme, and the convenience of opening the cover is improved. When the cover of the unmanned aerial vehicle hangar in the utility model is covered with snow in cold regions or winter, the blowing assembly is started, the airflow generated by the blowing assembly directly acts on the snow, and the snow is swept off by the wind power, so that the snow on the cover is cleaned. The setting of the utility model can avoid the possibility that the snowmelt water on the cover surface or edge is re-frozen to form an ice layer, reduce the difficulty of opening the cover, and improve the safety. The snow removal mode by the wind power avoids the problems of low efficiency and long waiting time of the electric heating mode, so that the unmanned aerial vehicle can take off quickly when needed, the flexibility and response speed of the unmanned aerial vehicle operation are improved, the power consumption in the snow removal process is reduced, and the operation cost is reduced. BRIEF DESCRIPTION OF DRAWINGS

[0016] The drawings constituting a part of the specification of the application serve to provide further understanding of the present application, the illustrative embodiments of the present application and their descriptions serve to explain the present application, and do not constitute improper limitation on the present application. In the drawings:

[0017] Figure 1 A partial structure schematic view of the unmanned aerial vehicle hangar provided by the present application is shown;

[0018] Figure 2 A partial structure schematic view of the unmanned aerial vehicle hangar provided by the present application is shown; Figure 1 A top view of the structure is shown;

[0019] Figure 3 A structure schematic view of the unmanned aerial vehicle hangar provided by the present application is shown;

[0020] Figure 4 A structure schematic view of the weather monitoring assembly of the unmanned aerial vehicle hangar provided by the present application is shown;

[0021] Figure 5 A partial structure explosion schematic view of the unmanned aerial vehicle hangar provided by the present application is shown.

[0022] Among them, the above drawings include the following reference signs:

[0023] 10, hangar body; 101, top plate;

[0024] 11, base; 12, cover; 121, first hatch; 122, second hatch;

[0025] 20, blowing assembly;

[0026] 30, adapter seat; 31, driving part;

[0027] 40, weather monitoring assembly;

[0028] 41, support part; 411, air outlet hole; 42, weather monitoring part. DETAILED DESCRIPTION

[0029] The technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application. Obviously, the described embodiments are only a part of the embodiments of the present application, rather than all the embodiments. The description of the at least one exemplary embodiment is actually only illustrative, and by no means constitutes any limitation on the present application and its application or use. Based on the embodiments in the present application, all other embodiments obtained by those skilled in the art without creative labor fall within the scope of protection of the present application.

[0030] As Figure 1 and Figure 2The utility model discloses an unmanned plane hangar, including hangar body 10 and blow -off subassembly 20. Hangar body 10 includes base 11 and cover 12, and cover 12 is movably arranged on base 11, and cover 12 and base 11 form the closed storehouse for accommodating unmanned plane, and blow -off subassembly 20 sets up on cover 12, and blow -off subassembly 20 is used to the outside surface of cover 12 is swept.

[0031] The utility model discloses a technical scheme, through blow -off subassembly 20 the snow of the outside surface of cover 12 is swept, can avoid traditional technical scheme, through heating assembly heating cover 12 to melt the snow of cover 12 surface after possibly icing condition, has promoted the convenience of opening cover 12. The unmanned plane hangar of the scheme, when the snow of cover 12 of unmanned plane hangar falls in cold region or winter, starts blow -off subassembly 20, and the airflow generated by blow -off subassembly 20 is directly acted on the snow, and the snow is swept down using wind power, thereby the snow on cover 12 is cleaned. In the scheme, blow -off subassembly 20 will not produce snowmelt water in the snow removal process, thereby avoid the possibility that snowmelt water re-freezes on the surface or edge of cover 12 and forms ice layer, reduce the difficulty of opening cover 12, improve the security. In addition, the mode of wind power blowing snow avoids the problem of low efficiency and long waiting time of using electric heating mode, so that the unmanned plane can take off quickly when needed, improve the flexibility and response speed of unmanned plane operation, and the power consumption of blow -off subassembly 20 is lower, reduces the energy consumption in the snow removal process, reduces operating cost.

[0032] The specific form of the blow -off subassembly 20 is not limited in the scheme, as long as the snow on the surface of the cover 12 can be swept.

[0033] In the embodiment of the scheme, the blow -off subassembly 20 includes a flow guide mechanism and a blow -off part, the flow guide mechanism is provided with a through flow guide channel, and the flow guide mechanism is arranged on the cover 12. The blow -off part is arranged in the flow guide channel, and the blow -off part blows along the extension direction of the flow guide channel. Through the flow guide channel of the flow guide mechanism, the wind power generated by the blow -off part can be concentrated and guided, so that the wind power is enhanced in a specific direction, the unnecessary diffusion of wind power is reduced, the snow can be handled more accurately, the blowing efficiency of the snow on the surface of the cover 12 is effectively improved, and the snow removal effect is enhanced. Moreover, under the protection of the flow guide mechanism, the blow -off part is not easily affected by external severe weather, such as strong wind, hail, etc., the reliability and environmental adaptability of the system are improved, and the snow removal work can be effectively carried out under various severe weather conditions.

[0034] In the embodiment of the scheme, the flow guide mechanism is a duct structure.

[0035] Further, the flow guide mechanism is rotatably arranged on the cover 12, when the cover 12 is in the closed state, at least part of the cover 12 forms the top plate 101 of the hangar body 10, and the extension direction of the flow guide mechanism is parallel to the top plate 101, and the rotation axis direction of the flow guide mechanism is perpendicular to the top plate 101. The above arrangement makes the blowing assembly 20 blow the snow on the top plate 101 of the hangar body 10 in the horizontal direction when the cover 12 is in the closed state, reduces the negative impact of the weight of the snow on the UAV hangar, and also reduces the obstruction of the snow to the opening and closing of the cover 12.

[0036] Further, the flow guide mechanism is rotatably arranged at the edge of the top plate 101, the flow guide mechanism has an air inlet end and an air outlet end arranged opposite to each other along the extension direction, the flow guide mechanism has a first limit position and a second limit position, and the air outlet end is directed to the outside of the cover 12 in both the first limit position and the second limit position. The rotatable characteristic of the flow guide mechanism enables flexible adjustment of the air outlet direction, when the cover 12 is closed, at least part of the cover 12 constitutes the top plate 101 of the hangar body 10, at this time, when the air outlet end of the flow guide mechanism rotates between the two limit positions, the airflow blown by the air outlet end of the flow guide mechanism can cover the entire top plate 101 as much as possible. This arrangement ensures that the snow on the entire surface of the top plate 101 can be touched and removed by the airflow of the blowing assembly 20 when the blowing assembly 20 is working, thereby achieving comprehensive snow removal on the entire surface of the top plate 101.

[0037] In the embodiment of the present scheme, the top plate 101 of the hangar body 10 is substantially rectangular plate-shaped structure, the flow guide mechanism is rotatably arranged at the edge of the length direction side of the top plate 101, and located at the center position of the length direction edge. Such arrangement can improve the uniformity of the distribution of the wind force generated by the blowing assembly 20 on the top plate 101, and improve the efficiency of snow removal.

[0038] Further, the blowing range of the air outlet end to the top plate 101 is set to 210° to 230°. Such arrangement can more accurately blow the snow covered on the top cover, avoid waste of wind force in the non-top plate 101 area, and ensure that the energy is efficiently used for snow removal. That is, the selection of this angle range not only covers the snow area of the top cover, but also avoids excessive rotation leading to excessive energy consumption, realizes the effective use of energy and cost control, reduces the overwork of the blowing assembly 20, prolongs the service life of the blowing assembly 20, and reduces the maintenance frequency and cost.

[0039] In the present scheme, the blowing range of the air outlet end to the top plate 101 can be set to 210°, 220° or 230°, etc., which can be adjusted according to specific conditions.

[0040] Further, the air guide mechanism is located on the median line of the length direction of the top plate 101 of the hangar body 10, and the air outlet end of the air guide mechanism is symmetrically arranged relative to the median line of the length direction of the top plate 101 when the air outlet end is in the first limit position and when the air outlet end is in the second limit position. In this way, the uniformity of the blowing of the top plate 101 can be further improved. As shown in Figure 2 the line L in the figure is the median line of the length direction of the top plate 101 of the hangar body 10, and the included angle A is the blowing range of the air outlet end to the top plate 101.

[0041] As shown in Figures 3 to 5 the embodiment of the present scheme, the part of the cover 12 forming the top plate 101 is provided with an adapter seat 30, and the air guide mechanism is rotatably arranged on the adapter seat 30; the unmanned aerial vehicle hangar further comprises a driving part 31, which is arranged on the adapter seat 30, and the driving part 31 is drivingly connected with the air guide mechanism to drive the air guide mechanism to rotate. The connection between the driving part 31 and the air guide mechanism makes the snow blowing process automatic, reduces the need for manual intervention, reduces the labor intensity of the operator, avoids the safety risks that may be caused by manual operation, and improves the operation convenience and safety of the unmanned aerial vehicle hangar in snowy weather. By installing the air guide mechanism and the driving part 31 through the adapter seat 30, the structure layout can be optimized, and the overall mechanical stability can be improved. The adapter seat 30 as an intermediate connecting piece can disperse the force generated when the air guide mechanism rotates, reduce the direct stress on the cover 12, protect the cover 12, and prolong the service life of the unmanned aerial vehicle hangar. Moreover, the design of the adapter seat 30 makes the air guide mechanism and the driving part 31 easy to disassemble and reassemble, which is convenient for regular maintenance and fault inspection.

[0042] The present scheme does not limit the specific form of the driving part 31. In the embodiment, the driving part 31 is a rudder. The rudder is well-known for its high-precision rotation angle control capability. The rudder can very accurately adjust the rotation angle of the air guide mechanism, ensuring that it works stably within the preset blowing range. The response speed of the rudder is fast, and it can quickly adjust the position of the air guide mechanism. In addition, the rudder is usually small in size and compact in structure, and is easy to integrate on the adapter seat 30.

[0043] Further, the unmanned aerial vehicle hangar further comprises a weather monitoring assembly 40, which is arranged on the hangar body 10 and is used for monitoring weather information. In the embodiment of the present scheme, the weather monitoring assembly 40 adopts the weather monitoring assembly 40 in the prior art, which can monitor parameters such as temperature, humidity, wind speed, and snowfall. Through the above-mentioned weather information, the worker can judge the snow accumulation situation and the snow removal demand, so as to adjust the working state of the air blowing assembly 20, realize intelligent snow removal control, and improve the efficiency and pertinence of snow removal.

[0044] In the embodiment of the present scheme, the weather monitoring assembly 40 comprises a support part 41 and a weather monitoring part 42. The support part 41 is arranged on the cover 12, and the support part 41 has a containing cavity. The side part of the support part 41 is provided with an air outlet hole 411, which is in communication with the containing cavity. The air blowing assembly 20 is located in the containing cavity and blows air to the outer surface of the cover 12 through the air outlet hole 411. The weather monitoring part 42 is arranged on the support part 41. The design of the support part 41 not only provides a mounting position for the weather monitoring part 42, but also provides a mounting space for the air blowing assembly 20. The air blowing assembly 20 can be installed in the hangar in a concealed manner, reducing the influence of the harsh environment on the air blowing assembly 20 and the influence on the appearance of the hangar, and achieving effective optimization of the structure and space.

[0045] In some embodiments of the present scheme, the hangar further comprises a control system. The weather monitoring part 42 and the driving part 31 are electrically connected to the control system. The weather monitoring part 42 feeds back the monitored weather information to the control system. The control system controls the driving speed of the driving part 31 according to the monitoring information of the weather monitoring part 42, so as to control the rotating speed of the flow guiding mechanism.

[0046] Further, the air outlet hole 411 is arranged in multiple groups. The multiple groups of air outlet holes 411 are distributed along the circumferential direction of the support part 41. Each group of air outlet holes 411 comprises multiple air outlet holes 411, which are distributed along the axial direction of the support part 41. The above arrangement can ensure that the airflow generated by the air blowing assembly 20 covers the surface of the cover 12 more uniformly, improving the efficiency and uniformity of snow removal.

[0047] The present scheme does not limit the specific connection mode of the cover 12 and the base 11.

[0048] In some embodiments of the present scheme, the base 11 has an open top structure. The cover 12 is slidably arranged on the base 11 in the horizontal direction to block or open the base 11.

[0049] In the embodiment of the present scheme, the cover 12 comprises a first hatch 121 and a second hatch 122 arranged symmetrically. The bottom ends of the first hatch 121 and the second hatch 122 are hingedly connected to the base 11. The first hatch 121 and the second hatch 122 are buckled to form a cover 12 with an open bottom. The air blowing assembly 20 is arranged on one of the first hatch 121 and the second hatch 122. When the first hatch 121 and the second hatch 122 are closed, the air blowing assembly 20 is located at the top of the first hatch 121, and the air blowing assembly 20 is located at the edge of the top of the first hatch 121 away from the second hatch 122.

[0050] It is to be understood that the terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of example embodiments in accordance with the present application. As used herein, the singular forms "a", "an" and "the" are intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms "comprises" and / or "comprising," when used in this specification, specify the presence of stated features, steps, operations, devices, components and / or combinations thereof, but do not preclude the presence or addition of one or more other features, steps, operations, devices, components and / or combinations thereof.

[0051] The relative arrangement of parts and steps, numerical expressions, and numerical values set forth in these embodiments are not intended to limit the scope of the present application unless otherwise specifically stated. At the same time, it should be understood that the sizes of the various parts shown in the drawings are not drawn in accordance with the actual proportional relationship. The technology, methods and devices known to those skilled in the related art can not be discussed in detail, but should be considered as part of the specification under appropriate circumstances. In all examples shown and discussed herein, any specific value should be interpreted as merely exemplary and not as a limitation. Therefore, other examples of exemplary embodiments can have different values. It should be noted that similar reference numbers and letters represent similar items in the following drawings, so further discussion is not needed in subsequent drawings once an item is defined in one drawing.

[0052] In the description of the present application, it should be understood that the orientation words such as "front, back, up, down, left, right", "horizontal, vertical, perpendicular, horizontal" and "top, bottom" and the like indicate the orientation or positional relationship shown in the drawings, which is only for the convenience of describing the present application and simplifying the description, and in the absence of contrary statements, these orientation words do not indicate and imply that the indicated device or element must have a particular orientation or be constructed and operated in a particular orientation, and therefore cannot be understood as limiting the scope of protection of the present application; the orientation words "inner, outer" refer to the inner and outer of the contour of each component itself.

[0053] For purposes of the description hereinafter, spatial relative terms, such as "above", "below", "upper", "lower", and the like, can be used to describe the relative position of one element or feature to another as illustrated in the figures. It will be understood that the spatial relative terms are intended to encompass different orientations of the device in use or operation in addition to the orientations depicted in the figures. For example, if the device in the figures is turned over, elements described as "above" or "up" other elements or features would then be oriented "below" or "down" the other elements or features. Thus, the exemplary term "above" can encompass both an orientation of above and below. The device can be otherwise oriented (rotated 90 degrees or at other orientations) and the spatially relative descriptors used herein interpreted accordingly. Well, the spatial relative terms used herein are for ease of description only and do not limit the scope of the present application.

[0054] In addition, it should be noted that the use of "first", "second", and the like words of distinction do not limit the corresponding parts, and are only used to distinguish the corresponding parts for convenience, and the above words have no special meaning unless otherwise stated, and therefore cannot be understood as limiting the scope of protection of the present application.

[0055] The above only describes the preferred embodiments of the present application and is not intended to limit the present application. For those skilled in the art, the present application can have various modifications and changes. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present application shall be included in the protection scope of the present application.

Claims

1. A drone hangar, characterized in that, The unmanned aerial vehicle hangar comprises: a hangar body (10) comprising a base (11) and a cover (12) movably arranged on the base (11), the cover (12) and the base (11) forming a closed compartment for accommodating an unmanned aerial vehicle; a blowing assembly (20) arranged on the cover (12) and used for blowing the outer surface of the cover (12).

2. The drone hangar of claim 1, wherein, The blowing assembly (20) comprises: a flow guide mechanism provided with a through flow guide channel, the flow guide mechanism being arranged on the cover (12); a blowing part arranged in the flow guide channel and blowing along the extension direction of the flow guide channel.

3. The drone hangar of claim 2, wherein, The flow guide mechanism is rotatably arranged on the cover (12), at least a part of the cover (12) forms a top plate (101) of the hangar body (10) when the cover (12) is in a closed state, the extension direction of the flow guide mechanism is parallel to the top plate (101), and the rotation axis direction of the flow guide mechanism is perpendicular to the top plate (101).

4. The drone hangar of claim 3, wherein, The flow guide mechanism is rotatably arranged at the edge of the top plate (101), the flow guide mechanism has an air inlet end and an air outlet end arranged oppositely along the extension direction, the flow guide mechanism has a first limit position and a second limit position, and the air outlet end is directed to the outside of the cover (12) in the first limit position and the second limit position.

5. The drone hangar of claim 4, wherein, The blowing range of the air outlet end to the top plate (101) is arranged at 210° to 230°.

6. The drone hangar of claim 3, wherein, The part of the cover (12) forming the top plate (101) is provided with an adapter seat (30), the flow guide mechanism is rotatably arranged on the adapter seat (30), the unmanned aerial vehicle hangar further comprises a driving part (31) arranged on the adapter seat (30), the driving part (31) is in driving connection with the flow guide mechanism to drive the flow guide mechanism to rotate.

7. The drone hangar of claim 1, wherein, The unmanned aerial vehicle hangar further comprises: a weather monitoring assembly (40) arranged on the hangar body (10) and used for monitoring weather information.

8. The drone hangar of claim 7, wherein, The weather monitoring assembly (40) comprises: a support part (41) arranged on the cover (12) and having an accommodation cavity, a side part of the support part (41) is provided with an air outlet hole (411) in communication with the accommodation cavity, the blowing assembly (20) is located in the accommodation cavity, and the blowing assembly (20) blows the outer surface of the cover (12) through the air outlet hole (411); a weather monitoring part (42) arranged on the support part (41).

9. The drone hangar of claim 8, wherein, The air outlet hole (411) is arranged in multiple groups, the multiple groups of air outlet holes (411) are distributed along the circumferential direction of the support part (41), each group of air outlet holes (411) is arranged in multiple, and the multiple air outlet holes (411) are distributed along the axis direction of the support part (41).

10. The drone hangar of claim 1, wherein, The cover (12) comprises a first hatch (121) and a second hatch (122) arranged symmetrically, bottom ends of the first hatch (121) and the second hatch (122) are respectively hinged to the base (11), the first hatch (121) and the second hatch (122) are buckled to form the cover (12) with an open bottom, and the blowing assembly (20) is arranged on one of the first hatch (121) and the second hatch (122).

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