Novel modularized light-weight unmanned aerial vehicle hangar cabin

Abstract

The utility model belongs to the technical field of unmanned aerial vehicles, and particularly relates to a novel modularized light-weight unmanned aerial vehicle hangar cabin. Comprising connecting pieces, baffles, a supporting table and connecting plates. The connecting pieces are spliced into a whole frame of the cabin body, the baffles are embedded in the periphery and the bottom of the frame, clamping grooves are formed in the bottoms of the connecting pieces, the baffles are clamped in the clamping grooves, the baffles are made of cellular boards, cabin doors capable of being opened and closed are formed in the baffles, and the supporting table is arranged in the cabin body formed by the baffles; at least two connecting plates are installed between the connecting pieces located at the bottom of the frame, and the supporting tables are installed on the connecting plates. The detachable baffle is installed between the connecting pieces, meanwhile, the cabin door capable of being opened and closed is installed on the baffle, the baffle can be replaced according to requirements, and components in the cabin body can be conveniently and rapidly maintained by opening the cabin door.

Description

TECHNICAL FIELD

[0001] The utility model belongs to the technical field of unmanned plane, concretely relates to a modularization light weight novel unmanned plane hangar cabin body. BACKGROUND

[0002] In the technical field of unmanned plane, the hangar is the core facility for storing, charging and maintaining unmanned plane, and the existing unmanned plane hangar cabin body generally has problems such as rigid structure, difficult maintenance and insufficient mobility: the traditional frame adopts welding process or integral forming design, is difficult to modularization dismounting, and the transportation and size adjustment efficiency is low; the cabin plate is mostly made of solid metal material, which meets the strength requirement but has too large self weight, seriously restricting the rapid deployment ability in the field; the maintenance passage is designed single, and the bottom equipment maintenance often needs to dismount the cabin plate, which is time-consuming and cumbersome to operate.

[0003] The utility model discloses a kind of unmanned plane hangars, belong to unmanned plane field.A kind of unmanned plane hangar, including storage bin, the support plate is slidably connected on the storage bin, the intercepting plate is slidably connected on the support plate surface, the placing plate is rotationally arranged in the support plate middle part, the support plate axle position is connected with the limit plate, the end of the placing plate extends to the top of limit plate, and placing plate can be with support plate in the same horizontal plane, when intercepting plate moves towards placing plate, limit plate is pressed by the end of placing plate;The utility model can utilize intercepting plate to push the position of rack, so that it can push the position of unmanned plane to specified range, adjust the position deviated when rack lands, prevent bumping to the wing of unmanned plane when storage. The above device frame adopts integral forming metal shell, so that the device is heavy as a whole, cannot realize the size of cabin body according to demand expansion, and when transporting, it needs to be hoisted as a whole, and the device is heavy as a whole, cannot be quickly maintained inside cabin body. Therefore, the above technical problems are solved by the technical personnel in the art. SUMMARY

[0004] The technical problem to be solved by the present application is that the integral forming metal shell in the above-mentioned prior art results in a heavy device as a whole, which cannot realize the size of the cabin body according to the demand expansion, and when transporting, it needs to be hoisted as a whole, and the device is heavy as a whole, which cannot quickly maintain the inside of the cabin body.

[0005] To solve the above technical problems, the technical solution adopted by the utility model has:

[0006] A modularization light weight novel unmanned plane hangar cabin body, comprising a connecting piece, a baffle, a support table and a connecting plate.

[0007] The connecting pieces are spliced to form a three-dimensional frame structure of the cabin body, the four surrounding vertical surfaces and the bottom plane of the frame are embedded with the baffle plates, the bottom of the connecting piece extends to form a clamping groove with a limiting protrusion, and the baffle plate is clamped and fixed in the clamping groove.

[0008] The baffle plate is molded by a honeycomb plate, and the front surface of the baffle plate is provided with an openable cabin door.

[0009] The support table is arranged inside the closed cabin body formed by the baffle plate.

[0010] At least two parallel connecting plates are arranged transversely between the adjacent connecting pieces at the bottom of the frame, and the support table is fixed to the connecting plates by bottom supports.

[0011] By adopting the above technical scheme, the aluminum alloy connecting pieces are spliced to form a frame structure, and the honeycomb plate baffle plates are clamped and fixed, so that the cabin body can be quickly disassembled and expanded in size as needed. The modular design supports the decomposition into lightweight components during transportation, which can be quickly assembled on site with only simple tools, solving the transportation problem of traditional hangars that need to be hoisted as a whole. At the same time, the light weight of aluminum alloy and honeycomb plate (significantly reducing the self weight, improving the ability of rapid deployment in the field, adapting to the expansion needs of different scenes, the traditional solid metal cabin plate is difficult to maintain due to its heavy weight, and the baffle plate molded by the honeycomb plate in the present scheme has a honeycomb structure with light weight and high strength, which significantly reduces the self weight of the cabin body and meets the structural strength requirement. The baffle plate is quickly disassembled through the clamping groove limiting protrusion, and the openable cabin door and maintenance window are matched, so that the internal equipment maintenance can be completed without completely disassembling, the heat insulation performance of the honeycomb plate can reduce the cabin temperature control energy consumption and improve the air conditioning efficiency.

[0012] Further, the baffle plate is provided with an air conditioner maintenance window, the air conditioner maintenance window is provided with an openable cover plate, and the cover plate is hinged on one side of the air conditioner maintenance window.

[0013] By adopting the technical scheme, the air conditioner maintenance window is arranged to allow direct access to the air conditioner without disassembling the baffle, and only the hinged cover plate needs to be opened for maintenance or replacement of parts, which is suitable for scenarios such as power inspection, emergency rescue and the like that require high-frequency operation, ensures continuous operation of the unmanned aerial vehicle system, and the air conditioner is a core device for controlling the temperature and humidity inside the hangar, and its normal operation directly affects the battery life and sensor accuracy of the unmanned aerial vehicle. When the hinged cover plate is closed, air-tight sealing can be achieved through magnetic attraction or buckling to prevent rainwater, dust or external high / low temperature from entering. When maintenance is performed, only the local window is opened to avoid sudden temperature changes in the cabin due to disassembly of the baffle, ensuring stable operation of the equipment. The hinged cover plate design supports manual opening and closing, and maintenance personnel can quickly access the air conditioner without carrying tools, which meets the needs of rapid deployment scenarios in the field. When the cover plate is closed, it can be locked to prevent accidental opening during flight or transportation, and to avoid the risk of foreign matter entering or accidental touch by personnel. The window can be designed of transparent material to allow observation of the air conditioner operating state without opening the cover plate, further improving maintenance efficiency.

[0014] Further, the support table bottom is further provided with an insert box mounting table, and the insert box mounting table is mounted on the connecting plate through bolts.

[0015] By adopting the technical scheme, the insert box mounting table is connected through bolts, and the insert box can be quickly installed or removed. When performing a power inspection task, a large-capacity battery insert box can be added. When performing an emergency rescue task, an emergency power supply or communication equipment insert box can be replaced to support plug-and-play of different brands or custom insert boxes, reduce customization costs, and if the insert box fails, the maintenance personnel only need to loosen the bolts to remove the insert box without cutting or welding. If the charging insert box fails, a spare insert box can be quickly replaced to ensure uninterrupted endurance of the unmanned aerial vehicle. Through independent replacement of the insert box, the entire support table or cabin body is prevented from being stopped due to maintenance, the availability of the hangar is improved, the insert box mounting table is horizontally arranged through the connecting plate and the frame bottom connecting piece to ensure uniform distribution of the weight of the insert box and prevent local overload, the weight of the large-capacity battery insert box can be distributed to multiple connecting pieces through the connecting plate to improve the structural safety, and the bolt connection in combination with the bottom support leg design of the support table can buffer the vibration during take-off and landing or transportation of the unmanned aerial vehicle to protect the precision components in the insert box.

[0016] Further, the bottom of the cabin body is further provided with an air conditioner, and the air conditioner is mounted on the two connecting plates through bolts.

[0017] By adopting the above technical solution, the bottom air conditioner is designed to be fixed to the connecting plate by bolts, combined with the temperature and humidity control requirements of the unmanned hangar in the knowledge base, the bolt connection allows the air conditioner to be quickly installed or disassembled without welding or complex tools, the bolt interface is standardized, supports future replacement of higher performance air conditioner models or expansion of multiple air conditioners, adapts to the temperature control requirements of different scale hangars, and the air conditioner is horizontally arranged at the bottom of the frame through two connecting plates. The weight is evenly distributed to the connecting parts to avoid local overload. For example, the weight of a high-power air conditioner can be distributed horizontally through the connecting plate to the entire frame to improve the structural safety, and the bolt connection combined with rubber gaskets or shock-absorbing bolts can buffer the vibration during the take-off and landing or transportation of the unmanned aerial vehicle, protect the internal precision components of the air conditioner, and prolong the service life.

[0018] Further, the plug-in box mounting table is mounted on the connecting plate through a support column, and the support column is mounted on the connecting plate through bolts.

[0019] By adopting the above technical solution, in the design of the unmanned aerial vehicle hangar cabin, the plug-in box mounting table is fixed to the connecting plate through a support column and bolts, which has significant advantages in structural stability, modular expansion, space optimization, and maintenance efficiency, allows the plug-in box mounting table to adjust the position according to the equipment height requirements (such as battery plug-in box, data processing unit, etc.), supports quick installation or replacement of different specifications of support columns and plug-in box mounting tables, reduces customized costs, the support column evenly distributes the weight of the plug-in box mounting table to the connecting plate and the connecting parts at the bottom of the frame, avoids local stress concentration, the weight of the large-capacity battery plug-in box is transmitted to the horizontal connecting plate through the support column, improves the overall structural safety, and the bolt connection combined with rubber shock-absorbing pads or elastic support columns can buffer the vibration during the take-off and landing or transportation of the unmanned aerial vehicle, and protect the precision components in the plug-in box.

[0020] Further, the connecting parts are made of aluminum alloy, and two adjacent connecting parts are welded together.

[0021] By adopting the technical scheme, the welding forms atomic-level combination through high-temperature molten metal, the strength of the welding seam is higher than that of bolt or rivet connection, and there is no risk of loosening of mechanical connection, the post-strength is significantly improved, the bearing requirement of the hangar frame can be met, the overall weight is reduced, the welding can realize precise combination of special-shaped connecting pieces, is suitable for the three-dimensional frame structure of the hangar cabin body, ensures the structural rigidity, the aluminum alloy surface naturally forms a dense oxide film, effectively isolates oxygen and moisture, reduces the corrosion risk, through argon arc welding and other protective gas welding, the oxide film can be prevented from being damaged in the welding process, the corrosion resistance of the welding seam area is consistent with that of the base material, is suitable for outdoor scenes such as electric power inspection and emergency logistics, prolongs the service life of the hangar, compared with a steel structure, the aluminum alloy connecting piece can reduce the self weight of the cabin body, significantly improves the transportation efficiency and field deployment capability, without bolts, nuts and other connecting pieces, further reduces the weight and simplifies the structure, through the design of detachable baffles and cabin doors, partial modularization can still be realized.

[0022] The utility model has the advantages of the following beneficial effects:

[0023] 1. The utility model discloses a frame structure is spliced into by aluminum alloy connecting piece, adopts the baffle of honeycomb board die forming, realizes the quick dismounting of cabin body and size on demand extension, and the lightweight material combination of aluminum alloy and honeycomb board makes cabin body self weight significantly reduce, supports the decomposition into lightweight assembly when transporting, only needs simple tool to be quick on -the -spot assembly, solved the transportation problem of traditional metal shell heavy, need integral hoisting, especially suitable for field rapid deployment and multi -scene extension demand;

[0024] 2. The utility model discloses the quick dismounting of baffle is realized through the clamping groove limiting protruding, cooperates the cabin door and air conditioning maintenance window of open -close, need not complete dismounting baffle to complete internal equipment maintenance, greatly shortens the maintenance time and guarantees the cabin humidity stability, and the air conditioner all adopts bolt installation in the connecting plate of plug -in box installation platform, supports the quick replacement and function extension of plug -in box, can replace the module independently when trouble, avoids the cabin body shutdown because of maintenance, significantly improves the sustained operation ability of hangar;

[0025] 3. The utility model discloses the aluminum alloy welding process is used through connecting piece, forms high -strength frame structure, combines the lightweight high -strength characteristic of honeycomb board baffle, gives consideration to structural rigidity and anticorrosion ability, and the bottom air conditioner is fixed through bolt in the connecting plate, evenly disperses weight and buffers vibration, cooperates the heat -insulating performance of honeycomb board, reduces temperature control energy consumption, ensures that the stable operation of unmanned aerial vehicle battery and sensor under extreme environment, adapts to complex task demand such as electric power inspection, emergency rescue. BRIEF DESCRIPTION OF DRAWINGS

[0026] Figure 1 It is whole structure schematic diagram of the utility model's removal cabin door;

[0027] Figure 2The utility model discloses a structure schematic drawing of connecting piece;

[0028] Figure 3 The utility model discloses a structure schematic drawing of frame;

[0029] Figure 4 The utility model discloses a structure schematic drawing of support platform;

[0030] Figure 5 The utility model discloses a structure schematic drawing of cabin door opening;

[0031] Figure 6 The utility model discloses a structure schematic drawing of cabin door closing.

[0032] Among them, 10-frame;11-connecting piece;111-slot;12-baffle;121-cabin door;13-air conditioner maintenance window;131-cover plate;

[0033] 20-support platform;21-insert box installation platform;22-connecting plate;23-strut;24-bottom support;

[0034] 30-air conditioner. Specific implementation

[0035] The utility model will be further explained in detail below in combination with the drawings and specific preferable implementation.

[0036] In the description of the utility model, it is understood that the orientation or position relation that the terms "left side", "right side", "upper part", "lower part" etc. indicate is based on the orientation or position relation shown in the drawing, and is only for the convenience of describing the utility model and simplifying the description, and does not indicate or imply that the device or element indicated must have a particular orientation, be constructed and operated in a particular orientation, "first", "second" etc. do not represent the importance of the parts, so it can not be understood as the limitation of the utility model. The specific size adopted in the embodiment is only for illustrating the technical scheme, and does not limit the protection scope of the utility model.

[0037] Refer to Figure 1 , Figure 2 , Figure 3 , Figure 4 , Figure 5 And Figure 6The utility model discloses a modular lightweight novel unmanned aerial vehicle hangar cabin body, and the device is a kind of modular lightweight unmanned aerial vehicle hangar cabin body, including the frame 10 being spliced by connecting piece 11, connecting piece 11 is made of aluminium alloy, and the three-dimensional frame 10 of cabin body is formed by welding each other splicing.By welding, the stable frame main body of adjacent connecting piece 11 is formed, as the basic support structure of cabin body, the bottom of each connecting piece 11 extends the clamping groove 111 with limiting protrusion, for fixed baffle 12, baffle 12 adopts honeycomb board moulding, and is embedded on the four around vertical surface and bottom plane of three-dimensional frame 10, is fixed by clamping groove 111, forms cabin body, baffle 12 front is provided with the cabin door 121 that can be opened and closed, for the repair inside component of cabin body, baffle 12 is equipped with air conditioner repair window 13, and its side edge is hinged the cover plate 131 that can be opened and closed, facilitate maintenance operation;Supporting platform 20 is located in the closed cabin body enclosed by baffle 12, for carrying unmanned aerial vehicle, four parallelly arranged connecting plates 22 are horizontally arranged between the adjacent connecting piece 11 of frame 10 bottom, as the installation base of supporting platform 20, supporting platform 20 is fixed on connecting plate 22 by bottom support 24, realizes rigid connection with frame 10, and plug-in box installation platform 21 is located at the bottom of supporting platform 20, and is directly installed on connecting plate 22 by bolt.Supporting column 23 is connected with connecting plate 22 by bolt, and forms layered support structure.Air conditioner 30 is installed at the bottom of cabin body, and is fixed between two parallel connecting plates 22 by bolt, to ensure the stable connection of air conditioner and frame.

[0038] In one embodiment, the baffle 12 of the device adopts modular design, and the replacement process is simple and efficient, first, the baffle 12 to be replaced is taken out from the clamping groove 111 of the frame 10. When operating, first, the connection of the connecting piece 11 is released, then the baffle 12 is taken out from the clamping groove 111 in the vertical direction of the clamping groove 111, and is pushed slightly until the baffle 12 is completely separated from the clamping groove 111. If the baffle 12 is integrated with the cabin door 121 or the air conditioner repair window 13, it is necessary to ensure that the cabin door 121 is in the closed state to avoid uneven stress leading to deformation, if the air conditioner repair window 13 on the baffle 12 needs to be retained or reused, the hinged cover plate 131 can be separately detached, the new baffle 12 is aligned with the clamping groove 111 of the frame 10, inserted into the clamping groove entrance at an inclined angle, then the baffle is horizontally pushed to make it slide into place along the clamping groove 111 of the connecting piece 11, then the connecting piece 11 is spliced as a whole to form the frame 10, and the baffle 12 is clamped between the connecting pieces 11. The baffle 12 realizes quick disassembly and assembly through standardized clamping structure, without disassembling the cabin body internal supporting platform 20, connecting plate 22 and other components, reducing the maintenance complexity, at the same time, the honeycomb plate material ensures that the replacement process is light and efficient, and adapts to the unmanned aerial vehicle hangar maintenance requirements in different environments.

[0039] In one embodiment, the support table 20 and the patch panel mounting table 21 of the device are quickly installed through a modular design. The connecting plates 22 are fixed at the bottom of the three-dimensional frame 10, and four parallel connecting plates 22 are transversely arranged between adjacent connecting members 11 and fixed with the connecting members 11 by welding to form a horizontal mounting base. The feet 24 at the bottom of the support table 20 are aligned with the preset mounting hole positions on the connecting plates 22, and the feet 24 are vertically fixed on the connecting plates 22 by bolts to ensure the rigid connection of the support table 20 and the connecting plates 22. The height of the feet 24 is adjusted to keep the support table 20 horizontal, and finally the locking bolts are tightened to complete the installation of the unmanned aerial vehicle carrying platform. The patch panel mounting table 21 is directly placed in the specified area of the connecting plate 22, and the mounting holes at the bottom of the patch panel mounting table 21 are penetrated by bolts and the reserved hole positions of the connecting plate 22, and are tightly fixed and rigidly connected with the connecting plate 22. If it is necessary to raise the patch panel mounting table 21 for layered layout, a support column 23 can be installed on the connecting plate 22 first, the bottom end of the support column 23 is fixed on the connecting plate 22 by bolts, and then the patch panel mounting table 21 is fixed at the top end of the support column 23 by bolts to form a layered support structure. The support table 20 and the patch panel mounting table 21 are connected with the connecting plate 22 by bolts without welding, which is convenient for disassembly, adjustment or function expansion. The patch panel mounting table 21 supports direct installation or lifting installation by replacing the length of the support column 23 to adapt to the layout requirements of different sizes of patch panel equipment. The parallel design of the connecting plates 22 disperses the load, and the rigid connection of the feet 24 and the support column 23 ensures the stability and reliability of the overall structure.

[0040] In one embodiment, the device realizes convenient maintenance of the equipment inside the cabin through the cabin door 121 and the air conditioner maintenance window 13. The cabin door 121 is arranged on the front of the baffle 12 as the main maintenance passage, and its size is suitable for personnel access and large equipment carrying requirements. After unlocking the locking mechanism and pushing open the cabin door, the unmanned aerial vehicle on the inner support table 20 and the patch panel mounting table 21 in the cabin can be maintained or replaced. The height of the support table can be adjusted or the equipment can be disassembled by loosening the bolts of the bottom feet 24 or the support column 23. After maintenance, the cabin door is closed and the locking mechanism is reset to ensure the sealing performance. The air conditioner maintenance window 13 is integrated on the baffle 12, and the hinged cover plate 131 is specially used for the quick maintenance of the air conditioner 30. Through the double-channel structure cabin door 121 for comprehensive maintenance, the air conditioner maintenance window 13 for quick maintenance of the air conditioner 30, and the modular connection without disassembly of other parts, the efficient operation and maintenance and the integrity of the cabin are considered, and the maintenance efficiency and environmental stability of the unmanned aerial vehicle hangar are significantly improved.

[0041] Working principle: the device is welded by aluminum alloy connecting piece 11 to form a three-dimensional frame 10 as the core load-bearing structure of the cabin, combined with the baffle 12 molded by the honeycomb panel embedded in the frame around and the bottom, the baffle is quickly clamped and fixed through the clamping groove 111 and integrates the cabin door 121 and the air conditioner maintenance window 13, taking into account the needs of sealing, functionality and lightweight; four parallel connecting plates 22 are horizontally arranged at the bottom of the frame to form a layered support system, the support table 20 is bolted to the connecting plate 22 through the support leg 24 to support the unmanned aerial vehicle, the plug-in box installation table 21 is installed by bolt or support column 23 to adapt to the equipment layout, and the air conditioner 30 is directly fixed between the connecting plates 22 to realize environmental control. The modular design improves efficiency through double maintenance channel door main repair and window local maintenance, the cabin door 121 provides personnel access and large equipment maintenance path, the hinged cover plate 131 of the air conditioner maintenance window 13 supports the daily operation such as filter replacement, and energy loss is reduced. The lightweight of the device is derived from the optimization of material and structure: the frame 10 made of aluminum alloy has low density and high strength, the hollow honeycomb structure in the baffle 11 reduces weight, and the clamping groove 111 is embedded and designed with parallel connecting plates to avoid redundant materials; the convenience is embodied in that the baffle is horizontally pushed into the clamping groove, the support table 20 and the plug-in box installation table 21 are adjusted in height by adjusting the support column 23, the non-destructive disassembly components can be directly reused without welding, and the environmental adaptability can quickly replace components to cope with different scenes, so that the weight is reduced, the operation and maintenance efficiency is improved, and an efficient, flexible and durable solution for the unmanned aerial vehicle hangar is provided.

[0042] The preferred embodiments of the utility model are described in detail above, but the utility model is not limited to the specific details in the above embodiments, and various equivalent transformations of the technical solutions of the utility model can be made within the technical concept of the utility model, and these equivalent transformations all belong to the protection scope of the utility model.

Claims

1. A novel modular and lightweight unmanned aerial vehicle (UAV) hangar cabin, characterized in that: Includes connector (11), baffle (12), support platform (20) and connecting plate (22); The connectors (11) are spliced ​​together to form a three-dimensional frame (10) structure of the cabin. The baffles (12) are embedded in the four sides and the bottom plane of the frame (10). The bottom of the connectors (11) extends to form a slot (111) with a limiting protrusion. The baffles (12) are snapped and fixed in the slot (111). The baffle (12) is formed by honeycomb plate molding, and the front of the baffle (12) is provided with an openable and closable hatch (121). The support platform (20) is provided inside the closed cabin formed by the baffle (12). At least two parallel connecting plates (22) are horizontally mounted between adjacent connecting parts (11) at the bottom of the frame (10), and the support platform (20) is fixed to the connecting plates (22) by bottom support feet (24).

2. The modular and lightweight novel UAV hangar cabin according to claim 1, characterized in that: The baffle (12) is provided with an air conditioning maintenance window (13), and the air conditioning maintenance window (13) is provided with an openable and closable cover (131), which is hinged to one side of the air conditioning maintenance window (13).

3. The modular and lightweight novel UAV hangar cabin according to claim 1, characterized in that: The bottom of the support platform (20) is also provided with a box mounting platform (21), which is mounted on the connecting plate (22) by bolts.

4. The modular and lightweight novel UAV hangar cabin according to claim 3, characterized in that: An air conditioner (30) is also provided at the bottom of the cabin, and the air conditioner (30) is installed on the two connecting plates (22) by bolts.

5. The modular and lightweight novel UAV hangar cabin according to claim 3, characterized in that: The insertion box mounting platform (21) is mounted on the connecting plate (22) by a support column (23), and the support column (23) is mounted on the connecting plate (22) by bolts.

6. The modular and lightweight novel UAV hangar cabin according to claim 1, characterized in that: The connector (11) is made of aluminum alloy, and two adjacent connectors (11) are welded together.

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