Carrying type full-folding multifunctional flying platform

Abstract

The utility model relates to the technical field of unmanned aerial vehicles, and provides a carrying type full-folding multifunctional flying platform which comprises a main body, the main body is provided with a connecting part, a transverse folding piece is arranged on the connecting part, a rod frame is arranged on the transverse folding piece, a supporting folding frame is arranged on the transverse folding piece, and the folding direction of the supporting folding frame is perpendicular to the folding direction of the transverse folding piece. The landing frame is arranged on the supporting folding frame. Through the technical scheme, the problem that a carrying type unmanned aerial vehicle in the prior art is inconvenient to transport is solved.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles (UAVs), and in particular to a carrier-type fully foldable multifunctional flying platform. Background Art

[0002] In today's era of booming drone technology, transport drones are playing an indispensable role in many fields, including surveying and mapping, agricultural plant protection, emergency rescue, and logistics distribution. However, existing transport drone technology has exposed a series of shortcomings that need to be addressed when meeting diverse operational needs.

[0003] The structural design of traditional drones often lacks consideration for portability and efficient space utilization. Their component layouts are often relatively fixed and fragmented, making them difficult to compress for transportation and storage, resulting in a bulky and irregular overall appearance. This places extremely stringent demands on the specifications of the transport vehicle. Limited space in the trunks of small vehicles often makes it impossible to accommodate drones, necessitating the use of larger vehicles, which significantly increases transportation costs. Furthermore, when frequent relocation is required, such as in field surveying projects requiring constant changes in measurement locations or emergency rescue operations requiring rapid transfers between complex environments, the cumbersome handling and placement process consumes significant time and effort, severely hindering operational efficiency and equipment mobility, making it difficult to meet the efficient and flexible pace of modern operations. Utility Model Content

[0004] The utility model provides a carrier-type fully foldable multifunctional flying platform, which solves the problem of inconvenient transportation of carrier-type UAVs in related technologies.

[0005] The technical solution of the utility model is as follows:

[0006] A fully foldable, multi-functional flying platform for transport, including:

[0007] a main body having a connecting portion,

[0008] a transverse folding member, the transverse folding member being arranged on the connecting portion,

[0009] a rod frame, the rod frame being arranged on the transverse folding member,

[0010] A supporting folding frame, wherein the supporting folding frame is arranged on the transverse folding member, and the folding direction is perpendicular to the folding direction of the transverse folding member,

[0011] A landing gear is provided on the supporting folding frame.

[0012] As a further technical solution, it also includes:

[0013] A rotation drive member is provided at an end of the rod frame away from the transverse folding member,

[0014] The blades are arranged at the output end of the rotary drive member.

[0015] As a further technical solution, the transverse folding member includes:

[0016] a first body, the first body being arranged on the connecting portion,

[0017] The second body is hingedly arranged on the first body.

[0018] As a further technical solution, the transverse folding member further includes:

[0019] a connecting rod, the connecting rod being hingedly arranged on the first body,

[0020] A swing rod, one end of which is hinged on the connecting rod, and the other end of which is hinged on the second body. After the second body swings relative to the first body, the second body is perpendicular to the first body.

[0021] As a further technical solution, the second body has a first connecting hole, the rod frame has a second connecting hole, the first connecting hole is concentric with the second connecting hole, and the supporting folding frame includes:

[0022] A connecting member, the connecting member is arranged on the second main body, the connecting member has a third connecting hole, and the third connecting hole is concentric with the second connecting hole,

[0023] A connecting bolt is threadedly disposed in the first connecting hole and the third connecting hole.

[0024] As a further technical solution, the supporting folding frame includes:

[0025] A fixing member, the fixing member is swingably arranged on the connecting member, and the landing gear is arranged on the fixing member,

[0026] a first connecting rod, the first connecting rod being hingedly arranged on the fixing member,

[0027] a second connecting rod, the second connecting rod being hingedly arranged on the first connecting rod, and the second connecting rod being hingedly arranged on the connecting member,

[0028] A spring, one end of which acts on the second connecting rod and the other end of which acts on the connecting member, provides a force for the fixing member to swing close to the rod bracket.

[0029] As a further technical solution, the subject includes:

[0030] A mounting platform, the mounting platform having the connecting portion,

[0031] A battery baffle is provided on the mounting platform and is used to fix the battery.

[0032] The mounting frame is arranged on the mounting platform, and the mounting frame and the battery baffle are respectively located on the upper and lower sides of the mounting platform.

[0033] As a further technical solution, the mounting frame has a limiting groove and further includes:

[0034] The swinging member is swingably arranged on the mounting frame, and after the swinging member swings, the limiting groove is opened or canceled.

[0035] As a further technical solution, it also includes:

[0036] An antenna is provided on the mounting platform and is used for receiving signals.

[0037] As a further technical solution, the mounting platform is rectangular, and there are four connecting parts, which are respectively arranged at the four vertex positions of the mounting platform.

[0038] The working principle and beneficial effects of the utility model are as follows:

[0039] In the present invention, compared to the carrier drones of the prior art, by setting the landing gear on the supporting folding frame, which is in turn set on the transverse folding member, an ingenious layout of the landing gear and the rod frame overlapping is achieved in the retracted state. This overlapping structure allows the whole to form a more compact and regular shape when retracted, and the various components rely on each other and work together, effectively enhancing the structural stability in the retracted state. During transportation or storage, even if there are external forces such as bumps and shaking, the stable whole constructed by the overlap of the landing gear and the rod frame can better withstand these external forces, avoid loosening, displacement or collision between components, ensure that the flight platform remains intact in the retracted state, and lay a solid foundation for subsequent rapid deployment and normal use.

[0040] This design, in which the landing gear and mast overlap when stowed, greatly optimizes spatial layout. This allows the flight platform to occupy less space and present a more compact form when folded. Compared to traditional carrier drones, where components are dispersed and occupy a large space when stowed, the compact stowage structure also facilitates faster deployment of components when the flight platform needs to be deployed quickly, reducing deployment time and improving operational efficiency. This is particularly useful for time-sensitive applications such as emergency rescue and incident monitoring. BRIEF DESCRIPTION OF THE DRAWINGS

[0041] The preferred implementation scheme will be described below in a clear and understandable manner with reference to the accompanying drawings to further illustrate the above-mentioned characteristics, technical features, advantages and implementation methods of the present invention.

[0042] Figure 1 This is a schematic diagram of the structure of the utility model;

[0043] Figure 2 for Figure 1 Schematic diagram of the enlarged structure of A in the middle;

[0044] Figure 3 for Figure 2 Schematic diagram of the enlarged structure of B;

[0045] Figure 4 It is a structural schematic diagram of the transverse folding member in the utility model.

[0046] In the figure: main body-1, connecting part-101, mounting platform-102, battery baffle-103, mounting frame-104, limiting groove-105, swinging member-106, antenna-107, horizontal folding member-2, first main body-201, second main body-202, connecting rod-204, swinging rod-205, rod frame-3, supporting folding frame-4, connecting part-401, connecting bolt-402, fixing part-403, first connecting rod-404, second connecting rod-405, spring-406, landing gear-5, rotating driving member-6, blade-7. DETAILED DESCRIPTION

[0047] In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the specific implementation methods of the present invention will be described below with reference to the accompanying drawings. Obviously, the drawings described below are only some embodiments of the present invention. For those skilled in the art, other drawings and other implementation methods can be obtained based on these drawings without inventive work.

[0048] To simplify the drawings, only the parts relevant to the utility model are schematically shown in each figure; they do not represent the actual structure of the product. Furthermore, to simplify the drawings and facilitate understanding, in some figures, only one of the components with the same structure or function is schematically shown or labeled. In this document, "one" not only means "only one" but also "more than one," and "several" includes "two" and "more than two."

[0049] It should be noted that, unless otherwise specified or limited, the terms "mounted," "connected," and "connected" should be understood broadly. For example, they can refer to fixed, detachable, or integral connections; mechanical or electrical connections; direct or indirect connections through an intermediary; and internal communication between two components. Those skilled in the art will understand the specific meanings of these terms in this utility model based on the specific circumstances.

[0050] In addition, in the description of the present application, the terms "first", "second", etc. are only used to distinguish the description and cannot be understood as indicating or implying relative importance.

[0051] Reference Figures 1 to 4 , which is the first embodiment of the utility model, proposes a carrier-type fully foldable multifunctional flying platform, including a main body 1, the main body 1 has a connecting portion 101, a transverse folding member 2 is arranged on the connecting portion 101, a rod frame 3 is arranged on the transverse folding member 2, a supporting folding frame 4 is arranged on the transverse folding member 2, the folding direction is perpendicular to the folding direction of the transverse folding member 2, and a landing gear 5 is arranged on the supporting folding frame 4.

[0052] In this embodiment, the design of the transverse folding member 2 endows the fully foldable, multifunctional, transportable flying platform with exceptional portability. For transportation and storage, it can be folded along a specific direction, significantly reducing its lateral dimensions and making it easily adaptable to various confined spaces, such as vehicle trunks and small storage rooms. This not only facilitates daily transport, lowering the requirements for the transport vehicle's specifications and reducing transportation costs, but also allows for efficient storage when not in use, saving storage space and improving space utilization. This provides significant convenience for applications requiring frequent relocation, such as field operations and emergency rescue operations.

[0053] The supporting folding frame 4 folds perpendicularly to the transverse folding member 2, further enhancing the overall compactness of the structure. The two work together, like a delicate origami technique, to cleverly adjust the flight platform's architecture from a two-dimensional perspective, achieving multi-dimensional size reduction and enabling organized storage within limited space. This ensures rapid deployment and flexible transfer of equipment, meeting the demands of modern, efficient, and mobile operations. The folding direction refers to the axial direction of the transverse folding frame 2 and the supporting folding frame 4.

[0054] Frame 3, supported by transverse folding members 2, forms a stable framework, providing a solid foundation for the flight platform to support key components such as the power plant and avionics. During flight, frame 3 evenly distributes the weight of the equipment and the forces of flight, ensuring balanced structural forces, preventing localized stress concentrations that could cause deformation and damage, and ensuring a stable flight attitude. Even in challenging weather conditions such as turbulence and strong winds, the stable structure maintains a steady flight trajectory, enhancing flight safety and reliability.

[0055] The combination of the support folding frame 4 and the landing gear 5 provides a solid foundation for the landing of the flight platform. The support folding frame 4 effectively shares the impact of landing, transmitting the force through its own structure to the lateral folding member 2 and the main body 1, achieving buffering and dispersion. The landing gear 5, with its appropriate ground contact design, such as the use of wear-resistant and non-slip materials and a reasonable support structure, ensures a smooth contact with the ground at the moment of landing, preventing accidents such as rollover and slipping. Whether landing on a flat hard runway or relatively soft outdoor surface, it ensures a safe and smooth landing of the flight platform, extending the service life of the equipment.

[0056] Main body 1 integrates various components via connectors 101, forming a multifunctional integrated carrier. This architecture allows the flight platform to conveniently carry diverse payloads, such as high-precision surveying instruments for surveying and mapping operations. By flexibly replacing specialized equipment to meet the needs of diverse fields, the platform can achieve a functional leap from basic transportation to complex specialized missions, broadening the breadth and depth of its application scenarios and meeting the demands of diverse industries.

[0057] Compared to existing carrier drones, by placing the landing gear 5 on the supporting folding frame 4, which is in turn placed on the transverse folding member 2, an ingenious layout is achieved in which the landing gear 5 overlaps the rod frame 3 when stowed. This overlapping structure creates a more compact and regular shape when stowed, and the various components rely on and cooperate with each other, effectively enhancing the structural stability in the stowed state. During transportation or storage, even if encountering external forces such as bumps and shaking, the stable whole formed by the overlap of the landing gear 5 and the rod frame 3 can better withstand these external forces, avoiding loosening, displacement, or collisions between components, ensuring that the flight platform remains intact in the stowed state, and laying a solid foundation for subsequent rapid deployment and normal use.

[0058] This design, in which the landing gear 5 overlaps the mast 3 in the stowed state, significantly optimizes the spatial layout. This results in a more compact and smaller overall footprint for the folded flight platform. Compared to traditional carrier drones, where components are dispersed and occupy a large space when stowed, the compact stowed structure also facilitates faster deployment of the components when the flight platform needs to be deployed quickly, reducing deployment time and improving operational efficiency. This is particularly useful for time-sensitive applications such as emergency rescue and incident monitoring.

[0059] Furthermore, it also includes a rotation driving member 6 , which is arranged at the end of the rod frame 3 away from the transverse folding member 2 , and the blade 7 is arranged at the output end of the rotation driving member 6 .

[0060] In this embodiment, the rotary drive member 6 is positioned at the end of the rod frame 3, distal from the transverse folding member 2, at a critical position within the entire flight platform structure. It provides a stable and efficient source of power transmission for the blades 7. Its secure connection to the rod frame 3 ensures that it can withstand various forces generated during power output, such as torque and centrifugal force, without loosening or displacement during operation, thus ensuring continuous and stable power transmission.

[0061] When the rotary drive member 6 drives the blades 7, it generates sufficient lift to allow the flight platform to successfully ascend and maintain flight. This configuration optimizes the power transmission path, reduces energy loss during transmission, and enables blades 7 to rotate more efficiently, thereby improving the flight performance of the flight platform, including flight speed, ceiling, and endurance. For example, under the same power conditions, compared with traditional power transmission structures with unreasonable layouts, this flight platform can fly higher, farther, and faster.

[0062] The precise control of the rotary drive 6 provides the flying platform with exceptional maneuverability. By precisely adjusting parameters such as the speed and direction of rotation, the rotational state of the blades 7 can be altered in real time, enabling precise control of the flying platform's flight attitude. Whether achieving smooth ascents and descents, or agile turns and sideways maneuvers, all can be accomplished with ease.

[0063] Positioning the rotary drive member 6 at the end of the rod frame 3, away from the transverse folding member 2, helps maintain the compactness of the overall structure of the flying platform. This coordinates with the spatial layout of other components, such as the transverse folding member 2, the supporting folding frame 4, and the landing gear 5, avoiding spatial conflicts between components and ensuring efficient use of space in both the folded and unfolded states of the flying platform.

[0064] When folded, this compact structure further reduces the overall size of the flight platform, facilitating transportation and storage. When unfolded, each component can perform its functions in an orderly manner, without compromising flight performance due to inappropriate spatial layout. This synergistic relationship not only enhances the flight platform's stability during flight but also effectively extends the service life of each component. By properly distributing external forces, the risk of damage to individual components due to excessive stress is reduced, allowing the flight platform to maintain excellent performance over extended periods of use, reducing maintenance costs and the frequency of component replacement.

[0065] Furthermore, the transverse folding member 2 includes a first body 201 , the first body 201 is disposed on the connecting portion 101 , and the second body 202 is hingedly disposed on the first body 201 .

[0066] In this embodiment, the transverse folding member 2 consists of a first body 201 and a second body 202, with the second body 202 hingedly mounted on the first body 201. This structural design provides an extremely convenient folding experience for the flying platform. To fold the flying platform for storage, simply rotate the second body 202 about the hinge point, folding it relative to the first body 201, and quickly reducing the horizontal size of the flying platform. Compared to traditional, integrated transverse structures, this hinged folding design significantly reduces the time and labor required for folding, improving folding efficiency.

[0067] Although the second body 202 is hingedly connected to the first body 201, this connection still provides reliable structural support when the flying platform is deployed and in use. When the flying platform is in flight, the first and second bodies 201, 202 work together to evenly distribute external forces, preventing structural deformation or damage due to excessive local forces.

[0068] The modular design of the transverse folding member 2, consisting of a first main body 201 and a second main body 202, offers significant advantages in terms of maintenance and component replacement. If, during long-term use, the first or second main body 201, 202 becomes damaged or malfunctions, the entire transverse folding member 2 need not be replaced; only the damaged portion can be replaced. Furthermore, during routine maintenance checks, the relatively clear and simple structure allows for easier inspection, cleaning, and maintenance of key areas such as hinges, ensuring that the transverse folding member 2 remains in good working condition. This reduces maintenance costs and complexity, and improves the maintainability of the flight platform.

[0069] Furthermore, the transverse folding member 2 also includes a connecting rod 204, which is hinged on the first body 201, and one end of the swing rod 205 is hinged on the connecting rod 204, and the other end is hinged on the second body 202. After the second body 202 swings relative to the first body 201, the second body 202 is perpendicular to the first body 201.

[0070] In this embodiment, the provision of the connecting rod 204 and the swinging lever 205 allows for more precise and controllable folding of the transverse folding member 2. When folding is required, the properly designed hinged structure allows the second body 202 to swing relative to the first body 201 along a predetermined trajectory. The swinging lever 205 is hinged at one end to the connecting rod 204 and at the other end to the second body 202. This connection creates a stable linkage, ensuring that the second body 202 maintains coordination with the other components during its swinging motion, accurately achieving a folded position perpendicular to the first body 201.

[0071] This precise folding action not only improves folding efficiency but also further optimizes the space occupied after folding. Compared to simple hinged folding methods, it can make the flying platform present a more regular and compact shape after folding, making more efficient use of storage space. Whether in the trunk of a transport vehicle or in the storage area of ​​a warehouse, it can meet storage needs with a smaller space occupation, facilitating the transportation and storage management of the flying platform.

[0072] When the flying platform is deployed and in use, the complex hinged structure formed by the connecting rod 204 and the swing rod 205, the first body 201, and the second body 202 provides greater structural stability for the entire horizontal folding member 2. When the flying platform is in flight, it is subject to air resistance, gravity, and various flight forces. These rods work together to evenly distribute external forces to various components.

[0073] The transverse folding member 2, constructed of multiple hinged rods, offers advantages in maintenance and troubleshooting. Because the structure is relatively clear and the connections between the rods are well-defined, maintenance personnel can easily observe the status of each rod during routine inspections, including any deformation, looseness, or wear.

[0074] Furthermore, if a fault occurs, such as an abnormal hinge or damaged rod, the problem can be quickly located and targeted repairs or replacements can be performed. This ease of maintenance and troubleshooting reduces maintenance costs and downtime for the flight platform, ensuring its normal operation and efficient use.

[0075] Furthermore, the second main body 202 has a first connecting hole, the rod frame 3 has a second connecting hole, the first connecting hole is concentric with the second connecting hole, the supporting folding frame 4 includes a connecting member 401, the connecting member 401 is arranged on the second main body 202, the connecting member 401 has a third connecting hole, the third connecting hole is concentric with the second connecting hole, and the connecting bolt 402 is threadedly arranged in the first connecting hole and the third connecting hole.

[0076] In this embodiment, the first connecting hole of the second body 202, the second connecting hole of the rod bracket 3, and the third connecting hole of the connector 401 are concentrically arranged. This design provides a highly precise positioning reference for the assembly of the components. When connected together by the connecting bolts 402, the components are accurately aligned during assembly, avoiding problems such as structural instability or malfunction caused by assembly deviations.

[0077] This coordination of the concentric holes and connecting bolts 402 allows the rod frame 3 and support folding frame 4 to be securely mounted on the second body 202, forming a tightly integrated structure. During operation, the flight platform maintains a tight connection between its components, effectively strengthening the structural integrity of the entire flight platform and ensuring its stable operation, regardless of air resistance, vibration, or impact during takeoff and landing.

[0078] The use of connecting bolts 402 facilitates the installation and removal of the rod frame 3, the folding support frame 4, and the second body 202. During assembly of the flight platform, simply inserting the connecting bolts 402 through the first and third connecting holes and tightening them quickly completes the connection. This eliminates the need for complex specialized tools or specialized processes, reducing assembly complexity and improving production efficiency.

[0079] Similarly, when the flying platform needs to be repaired, maintained or parts replaced, the rod frame 3 and the supporting folding frame 4 can be easily removed from the second body 202 by loosening the connecting bolts 402, making it convenient to inspect, repair or replace each component separately, saving maintenance time and labor costs, and improving the maintainability of the flying platform.

[0080] The connection structure of the concentric holes and the connecting bolts 402 facilitates the flexible adaptation and scalability of the flight platform. Because this connection method is relatively simple and standardized, other components can be easily added or replaced in the corresponding positions when the flight platform is subsequently upgraded or modified to meet different mission requirements.

[0081] When the flight platform is in operation and subjected to external forces, the connection structure between the concentric holes and the connecting bolts 402 ensures that all components are evenly stressed. As the primary force transmission component, the connecting bolts 402 evenly transfer external forces to all connected components, preventing damage caused by localized stress concentration.

[0082] This uniform stress distribution helps extend the service life of components such as the rod frame 3, the folding support frame 4, and the second body 202. By reducing wear and deformation caused by uneven stress on components, the frequency of component replacement is reduced, further reducing the operating costs of the flight platform and ensuring the long-term stable operation of the flight platform.

[0083] Furthermore, the supporting folding frame 4 includes a fixing member 403, the fixing member 403 is swingably set on the connecting member 401, the landing gear 5 is set on the fixing member 403, one end of the first connecting rod 404 is hingedly set on the fixing member 403, one end of the second connecting rod 405 is hingedly set on the other end of the first connecting rod 404, and the other end of the second connecting rod 405 is hingedly set on the connecting member 401, one end of the spring 406 acts on the second connecting rod 405, and the other end acts on the connecting member 401, providing a force to fix the fixing member 403 when it is parallel to the rod frame 3.

[0084] In this embodiment, the fixing member 403 is pivotally mounted on the connecting member 401, and the landing gear 5 is mounted thereon, enabling flexible attitude adjustment. Furthermore, the linkage mechanism formed by the first connecting rod 404, the second connecting rod 405, and the spring 406 provides cushioning and stability for attitude adjustment of the landing gear 5. When the landing gear 5 is subjected to ground impact or external forces resulting from changes in flight attitude, these connecting rods and springs work together to effectively cushion the impact of these external forces on the landing gear 5 and the entire flight platform through their own deformation and conversion of elastic potential energy, thus preventing component damage or loss of flight platform attitude control due to excessive impact.

[0085] When the flying platform needs to be folded and stored, the structural design of the fixing member 403, first connecting rod 404, second connecting rod 405, and spring 406 facilitates the folding operation of the supporting folding frame 4. By properly manipulating the hinge points of each connecting rod and utilizing the elastic properties of spring 406, the fixing member 403 and the landing gear 5 connected to it can be folded in a predetermined manner. This, in conjunction with other folding components such as the transverse folding member 2, further reduces the overall size of the flying platform, optimizes space utilization, and facilitates transportation and storage.

[0086] This convenient folding operation enables the flight platform to be stored in a relatively short time, improving the efficiency of transferring the equipment between different operating scenarios and meeting the needs of application scenarios with high requirements for equipment mobility, such as field operations and emergency rescue.

[0087] One end of spring 406 acts on second connecting rod 405, and the other end acts on connector 401, providing a fixed force to maintain the fixture 403 parallel to the mast 3, thus providing an adaptive force feedback mechanism for the entire structure. When the platform is in flight or parked on the ground, if external forces such as a breeze or a minor collision cause the fixture 403 to deflect slightly or change its posture, spring 406, based on its own elastic properties, can promptly provide a reverse restoring force, quickly returning the fixture 403 to its initial position parallel to the mast 3, thus maintaining the stability of the entire structure.

[0088] This adaptive force feedback and state maintenance capability helps reduce unnecessary component adjustments and potential structural damage risks caused by external interference factors, improves the stability and reliability of the flight platform under various working conditions, and ensures its normal operation.

[0089] Furthermore, the main body 1 includes a mounting platform 102, the mounting platform 102 has a connecting portion 101, a battery baffle 103 is arranged on the mounting platform 102, the battery baffle 103 is used to fix the battery, and the mounting frame 104 is arranged on the mounting platform 102, and is located on the upper and lower sides of the mounting platform 102 respectively with the battery baffle 103.

[0090] In this embodiment, the mounting platform 102 within the main body 1 serves as the core load-bearing area. Connectors 101 effectively connect to other components, forming the overall structure of the flight platform. Battery baffles 103 and mounting racks 104 are located above and below the mounting platform 102, respectively. This optimal layout allows for efficient loading and zoning management of various devices.

[0091] Battery baffle 103 is used to secure the batteries, ensuring their stability during flight and preventing them from shifting or loosening due to factors such as flight vibration and attitude changes, thereby ensuring a stable power supply for the flight platform. Mounting rack 104 provides additional mounting space for various mission payloads, such as surveying and mapping equipment, monitoring equipment, and rescue material delivery devices. This layout allows the flight platform to flexibly configure equipment based on different mission requirements, with each device working independently and collaboratively, enhancing the flight platform's versatility and mission adaptability.

[0092] The placement of battery baffles 103 and mounting brackets 104 above and below mounting platform 102 helps enhance the structural stability of the entire flight platform. Batteries, a crucial power source for the flight platform, are relatively heavy. Securely securing the batteries beneath mounting platform 102 with battery baffles 103 effectively lowers the platform's center of gravity, improving its distribution and enhancing flight stability.

[0093] At the same time, when the mounting rack 104 mounts equipment above the installation platform 102, it will also affect the overall center of gravity. However, due to its reasonable layout with the battery baffle 103, the weight and position of the mounted equipment can be appropriately adjusted to achieve the balance of the overall center of gravity of the flight platform, avoiding problems such as loss of control of the flight attitude or degradation of flight performance due to center of gravity shift, thereby ensuring flight safety and stability.

[0094] The arrangement of battery baffle 103 and mounting bracket 104 greatly facilitates device installation and maintenance. Battery installation is quick and easy, requiring only placement within the area defined by battery baffle 103 and securing. Devices mounted on mounting bracket 104 can also be easily attached, removed, and replaced without the need for complex tools or tedious procedures.

[0095] During the daily maintenance and inspection of the flight platform, this partitioned structure enables maintenance personnel to clearly locate the location of batteries and mounted equipment, facilitating separate inspection, maintenance and repair operations on them. This reduces maintenance difficulty, improves maintenance efficiency, reduces downtime, and ensures that the flight platform can quickly return to normal operating conditions.

[0096] Mounting rack 104, located beneath mounting platform 102, provides ample room for expansion. As mission requirements evolve, various specialized equipment can be flexibly mounted on mounting rack 104, enabling the transition from basic transportation tasks to complex specialized missions such as high-precision mapping and precision agriculture.

[0097] Furthermore, the mounting frame 104 has a limiting groove 105 and also includes a swinging member 106. The swinging member 106 is swingably set on the mounting frame 104. After the swinging member 106 swings, the limiting groove 105 is opened or unopened.

[0098] In this embodiment, the retaining grooves 105 provided on the mounting frame 104 provide precise positioning and initial securing for the mounted equipment. When mounting various mission payloads such as surveying instruments and monitoring equipment, the corresponding parts of the equipment can be placed in the retaining grooves 105, ensuring that they are accurately positioned. This ensures that the equipment will not undergo significant displacement during flight due to factors such as flight vibration and attitude changes, ensuring the stability of the connection between the equipment and the flight platform, thereby maintaining the overall performance of the flight platform and the reliability of mission execution.

[0099] The swinging member 106 is swingably mounted on the mounting frame 104, and its swinging motion can open or close the limiting slot 105. This design further optimizes the device mounting process. When mounting a device, simply swing the swinging member 106 to open the limiting slot 105, easily insert the device into the limiting slot 105, and then swing the swinging member 106 to cancel the open state, that is, to close the limiting slot 105. This quickly completes the mounting and securing of the device. This simple and convenient operation does not require complex tools or tedious steps, greatly improving the efficiency of device mounting. This advantage is particularly evident in application scenarios where different mission payloads need to be frequently changed.

[0100] Thanks to the coordinated mechanism between the retaining slots 105 and the swinging member 106, the mount 104 is better able to accommodate equipment of varying sizes and shapes. Different types of payloads often have varying shapes and dimensions. By adjusting the size of the retaining slots 105, multiple specifications can be accommodated during design, or by utilizing a specific adjustment mechanism. Furthermore, the swinging member 106 allows for flexible opening and closing of the retaining slots 105, meeting the mounting requirements of a wide range of equipment and enhancing the versatility of the mount 104.

[0101] For smaller sensor equipment and relatively larger material delivery devices, they can be stably mounted on the mounting frame 104 by reasonably adjusting the limit slot 105 and the swing member 106, ensuring that the flight platform can carry various required equipment to complete different tasks, and deliver mounted materials or equipment when needed, broadening the application scope and mission execution capabilities of the flight platform.

[0102] During flight, regardless of turbulence or flight attitude adjustments, the closed position limit slot 105 and the swing member 106 can work closely together to secure the mounted device to the mounting bracket 104. This not only prevents the device from being separated from the mounting bracket 104 due to external forces, thus avoiding damage and potential safety hazards caused by the device falling, but also ensures that the device is relatively fixed in position on the flight platform, maintains the stability of the flight platform's overall center of gravity, and ensures that the flight attitude and performance of the flight platform are not affected, thereby improving flight safety and reliability.

[0103] At the same time, this stable mounting structure also helps to reduce the friction and collision caused by vibration between the equipment and the mounting frame 104, protects the equipment from unnecessary damage, extends the service life of the equipment, reduces equipment maintenance costs, and further ensures the normal operation of the flight platform and mission execution efficiency.

[0104] When maintenance, inspection, or replacement of mounted equipment is required, the ability of swing member 106 to swing open retaining slot 105 becomes particularly important. Maintenance personnel can simply operate swing member 106 to easily open retaining slot 105 and conveniently remove the equipment from mounting bracket 104. After performing the appropriate operations, they can then remount the new or maintained equipment onto mounting bracket 104 according to the aforementioned mounting process.

[0105] This design, which facilitates equipment maintenance and replacement, reduces the difficulty and workload of equipment maintenance, shortens maintenance time, and reduces downtime, allowing the flight platform to return to normal operating conditions more quickly, improving the maintainability and overall operating efficiency of the flight platform, and ensuring that the flight platform can continuously and efficiently complete various tasks.

[0106] Furthermore, an antenna 107 is included. The antenna 107 is set on the installation platform 102 and is used to receive signals.

[0107] In this embodiment, antenna 107 is mounted on mounting platform 102. Its primary function is signal reception, which is crucial for the proper operation of the flight platform. During flight, antenna 107 ensures a stable communication connection between the flight platform and the outside world, whether receiving control commands from the ground control station or acquiring various mission-related data signals, such as terrain data feedback in surveying and mapping missions or target location information in rescue missions. By accurately receiving these signals, the flight platform can adjust its flight attitude and operate its payload according to predetermined commands, achieving precise flight control and efficient mission execution.

[0108] Placing antenna 107 on mounting platform 102 is a relatively rational layout. As the core support area of ​​the flight platform, mounting platform 102 provides ample space for antenna 107 installation without significantly interfering with the layout and function of other key components, such as battery baffle 103 and mounting bracket 104. This layout ensures that antenna 107 is positioned in a relatively open space, facilitating better signal reception, while also fully utilizing the space available on mounting platform 102, improving the overall space efficiency of the flight platform.

[0109] Furthermore, the mounting platform 102 is rectangular, and there are four connecting parts 101 , which are respectively arranged at the four vertices of the mounting platform 102 .

[0110] In this embodiment, the mounting platform 102 adopts a rectangular design with connecting portions 101 positioned at each of its four vertices, creating a highly stable and balanced structural connection foundation for the entire fully foldable, multi-functional, transportable flying platform. This layout ensures that the connection points between the various components and the mounting platform 102 are evenly distributed. Once the flying platform is assembled and operational, the forces exerted on each component are effectively distributed throughout the entire platform structure.

[0111] When the flying platform is flying in the air and is affected by air resistance, gravity and various forces generated during the flight, these forces can be evenly transmitted to the mounting platform 102 through the connection parts 101 at the four vertex positions, thereby avoiding local stress concentration that causes structural deformation or damage, and ensuring the structural integrity and flight safety of the flying platform.

[0112] The arrangement of four connecting portions 101 provides a wide range of connection options and flexible layout adaptation for the assembly of different components. Each component, such as the transverse folding member 2 and the rod frame 3, can be connected by selecting the appropriate connecting portion 101 based on its functional and spatial requirements, thereby achieving a rational layout and efficient assembly of the entire flight platform.

[0113] This flexibility allows for the optimization and adjustment of the assembly sequence and layout of components during the design and manufacture of the flight platform, based on specific mission requirements and application scenarios. For example, for missions requiring a strong focus on center-of-gravity distribution, such as transporting heavy payloads, the center-of-gravity position of the flight platform can be precisely controlled by properly selecting the connection methods between components and different connectors 101, ensuring stability and maneuverability during flight.

[0114] When the flight platform needs to be folded or unfolded, the connecting portions 101 at the four vertices of the rectangular mounting platform 102 play an important guiding and supporting role. When the foldable components, such as the transverse folding members 2, are folded, their connection to the connecting portions 101 ensures that the folding process proceeds along a predetermined trajectory and pattern, ensuring that the components fit tightly together after folding, achieving efficient space compression.

[0115] Similarly, during the deployment operation, the connecting portion 101 provides an accurate positioning reference for each component, so that each component can quickly return to the predetermined deployment position, ensuring that the flight platform can quickly convert from a folded state to a flyable state, improving the efficiency of the equipment's conversion between different operating scenarios, and meeting the needs of application scenarios such as field operations and emergency rescue that have high requirements for equipment mobility.

[0116] It should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention and are not intended to limit the present invention. Although the present invention has been described in detail with reference to the preferred embodiments, those skilled in the art should understand that the technical solutions of the present invention may be modified or replaced by equivalents without departing from the spirit and scope of the technical solutions of the present invention, and all of these should be included in the scope of the claims of the present invention.

Claims

1. A fully foldable, multifunctional flying platform, characterized by: include: A main body (1), wherein the main body (1) has a connecting portion (101), a transverse folding member (2), wherein the transverse folding member (2) is arranged on the connecting portion (101), a rod frame (3), the rod frame (3) being arranged on the transverse folding member (2), A supporting folding frame (4), wherein the supporting folding frame (4) is arranged on the transverse folding member (2), and the folding direction is perpendicular to the folding direction of the transverse folding member (2). A landing gear (5), wherein the landing gear (5) is arranged on the supporting folding frame (4).

2. The carrier-type fully foldable multifunctional flying platform according to claim 1, characterized in that: Also includes: A rotating drive member (6), the rotating drive member (6) being arranged at an end of the rod frame (3) away from the transverse folding member (2), A blade (7), wherein the blade (7) is arranged at the output end of the rotary drive member (6).

3. The carrier-type fully foldable multifunctional flying platform according to claim 1, characterized in that: The transverse folding member (2) comprises: a first body (201), the first body (201) being arranged on the connecting portion (101), A second body (202), wherein the second body (202) is hingedly arranged on the first body (201).

4. The carrier-type fully foldable multifunctional flying platform according to claim 3, characterized in that: The transverse folding member (2) further comprises: a connecting rod (204), the connecting rod (204) being hingedly arranged on the first body (201), A swing rod (205), one end of the swing rod (205) is hingedly arranged on the connecting rod (204), and the other end is hingedly arranged on the second body (202), and after the second body (202) swings relative to the first body (201), the second body (202) is perpendicular to the first body (201).

5. The carrier-type fully foldable multifunctional flying platform according to claim 4, characterized in that: The second main body (202) has a first connecting hole, the rod frame (3) has a second connecting hole, the first connecting hole and the second connecting hole are concentric, and the supporting folding frame (4) comprises: A connecting member (401), the connecting member (401) is arranged on the second main body (202), the connecting member (401) has a third connecting hole, the third connecting hole is concentric with the second connecting hole, A connecting bolt (402), wherein the connecting bolt (402) is threadedly disposed in the first connecting hole and the third connecting hole.

6. The carrier-type fully foldable multifunctional flying platform according to claim 5, characterized in that: The supporting folding frame (4) comprises: A fixing member (403), wherein the fixing member (403) is swingably arranged on the connecting member (401), and the landing gear (5) is arranged on the fixing member (403). a first connecting rod (404), the first connecting rod (404) being hingedly arranged on the fixing member (403), a second connecting rod (405), the second connecting rod (405) being hingedly arranged on the first connecting rod (404), and the second connecting rod (405) being hingedly arranged on the connecting member (401), A spring (406), one end of which acts on the second connecting rod (405) and the other end of which acts on the connecting member (401), provides a force for the fixing member (403) to swing close to the rod frame (3).

7. The carrier-type fully foldable multifunctional flying platform according to claim 1, characterized in that: The main body (1) includes: A mounting platform (102), the mounting platform (102) having the connecting portion (101), A battery baffle (103), the battery baffle (103) is arranged on the mounting platform (102), and the battery baffle (103) is used to fix the battery. A mounting frame (104), the mounting frame (104) is arranged on the mounting platform (102), and the mounting frame and the battery baffle (103) are respectively located on the upper and lower sides of the mounting platform (102).

8. The carrier-type fully foldable multifunctional flying platform according to claim 7, characterized in that: The mounting frame (104) has a limiting groove (105) and further includes: A swinging member (106) is swingably arranged on the mounting frame (104); after the swinging member (106) swings, the limiting slot (105) is opened or unopened.

9. The carrier-type fully foldable multifunctional flying platform according to claim 7, characterized in that: Also includes: An antenna (107) is provided on the installation platform (102), and the antenna (107) is used to receive signals.

10. The carrier-type fully foldable multifunctional flying platform according to claim 8, characterized in that: The mounting platform (102) is rectangular, and there are four connecting portions (101), which are respectively arranged at four vertex positions of the mounting platform (102).

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