Quick-release type portable unmanned aerial vehicle

Abstract

The utility model relates to the technical field of unmanned aerial vehicles, in particular to a quick-release portable unmanned aerial vehicle which comprises an unmanned aerial vehicle body and two unmanned aerial vehicle wings, clamping grooves are formed in the two sides of the unmanned aerial vehicle body, clamping blocks are arranged on the outer side of the unmanned aerial vehicle body and connected with the clamping grooves in a clamped mode, and first connectors are arranged on the two sides of the unmanned aerial vehicle body. Slide ways are arranged at the edges of the unmanned aerial vehicle wings and communicate with the outer sides of the unmanned aerial vehicle wings, connecting blocks are arranged in the slide ways and provided with second connectors, sliding blocks are arranged at the tops of the second connectors, guide grooves are formed in the tops of the unmanned aerial vehicle wings and communicate with the slide ways, and the sliding blocks penetrate through the guide grooves. The first connector is connected with the second connector. According to the utility model, the operation convenience is improved, the connection process is ensured to be stable and reliable, the loosening problem caused by vibration or impact in the flight process is avoided, the flight safety and reliability are improved, and the accuracy and stability of electric connection are ensured.

Description

TECHNICAL FIELD

[0001] The utility model relates to unmanned plane technical field, especially a kind of quick-release portable unmanned plane. BACKGROUND

[0002] With the continuous development of unmanned plane technology, its application field is also increasingly extensive, from aerial photography, surveying and mapping to logistics, agriculture and other industries have been widely applied. Traditional unmanned plane usually adopts fixed or foldable wing structure, although it improves portability to some extent, but there are still problems such as complex disassembly and assembly, inconvenient carrying and difficult maintenance in actual use.

[0003] In order to solve the above problems, in recent years, a variety of quick-release unmanned plane structure design has appeared. This kind of design aims to realize the quick installation and separation between unmanned plane components by optimizing the connection mode and modular layout. For example, the quick-release structure based on buckle, magnetic attraction and other ways can complete the assembly and disassembly of main components of unmanned plane without using tools. However, these schemes still have certain limitations in connection stability, electrical path reliability and overall structure strength, especially when facing high-speed flight or complex environment, connection loosening, signal interruption and other safety hazards are easy to occur. SUMMARY

[0004] The utility model aims at at least solving the technical problems existing in prior art. For this purpose, the utility model provides a quick-release portable unmanned plane, which has a quick-release unmanned plane structure with stable mechanical connection and reliable electrical connection, and realizes efficient, safe and convenient unmanned plane use experience.

[0005] According to some embodiments of the utility model, a quick-release portable unmanned plane comprises an unmanned plane body and two unmanned plane wings, both sides of the unmanned plane body are provided with clamping grooves, the outer side of the unmanned plane body is provided with clamping blocks, the clamping blocks are connected with the clamping grooves, both sides of the unmanned plane body are provided with first connectors, the edge of the unmanned plane wing is provided with a slide, the slide is communicated with the outer side of the unmanned plane wing, a connecting block is arranged in the slide, a second connector is arranged on the connecting block, a sliding block is arranged on the top of the second connector, a guide groove is arranged on the top of the unmanned plane wing, the guide groove is communicated with the slide, the sliding block is arranged in the guide groove, and the first connector is connected with the second connector.

[0006] According to some embodiments of the utility model, a quick-release portable unmanned plane has at least the following beneficial effects:

[0007] The utility model discloses a preliminary positioning is realized through the cooperation of the clamping block and the clamping groove, and then the second connector is automatically docked with the first connector through the sliding connecting block, which simplifies the installation steps, and the user can complete the quick assembly or separation of the wing and the fuselage without the aid of tools, greatly improving the operation convenience, the cooperation structure of the sliding block and the guide groove can effectively guide the connecting block to slide along the predetermined path, ensuring that the connecting process is stable and reliable, and meanwhile, the limiting effect of the clamping block and the clamping groove further enhances the stability of the overall structure, avoids the loosening problem caused by vibration or impact during flight, improves the flight safety and reliability, the first connector and the second connector are docked in the sliding process, ensuring the accuracy and stability of the electrical connection, and after the completion of the connection between the fuselage and the wing, the clamping block, the clamping groove, the first connector and the second connector are all not exposed on the outer surface of the unmanned aerial vehicle, which is beneficial to the flight of the unmanned aerial vehicle.

[0008] According to some embodiments of the utility model, a quick-release portable unmanned aerial vehicle, the clamping groove includes a protruding groove and a positioning groove, the cross section of the positioning groove is circular, the protruding groove is located on the outside of the positioning groove, the protruding groove is communicated with the outside of the unmanned aerial vehicle wing, the clamping block includes a connecting column and a protruding part, the connecting column is connected with the outside of the unmanned aerial vehicle wing, the protruding part is connected with the outside of the connecting column, the protruding part is correspondingly arranged with the protruding groove, so that the protruding part rotates and positions in the positioning groove from the protruding groove.

[0009] According to some embodiments of the utility model, a quick-release portable unmanned aerial vehicle, the unmanned aerial vehicle fuselage includes a lower fuselage and an upper fuselage, the top of the lower fuselage is connected with the bottom of the upper fuselage, the lower fuselage and the upper fuselage enclose the clamping groove and the sliding channel.

[0010] According to some embodiments of the utility model, a quick-release portable unmanned aerial vehicle, the unmanned aerial vehicle fuselage is provided with a containing cavity.

[0011] According to some embodiments of the utility model, a quick-release portable unmanned aerial vehicle, the upper and lower ends of the unmanned aerial vehicle fuselage are provided with the guide groove, the upper and lower ends of the second connector are provided with the sliding block, the upper and lower ends of the unmanned aerial vehicle wing are provided with the guide groove, the upper and lower ends of the two guide grooves are communicated with the sliding channel respectively, and the sliding block is arranged in the guide groove.

[0012] According to some embodiments of the utility model, a quick-release portable unmanned aerial vehicle, the outside of the sliding block is provided with an operating block, and the operating block is located on the outside of the guide groove.

[0013] Additional aspects and advantages of the utility model will be partially given in the following description, partially will become obvious from the following description, or will be understood by the practice of the utility model. BRIEF DESCRIPTION OF DRAWINGS

[0014] The above and / or additional aspects and advantages of the present utility model will become apparent and more readily appreciated from the following description of the embodiments, taken in conjunction with the references to the following drawings, of which:

[0015] Figure 1 It is a structural schematic view of the utility model embodiment.

[0016] Figure 2 It is a structural schematic view of the utility model embodiment's unmanned aerial vehicle wing.

[0017] Figure 3 It is a structural schematic view of the utility model embodiment's unmanned aerial vehicle wing without the second connector.

[0018] Figure 4 It is a structural schematic view of the utility model embodiment's unmanned aerial vehicle body.

[0019] Figure 5 It is a structural schematic view of the utility model embodiment's lower body.

[0020] Figure 6 It is a structural schematic view of the utility model embodiment's connecting block.

[0021] Reference signs: 1, unmanned aerial vehicle body, 2, unmanned aerial vehicle wing, 3, clamping block, 4, clamping groove, 5, first connector, 6, slide, 7, connecting block, 8, second connector, 9, sliding block, 10, guide slot, 11, insertion slot, 12, positioning slot, 13, connecting column, 14, insertion part, 15, lower body, 16, upper body, 17, accommodating cavity, 18, operating block. DETAILED DESCRIPTION

[0022] The embodiments of the present utility model will be described in detail below, and examples of the embodiments are shown in the drawings, wherein the same or similar reference signs represent the same or similar elements or elements with the same or similar functions throughout. The embodiments described below by referring to the drawings are exemplary and are only used to explain the present utility model, and cannot be understood as a limitation on the present utility model.

[0023] In the description of the present utility model, it is understood that the orientation description, such as the orientation or position relationship indicated by up, down, left, right, front, back, etc. is based on the orientation or position relationship shown in the drawings, and is only for the convenience of describing the present utility model and simplifying the description, and does not indicate or imply that the modules or elements referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as a limitation on the present utility model.

[0024] In the description of the utility model, if it is described to first, second only is used for distinguishing technical feature for purpose, and can not be understood as indicating or suggesting relative importance or implicitly indicating the quantity of indicated technical feature or implicitly indicating the precedence relation of indicated technical feature.

[0025] In the description of the utility model, unless otherwise explicitly limited, the words such as setting, installation, connection should be broadly understood, and the specific meaning of the above words in the utility model can be reasonably determined by the person skilled in the art in combination with the specific content of the technical scheme.

[0026] As Figures 1-6 Indicated, the utility model embodiment provides a quick detachable portable unmanned plane.

[0027] A quick detachable portable unmanned plane, including unmanned plane fuselage 1 and two unmanned plane wings 2, the both sides of unmanned plane fuselage 1 are provided with clamping groove 4, the outside of unmanned plane fuselage 2 is provided with clamping block 3, clamping block 3 is connected with clamping groove 4, the both sides of unmanned plane fuselage 1 are provided with first connector 5, the edge of unmanned plane wing 2 is provided with slide 6, and the outside of unmanned plane wing 2 is communicated with slide 6, and connecting block 7 is arranged in slide 6, second connector 8 is arranged on connecting block 7, the top of second connector 8 is provided with sliding block 9, the top of unmanned plane wing 2 is provided with guide slot 10, and guide slot 10 is communicated with slide 6, and sliding block 9 is arranged in guide slot 10, and first connector 5 is connected with second connector 8.

[0028] The utility model discloses the cooperation of clamping block 3 and clamping groove 4 realizes preliminary positioning, and then makes second connector 8 and first connector 5 automatic docking through sliding connecting block 7, simplifies the installation step, and the user can complete the quick assembly or separation of wing and fuselage without the aid of tools, greatly improves the operation convenience.The cooperation structure of sliding block 9 and guide slot 10 can effectively guide connecting block 7 to slide along the predetermined path, ensure that the connection process is stable and reliable, and the limiting effect of clamping block 3 and clamping groove 4 further enhances the stability of the overall structure, avoids the loosening problem caused by vibration or impact during flight, and improves flight safety and reliability.The first connector 5 and the second connector 8 realize docking in the sliding process, ensure the accuracy and stability of electrical connection, and after the unmanned plane fuselage 1 and the unmanned plane wing 2 are connected, the clamping block 3, the clamping groove 4, the first connector 5 and the second connector 8 are not exposed on the outer surface of the unmanned plane, which is beneficial to the flight of the unmanned plane.

[0029] It can be understood that the power supply, communication and other power layout between the unmanned aerial vehicle body 1 and the unmanned aerial vehicle wing 2 are prior art, and the improvement point of the utility model is not in this, and it will not be described one by one. Similarly, the setting of the power unit and the steering unit of the unmanned aerial vehicle is also prior art, and the improvement point of the utility model is not in this, and it will not be described one by one.

[0030] The quick-release portable unmanned aerial vehicle described in the embodiment, the clamping groove 4 includes a protruding groove 11 and a positioning groove 12, the cross section of the positioning groove 12 is circular, the protruding groove 11 is located outside the positioning groove 12, the protruding groove 11 is in communication with the outside of the unmanned aerial vehicle wing 2, the clamping block 3 includes a connecting column 13 and a protruding part 14, the connecting column 13 is connected with the outside of the unmanned aerial vehicle wing 2, the protruding part 14 is connected with the outside of the connecting column 13, the protruding part 14 is correspondingly arranged with the protruding groove 11, so that the protruding part 14 can rotate and position in the positioning groove 12 from the protruding groove 11.

[0031] It can be understood that when the protruding part 14 protrudes from the protruding groove 11, the unmanned aerial vehicle wing 2 needs to be perpendicular to the unmanned aerial vehicle body 1, and the protruding part 14 rotates 90° after protruding from the protruding groove 11, at this time the protruding part 14 cannot exit from the protruding groove 11, and the unmanned aerial vehicle wing 2 is parallel to the unmanned aerial vehicle body 1, and then the first connector 5 and the second connector 8 are connected to realize locking, precise positioning and anti-misconnection between the wing and the body, and the stability and assembly efficiency of the connection are improved.

[0032] The quick-release portable unmanned aerial vehicle described in the embodiment, the unmanned aerial vehicle body 1 includes a lower body 15 and an upper body 16, the top of the lower body 15 is connected with the bottom of the upper body 16, and the lower body 15 and the upper body 16 form the clamping groove 4 and the slide 6. Specifically, by dividing the unmanned aerial vehicle body 1 into two parts of the lower body 15 and the upper body 16, and forming the clamping groove 4 and the slide 6 structure by the two, not only is convenient for internal space layout and component assembly, but also simplifies the manufacturing process, improves the overall strength and sealing performance of the structure, and is also conducive to the stability and modular maintenance of the quick-release structure.

[0033] The quick-release portable unmanned aerial vehicle described in the embodiment, the unmanned aerial vehicle body 1 is provided with a containing cavity 17. Specifically, by arranging the containing cavity 17 in the unmanned aerial vehicle body 1, the battery, control module or other electronic devices can be stored, the space utilization and integration of the whole machine are improved, the internal elements are protected, the functionality and safety of the unmanned aerial vehicle are enhanced.

[0034] The quick-release portable unmanned plane provided by the embodiment is characterized in that the upper end and the lower end of the unmanned plane body 1 are both provided with the guide groove 10, the upper end and the lower end of the second connector 8 are both provided with the sliding block 9, the upper end and the lower end of the unmanned plane wing 2 are both provided with the guide groove 10, the two guide grooves 10 are respectively communicated with the upper end and the lower end of the sliding channel 6, and the sliding block 9 is arranged in the guide groove 10. Specifically, the guide groove 10 is arranged at the upper end and the lower end of the unmanned plane wing 2, and the corresponding sliding block 9 is arranged at the upper end and the lower end of the second connector 8, so that the connection block 7 is controlled synchronously up and down when sliding in the sliding channel 6, the stability and the guiding accuracy in the sliding process are enhanced, the deviation or the jamming phenomenon is avoided, and the smoothness and the reliability of the connection are improved.

[0035] The quick-release portable unmanned plane provided by the embodiment is characterized in that the outer side of the sliding block 9 is provided with the operation block 18, and the operation block 18 is located outside the guide groove 10. Specifically, the operation block 18 is arranged outside the sliding block 9 and located outside the guide groove 10, so that the user can directly manually push or pull the operation block 18 to drive the connection block 7 to move, the wing is quickly installed or disassembled, and the humanization degree and the use convenience of the operation are improved.

[0036] Although the embodiments of the utility model have been shown and described, those skilled in the art can understand that various changes, modifications, replacements and variations can be made to these embodiments without departing from the principles and purposes of the utility model, the scope of the utility model is defined by the claims and its equivalents.

Claims

1. A quick release portable unmanned aerial vehicle, characterized in that: The utility model provides a kind of unmanned aerial vehicle, including unmanned aerial vehicle fuselage and two unmanned aerial vehicle wings, the both sides of the unmanned aerial vehicle fuselage are provided with clamping slot, the outside of the unmanned aerial vehicle fuselage is provided with clamping block, the clamping block is connected with the clamping slot, the both sides of the unmanned aerial vehicle fuselage are provided with first connector, the edge of the unmanned aerial vehicle wing is provided with slide, the outside of the unmanned aerial vehicle wing is communicated with the slide, the slide is provided with connecting block, the connecting block is provided with second connector, the top of the second connector is provided with sliding block, the top of the unmanned aerial vehicle wing is provided with guide slot, the guide slot is communicated with the slide, the sliding block is arranged in the guide slot, the first connector is connected with the second connector.

2. The quick-release portable unmanned aerial vehicle of claim 1, wherein: The clamping slot includes extension slot and positioning slot, the cross section of the positioning slot is circular, the extension slot is located on the outside of the positioning slot, the extension slot is communicated with the outside of the unmanned aerial vehicle wing, the clamping block includes connecting column and extension part, the connecting column is connected with the outside of the unmanned aerial vehicle wing, the extension part is connected with the outside of the connecting column, the extension part is correspondingly arranged with the extension slot, so that extension part is rotated and positioned in positioning slot from extension slot.

3. The quick-release portable unmanned aerial vehicle of claim 1, wherein: The unmanned aerial vehicle fuselage includes lower fuselage and upper fuselage, the top of the lower fuselage is connected with the bottom of the upper fuselage, the lower fuselage and the upper fuselage are combined to form the clamping slot and the slide.

4. The quick-release portable unmanned aerial vehicle of claim 1, wherein: The unmanned aerial vehicle fuselage is provided with accommodating cavity.

5. The quick-release portable unmanned aerial vehicle of claim 1, wherein: The upper and lower ends of the unmanned aerial vehicle fuselage are provided with the guide slot, the upper and lower ends of the second connector are provided with the sliding block, the upper and lower ends of the unmanned aerial vehicle wing are provided with the guide slot, the upper and lower ends of the slide are communicated with the guide slot respectively, and the sliding block is arranged in the guide slot.

6. The quick-release portable drone of claim 1, wherein: The outside of the sliding block is provided with operating block, and the operating block is located on the outside of the guide slot.

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