Unmanned aerial vehicle undercarriage

Abstract

The utility model provides an unmanned aerial vehicle undercarriage, and belongs to the technical field of unmanned aerial vehicles. Comprising a supporting base frame, adaptive adjusting mechanisms are installed on the upper portion and the two sides of the supporting base frame, dual-purpose stabilizing mechanisms are installed on the periphery of the supporting base frame, and each adaptive adjusting mechanism comprises a first platform. By arranging the adaptive adjusting mechanism, when a worker flies unmanned aerial vehicles of different sizes, the distance between the second platforms on the two sides of the first platform and the worker can be properly adjusted according to the different sizes of the unmanned aerial vehicles, and the adjusting mode is that a motor is started to enable a transmission rod and a second bevel gear at the end of the transmission rod to rotate; at the moment, a first bevel gear meshed with the gear can synchronously drive a positive screw rod and a negative screw rod to rotate, and at the moment, two opposite screw rod sliding sleeves acting with the screw rod can drive second platforms fixed above the screw rod sliding sleeves to be matched with guide rods for guiding to perform relative displacement, so that the carrying range among the three platforms is adjusted, and the unmanned aerial vehicles with different sizes can be adapted.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles, and particularly relates to an undercarriage of an unmanned aerial vehicle. Background Art

[0002] An unmanned aerial vehicle can fly autonomously by remote control or a preset flight path, has a certain payload capacity and carries various sensors, cameras or other devices, and can be applied to various fields for targeted search and rescue or detection. When the unmanned aerial vehicle is working, in order to ensure a certain protective effect when the unmanned aerial vehicle lands and prevent the unmanned aerial vehicle from being scratched or damaged during landing, an undercarriage for support is designed at the landing location of the unmanned aerial vehicle.

[0003] For example, patent CN221438423U discloses a buffer undercarriage for an unmanned aerial vehicle, which includes a main body base plate. Both sides of the upper end of the main body base plate are fixedly connected with buffer adjustment devices. A landing support platform is inserted into the upper ends of the buffer adjustment devices. Rubber anti-slip pads are fixedly connected to both sides of the upper end of the landing support platform. Support feet are fixedly connected to both sides of the lower end of the main body base plate.

[0004] During the use of the above buffer undercarriage for an unmanned aerial vehicle, its landing support platform cannot adjust its own size according to different sizes of unmanned aerial vehicles, resulting in that larger unmanned aerial vehicles cannot be adapted for use. Therefore, the present application provides an undercarriage for an unmanned aerial vehicle to meet the requirements. Summary of the Utility Model

[0005] The technical problem to be solved by the utility model is to provide an undercarriage for an unmanned aerial vehicle to solve the problem that the existing landing support platform cannot adjust its own size according to different sizes of unmanned aerial vehicles, resulting in that larger unmanned aerial vehicles cannot be adapted for use.

[0006] To solve the above technical problem, the utility model provides the following technical solutions:

[0007] An undercarriage for an unmanned aerial vehicle includes a support base frame. An adaptation adjustment mechanism is installed above and on both sides of the support base frame, and a dual-purpose stabilizing mechanism is installed on the four peripheral edges of the support base frame. The adaptation adjustment mechanism includes a first platform, and the first platform is fixed to the middle of the upper part of the support base frame. Side mounting frames are fixed to both sides of the first platform, and an adjustment component is installed inside the side mounting frames. The adjustment component includes a lead screw sliding sleeve, and a second platform is fixed above the lead screw sliding sleeve. Auxiliary support components are installed on both sides of the bottom of one end of the second platform. A shock-absorbing anti-slip pad is attached to the upper parts of the second platform and the first platform.

[0008] Optionally, the adjusting component includes a positive and negative lead screw, and the positive and negative lead screw is installed inside one side of the first platform and the two side mounting frames. A first bevel gear is fixed around one side of the middle of the positive and negative lead screw, and a second bevel gear is engaged with one side of the first bevel gear. A transmission rod is fixed in the middle of the second bevel gear, and a motor is connected and installed at one end of the transmission rod. Screw sleeves are screwed around both sides of the middle of the positive and negative lead screw. Guide rods are fixed inside the other sides of the two side mounting frames.

[0009] Optionally, the positive and negative lead screw is installed through one side inside of the first platform.

[0010] Optionally, the guide rod and the second platform are movably and guidingly connected.

[0011] Optionally, the auxiliary support component includes support rods, and the support rods are fixed to one side of the bottom end of the second platform. Rotating shafts are installed at the bottoms of the two support rods, and guide wheels are installed below the rotating shafts.

[0012] Optionally, the support rods are symmetrically fixed along the middle of one side of the bottom end of the second platform.

[0013] Optionally, the dual-purpose stabilizing mechanism includes side fixing blocks, and the side fixing blocks are distributed and fixed on the four peripheral edges of the support base frame. Screw mounting slots are opened in the middle of the four side fixing blocks, and threaded columns are screwed in the middle of the screw mounting slots. External threads are opened around the lower section of the threaded column, and screw mounting cones are screwed around the external threads. Screw mounting suckers can also be screwed around the external threads.

[0014] Optionally, the threaded column and the screw mounting slot opened in the middle of the side fixing block are in threaded lifting connection.

[0015] Optionally, the screw mounting cone and the external threads provided around the lower section of the threaded column are in threaded assembly connection.

[0016] Optionally, the screw mounting sucker and the external threads provided around the lower section of the threaded column are in threaded assembly connection.

[0017] Compared with the prior art, the present utility model has at least the following beneficial effects:

[0018] In the above solution, by setting an adaptation and adjustment mechanism, when the staff operates drones of different sizes, the distance between the two second platforms on both sides of the first platform and itself can be appropriately adjusted according to the different sizes of the drones. The adjustment method is to start the motor to make the transmission rod and the second bevel gear at its end rotate. At this moment, the first bevel gear meshing with the gear will synchronously drive the positive and negative lead screws to rotate. At this time, the two relative lead screw sleeves acting on the lead screws will drive the second platforms fixed above them to perform relative displacement along with the guidance of the guide rods, so as to adjust the loadable range between the three platforms, thereby adapting to drones of different sizes. It is worth mentioning that on both sides below the ends of the two second platforms, there are support rods, movable rotating shafts and guiding wheels, which can assist the second platforms to move smoothly and achieve the effect of stable support at the same time.

[0019] By setting a dual-purpose stability mechanism, according to the different placement locations of the support base frame, personnel can choose to screw on a screw cone head or a screw sucker under the threaded column using the external thread. When in some soft soil or lawns, personnel can assemble a screw cone head with a sharp tip. When dealing with a hard bottom surface, personnel can assemble a screw sucker. The threading between the threaded column and the screw slot can make the above two rise and fall to achieve the stability of the loading position of the entire support base frame and improve safety. BRIEF DESCRIPTION OF THE DRAWINGS

[0020] The drawings incorporated herein and constituting a part of the specification illustrate embodiments of the present invention and, together with the specification, are further used to explain the principles of the present invention and enable those skilled in the relevant art to implement and use the present invention.

[0021] Figure 1 is a three-dimensional structural schematic diagram of a drone landing gear;

[0022] Figure 2 is a partial structural schematic diagram of an adjustment component of a drone landing gear;

[0023] Figure 3 is for a drone landing gear Figure 1 structural schematic diagram at position A therein;

[0024] Figure 4 is a partial structural schematic diagram of a dual-purpose stability mechanism of a drone landing gear.

[0025] [Reference Numerals]

[0026] 1. Support base frame; 2. Adaptation adjustment mechanism; 21. First platform; 22. Side mounting frame; 23. Adjustment component; 231. Positive and negative lead screw; 232. First bevel gear; 233. Second bevel gear; 234. Transmission rod; 235. Motor; 236. Lead screw sliding sleeve; 237. Guide rod; 24. Second platform; 25. Auxiliary support component; 251. Support rod; 252. Rotating shaft; 253. Guide wheel; 26. Shock-absorbing and anti-slip pad; 3. Dual-purpose stabilization mechanism; 31. Side fixing block; 32. Threaded mounting slot hole; 33. Threaded column; 34. External thread; 35. Threaded taper head; 36. Threaded suction cup.

[0027] As shown in the figure, in order to clearly implement the structure of the embodiments of the present invention, specific structures and devices are marked in the figure. However, this is only for schematic purposes and is not intended to limit the present invention to this specific structure, device, and environment. According to specific needs, those of ordinary skill in the art can adjust or modify these devices and environments. Detailed implementation manners

[0028] The following describes in detail a drone landing gear provided by the present invention with reference to the accompanying drawings and specific embodiments. At the same time, it should be noted here that in order to make the embodiments more detailed, the following embodiments are the best and preferred embodiments. For some well-known technologies, those skilled in the art can also adopt other alternative methods for implementation; moreover, the accompanying drawings are only for more specifically describing the embodiments and are not intended to specifically limit the present invention.

[0029] It should be pointed out that in the specification, references to "one embodiment", "embodiment", "exemplary embodiment", "some embodiments", etc. indicate that the described embodiments may include specific features, structures, or characteristics, but not necessarily every embodiment includes such specific features, structures, or characteristics. Additionally, when combining embodiments to describe specific features, structures, or characteristics, implementing such features, structures, or characteristics in combination with other embodiments (whether explicitly described or not) should be within the knowledge of those skilled in the relevant art.

[0030] Generally, terms can be understood at least in part from their use in context. For example, at least in part depending on the context, the term "one or more" as used herein can be used to describe any feature, structure, or characteristic in a singular sense, or can be used to describe a combination of features, structures, or characteristics in a plural sense. Additionally, the term "based on" can be understood as not necessarily intended to convey a set of exclusive factors, but rather, at least in part depending on the context, can allow for the existence of other factors that may not be explicitly described.

[0031] It will be understood that the meanings of "on", "above", and "over" in the present utility model should be construed in the broadest manner such that "on" not only means "directly on" something, but also includes the meaning of being "on" something with intervening features or layers therebetween, and "above" or "over" not only means "above" or "over" something, but may also include the meaning of being "above" or "over" something with no intervening features or layers therebetween.

[0032] In addition, spatial relative terms such as "under", "below", "lower", "above", "upper", etc. may be used herein for convenience of description to describe the relationship of one element or feature to another or other elements or features, as shown in the drawings. The spatial relative terms are intended to cover different orientations in the use or operation of the device in addition to the orientation depicted in the drawings. The device may be oriented in other ways, and the spatial relative descriptors used herein may be interpreted accordingly.

[0033] As Figure 1 and Figure 2As shown in the figure, an embodiment of the present utility model provides a landing gear for a drone, which includes a support base frame 1. An adaptation and adjustment mechanism 2 is installed above and on both sides of the support base frame 1, and a dual-purpose stability mechanism 3 is installed on the four peripheral edges of the support base frame 1. The adaptation and adjustment mechanism 2 includes a first platform 21, and the first platform 21 is fixed to the middle above the support base frame 1. Side mounting frames 22 are fixed on both sides of the first platform 21, and an adjustment component 23 is installed inside the side mounting frames 22. The adjustment component 23 includes a positive and negative screw rod 231, and the positive and negative screw rod 231 is installed inside one side of the first platform 21 and the side mounting frames 22 on both sides. The positive and negative screw rod 231 penetrates and is installed inside one side of the first platform 21. A first bevel gear 232 is fixed around one side of the middle of the positive and negative screw rod 231, and a second bevel gear 233 is meshed with one side of the first bevel gear 232. A transmission rod 234 is fixed in the middle of the second bevel gear 233, and a motor 235 is connected and installed at one end of the transmission rod 234. Screw rod sliding sleeves 236 are screwed on the peripheries on both sides of the middle of the positive and negative screw rod 231. Guide rods 237 are fixed inside the other sides of the two side mounting frames 22. The guide rods 237 and the second platform 24 are movably and guidingly connected. The second platform 24 is fixed above the screw rod sliding sleeves 236. Auxiliary support components 25 are installed on both sides of the bottom of one end of the second platform 24. A shock-absorbing and anti-slip pad 26 is attached to the upper sides of the second platform 24 and the first platform 21. The auxiliary support component 25 includes support rods 251, and the support rods 251 are fixed to one side of the bottom end of the second platform 24. Rotating shafts 252 are installed at the bottoms of the two support rods 251, and guide wheels 253 are installed below the rotating shafts 252. The support rods 251 are symmetrically fixed along the middle of one side of the bottom end of the second platform 24. When the staff flies drones of different sizes, the distance between the second platforms 24 on both sides of the first platform 21 and itself can be appropriately adjusted according to the different sizes of the drones. The adjustment method is to start the motor 235 to make the transmission rod 234 and the second bevel gear 233 at its end rotate. At this moment, the first bevel gear 232 meshed with the gear will synchronously drive the positive and negative screw rod 231 to rotate. At this time, the two opposite screw rod sliding sleeves 236 acting on the screw rod will drive the second platforms 24 fixed above them to perform relative displacement in cooperation with the guiding of the guide rods 237, so as to adjust the loadable range between the three platforms, thereby adapting to drones of different sizes. It is worth mentioning that support rods 251, movable rotating shafts 252, and guide wheels 253 are provided on both sides below the respective ends of the two second platforms 24, so that while assisting the second platforms 24 to move smoothly, the effect of support and stability can also be achieved.

[0034] As Figures 1 to 4As shown, the dual-purpose stabilizing mechanism 3 includes side fixing blocks 31, and the side fixing blocks 31 are distributed and fixed on the four peripheral parts of the supporting base frame 1. The middle parts of the four side fixing blocks 31 are provided with screw-mounted slots 32, and the middle parts of the screw-mounted slots 32 are screwed with threaded columns 33. The threaded columns 33 and the screw-mounted slots 32 opened in the middle of the side fixing blocks 31 are connected by threaded lifting. The lower part of the threaded column 33 is provided with an external thread 34, and the periphery of the external thread 34 is screwed with a screw-mounted cone head 35. The screw-mounted cone head 35 and the external thread 34 provided on the periphery of the lower part of the threaded column 33 are threadedly assembled. The periphery of the external thread 34 can also be screwed with a screw. The suction cup 36 is installed, and the screw-mounted suction cup 36 and the external thread 34 provided around the lower section of the threaded column 33 are threadedly assembled and connected. According to the different placement locations of the support base frame 1, personnel can use the external thread 34 under the threaded column 33 to choose to screw on the screw-mounted cone head 35 or the screw-mounted suction cup 36. When it is on some sparse soft soil or lawn, personnel can assemble the screw-mounted cone head 35 with a sharp point. When it involves a hard bottom surface, personnel can assemble the screw-mounted suction cup 36. The threaded nature between the threaded column 33 and the screw-mounted slot 32 can make the above two be raised and lowered to achieve the stability of the mounting position of the entire support base frame 1 and improve safety.

[0035] The working principle of the technical solution provided by the utility model is as follows:

[0036] When the staff is involved in flying drones of different sizes, the distance between the second platforms 24 on both sides of the first platform 21 and itself can be appropriately adjusted according to the size of the drones. The adjustment method is to start the motor 235 to rotate the transmission rod 234 and the second bevel gear 233 at its end. At this moment, the first bevel gear 232 engaged with the gear will synchronously drive the forward and reverse screw rods 231 to rotate. At this time, the two relative screw rod sleeves 236 acting on the screw rod will drive the second platforms 24 fixed above each other to cooperate with the guide rod 237 for relative displacement, so as to adjust the carrying range between the three platforms, thereby adapting to drones of different sizes. It is worth mentioning that on each of the two second platforms 24, Support rods 251, movable rotating shafts 252 and guide wheels 253 are provided on both sides below the end, so that they can assist the second platform 24 to move smoothly while achieving a stable support effect. Finally, according to the different placement locations of the support base frame 1, personnel can use the external thread 34 under the threaded column 33 to select a screw-mounted screw cone head 35 or a screw-mounted suction cup 36. When it is in some sparse soft soil or lawn, personnel can assemble a sharp screw-mounted cone head 35. When it involves a hard bottom surface, personnel can assemble a screw-mounted suction cup 36. The threaded nature between the threaded column 33 and the screw-mounted slot 32 can make the above two be raised and lowered to achieve the stability of the mounting position of the entire support base frame 1 and improve safety.

[0037] The present utility model covers any alternatives, modifications, equivalent methods, and solutions made to the essence and scope of the present utility model. For the public to have a thorough understanding of the present utility model, specific details are described in detail in the following preferred embodiments of the present utility model, and those skilled in the art can fully understand the present utility model without the description of these details. Additionally, well-known methods, processes, procedures, components, and circuits are not described in detail to avoid unnecessary confusion to the essence of the present utility model.

[0038] The above description is only a preferred embodiment of the present utility model. It should be noted that for those of ordinary skill in the art, without departing from the principle of the present utility model, several improvements and refinements can be made, and these improvements and refinements should also be regarded as the protection scope of the present utility model.

Claims

1. An unmanned aerial vehicle landing gear, characterized in that, It includes a support base frame, an adaptor and adjustment mechanism is installed on the top and both sides of the support base frame, and a dual-purpose stabilizing mechanism is installed on the four peripheral parts of the support base frame, the adaptor and adjustment mechanism includes a first platform, and the first platform is fixed to the upper middle part of the support base frame, side mounting frames are fixed on both sides of the first platform, and an adjustment component is installed inside the side mounting frame, the adjustment component includes a screw sleeve, and a second platform is fixed above the screw sleeve, auxiliary support components are installed on both sides of the bottom of one end of the second platform, and shock-absorbing and anti-slip pads are attached to the second platform and the first platform.

2. The drone landing gear according to claim 1, wherein, The adjusting assembly includes forward and reverse screw rods, and the forward and reverse screw rods are installed inside one side of the first platform and the side mounting frames on both sides. A first bevel gear is fixed on the periphery of one side of the middle part of the forward and reverse screw rods, and a second bevel gear is meshed with one side of the first bevel gear. A transmission rod is fixed on the middle part of the second bevel gear, and one end of the transmission rod is connected to and installed with a motor. Screw sleeves are screwed on the periphery of both sides of the middle part of the forward and reverse screw rods, and a guide rod is fixed inside the other side of the two side mounting frames.

3. The UAV landing gear according to claim 2, characterized in that: The forward and reverse screw rods are installed through one side of the first platform.

4. The drone landing gear according to claim 2, wherein, The guide rod and the second platform are connected in a movable guide manner.

5. The UAV landing gear according to claim 1, characterized in that: The auxiliary support assembly includes a support rod, and the support rod is fixed to one side of the bottom end of the second platform. A rotating shaft is installed at the bottom of the two support rods, and a guide wheel is installed below the rotating shaft.

6. The drone landing gear according to claim 5, characterized in that, The support rods are symmetrically fixed along the middle portion of one side of the bottom end of the second platform.

7. The landing gear of the unmanned aerial vehicle according to claim 1, wherein, The dual-purpose stabilizing mechanism includes side fixing blocks, and the side fixing blocks are distributed and fixed on the four peripheral parts of the support base frame. The middle parts of the four side fixing blocks are provided with screw-mounted slots, and the middle parts of the screw-mounted slots are screwed with threaded columns. The lower part of the threaded column is provided with an external thread, and the periphery of the external thread is screwed with a screw-mounted cone head. The periphery of the external thread can also be screwed with a screw-mounted suction cup.

8. The landing gear of the drone according to claim 7, characterized in that, The threaded column and the screw-mounted slotted hole provided in the middle of the edge fixing block are connected by a threaded lifting connection.

9. The landing gear of the drone according to claim 7, characterized in that, The screw-mounted cone head and the external threads arranged around the lower section of the threaded column are connected by a threaded assembly.

10. The landing gear of the drone according to claim 7, characterized in that, The screw-mounted suction cup is connected to the external threads arranged around the lower section of the threaded column by a threaded assembly.

Images