Low-altitude inspection unmanned aerial vehicle with protective structure
By using a modularly designed landing gear and snap-fit components, the structural damage problem of low-altitude inspection UAVs during landing in complex environments has been solved, enabling stable landing and convenient maintenance, and reducing maintenance costs.
Patent Information
- Application Number
- CN202520335259.5
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-02-28
- Publication Date
- 2025-12-30
- Estimated Expiration
- 2035-02-28
AI Technical Summary
When existing low-altitude inspection drones land in complex environments, their landing gear is easily damaged, causing the drone to lose balance and suffer structural damage, resulting in long repair times and high costs.
The landing gear features a modular design, incorporating rubber pads and snap-fit components to increase friction and cushioning. Damaged parts can be easily replaced using limit components, reducing maintenance costs.
It improves the service life of the landing gear and landing stability, shortens maintenance time, reduces maintenance costs, and enhances the economic efficiency of use.
Smart Images
Figure CN223736283U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to the technical field of hoist, especially with protection structure's low altitude inspection unmanned plane. BACKGROUND
[0002] The unmanned plane is the no -person aircraft that uses radio remote control equipment and self -provided program control device to manipulate, or by vehicle -mounted computer completely or intermittently autonomously, it has small, low cost, convenient to use and so on Advantage, therefore uses low altitude inspection unmanned plane to carry out the inspection in the use scene such as electric power inspection, water conservancy patrol, forestry protection, building construction site monitoring,
[0003] The low altitude inspection unmanned plane in prior art is in use when the fuselage main part, power system, communication system landing gear, propeller and other structures are formed, in use, through the remote operation unmanned plane of using operator, to carry out the inspection, after the inspection is completed, when unmanned plane lands, landing gear first contacts the ground, carries out the buffering shock absorption to the fuselage, to reach the effect of protecting unmanned plane.
[0004] However, because the use environment of low altitude inspection unmanned plane is more complex, and further in the case that the ground environment is hard, the ground is uneven or there are small stones on the ground, and the operator operates the unmanned plane to land, the bottom of landing gear will be scratched, even cause the indentation, fracture of landing gear, so that the unmanned plane cannot land smoothly, lead to the unmanned plane lose balance and roll over, and further cause the damage such as distortion, stretching of landing gear and propeller, so that a certain time and economy are needed for maintenance. INVENTION CONTENTS
[0005] In view of the above defects or deficiencies in the prior art, it is desirable to provide a low altitude inspection unmanned plane with a protection structure, which can operate normally in a low temperature outdoor environment and ensure the safety of operation.
[0006] The utility model provides a low altitude inspection unmanned plane with a protection structure, which comprises a body, two support rods are fixedly connected to the bottom end of the body, an installation slot is formed in the inside of the support rod, an installation rod is inserted into the inside of the installation slot, a contact rod is fixedly connected to the bottom end of the installation rod, a protection assembly is arranged on the outside lower side of the contact rod, a limiting assembly is arranged on the outside upper side of the contact rod, and a clamping assembly is arranged between the limiting assembly and the contact rod.
[0007] Further, the protection assembly comprises a rubber pad sleeved on the outside lower side of the contact rod, two clamping pieces one are fixedly connected to one side of the rubber pad, two clamping pieces two are fixedly connected to the other side of the rubber pad, and the rubber pad is clamped with the clamping pieces one.
[0008] Further, the limiting component includes a first limiting groove respectively opened on both sides of the support rod and two second limiting grooves opened inside the upper side of the contact rod. A limiting plate is hinged to the lower side inside the first limiting groove. A connecting block is fixedly connected to one side of the limiting plate close to the mounting rod. A connecting groove is opened on one side of the mounting rod close to the limiting plate.
[0009] Further, the clamping component includes a slot opened on the inner bottom wall of the second limiting groove. Clamping grooves are opened on both sides of the inner wall of the slot. A plug rod is inserted into the slot. A placing groove is opened at a position parallel to the clamping groove inside the plug rod. A clamping block is clamped in the clamping groove. A pull rope is fixedly connected to one side of the clamping block away from the clamping groove. An elastic member is sleeved outside the pull rope.
[0010] Further, the limiting plate is swingably installed inside the second limiting groove. The top end of the limiting plate is in contact with the bottom end of the second clamping member.
[0011] Further, the connecting block is rotatably connected inside the contact rod. The connecting block is clamped inside the connecting groove.
[0012] Further, the top end of the plug rod is fixedly connected to the bottom end of the limiting plate. The clamping block is of a "T" - shaped block structure and is slidably connected inside the placing groove. The pull rope is slidably connected inside the placing groove.
[0013] Further, one end of the pull rope away from the placing groove is fixedly connected to a pull ring. The pull ring is of a "return" - shaped structure.
[0014] Compared with the prior art, the beneficial effects of the present utility model are as follows:
[0015] By modularizing the landing gear of the low - altitude inspection unmanned aerial vehicle of the present utility model and using the clamping component to sleeve the rubber pad outside the mounting rod, not only can the friction between the landing gear and the ground be increased to prevent slipping due to the smooth ground, but also the scratching between the landing gear and the ground can be reduced, and the impact force during landing can be buffered, so that the landing gear has a long service life. Furthermore, when the unmanned aerial vehicle lands, it can be kept stable. And when the landing gear is accidentally damaged, the mounting rod can be disassembled from the support rod by using the limiting component, so as to quickly replace and maintain the landing gear, resulting in a short maintenance time. And by repairing and replacing locally, the maintenance cost is low, and the economic efficiency of use is high.
[0016] It should be understood that the content described in the utility model content part is not intended to limit the key or important features of the embodiments of the present utility model, nor to limit the scope of the present utility model. Other features of the present utility model will become easily understandable through the following description. BRIEF DESCRIPTION OF THE DRAWINGS
[0017] Other features, objects, and advantages of the present application will become more apparent from the following detailed description of non-limiting embodiments thereof, when read in conjunction with the accompanying drawings:
[0018] Figure 1 is a perspective view of the low-altitude patrol unmanned aerial vehicle;
[0019] Figure 2 is a schematic view of the landing gear from a top view;
[0020] Figure 3 is a schematic view of the landing gear from a top view; Figure 2 is a sectional view of the structure at A-A;
[0021] Figure 4 is a schematic view of the landing gear from a top view; Figure 3 is an enlarged schematic view of the structure at A;
[0022] Figure 5 is a schematic view of the landing gear from a top view; Figure 2 is a sectional view of the structure at B-B;
[0023] Figure 6 is an enlarged schematic view of the structure at B; Figure 5
[0024] Figure 7 is a schematic view of the landing gear from a top view;
[0025] Figure 8 is a schematic view of the landing gear from a top view;
[0026] Figure 9 is an enlarged schematic view of the structure at C. Figure 8 Reference signs in the drawings: 1, body; 2, support rod; 3, mounting groove; 4, mounting rod; 5, contact rod; 6, protection assembly; 7, limiting assembly; 8, clamping assembly;
[0027] 61, rubber pad; 62, clamping piece one; 63, clamping piece two;
[0028] 71, limiting plate; 72, limiting groove one; 73, limiting groove two; 74, connecting block; 75, connecting groove;
[0029] 81, insertion groove; 82, insertion rod; 83, clamping groove; 84, placement groove; 85, clamping block; 86, elastic piece; 87, pull rope; 88, pull ring.
[0030] DETAILED DESCRIPTION
[0031] The utility model will be explained in further detail below with reference to the drawings and embodiments. It can be understood that the specific embodiments described herein are merely intended to explain the related utility model and not limit the utility model. In addition, it should be noted that only the parts related to the utility model are shown in the drawings for ease of description.
[0032] It should be noted that the embodiments in the utility model and the features in the embodiments can be combined with each other without conflict. The utility model will be explained in detail below with reference to the drawings and embodiments.
[0033] Please refer to Figures 1-8 The embodiment of the utility model provides a low-altitude patrol inspection unmanned plane with a protection structure, which comprises a body 1, two support rods 2 are fixedly connected to the bottom end of the body 1, an installation groove 3 is arranged in the inside of the support rod 2, an installation rod 4 is inserted into the inside of the installation groove 3, a contact rod 5 is fixedly connected to the bottom end of the installation rod 4, a protection assembly 6 is arranged on the outside lower side of the contact rod 5, a limiting assembly 7 is arranged on the outside upper side of the contact rod 5, and a clamping assembly 8 is arranged between the limiting assembly 7 and the contact rod 5.
[0034] In the embodiment, the landing gear is divided into the support rod 2, the installation groove 3, the installation rod 4 and the contact rod 5, so that the landing gear is modularized, and then when the unmanned plane accidentally falls, even if the contact rod 5 is damaged, the contact rod 5 can be conveniently replaced by pulling out the installation rod 4 from the inside of the installation groove 3, so that the time for maintenance and replacement is less, the cost for maintenance and replacement is lower, and the use economy is better.
[0035] The installation groove 3 provides an installation space for the installation rod 4, so that the contact rod 5 can be inserted on the support rod 2.
[0036] In a preferred embodiment, as shown in Figure 8 and Figure 9 The protection assembly 6 comprises a rubber pad 61 sleeved on the outside lower side of the contact rod 5, two clamping pieces one 62 are fixedly connected to one side of the rubber pad 61, two clamping pieces two 63 are fixedly connected to the other side of the rubber pad 61, and the rubber pad 61 is clamped with the clamping pieces one 62.
[0037] In the embodiment, the protection assembly 6 is sleeved on the contact rod 5, one side of the clamping pieces two 63 is attached to the outside of the contact rod 5, the other side of the clamping pieces two 63 is attached to the clamping pieces one 62, the protrusions on the clamping pieces two 63 enter the grooves in the clamping pieces one 62, the clamping pieces two 63 are attached to the clamping pieces one 62, and then the rubber pad 61 can be conveniently installed, and the rubber pad 61 can protect the contact rod 5.
[0038] When the unmanned aerial vehicle lands at a high speed or falls at a low altitude, the rubber pad 61 first contacts the ground, increasing the contact area of the contact rod 5 with the ground, so as to disperse the impact force to a larger area, avoiding excessive local stress on the contact rod 5 and causing damage to the contact rod 5 and the support rod 2, and when the ground is uneven or contains small stones and other impurities, the rubber pad 61 can avoid direct contact between the ground or small stones and other impurities and the contact rod 5, so that the contact rod 5 will not be rubbed and damaged, and the service life of the contact rod 5 will be longer.
[0039] In a preferred embodiment, as shown in Figure 3 、 4 , 5, 6, the limiting assembly 7 includes limiting slot one 72 respectively provided on both sides of the support rod 2 and two limiting slot two 73 provided on the upper side of the contact rod 5, the inner lower side of the limiting slot one 72 is hingedly connected with a limiting plate 71, the side of the limiting plate 71 close to the mounting rod 4 is fixedly connected with a connecting block 74, and the side of the mounting rod 4 close to the limiting plate 71 is provided with a connecting slot 75.
[0040] In this embodiment, when the contact rod 5 is not installed, the limiting plate 71 is placed in the limiting slot one 72, and when the contact rod 5 and the protection assembly 6 need to be installed, the protection assembly 6 is installed on the contact rod 5, and then the mounting rod 4 is inserted into the mounting slot 3, at this time the upper side of the contact rod 5 is in contact with the bottom end of the support rod 2, thereby the limiting plate 71 is buckled, so that the lower side of the limiting plate 71 in the vertical state can be rotated, and when the limiting plate 71 remains in the horizontal state, the limiting plate 71 can enter the inside of the limiting slot two 73, at this time the limiting plate 71 can clamp the clamping piece one 62 and the clamping piece two 63 at the plane between the limiting slot two 73 and the contact rod 5.
[0041] In a preferred embodiment, as shown in Figure 4 , the clamping assembly 8 includes a slot 81 provided in the inner bottom wall of the limiting slot two 73, the inner wall of the slot 81 is provided with a clamping slot 83 on both sides, the inside of the slot 81 is inserted with a plug rod 82, the inside of the plug rod 82 is provided with a placing slot 84 in parallel with the clamping slot 83, the inside of the clamping slot 83 is clamped with a clamping block 85, the side of the clamping block 85 away from the clamping slot 83 is fixedly connected with a pull rope 87, and the outside of the pull rope 87 is sleeved with an elastic piece 86.
[0042] In this embodiment, when the limiting plate 71 enters the inside of the limiting slot two 73, the plug rod 82 can be inserted into the inside of the slot 81, thereby limiting the limiting plate 71, and the elastic piece 86 can be reset, so that it can push the clamping block 85 to be clamped with the inside of the clamping slot 83, thereby the limiting plate 71 can be stably installed on the contact rod 5, so that the connection between the contact rod 5 and the support rod 2, the limiting plate 71 and the contact rod 5 is more stable, thereby the use safety of the protection assembly 6 and the contact rod 5 is higher.
[0043] The plug rod 82 is made of polyamide material, which has deformation resistance and good elasticity. When the plug rod 82 is pulled upward, it can be separated from the plug slot 81.
[0044] When the rubber pad 61 needs to be replaced, the pull rope 87 is pulled upward to move the clamping block 85 inward, so that the clamping block 85 is separated from the inside of the clamping slot 83, and the elastic element 86 is deformed. When the elastic element 86 reaches the limit compression position, continue to pull the pull rope 87 to move the plug rod 82 upward, so that the plug rod 82 is separated from the inside of the plug slot 81, and then the limiting plate 71 is separated from the inside of the limiting slot two 73. At this time, the clamping piece one 62 and the clamping piece two 63 are not limited by the limiting plate 71, so that the rubber pad 61 can be disassembled and replaced. At this time, the rubber pad 61 can be replaced with different models to adapt to different use environments, so that the use flexibility is high.
[0045] In a preferred embodiment, as shown in Figure 4 and Figure 9 , the limiting plate 71 is swingly installed in the inside of the limiting slot two 73, the top end of the limiting plate 71 is in contact with the bottom end of the clamping piece two 63, and the limiting slot two 73 provides installation space for the limiting plate 71. When the limiting plate 71 slides into the inside of the limiting slot two 73, the limiting plate 71 can limit the clamping piece two 63 to limit the rubber pad 61.
[0046] In a preferred embodiment, as shown in Figure 4 , the connecting block 74 is rotatably connected in the inside of the contact rod 5, and the connecting block 74 is clamped in the inside of the connecting slot 75. When the contact rod 5 needs to be disassembled, the limiting plate 71 is rotated away from the limiting slot two 73, so that the limiting plate 71 is accommodated in the inside of the limiting slot one 72. At this time, the connecting block 74 is not in contact with the connecting slot 75, so that the mounting rod 4 is not limited, and the contact rod 5 can be disassembled and replaced. The limiting plate 71 not only limits the mounting rod 4, but also limits the protection assembly 6, achieving the effect of one thing serving multiple purposes.
[0047] In a preferred embodiment, as shown in Figure 4 , the top end of the plug rod 82 is fixedly connected to the bottom end of the limiting plate 71, the clamping block 85 is a “T”-shaped block structure, and is slidably connected in the inside of the placing slot 84. The pull rope 87 is slidably connected in the inside of the placing slot 84. The placing slot 84 limits the clamping block 85, so that the side of the clamping block 85 away from the clamping slot 83 cannot be separated from the inside of the placing slot 84, thereby ensuring the structural stability and good safety.
[0048] In a preferred embodiment, such as Figure 4 As shown, a pull ring 88 is fixedly connected to the end of the pull rope 87 away from the placement groove 84. The pull ring 88 has a "U" shaped structure, so the pull rope 87 can be pulled by snapping the pull ring 88, which makes it easy to use.
[0049] In the description of this specification, the terms "connection," "installation," and "fixing," etc., should be interpreted broadly. For example, "connection" can be a fixed connection, a detachable connection, or an integral connection; it can be a direct connection or an indirect connection through an intermediate medium. Those skilled in the art can understand the specific meaning of the above terms in this application according to the specific circumstances.
[0050] In the description of this specification, the terms "one embodiment," "some embodiments," etc., refer to specific features, structures, materials, or characteristics described in connection with that embodiment or example, which are included in at least one embodiment or example of this application. In this specification, the illustrative expressions of the above terms do not necessarily refer to the same embodiment or example. Furthermore, the specific features, structures, materials, or characteristics described may be combined in any suitable manner in one or more embodiments or examples.
[0051] The above are merely preferred embodiments of this application and are not intended to limit this application. Various modifications and variations can be made to this application by those skilled in the art. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of this application should be included within the protection scope of this application.
Claims
1. A low-altitude inspection unmanned aerial vehicle with a protective structure, characterized in that, The application relates to a machine body (1) which is fixedly connected with two supporting rods (2) at the bottom end, the inside of the supporting rods (2) is provided with mounting grooves (3), the inside of the mounting grooves (3) is inserted with mounting rods (4), the bottom end of the mounting rods (4) is fixedly connected with contact rods (5), the outer lower side of the contact rods (5) is provided with a protection assembly (6), the outer upper side of the contact rods (5) is provided with a limiting assembly (7), and a clamping assembly (8) is arranged between the limiting assembly (7) and the contact rods (5).
2. The low-altitude inspection unmanned aerial vehicle with a protection structure according to claim 1, characterized in that, The protection assembly (6) comprises rubber pads (61) which are arranged on the outer lower side of the contact rods (5), one side of the rubber pads (61) is fixedly connected with two clamping pieces one (62), the other side of the rubber pads (61) is fixedly connected with two clamping pieces two (63), and the rubber pads (61) are clamped with the clamping pieces one (62).
3. The low-altitude inspection unmanned aerial vehicle with a protection structure according to claim 2, characterized in that, The limiting assembly (7) comprises limiting grooves one (72) which are respectively arranged on the two sides of the supporting rods (2) and two limiting grooves two (73) which are arranged on the inner upper side of the contact rods (5), the inner lower side of the limiting grooves one (72) is hingedly connected with limiting plates (71), one side of the limiting plates (71) close to the mounting rods (4) is fixedly connected with connecting blocks (74), and the side of the mounting rods (4) close to the limiting plates (71) is provided with connecting grooves (75).
4. The low-altitude inspection unmanned aerial vehicle with a protection structure according to claim 3, characterized in that, The clamping assembly (8) comprises insertion grooves (81) which are arranged in the inner bottom walls of the limiting grooves two (73), clamping grooves (83) are arranged on the inner walls of the insertion grooves (81), insertion rods (82) are inserted into the insertion grooves (81), placing grooves (84) which are parallel to the clamping grooves (83) are arranged in the insertion rods (82), clamping blocks (85) are clamped in the clamping grooves (83), pulling ropes (87) are fixedly connected to the sides of the clamping blocks (85) away from the clamping grooves (83), and elastic pieces (86) are arranged on the outer sides of the pulling ropes (87).
5. The low-altitude inspection unmanned aerial vehicle with a protection structure according to claim 3, characterized in that, The limiting plates (71) are swingably arranged in the limiting grooves two (73), and the top end of the limiting plates (71) is in abutment with the bottom end of the clamping pieces two (63).
6. The low-altitude inspection unmanned aerial vehicle with a protection structure according to claim 4, characterized in that, The connecting blocks (74) are rotatably connected in the inside of the contact rods (5), and the connecting blocks (74) are clamped in the connecting grooves (75).
7. The low-altitude inspection unmanned aerial vehicle with a protective structure according to claim 4, characterized in that, The top end of the insertion rods (82) is fixedly connected to the bottom end of the limiting plates (71), the clamping blocks (85) are T-shaped blocks, are slidably connected in the placing grooves (84), and the pulling ropes (87) are slidably connected in the placing grooves (84).
8. The low-altitude inspection unmanned aerial vehicle with a protection structure according to claim 4, characterized in that, The pulling ropes (87) are fixedly connected with pull rings (88) at the ends away from the placing grooves (84), and the pull rings (88) are in the shape of a Chinese character 'hui'.