Unmanned aerial vehicle undercarriage and unmanned aerial vehicle

Abstract

The utility model provides an unmanned aerial vehicle undercarriage and an unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicles, the unmanned aerial vehicle undercarriage comprises an operation platform, wings are uniformly arranged on the side surface of an unmanned aerial vehicle main body, the undercarriage is arranged at the bottom of the unmanned aerial vehicle main body, and a fixing device is arranged at the bottom of the unmanned aerial vehicle main body. A protective device is arranged on one side of the undercarriage, the fixing device comprises a fixing block, the fixing block is fixedly connected with the bottom of the unmanned aerial vehicle body, the surface of the fixing block is slidably sleeved with a fixing frame, the bottom of the fixing frame is fixedly connected with the top of the undercarriage, and a connecting groove is formed in the surface of the fixing block; the inner wall of the connecting groove is slidably connected with a connecting strip, the connecting strip is fixedly connected with the inner wall of the fixing frame, when the fixing device is used, the fixing frame is manually slid to the bottom of the fixing block, then the connecting strip is slid into the connecting groove, and therefore the undercarriage can be conveniently arranged at the bottom of the unmanned aerial vehicle body.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) technology, and in particular to a UAV landing gear and a UAV. Background Technology

[0002] A drone is an unmanned takeoff device that can be remotely controlled. When using a drone, the wings carry the main body of the drone into the air, and then the drone can be remotely controlled. This allows the drone to be used for remote monitoring and other purposes.

[0003] The inventor discovered in his daily work that drones still have at least the following problems: When using a drone, the wings carry the main body of the drone into the air, and then the drone can be remotely controlled by the remote control. This allows for remote monitoring and other functions. However, in actual use, because the drone and its landing gear are mostly connected by bolts, when using the drone outdoors, the landing gear, which plays a cushioning role, is prone to damage when the drone lands. This makes replacing the landing gear outdoors quite troublesome. Utility Model Content

[0004] The purpose of this utility model is to address the shortcomings of existing technologies by proposing a drone landing gear and a drone.

[0005] To achieve the above objectives, the present invention adopts the following technical solution: a drone landing gear and a drone, comprising a drone body, with wings evenly arranged on the side of the drone body, a landing gear at the bottom of the drone body, a fixing device at the bottom of the drone body, a protective device on one side of the landing gear, the fixing device comprising a fixing block, the fixing block being fixedly connected to the bottom of the drone body, a fixing frame being slidably fitted on the surface of the fixing block, the bottom of the fixing frame being fixedly connected to the top of the landing gear, a connecting groove being formed on the surface of the fixing block, a connecting strip being slidably connected to the inner wall of the connecting groove, and the connecting strip being fixedly connected to the inner wall of the fixing frame.

[0006] The effect achieved by the above components is as follows: when using the fixing device, the fixing frame is manually slid to the bottom of the fixing block, and then the connecting strip is slid into the inside of the connecting groove. This makes it easy to set the landing gear to the bottom of the drone body, so that the landing gear can be replaced without the need for tools.

[0007] Preferably, a limiting groove is provided on one side of the fixing block, a limiting frame is slidably connected to the inner wall of the limiting groove, a U-shaped plate is fixedly connected to the bottom of the limiting frame, the U-shaped plate is slidably sleeved on the bottom of the fixing block, and the fixing block is located on one side of the fixing frame.

[0008] The effect achieved by the above components is that the U-shaped plate is manually slid onto the surface of the fixed block, and then the limiting frame is slid into the inside of the limiting groove. In this way, the connecting strip can be restricted inside the connecting groove by the U-shaped plate.

[0009] Preferably, a slot is provided on one side of the fixing block, and a slotting plate is slidably connected to the inner wall of the slot, and the slotting plate is slidably connected to the inner wall of the limiting frame.

[0010] The effect achieved by the above components is: to slide the positioning plate into the inside of the positioning groove, and then slide the positioning plate into the inside of the limiting frame, so as to restrict the limiting frame inside the limiting groove, and thus restrict the U-shaped plate to the surface of the fixing block.

[0011] Preferably, a first damping rod is fixedly connected to one side of the inner wall of the slot, the end of the first damping rod away from the slot is fixedly connected to one side of the slot plate, a first spring is sleeved on the surface of the first damping rod, one end of the first spring is fixedly connected to one side of the inner wall of the slot, and the end of the first spring near the first damping rod is fixedly connected to one side of the slot plate.

[0012] The effect achieved by the above components is that the first spring pulls the positioning plate closer to the positioning slot, thereby making it easier to confine the positioning plate inside the positioning slot.

[0013] Preferably, the protective device includes a support rod, a fixing strip is fixedly connected to one side of the landing gear, a connecting frame is fixedly connected to the side of the fixing strip away from the landing gear, a round rod is fixedly connected to the inner wall of the connecting frame, and the support rod is rotatably sleeved on the surface of the round rod.

[0014] The effect achieved by the above components is that when the protective device is used, when the drone lands and the drone is tilted to a certain extent, the support rod rotates on the surface of the round rod, which makes it easier to support the drone through the support rod, thereby preventing the drone from tipping over to a certain extent.

[0015] Preferably, a limiting strip is fixedly connected to the side of the connecting frame away from the fixing strip.

[0016] The effect achieved by the above components is that the limiting strip prevents the support rod from rotating too much and causing the drone to tip over.

[0017] Preferably, a third spring is fixedly connected to one side of the fixing strip, and the end of the third spring away from the fixing strip is fixedly connected to the bottom of the support rod.

[0018] The effect achieved by the above components is that the support rod is pulled closer to the fixed bar by the third spring, which makes it easier to set the support rod on both sides of the landing gear.

[0019] Preferably, a second damping rod is uniformly and fixedly connected to the bottom of the landing gear, a connecting plate is fixedly connected to the bottom of the second damping rod, a second spring is sleeved on the surface of the second damping rod, the bottom of the second spring is fixedly connected to the top of the connecting plate, and the top of the second spring is fixedly connected to the bottom of the landing gear.

[0020] The effect achieved by the above components is that the second spring presses the connecting plate away from the bottom of the landing gear, so that when the landing gear falls to the ground, it can play a certain role in cushioning and prevent the main body of the drone from being hit.

[0021] A drone includes a drone body, wherein wings are evenly arranged on the sides of the drone body.

[0022] Beneficial effects

[0023] In this invention, by setting a fixing device, when using the fixing device, the fixing frame is manually slid to the bottom of the fixing block, and then the connecting strip is slid into the inside of the connecting groove. This makes it easy to set the landing gear to the bottom of the drone body, so that the landing gear can be replaced without the need for tools. Attached Figure Description

[0024] Figure 1 This utility model provides a three-dimensional structural diagram of a drone landing gear and a drone.

[0025] Figure 2 A three-dimensional structural diagram of the novel fixing frame proposed in this utility model is provided.

[0026] Figure 3 A three-dimensional structural diagram of the novel U-shaped plate proposed in this utility model is provided.

[0027] Figure 4 A three-dimensional structural diagram of the novel support rod proposed in this utility model is provided.

[0028] Legend: 1. UAV body; 2. Wing; 3. Landing gear; 4. Fixing device; 401. Fixing block; 402. Connecting groove; 403. Fixing frame; 404. Connecting strip; 405. U-shaped plate; 406. Limiting groove; 407. Limiting frame; 408. Locking groove; 409. Locking plate; 410. First damping rod; 411. First spring; 5. Protective device; 501. Second damping rod; 502. Second spring; 503. Connecting plate; 504. Fixing strip; 505. Connecting frame; 506. Round rod; 507. Support rod; 508. Limiting strip; 509. Third spring. Detailed Implementation

[0029] Example 1, such as Figure 1-4As shown, a drone landing gear and a drone are provided. The drone body 1 has wings 2 evenly arranged on its side. The drone body 1 has a landing gear 3 at its bottom and a fixing device 4 at its bottom. A protective device 5 is provided on one side of the landing gear 3. When using the drone, the wings 2 carry the drone body 1 into the air, and then the drone can be remotely controlled by remote control. This allows the drone to perform remote monitoring and other functions.

[0030] Reference Figure 2 and Figure 3 The fixing device 4 includes a fixing block 401, which is fixedly connected to the bottom of the UAV body 1. A fixing frame 403 is slidably fitted onto the surface of the fixing block 401. The bottom of the fixing frame 403 is fixedly connected to the top of the landing gear 3. A connecting groove 402 is formed on the surface of the fixing block 401. A connecting strip 404 is slidably connected to the inner wall of the connecting groove 402. The connecting strip 404 is fixedly connected to the inner wall of the fixing frame 403. When using the fixing device 4, the fixing frame 403 is manually slid to the bottom of the fixing block 401, and then the connecting strip 404 is slid into the connecting groove 402. The landing gear 3 is positioned inside the body of the UAV 1, making it easy to replace without tools. A limiting groove 406 is provided on one side of the fixing block 401. A limiting frame 407 is slidably connected to the inner wall of the limiting groove 406. A U-shaped plate 405 is fixedly connected to the bottom of the limiting frame 407. The U-shaped plate 405 is slidably fitted onto the bottom of the fixing block 401. The fixing block 401 is located on one side of the fixing frame 403. The U-shaped plate 405 can be manually slid onto the surface of the fixing block 401, thereby sliding the limiting frame 407 into the limiting groove 406. Internally, the connecting strip 404 is confined within the connecting groove 402 by the U-shaped plate 405. A locking groove 408 is provided on one side of the fixing block 401. A locking plate 409 is slidably connected to the inner wall of the locking groove 408. The locking plate 409 is slidably connected to the inner wall of the limiting frame 407. Sliding the locking plate 409 into the locking groove 408, and then into the limiting frame 407, facilitates confining the limiting frame 407 within the limiting groove 406. This, in turn, confines the U-shaped plate 405 to the surface of the fixing block 401. The locking groove 408... A first damping rod 410 is fixedly connected to one side of the wall. The end of the first damping rod 410 away from the locking groove 408 is fixedly connected to one side of the locking plate 409. A first spring 411 is sleeved on the surface of the first damping rod 410. One end of the first spring 411 is fixedly connected to one side of the inner wall of the locking groove 408. The end of the first spring 411 near the first damping rod 410 is fixedly connected to one side of the locking plate 409. The locking plate 409 is pulled towards the locking groove 408 by the first spring 411, thereby making it easier to restrict the locking plate 409 inside the locking groove 408.

[0031] Reference Figure 4The protective device 5 includes a support rod 507. A fixing strip 504 is fixedly connected to one side of the landing gear 3. A connecting frame 505 is fixedly connected to the side of the fixing strip 504 away from the landing gear 3. A round rod 506 is fixedly connected to the inner wall of the connecting frame 505. The support rod 507 rotates on the surface of the round rod 506. When the protective device 5 is used, if the drone is landing and tilted, the support rod 507 rotates on the surface of the round rod 506, thus supporting the drone and preventing it from tipping over to some extent. A limit strip 508 is fixedly connected to the side of the connecting frame 505 away from the fixing strip 504. The limit strip 508 prevents the support rod 507 from rotating too much and causing the drone to tip over. A third spring 5 is fixedly connected to one side of the fixing strip 504. 09. The end of the third spring 509 away from the fixing bar 504 is fixedly connected to the bottom of the support rod 507. The third spring 509 pulls the support rod 507 towards the fixing bar 504, which facilitates the placement of the support rod 507 on both sides of the landing gear 3. The bottom of the landing gear 3 is evenly fixedly connected to the second damping rod 501. The bottom of the second damping rod 501 is fixedly connected to the connecting plate 503. The surface of the second damping rod 501 is fitted with a second spring 502. The bottom of the second spring 502 is fixedly connected to the top of the connecting plate 503. The top of the second spring 502 is fixedly connected to the bottom of the landing gear 3. The second spring 502 presses the connecting plate 503 away from the bottom of the landing gear 3. This can provide a certain buffer when the landing gear 3 falls to the ground, which can prevent the main body of the UAV 1 from being hit.

[0032] Working principle: When using the drone, the wing 2 carries the drone body 1 into the air, and then the drone can be remotely controlled via remote control. This allows for remote monitoring and other functions. When using the fixing device 4, manually slide the fixing frame 403 to the bottom of the fixing block 401, then slide the connecting strip 404 into the inside of the connecting groove 402. Manually slide the U-shaped plate 405 onto the surface of the fixing block 401, then slide the limiting frame 407 into the inside of the limiting groove 406. Then slide the locking plate 409 into the inside of the locking groove 408. The first spring 411 pulls the locking plate 409 towards the locking groove 408, thus confining the locking plate 409 within the locking groove 408. Then, slide the locking plate 409 into the inside of the limiting frame 407, thus confining the limiting frame 407 within the limiting groove 406. The U-shaped plate 405 is constrained on the surface of the fixing block 401. This allows the connecting strip 404 to be confined inside the connecting groove 402, facilitating the placement of the landing gear 3 at the bottom of the drone body 1. This makes it easy to replace the landing gear 3 without the need for tools. When the protective device 5 is used, if the drone is landing and tilted, the support rod 507 rotates on the surface of the round rod 506. The third spring 509 pulls the support rod 507 towards the fixing strip 504, making it easier to place the support rod 507 on both sides of the landing gear 3. This allows the drone to be supported by the support rod 507, thus preventing it from tipping over to some extent. When the landing gear 3 falls to the ground, it provides a certain degree of cushioning, preventing the drone body 1 from being hit.

[0033] It should be noted that all damping rods in this case are telescopic dampers, which can absorb energy during the extension and retraction process.

Claims

1. A landing gear for an unmanned aerial vehicle (UAV), characterized in that: The device includes a landing gear (3) at the bottom of the drone body (1), a fixing device (4) at the bottom of the drone body (1), a protective device (5) on one side of the landing gear (3), and a fixing block (401) at the bottom of the drone body (1). The fixing block (401) is fixedly connected to the bottom of the drone body (1). A fixing frame (403) is slidably fitted on the surface of the fixing block (401). The bottom of the fixing frame (403) is fixedly connected to the top of the landing gear (3). A connecting groove (402) is opened on the surface of the fixing block (401). A connecting strip (404) is slidably connected to the inner wall of the connecting groove (402). The connecting strip (404) is fixedly connected to the inner wall of the fixing frame (403).

2. The unmanned aerial vehicle landing gear according to claim 1, characterized in that: A limiting groove (406) is provided on one side of the fixing block (401), and a limiting frame (407) is slidably connected to the inner wall of the limiting groove (406). A U-shaped plate (405) is fixedly connected to the bottom of the limiting frame (407), and the U-shaped plate (405) is slidably sleeved on the bottom of the fixing block (401). The fixing block (401) is located on one side of the fixing frame (403).

3. The unmanned aerial vehicle landing gear according to claim 1, characterized in that: A slot (408) is provided on one side of the fixing block (401), and a slot plate (409) is slidably connected to the inner wall of the slot (408). The slot plate (409) is slidably connected to the inner wall of the limiting frame (407).

4. The unmanned aerial vehicle landing gear according to claim 3, characterized in that: A first damping rod (410) is fixedly connected to one side of the inner wall of the slot (408). The end of the first damping rod (410) away from the slot (408) is fixedly connected to one side of the slot plate (409). A first spring (411) is sleeved on the surface of the first damping rod (410). One end of the first spring (411) is fixedly connected to one side of the inner wall of the slot (408). The end of the first spring (411) near the first damping rod (410) is fixedly connected to one side of the slot plate (409).

5. The unmanned aerial vehicle landing gear according to claim 1, characterized in that: The protective device (5) includes a support rod (507), a fixing strip (504) is fixedly connected to one side of the landing gear (3), a connecting frame (505) is fixedly connected to the side of the fixing strip (504) away from the landing gear (3), a round rod (506) is fixedly connected to the inner wall of the connecting frame (505), and the support rod (507) is rotated and sleeved on the surface of the round rod (506).

6. The unmanned aerial vehicle landing gear according to claim 5, characterized in that: A limiting strip (508) is fixedly connected to the side of the connecting frame (505) away from the fixing strip (504).

7. The unmanned aerial vehicle landing gear according to claim 5, characterized in that: A third spring (509) is fixedly connected to one side of the fixing bar (504), and the end of the third spring (509) away from the fixing bar (504) is fixedly connected to the bottom of the support rod (507).

8. The unmanned aerial vehicle landing gear according to claim 1, characterized in that: The landing gear (3) is uniformly and fixedly connected to a second damping rod (501). The bottom of the second damping rod (501) is fixedly connected to a connecting plate (503). A second spring (502) is sleeved on the surface of the second damping rod (501). The bottom of the second spring (502) is fixedly connected to the top of the connecting plate (503). The top of the second spring (502) is fixedly connected to the bottom of the landing gear (3).

9. An unmanned aerial vehicle (UAV), characterized in that: It includes a drone body (1), wherein the drone body (1) has wings (2) evenly arranged on its sides.

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