A low-cost simple UAV with a pod structure

By installing mechanical components and counterweight mechanisms that adjust specific gravity on the fixture of the drone, the shaking problem caused by wind power when transporting liquids is solved, and the stability and safety of the drone are improved.

CN116692011BActive Publication Date: 2025-06-06PLA AIR FORCE AVIATION UNIVERSITY
View PDF 3 Cites 0 Cited by

Patent Information

Application Number
CN202310760000.0
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2023-06-26
Publication Date
2025-06-06
Estimated Expiration
2043-06-26

AI Technical Summary

Technical Problem

When existing drone pods transport liquid, the liquid shakes due to wind power, which may cause uneven weight at both ends of the pod, affecting the stability of the drone, and even causing falls.

Method used

By installing the first guide rod, the first slider, the first spring and the limiting column on the fixing frame of the drone, the specific gravity of the pod is adjusted to reduce liquid shaking; at the same time, the counterweight mechanism that is matched with the dovetail slot and the dovetail card plate is used to select the counterweight block according to the weight of the cargo in the pod, match the weight of the liquid, and improve stability.

Benefits of technology

It effectively avoids large shaking of liquid in the pod, improves the stability of the drone, prevents falls caused by uneven weight, and improves the stability and safety of the pod through the use of the counterweight mechanism.

✦ Generated by Eureka AI based on patent content.

Smart Images

  • Figure CN116692011B_ABST
    Figure CN116692011B_ABST
Patent Text Reader

Abstract

The present invention provides a low-cost simple UAV with a pod structure, comprising a UAV body, a first slider being sleeved on the outer wall of the first guide rod, a connecting rod being rotatably installed inside the first rotating seat, a limiting column being fixedly installed on the inner wall of the second groove, the connecting rod being rotatably installed in the second groove through the limiting column and the first limiting groove, a second guide rod being fixedly installed on the inner wall of the third groove, a second slider being sleeved on the outer wall of the second guide rod, an extension rod being fixedly installed on one side of the second slider, one end of the extension rod passing through one end of the connecting rod and being installed with a counterweight mechanism, a mounting mechanism being fixedly installed on the bottom of the first slider, and by adjusting the front and rear specific gravity of the UAV body when the front and rear weights of the pod are uneven, it is possible to avoid a large shaking amplitude of the liquid in the pod, to improve the stability of the UAV body to a certain extent, and to prevent the UAV body from falling due to uneven weight.
Need to check novelty before this filing date? Find Prior Art

Description

Technical Field

[0001] The invention relates to the technical field of unmanned aerial vehicle pods, and in particular to a low-cost simple unmanned aerial vehicle with a pod structure. Background Art

[0002] With the maturity of drone technology, the application scope of drones is becoming wider and wider. For example, in order to solve the problem of the last mile of logistics transportation, people have proposed to use drones to transport goods. The way to use drones to transport goods is usually to load the goods into the cargo hold of the drone. At present, the society's demand for easy-to-disassemble logistics drone pods basically meets people's needs, but there are still some problems. Drone pods are a mission payload installed on drones, mainly used for drones to transport and deliver materials. Traditional drone pods have complex structural designs, a large number of parts, high processing difficulty, and high subsequent assembly difficulty; when used, cargo loading is complex and inefficient, which increases the cost of use. Because the traditional drone pod structure contains too many parts and the overall structure is very complex, the pod is easily damaged after the delivery mission is completed. Due to the high cost of the pod itself, a lot of repairs and secondary use are required, which further increases the cost of use.

[0003] A low-cost simple drone pod structure provided by the publication number "CN114229010A" includes a pod, a lug is arranged on the upper part of the pod, and the surface of the pod is wrapped by a waterproof layer; an opening is arranged at the rear of the pod, and the waterproof layer forms a plurality of folding structures at the opening; the pod includes an upper pod and a lower pod, the upper pod and the lower pod are arranged opposite to each other and connected and fixed by a fastening structure, a storage space is formed between the upper pod and the lower pod, a buffer is arranged at the front end of the storage space, and a main support beam is arranged at the top of the storage space, and the two ends of the main support beam are respectively provided with a front support member and a rear support member. The present invention can increase the amount of cargo carried by the drone; after being dropped, the impact on the pod body is minimized by the flexible buffer member to avoid damage to the pod and improve the protection of the internal cargo; the pod has high processing and assembly efficiency, reduces the use cost, and makes drone cargo transportation more economical.

[0004] However, the above device still has the following problems during implementation:

[0005] There is still room for improvement in the pods used by drones. While meeting the load-bearing capacity of the pod, the existing device may transport liquids when in use. However, when the pod loaded with liquid is in operation, the drone is easily affected by wind in the air, which can cause the liquid to sway back and forth in the pod, and may even cause the liquid to move to one side, resulting in uneven weight on both ends of the pod, causing the drone to lose stability and easily cause the drone to fall. Therefore, a more reasonable technical solution should be proposed to optimize and improve drones with pods and solve the technical problems existing in the prior art. Summary of the invention

[0006] The purpose of the present invention is to provide a low-cost simple UAV with a pod structure to solve the problems raised in the above background technology.

[0007] To achieve the above object, the present invention provides the following technical solutions:

[0008] A low-cost simple drone with a pod structure comprises a drone body, a fixing frame is fixedly installed at the bottom of the drone body, a first groove is provided inside the fixing frame, a first guide rod is fixedly installed on the inner wall of the first groove, a first slider is sleeved on the outer wall of the first guide rod, first springs are fixedly installed on both sides of the first slider, one end of the first spring away from the first slider is fixedly installed on the inner wall of the first groove, a first rotating seat is fixedly installed on both sides of the first slider, a connecting rod is rotatably installed inside the first rotating seat, second grooves are provided on the inner walls of both sides of the first groove, a limiting column is fixedly installed on the inner wall of the second groove, a first limiting groove is provided inside the connecting rod, and the connecting rod is rotatably installed in the second groove through the limiting column and the first limiting groove;

[0009] A third groove is formed on the inner walls on both sides of the first limiting groove, a second guide rod is fixedly installed on the inner wall of the third groove, a second slider is sleeved on the outer wall of the second guide rod, a second spring is fixedly installed on one side of the second slider, and the second spring is fixedly installed on the inner wall of the third groove at one end away from the second slider, an extension rod is fixedly installed on one side of the second slider, one end of the extension rod passes through one end of the connecting rod and is installed with a counterweight mechanism, a mounting mechanism is fixedly installed on the bottom of the first slider, and a pod body is installed on the bottom of the mounting mechanism.

[0010] Preferably, the counterweight mechanism comprises a dovetail slot, which is arranged at one end of the extension rod away from the second slider, a dovetail clamping plate is clamped on the inner wall of the dovetail slot, and a counterweight block is fixedly mounted on one side of the dovetail clamping plate.

[0011] Preferably, the mounting mechanism comprises a second rotating seat, the second rotating seat is fixedly mounted on the bottom of the first sliding block, and a fixed seat is rotatably mounted inside the second rotating seat.

[0012] Preferably, a support plate is fixedly installed on the bottom of the fixed seat, and a first mounting seat and a second mounting seat are fixedly installed on the bottom of the support plate respectively, a sliding groove is provided inside the first mounting seat, and fourth grooves are provided on both sides of the sliding groove.

[0013] Preferably, a third guide rod is fixedly mounted on the inner wall of the fourth groove, a third slider is sleeved on the outer wall of the third guide rod, a third spring is fixedly mounted on one side of the third slider, and one end of the third spring away from the third slider is fixedly mounted on the inner wall of the fourth groove.

[0014] Preferably, a connecting plate is fixedly installed on one side of the third sliding block, a first plug rod is installed through the inside of the connecting plate, a handle is fixedly installed on one end of the first plug rod, the end of the first plug rod away from the handle is conical, a mounting frame is provided on the outer wall of the first plug rod, and the pod body is fixedly installed on the bottom of the mounting frame.

[0015] Preferably, a sliding groove is also provided inside the second mounting seat, and fifth grooves are provided on both sides of the sliding groove in the second mounting seat, and a fourth guide rod is fixedly installed on the inner wall of the fifth groove.

[0016] Preferably, a fourth sliding block is sleeved on the outer wall of the fourth guide rod, a fourth spring is fixedly mounted on one side of the fourth sliding block, and one end of the fourth spring away from the fourth sliding block is fixedly mounted on the inner wall of the fifth groove.

[0017] Preferably, a second plug rod is fixedly mounted on one side of the fourth sliding block, and one end of the second plug rod passes through the bottom of the second mounting seat and is also fixedly connected to a handle.

[0018] Preferably, a slot is also provided inside the second mounting seat, the slot is matched with the tapered end of the first plug rod, a second limiting groove is provided at the bottom of the tapered end of the first plug rod, and the second limiting groove is matched with the top end of the second plug rod.

[0019] Compared with the prior art, the present invention has the following beneficial effects:

[0020] 1. Through the cooperation of the first guide rod, the first spring, the limit column, the second guide rod, the second slider, the second spring, the extension rod and the components in the counterweight mechanism, the front and rear specific gravity of the drone body can be adjusted when the front and rear weights of the pod are uneven, which can avoid a large shaking amplitude of the liquid in the pod, and can improve the stability of the drone body to a certain extent, and can prevent the drone body from falling due to uneven weight;

[0021] 2. The dovetail slot and the dovetail plate cooperate with each other, so that the counterweight can be disassembled and replaced, and the counterweight can be selected according to the weight of the cargo in the pod, which can match the weight of the liquid in the pod to a certain extent, thereby improving the stability of the device;

[0022] 3. Through the cooperation of various components in the installation mechanism, the pod can be conveniently locked and installed, which can prevent the pod from falling to a certain extent, thereby protecting the people below to a certain extent and avoiding the occurrence of danger to a certain extent. BRIEF DESCRIPTION OF THE DRAWINGS

[0023] Figure 1 It is a schematic diagram of the three-dimensional structure of the present invention;

[0024] Figure 2 It is a schematic diagram of a first partial three-dimensional structure of the present invention;

[0025] Figure 3 It is a schematic diagram of a second partial three-dimensional structure of the present invention;

[0026] Figure 4 It is a schematic diagram of a first partial cross-sectional three-dimensional structure of the present invention;

[0027] Figure 5 For the present invention Figure 4 A is a schematic diagram of the enlarged structure of the middle part;

[0028] Figure 6 It is a schematic diagram of a third partial three-dimensional structure of the present invention;

[0029] Figure 7 is a schematic diagram of a fourth partial three-dimensional structure of the present invention;

[0030] Figure 8 is a schematic diagram of a fifth partial three-dimensional structure of the present invention;

[0031] Fig. 9 It is a schematic diagram of a second partial cross-sectional three-dimensional structure of the present invention;

[0032] Fig.10 For the present invention Fig. 9 Schematic diagram of the enlarged structure of B;

[0033] Fig.11 It is a schematic diagram of a third partial cross-sectional three-dimensional structure of the present invention;

[0034] Fig.12 For the present invention Fig.11 Schematic diagram of the enlarged structure of C;

[0035] Fig.13 It is a sixth partial three-dimensional structural schematic diagram of the present invention.

[0036] In the figure: 101, drone body; 102, fixing frame; 103, first guide rod; 104, first slider; 105, first spring; 106, first rotating seat; 107, connecting rod; 108, limiting column; 109, second guide rod; 110, second slider; 111, second spring; 112, extension rod; 113, pod body; 200, counterweight mechanism; 201, dovetail clamp; 202, counterweight block; 300, mounting mechanism; 301, second rotating seat; 302, fixing seat; 303, supporting plate; 304, first mounting seat; 305, second mounting seat; 306, third guide rod; 307, third slider; 308, third spring; 309, connecting plate; 310, first plug rod; 311, mounting frame; 312, fourth guide rod; 313, fourth slider; 314, fourth spring; 315, second plug rod. DETAILED DESCRIPTION

[0037] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0038] See also Figure 1-13 , the present invention provides a technical solution: Example

[0039] A low-cost simple drone with a pod structure comprises a drone body 101, a fixing frame 102 is fixedly installed at the bottom of the drone body 101, a first groove is provided inside the fixing frame 102, a first guide rod 103 is fixedly installed on the inner wall of the first groove, a first slider 104 is sleeved on the outer wall of the first guide rod 103, first springs 105 are fixedly installed on both sides of the first slider 104, one end of the first spring 105 away from the first slider 104 is fixedly installed on the inner wall of the first groove, first rotating seats 106 are fixedly installed on both sides of the first slider 104, a connecting rod 107 is rotatably installed inside the first rotating seat 106, second grooves are provided on the inner walls of both sides of the first groove, limiting columns 108 are fixedly installed on the inner wall of the second groove, a first limiting groove is provided inside the connecting rod 107, and the connecting rod 107 is fixedly installed through the limiting columns 108 The first limit groove is rotatably installed in the second groove. When the drone body 101 is flying in the air with the pod body 113, once it encounters airflow, the liquid will slosh in the pod body 113, which will cause the drone body 101 and the pod body 113 to tilt. During the tilting process, the pod body 113 will control the first slider 104 to slide on the first guide rod 103. The first slider 104 will squeeze one first spring 105 and stretch another first spring 105. During the sliding process, the first slider 104 can drive the first rotating seat 106 to move. During the movement of the first rotating seat 106, one end of the connecting rod 107 will be driven to rotate in the first rotating seat 106, and at the same time, the connecting rod 107 will be controlled to slide on the outer wall of the limiting column 108 through the first limit groove.

[0040] The inner walls on both sides of the first limiting groove are provided with third grooves, the inner wall of the third groove is fixedly installed with a second guide rod 109, the outer wall of the second guide rod 109 is sleeved with a second slider 110, a second spring 111 is fixedly installed on one side of the second slider 110, and the second spring 111 is fixedly installed on the inner wall of the third groove away from one end of the second slider 110, an extension rod 112 is fixedly installed on one side of the second slider 110, one end of the extension rod 112 passes through one end of the connecting rod 107 and is installed with a counterweight mechanism 200, a mounting mechanism 300 is fixedly installed at the bottom of the first slider 104, and a pod body 113 is installed at the bottom of the mounting mechanism 300, and when the connecting rod 107 slides on the outer wall of the limiting column 108, one end of the extension rod 112 will press the limiting column 108 The second slider 110 can slide on the second guide rod 109 during the movement of the extension rod 112, and the second slider 110 can squeeze the second spring 111 during the sliding process, so that the counterweight mechanism 200 can be controlled to match the liquid in the pod body 113. The counterweight mechanism 200 can be selected according to the weight of the goods in the pod, and can match the weight of the liquid in the pod body 113 to a certain extent, so as to improve the stability of the device. The installation mechanism 300 can facilitate the installation of the pod body 113, and can prevent the pod body 113 from falling to a certain extent, so as to avoid the occurrence of danger. Example

[0041] On the basis of Example 1, this example describes the counterweight mechanism 200 in Example 1. The counterweight mechanism 200 includes a dovetail slot, which is arranged at the end of the extension rod 112 away from the second slider 110. A dovetail clamping plate 201 is clamped on the inner wall of the dovetail slot. A counterweight block 202 is fixedly installed on one side of the dovetail clamping plate 201. The counterweight block 202 can be easily installed and disassembled through the cooperation between the limiting slot and the dovetail clamping plate 201, so as to match the weight of the liquid in the pod body 113. Example

[0042] Based on the first embodiment, this embodiment describes the installation mechanism 300 in the first embodiment.

[0043] The mounting mechanism 300 includes a second rotating seat 301, which is fixedly mounted on the bottom of the first slider 104, a fixed seat 302 is rotatably mounted inside the second rotating seat 301, a support plate 303 is fixedly mounted on the bottom of the fixed seat 302, a first mounting seat 304 and a second mounting seat 305 are fixedly mounted on the bottom of the support plate 303, a sliding groove is provided inside the first mounting seat 304, fourth grooves are provided on both sides of the sliding groove, a third guide rod 306 is fixedly mounted on the inner wall of the fourth groove, a third slider 307 is sleeved on the outer wall of the third guide rod 306, a third spring 308 is fixedly mounted on one side of the third slider 307, an end of the third spring 308 away from the third slider 307 is fixedly mounted on the inner wall of the fourth groove, and a connecting rod 306 is fixedly mounted on one side of the third slider 307 The connecting plate 309 has a first plug rod 310 installed inside it, a handle is fixedly installed at one end of the first plug rod 310, and the end of the first plug rod 310 away from the handle is tapered. A mounting frame 311 is sleeved on the outer wall of the first plug rod 310, and a slot matching the first plug rod 310 is opened inside the mounting frame 311. The pod body 113 is fixedly installed at the bottom of the mounting frame 311. The user can pull the handle. In the process of pulling the handle, the connecting plate 309 can be pulled, and the first plug rod 310 can be pulled at the same time. During the movement of the first plug rod 310, the third slider 307 can be driven to slide on the third guide rod 306, and the third slider 307 can compress the third spring 308 during the movement.

[0044] The second mounting seat 305 is also provided with a sliding groove, and both sides of the sliding groove in the second mounting seat 305 are provided with fifth grooves, the inner wall of the fifth groove is fixedly installed with a fourth guide rod 312, the outer wall of the fourth guide rod 312 is sleeved with a fourth sliding block 313, a fourth spring 314 is fixedly installed on one side of the fourth sliding block 313, and the fourth spring 314 is fixedly installed on the inner wall of the fifth groove at one end away from the fourth sliding block 313, and a second plug rod 315 is fixedly installed on one side of the fourth sliding block 313, and one end of the second plug rod 315 passes through the bottom of the second mounting seat 305 and is also fixedly connected to a handle, and a slot is also provided inside the second mounting seat 305, and the slot is matched with the tapered end of the first plug rod 310, and a second limiting slot is provided at the bottom of the tapered end of the first plug rod 310, and the second limiting slot is matched with the top of the second plug rod 315. When the first plug rod 310 moves to a certain position, the mounting bracket 311 at the top of the pod body 113 is then mounted on the first The third slider 307 drives the connecting plate 309 and the first rod 310 to move toward the mounting bracket 311, and then passes through the slot into the slot of the second mounting seat 305, and then pulls the handle at the bottom of the second rod 315, and then pulls the second rod 315. During the movement, the second rod 315 can control the fourth slider 313 to slide on the fourth guide rod 312 and squeeze the fourth spring 314. When the second limiting groove at the bottom of the first rod 310 moves above the second rod 315, the second rod 315 is released, and under the action of the fourth spring 314, the second rod 315 enters the second limiting groove to lock the first rod 310, so that the pod body 113 can be installed conveniently to prevent the pod body 113 from falling.

[0045] Working principle: When the device is in use, the user can pull the handle. In the process of pulling the handle, the connecting plate 309 can be pulled, and the first plug rod 310 can be pulled at the same time. The first plug rod 310 can drive the third slider 307 to slide on the third guide rod 306 during the movement. The third slider 307 can compress the third spring 308 during the movement. When the first plug rod 310 moves to a certain position, the mounting bracket 311 on the top of the pod body 113 is then installed between the first mounting seat 304 and the second mounting seat 305. Then the handle is released. Under the action of the third spring 308, the third slider 307 will drive the connecting plate 309 and the first plug rod 310 to move toward the mounting bracket 311.

[0046] After that, the second rod 315 is pushed and the fourth slider 313 is pushed on the fourth guide rod 312, and the fourth spring 314 is squeezed. When the second limiting groove at the bottom of the first rod 310 moves to the top of the second rod 315, the second rod 315 is released. Under the action of the fourth spring 314, the second rod 315 enters the second limiting groove to lock the first rod 310. Then, the limiting groove cooperates with the dovetail card plate 201 to facilitate the installation and removal of the counterweight block 202, thereby matching the weight of the liquid in the pod body 113, and improving the stability of the device to a certain extent, so as to prevent the drone body 101 from falling due to uneven weight when driving the pod body 113 in flight.

[0047] Then, the drone body 101 is started. When the drone body 101 is flying in the air with the pod body 113, once it encounters airflow, the liquid in the pod body 113 will slosh, thereby causing the drone body 101 and the pod body 113 to tilt. During the tilting process, the pod body 113 will control the first slider 104 to slide on the first guide rod 103, and the first slider 104 will squeeze one first spring 105 and stretch the other first spring 105 at the same time. During the sliding process, the first slider 104 can drive the first rotating seat 106 to move, and during the movement of the first rotating seat 106, it will drive the connecting rod 104 to move. One end of the rod 107 rotates in the first rotating seat 106, and at the same time controls the connecting rod 107 to slide on the outer wall of the limiting column 108 through the first limiting groove. During the sliding process of the connecting rod 107 on the outer wall of the limiting column 108, one end of the extension rod 112 will resist the limiting column 108, thereby controlling the extension rod 112 to move in the first limiting groove. During the movement of the extension rod 112, it can drive the second slider 110 to slide on the second guide rod 109. During the sliding process of the second slider 110, it can squeeze the second spring 111, thereby controlling the counterweight block 202 to match the weight of the liquid in the pod body 113 under the action of the lever.

[0048] It should be noted that the drone body 101 is a device or equipment existing in the prior art, or a device or equipment that can be realized in the prior art. Its power supply, specific composition and principle are clear to those skilled in the art, so they are not described in detail.

[0049] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. A low-cost simple drone with a pod structure, comprising a drone body (101), Features: A fixing frame (102) is fixedly mounted on the bottom of the drone body (101), a first groove is provided inside the fixing frame (102), a first guide rod (103) is fixedly mounted on the inner wall of the first groove, a first slider (104) is sleeved on the outer wall of the first guide rod (103), first springs (105) are fixedly mounted on both sides of the first slider (104), one end of the first spring (105) away from the first slider (104) is fixedly mounted on the inner wall of the first groove, first rotating seats (106) are fixedly mounted on both sides of the first slider (104), a connecting rod (107) is rotatably mounted inside the first rotating seat (106), second grooves are provided on both sides of the inner walls of the first groove, a limiting column (108) is fixedly mounted on the inner wall of the second groove, a first limiting groove is provided inside the connecting rod (107), and the connecting rod (107) is rotatably mounted in the second groove through the limiting column (108) and the first limiting groove; A third groove is formed on the inner walls of both sides of the first limiting groove, a second guide rod (109) is fixedly mounted on the inner wall of the third groove, a second slider (110) is sleeved on the outer wall of the second guide rod (109), a second spring (111) is fixedly mounted on one side of the second slider (110), an end of the second spring (111) away from the second slider (110) is fixedly mounted on the inner wall of the third groove, an extension rod (112) is fixedly mounted on one side of the second slider (110), one end of the extension rod (112) passes through one end of the connecting rod (107) and is mounted with a counterweight mechanism (200), a mounting mechanism (300) is fixedly mounted on the bottom of the first slider (104), and a pod body (113) is mounted on the bottom of the mounting mechanism (300).

2. A low-cost simple UAV with a pod structure according to claim 1, Features: The counterweight mechanism (200) comprises a dovetail slot, the dovetail slot being formed at an end of the extension rod (112) away from the second slider (110), a dovetail clamping plate (201) being clamped onto the inner wall of the dovetail slot, and a counterweight block (202) being fixedly mounted on one side of the dovetail clamping plate (201).

3. A low-cost simple UAV with a pod structure according to claim 1, Features: The mounting mechanism (300) comprises a second rotating seat (301), the second rotating seat (301) being fixedly mounted on the bottom of the first sliding block (104), and a fixed seat (302) being rotatably mounted inside the second rotating seat (301).

4. A low-cost simple UAV with a pod structure according to claim 3, Features: A support plate (303) is fixedly mounted on the bottom of the fixed seat (302), and a first mounting seat (304) and a second mounting seat (305) are respectively fixedly mounted on the bottom of the support plate (303), a sliding groove is provided inside the first mounting seat (304), and fourth grooves are provided on both sides of the sliding groove; A third guide rod (306) is fixedly mounted on the inner wall of the fourth groove, a third slider (307) is sleeved on the outer wall of the third guide rod (306), a third spring (308) is fixedly mounted on one side of the third slider (307), and one end of the third spring (308) away from the third slider (307) is fixedly mounted on the inner wall of the fourth groove; A connecting plate (309) is fixedly mounted on one side of the third sliding block (307), a first plug rod (310) is installed through the interior of the connecting plate (309), a handle is fixedly mounted on one end of the first plug rod (310), an end of the first plug rod (310) away from the handle is tapered, a mounting frame (311) is sleeved on the outer wall of the first plug rod (310), and the pod body (113) is fixedly mounted on the bottom of the mounting frame (311).

5. A low-cost simple UAV with a pod structure according to claim 4, Features: A sliding groove is also provided inside the second mounting seat (305), and fifth grooves are provided on both sides of the sliding groove in the second mounting seat (305), and a fourth guide rod (312) is fixedly installed on the inner wall of the fifth groove; A fourth slider (313) is sleeved on the outer wall of the fourth guide rod (312), a fourth spring (314) is fixedly mounted on one side of the fourth slider (313), and an end of the fourth spring (314) away from the fourth slider (313) is fixedly mounted on the inner wall of the fifth groove; A second insertion rod (315) is fixedly mounted on one side of the fourth sliding block (313); one end of the second insertion rod (315) passes through the bottom of the second mounting seat (305) and is also fixedly connected to a handle; A slot is also provided inside the second mounting seat (305), and the slot is matched with the tapered end of the first insertion rod (310). A second limiting groove is provided at the bottom of the tapered end of the first insertion rod (310), and the second limiting groove is matched with the top of the second insertion rod (315).

Citation Information

Patent Citations

  • Low-cost simple unmanned aerial vehicle pod structure

    CN114229010A

  • Dynamic counterweight balancing system for autostability of unmanned aerial vehicle and balancing method thereof

    CN110217381A

  • Oil-driven unmanned aerial vehicle control method and device

    CN112829927A