Quick-balancing flying sky curtain unmanned aerial vehicle suspension mechanism
By introducing a synchronous motion mechanism of synchronous belt and counterweight blocks into the flying sky curtain suspension mechanism, the problem of slow balance adjustment speed of traditional flying sky curtain is solved, and rapid balance adjustment and improvement of use effect is achieved, while optimizing the aesthetics of the equipment and the screen Protect.
Patent Information
- Application Number
- CN202421290378.5
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-06-06
- Publication Date
- 2025-01-10
- Estimated Expiration
- 2034-06-06
AI Technical Summary
The balance adjustment speed of traditional flying sky curtain is slow, resulting in poor use.
A fast balanced flying sky curtain drone suspension mechanism including suspension, adjustment structure and motor-driven is designed to quickly adjust the center of gravity of the flying sky curtain through the coordinated movement of the synchronous belt and counterweight block.
The flying sky curtain is quickly adjusted to a balanced state when it loses balance, improving the use effect, and avoiding screen damage and aesthetic improvement through the support structure.
Smart Images
Figure CN222329993U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to a flying canopy unmanned aerial vehicle suspension mechanism, in particular to a fast-balancing flying canopy unmanned aerial vehicle suspension mechanism, and belongs to the technical field of flying canopy components. Background Art
[0002] A flying sky dome refers to a display screen mounted on a drone. The display screen is made to fly into the air under the action of the drone to display content. By arranging the display screen according to specific rules, some special content can be displayed. Generally, a flying sky dome is mainly composed of a drone, a suspension and a screen. The drone is installed on the suspension, and a screen is installed at the bottom of the suspension.
[0003] However, most traditional flying canopies are balanced by adjusting the rotors of drones. This method is slow to adjust and is not convenient for rapid balancing, resulting in poor use effects. Utility Model Content
[0004] The purpose of the utility model is to provide a fast-balancing flying canopy UAV suspension mechanism in order to solve the above-mentioned problem, which can quickly adjust the balance of the flying canopy, thereby improving the use effect.
[0005] The utility model achieves the above-mentioned purpose through the following technical solutions: a fast-balancing flying canopy UAV suspension mechanism, comprising a suspension, an adjustment structure provided on the suspension, the adjustment structure comprising a connecting frame and a first connecting shaft, the top end of the suspension is fixedly connected to the connecting frame, the connecting frame is rotatably connected to two first connecting shafts, a first motor is installed on the connecting frame, the output shaft of the first motor is fixedly connected to one of the first connecting shafts, a first synchronous wheel is fixedly connected to the first connecting shaft, a first synchronous belt is wound around the two first synchronous wheels, two first counterweights are slidably connected to the connecting frame, the two first counterweights are fixedly connected to one side of the first synchronous belt, two second connecting shafts are rotatably connected to the connecting frame, a second motor is installed on the connecting frame, the output shaft of the second motor is fixedly connected to one of the second connecting shafts, a second synchronous wheel is fixedly connected to the second connecting shaft, the same second synchronous belt is wound around the two second synchronous wheels, two second counterweights are slidably connected to the connecting frame, and the two second counterweights are fixedly connected to one side of the second synchronous belt.
[0006] Preferably, the connecting frame is in a cross-shaped structure, and the first synchronous belt and the second synchronous belt are arranged in an alternating manner.
[0007] Preferably, the axis of the first connecting shaft and the axis of the second connecting shaft are perpendicular to each other, and the movement directions of the first counterweight block and the second counterweight block are perpendicular to each other.
[0008] Preferably, the two first counterweights move in the same direction, and the two second counterweights move in the same direction.
[0009] Preferably, a drone is installed on the top of the suspension, and four sets of rotors are installed on the drone.
[0010] Preferably, a plurality of batteries are mounted on the suspension, and a screen is mounted at the bottom end of the suspension.
[0011] Preferably, a support structure is provided on the suspension, and the support structure includes an electric push rod and a cross bar. Two electric push rods are installed on the suspension, and the ends of the electric push rods are fixedly connected to the cross bar.
[0012] Preferably, four sliding rods are fixedly connected to the cross bar, the sliding rods are slidably connected to the sliding sleeves, the sliding sleeves are fixedly connected to the suspension, the sliding rods are rotatably connected to the connecting rods, one end of the connecting rods is rotatably connected to the support rods, and the support rods are rotatably connected to the suspension.
[0013] Preferably, the support rod is in a bent structure, and the end of the sliding rod is in an L-shaped structure.
[0014] Preferably, one end of the electric push rod is located in the middle of the cross bar, and the middle of the cross bar is in a T-shaped structure.
[0015] The beneficial effect of the utility model is that when the flying canopy loses balance in the air, the first motor can be started, and the output shaft of the first motor rotates to start one of the first connecting shafts to rotate. The rotation of the first connecting shaft drives the first synchronous wheel to rotate. The rotation of the first synchronous wheel will drive the first synchronous belt to move. The movement of the first synchronous belt will drive the two first counterweights to move in the same direction. At the same time as the output shaft of the first motor rotates, the output shaft of the second motor can also rotate. The rotation of the output shaft of the second motor will drive one of the second connecting shafts to rotate. The rotation of the second connecting shaft will drive the second synchronous wheel to rotate. The rotation of the second synchronous wheel will drive the second synchronous belt to move. The movement of the second synchronous belt will drive the two second counterweights to move in the same direction. The center of gravity of the flying canopy can be quickly changed through the synchronous movement of the two first counterweights and the two second counterweights. When the flying canopy loses balance, it can be quickly adjusted to a balanced state, thereby improving the effect of use. BRIEF DESCRIPTION OF THE DRAWINGS
[0016] Figure 1 It is a schematic diagram of the overall structure of the utility model;
[0017] Figure 2 for Figure 1 An enlarged schematic diagram of part A is shown;
[0018] Figure 3 for Figure 1 An enlarged schematic diagram of part B is shown;
[0019] Figure 4 for Figure 1 An enlarged schematic diagram of part C is shown;
[0020] Figure 5 for Figure 1 An enlarged schematic diagram of part D is shown.
[0021] In the figure: 1. suspension; 2. adjustment structure; 201. connecting frame; 202. first motor; 203. first connecting shaft; 204. first synchronous wheel; 205. first synchronous belt; 206. first counterweight; 207. second motor; 208. second connecting shaft; 209. second synchronous wheel; 210. second synchronous belt; 211. second counterweight; 3. drone; 4. rotor; 5. battery; 6. screen; 7. supporting structure; 701. electric push rod; 702. cross bar; 703. sliding rod; 704. sliding sleeve; 705. connecting rod; 706. supporting rod. DETAILED DESCRIPTION
[0022] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.
[0023] See also Figure 1 , Figure 2 and Figure 3As shown, a fast-balancing flying canopy UAV suspension mechanism comprises a suspension 1, the suspension 1 is provided with an adjustment structure 2, the adjustment structure 2 comprises a connecting frame 201 and a first connecting shaft 203, the top of the suspension 1 is fixedly connected with the connecting frame 201, the connecting frame 201 is rotatably connected with two first connecting shafts 203, a first motor 202 is installed on the connecting frame 201, the output shaft of the first motor 202 is fixedly connected to one of the first connecting shafts 203, a first synchronous wheel 204 is fixedly connected to the first connecting shaft 203, a first synchronous belt 205 is wound around the two first synchronous wheels 204, and a first synchronous belt 205 is slidably connected to the connecting frame 201. Two first counterweights 206 are fixedly connected to one side of the first synchronous belt 205. Two second connecting shafts 208 are rotatably connected to the connecting frame 201. A second motor 207 is installed on the connecting frame 201. The output shaft of the second motor 207 is fixedly connected to one of the second connecting shafts 208. A second synchronous wheel 209 is fixedly connected to the second connecting shaft 208. The same second synchronous belt 210 is wound around the two second synchronous wheels 209. Two second counterweights 211 are slidably connected to the connecting frame 201. The two second counterweights 211 are fixedly connected to one side of the second synchronous belt 210.
[0024] As a technical optimization solution of the utility model, Figure 1 , Figure 2 and Figure 3 As shown, the connecting frame 201 has a cross-shaped structure, the first synchronous belt 205 and the second synchronous belt 210 are staggered, the axis of the first connecting shaft 203 and the axis of the second connecting shaft 208 are perpendicular to each other, the movement directions of the first counterweight block 206 and the second counterweight block 211 are perpendicular to each other, the movement directions of the two first counterweight blocks 206 are the same, and the movement directions of the two second counterweight blocks 211 are the same, so the balance of the flying canopy can be quickly adjusted by the perpendicular movement of the first counterweight block 206 and the second counterweight block 211.
[0025] As a technical optimization solution of the utility model, Figure 1 As shown, a drone 3 is installed on the top of the suspension 1, and four sets of rotors 4 are installed on the drone 3, so that the flying sky curtain can be lifted into the air to display the content.
[0026] As a technical optimization solution of the utility model, Figure 1 As shown, a plurality of batteries 5 are installed on the suspension 1 , and a screen 6 is installed at the bottom end of the suspension 1 , so that the flying canopy can be powered by the batteries 5 .
[0027] As a technical optimization solution of the utility model, Figure 1 and Figure 4 As shown, the suspension 1 is provided with a support structure 7, and the support structure 7 includes an electric push rod 701 and a cross bar 702. Two electric push rods 701 are installed on the suspension 1, and the ends of the electric push rods 701 are fixedly connected to the cross bar 702, and four sliding rods 703 are fixedly connected to the cross bar 702, and the sliding rod 703 is slidably connected to the sliding sleeve 704, and the sliding sleeve 704 is fixedly connected to the suspension 1, and a connecting rod 705 is rotatably connected to the sliding rod 703, and one end of the connecting rod 705 is rotatably connected to a support rod 706, and the support rod 706 is rotatably connected to the suspension 1, and the support rod 706 is a bent structure, and the end of the sliding rod 703 is an L-shaped structure, one end of the electric push rod 701 is located in the middle of the cross bar 702, and the middle of the cross bar 702 is a T-shaped structure. Therefore, after the flying sky curtain is launched, multiple support rods 706 can be stored, thereby improving the overall aesthetics.
[0028] When the utility model is in use, when the flying sky curtain loses balance in the air, the first motor 202 can be started, and the output shaft of the first motor 202 rotates to start one of the first connecting shafts 203 to rotate, and the rotation of the first connecting shaft 203 drives the first synchronous wheel 204 to rotate, and the rotation of the first synchronous wheel 204 will drive the first synchronous belt 205 to move, and the movement of the first synchronous belt 205 will drive the two first counterweights 206 to move in the same direction, and when the output shaft of the first motor 202 rotates, the output shaft of the second motor 207 can also rotate, and the rotation of the output shaft of the second motor 207 will drive one of the second connecting shafts 208 to rotate, and the rotation of the second connecting shaft 208 will drive the second synchronous wheel 209 to rotate, and the rotation of the second synchronous wheel 209 will drive the second synchronous belt 210 to move, and the movement of the second synchronous belt 210 will drive the two second counterweights 211 to move in the same direction. By means of the synchronous movement of the two first counterweights 206 and the two second counterweights 211, the center of gravity of the flying canopy can be changed rapidly, so that when the flying canopy loses balance, it can be quickly adjusted to a balanced state, thereby improving the use effect. When the flying canopy lands, it can be supported by a plurality of support rods 706, thereby preventing the screen 6 from being directly in contact with the ground and being damaged. When the flying canopy is launched, the two electric push rods 701 can be started at the same time, and the electric push rods 701 contract to drive the cross bar 702 to move. The movement of the cross bar 702 will drive the four sliding rods 703 to slide on the sliding sleeve 704. During the movement, the sliding rods 703 will drive the support rods 706 to rotate through the connecting rods 705, thereby storing the plurality of support rods 706 on the back of the screen 6, thereby preventing the support rods 706 from being exposed during the display process, thereby effectively improving the overall aesthetics.
[0029] It is obvious to those skilled in the art that the present invention is not limited to the details of the exemplary embodiments described above, and that the present invention can be implemented in other specific forms without departing from the spirit or essential features of the present invention. Therefore, the embodiments should be regarded as exemplary and non-restrictive from any point of view, and the scope of the present invention is defined by the appended claims rather than the above description, and it is intended that all changes falling within the meaning and scope of the equivalent elements of the claims be included in the present invention. Any reference numeral in a claim should not be regarded as limiting the claim to which it relates.
[0030] In addition, it should be understood that although the present specification is described according to implementation modes, not every implementation mode contains only one independent technical solution. This description of the specification is only for the sake of clarity. Those skilled in the art should regard the specification as a whole. The technical solutions in each embodiment may also be appropriately combined to form other implementation modes that can be understood by those skilled in the art.
Claims
1. A fast-balancing flying canopy UAV suspension mechanism, comprising a suspension (1), characterized in that: The suspension (1) is provided with an adjustment structure (2), the adjustment structure (2) comprising a connecting frame (201) and a first connecting shaft (203), the top end of the suspension (1) is fixedly connected to the connecting frame (201), two first connecting shafts (203) are rotatably connected to the connecting frame (201), a first motor (202) is mounted on the connecting frame (201), an output shaft of the first motor (202) is fixedly connected to one of the first connecting shafts (203), a first synchronous wheel (204) is fixedly connected to the first connecting shaft (203), a first synchronous belt (205) is wound around the two first synchronous wheels (204), and two first counterweights (206) are slidably connected to the connecting frame (201), The two first counterweights (206) are fixedly connected to one side of the first synchronous belt (205); the connecting frame (201) is rotatably connected to two second connecting shafts (208); a second motor (207) is installed on the connecting frame (201); an output shaft of the second motor (207) is fixedly connected to one of the second connecting shafts (208); a second synchronous wheel (209) is fixedly connected to the second connecting shaft (208); the two second synchronous wheels (209) are wound with the same second synchronous belt (210); two second counterweights (211) are slidably connected to the connecting frame (201); the two second counterweights (211) are fixedly connected to one side of the second synchronous belt (210).
2. A fast-balancing flying canopy UAV suspension mechanism according to claim 1, characterized in that: The connecting frame (201) is in a cross-shaped structure, and the first synchronous belt (205) and the second synchronous belt (210) are arranged in a staggered manner.
3. A fast-balancing flying canopy UAV suspension mechanism according to claim 1, characterized in that: The axis of the first connecting shaft (203) and the axis of the second connecting shaft (208) are perpendicular to each other, and the movement directions of the first counterweight block (206) and the second counterweight block (211) are perpendicular to each other.
4. A fast-balancing flying canopy UAV suspension mechanism according to claim 1, characterized in that: The two first counterweights (206) move in the same direction, and the two second counterweights (211) move in the same direction.
5. The fast-balancing flying canopy UAV suspension mechanism according to claim 1, characterized in that: A drone (3) is installed on the top of the suspension (1), and four sets of rotors (4) are installed on the drone (3).
6. The fast-balancing flying canopy UAV suspension mechanism according to claim 1, characterized in that: A plurality of batteries (5) are installed on the suspension (1), and a screen (6) is installed at the bottom end of the suspension (1).
7. The fast-balancing flying canopy UAV suspension mechanism according to claim 1, characterized in that: The suspension (1) is provided with a support structure (7), the support structure (7) comprising an electric push rod (701) and a cross bar (702), two electric push rods (701) are installed on the suspension (1), and the ends of the electric push rods (701) are fixedly connected to the cross bar (702).
8. The fast-balancing flying canopy UAV suspension mechanism according to claim 7, characterized in that: Four sliding rods (703) are fixedly connected to the cross bar (702), the sliding rods (703) are slidably connected to the sliding sleeves (704), the sliding sleeves (704) are fixedly connected to the suspension (1), the sliding rods (703) are rotatably connected to the connecting rods (705), one end of the connecting rods (705) is rotatably connected to the supporting rods (706), and the supporting rods (706) are rotatably connected to the suspension (1).
9. A fast-balancing flying canopy UAV suspension mechanism according to claim 8, characterized in that: The support rod (706) is in a bent structure, and the end of the sliding rod (703) is in an L-shaped structure.
10. The fast-balancing flying canopy UAV suspension mechanism according to claim 8, characterized in that: One end of the electric push rod (701) is located in the middle of the cross bar (702), and the middle of the cross bar (702) is in a T-shaped structure.