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CN-224197978-U - New forms of energy unmanned aerial vehicle with anticollision function

CN224197978UCN 224197978 UCN224197978 UCN 224197978UCN-224197978-U

Abstract

The utility model provides a new energy unmanned aerial vehicle with an anti-collision function, and relates to the technical field of unmanned aerial vehicles. According to the utility model, the machine body and the wing structure are arranged, and when the equipment is used, the plurality of structures are arranged to perform cooperative movement, so that collision with obstacles can be avoided. In the aerial photography scene, obstacles of high-rise buildings can be encountered, and towers and supports can be encountered when the power line is inspected. When encountering the obstacles, the damage to the collision can be avoided, the normal flight is effectively prevented from being influenced, the task interruption caused by the collision is prevented, and therefore, the complete data cannot be acquired or the scheduled operation is completed, and the loss to related work is effectively avoided. Meanwhile, the first gear and the second gear are arranged, so that the folding storage can be carried out, collision and damage can be effectively prevented in the storage and transportation processes of the unmanned aerial vehicle, and the protectiveness of equipment can be effectively improved.

Inventors

  • YANG BO
  • WANG WEIJIAN
  • JIANG HUA
  • HUA CHEN
  • ZHANG RONGRONG
  • ZHONG YUAN
  • CAO XIAOJUAN

Assignees

  • 合肥合创技术服务有限公司

Dates

Publication Date
20260505
Application Date
20250423

Claims (8)

  1. 1. The novel energy unmanned aerial vehicle with the anti-collision function comprises a machine body (1), and is characterized in that a first wing (2) is fixedly arranged on the surface of the machine body (1), a second wing (3) is fixedly sleeved on the inner side of the first wing (2), a first rotating rod (4) is fixedly arranged at the other end of the second wing (3), a circular plate (5) is fixedly arranged on the surface of the first rotating rod (4), a groove (6) is formed in the inner side of the circular plate (5), a movable rod (7) is sleeved on the inner side of the groove (6), a first spring (8) is sleeved on the outer surface of the movable rod (7), a protection plate (9) is fixedly arranged at the other end of the movable rod (7), a fan blade (10) is fixedly arranged at the top end of the first rotating rod (4), a motor (11) is fixedly arranged in the inner side of the machine body (1), a first gear (12) is fixedly arranged at the output end of the motor (11), a placing groove (13) is formed in the inner side of the machine body (1), a ring-shaped block (14) is arranged in the inner side of the placing groove (13), a ring-shaped block (14) is fixedly arranged on the outer surface of the ring-shaped block (14), a second gear (16) is fixedly arranged on the inner side of the ring-shaped block (14), the wing is characterized in that a rotating rod II (18) is sleeved on the surface of the wing I (2), a belt pulley I (19) is fixedly arranged on the surface of the rotating rod II (18), a gear III (20) is fixedly arranged at the bottom end of the belt pulley I (19), a belt pulley II (21) is fixedly arranged at the bottom end of the wing II (3), a belt (22) is sleeved on the outer surface of the belt pulley I (19) and the outer surface of the belt pulley II (21), a fixing block I (23) is fixedly arranged at the bottom end of the machine body (1), a supporting column (24) is sleeved on the inner portion of the fixing block I (23), and a roller (25) is sleeved on the inner portion of the other end of the supporting column (24).
  2. 2. The new energy unmanned aerial vehicle with the anti-collision function according to claim 1, wherein the surface of the first gear (12) is meshed with the surface of the second gear (16), the surface of the second gear (17) is meshed with the surface of the first gear (15), and the surface of the third gear (20) is meshed with the surface of the second gear (17).
  3. 3. The new energy unmanned aerial vehicle with the anti-collision function of claim 1, wherein the number of the first wing (2), the second wing (3) and the fan blades (10) is four groups, the first wing (2) and the second wing (3) are circumferentially distributed on the surface of the engine body (1), and round corners are formed on the surfaces of the first wing (2) and the second wing (3).
  4. 4. The new energy unmanned aerial vehicle with the anti-collision function according to claim 1, wherein the protection plates (9) are arc-shaped, the number of the movable rods (7) and the springs (8) is two, the surfaces of the protection plates (9) are symmetrically distributed, and the number of the protection plates (9) is four, and the protection plates are symmetrically distributed on the surfaces of the round plates (5).
  5. 5. The new energy unmanned aerial vehicle with the anti-collision function according to claim 1, wherein one end of the first spring (8) is fixedly connected with the surface of the protection plate (9), the other end of the first spring (8) is fixedly connected with the surface of the circular plate (5), and the circular plate (5) is sleeved on the outer surface of the fan blade (10).
  6. 6. The new energy unmanned aerial vehicle with anti-collision function according to claim 1, wherein a second fixing block (26) is fixedly arranged on the surface of the supporting column (24), a second fixing cylinder (27) is fixedly arranged at the bottom end of the machine body (1), a second spring (28) is sleeved in the second fixing cylinder (27), a push rod (29) is sleeved in the second fixing cylinder (27), a fixing plate (30) is fixedly arranged at the bottom end of the push rod (29), a third fixing block (31) is fixedly arranged on the surface of the fixing plate (30), a connecting column (32) is sleeved in the third fixing block (31) and the second fixing block (26), and a movable column (33) is fixedly arranged at the bottom end of the fixing plate (30).
  7. 7. The new energy unmanned aerial vehicle with the anti-collision function of claim 6, wherein the number of the supporting columns (24), the rollers (25) and the second fixing blocks (26) is four groups, the second fixing blocks are circumferentially distributed at the bottom end of the machine body (1), and the number of the third fixing blocks (31) is four groups, and the third fixing blocks are circumferentially distributed on the surface of the fixing plate (30).
  8. 8. The new energy unmanned aerial vehicle with anti-collision function according to claim 6, wherein one end of the second spring (28) is fixedly connected with the inner top end of the fixed cylinder (27), the other end of the second spring (28) is fixedly connected with the top end of the push rod (29), round corners are formed at two ends of the connecting column (32), and the bottom end of the moving column (33) is round.

Description

New forms of energy unmanned aerial vehicle with anticollision function Technical Field The utility model relates to the technical field of unmanned aerial vehicles, in particular to a new energy unmanned aerial vehicle with an anti-collision function. Background Along with the continuous development of technology and the increasing environmental awareness, the new energy unmanned aerial vehicle is widely applied in various fields, such as aerial photography, inspection, agricultural plant protection and the like. By means of environment protection, high-efficiency energy utilization mode and flexible flying performance, bringing convenience to various industries. However, in the actual use process, the new energy unmanned aerial vehicle also faces some problems. On the one hand, unmanned aerial vehicle is in the flight, especially when carrying out the task under the complex environment, very easy collision with the obstacle. For example, in an aerial scene, obstacles such as high-rise buildings, trees and the like may be encountered, and facilities such as towers and supports may be encountered when inspecting power lines or pipelines. In case of collision, the unmanned aerial vehicle can be damaged, normal flight and service life of the unmanned aerial vehicle are affected, tasks can be possibly interrupted, complete data can not be obtained or preset operation can not be completed, and loss is brought to related work. On the other hand, in unmanned aerial vehicle's storage and transportation, its comparatively fragile parts, such as wing, flabellum etc. also easily damage because of colliding with. Traditional unmanned aerial vehicle often does not fully consider these circumstances in structural design, lacks effectual anticollision and accomodate protection mechanism. However, in the case of the conventional apparatus, the conventional apparatus is easily collided with an obstacle during a flight, particularly, when performing a task in a complex environment. For example, in an aerial scene, obstacles such as high-rise buildings, trees and the like may be encountered, and facilities such as towers and supports may be encountered when inspecting power lines or pipelines. In case of collision, the unmanned aerial vehicle can be damaged, normal flight and service life of the unmanned aerial vehicle are affected, tasks can be possibly interrupted, complete data can not be obtained or preset operation can not be completed, and loss is brought to related work. On the other hand, in unmanned aerial vehicle's storage and transportation, its comparatively fragile parts, such as wing, flabellum etc. also easily damage because of colliding with. Traditional unmanned aerial vehicle often does not fully consider these circumstances in structural design, lacks effective anticollision and accomodate protection mechanism, needs to be improved. Disclosure of utility model The present utility model is directed to solving the technical problems set forth in the background art. The novel energy unmanned aerial vehicle with the anti-collision function comprises a machine body, wherein a first wing is fixedly arranged on the surface of the machine body, a second wing is sleeved inside the first wing, a first rotating rod is fixedly arranged at the other end of the second wing, a circular plate is fixedly arranged on the surface of the first rotating rod, a groove is formed in the circular plate, a moving rod is sleeved inside the groove, a first spring is sleeved on the outer surface of the moving rod, a protection plate is fixedly arranged at the other end of the moving rod, fan blades are fixedly arranged at the top end of the first rotating rod, a motor is fixedly arranged inside the machine body, a gear is fixedly arranged at the output end of the motor, a placing groove is formed in the inner portion of the machine body, a circular block is fixedly arranged on the outer surface of the circular block, a second gear is fixedly arranged on the inner surface of the circular block, a second rotating rod is sleeved on the inner surface of the first wing, a first belt pulley of the rotating rod is fixedly arranged on the surface of the first belt pulley, a second belt pulley is fixedly arranged on the bottom end of the second rotating rod, a third belt pulley is fixedly arranged on the bottom end of the machine body, a second belt pulley is fixedly arranged on the bottom end of the first belt pulley is fixedly arranged on the inner side of the machine body, and a first belt pulley is fixedly arranged on the bottom end of the belt pulley fixedly arranged on the second belt pulley. Preferably, the surface of the first gear is meshed with the surface of the second rack, the surface of the second gear is meshed with the surface of the first rack, and the surface of the third gear is meshed with the surface of the second gear. Here, precise gear-to-rack engagement ensures accurate, stable power transfer between the relevant compo