Quick disassembly type unmanned aerial vehicle propeller

Abstract

The utility model relates to the technical field of unmanned aerial vehicle propellers, in particular to a quick disassembly type unmanned aerial vehicle propeller. The quick disassembly type unmanned aerial vehicle propeller comprises a connecting plate, a motor, a connecting shaft, a fixing sleeve and spiral blades, the motor is installed at the top of the connecting plate, an output shaft of the motor is connected with the connecting shaft through a coupler, the top of the connecting shaft is covered with the fixing sleeve, and the left side and the right side of the fixing sleeve are fixedly connected with the spiral blades. The device further comprises contact blocks, springs and clamping balls, the contact blocks are fixedly connected to the left side and the right side in the fixing sleeve, the two clamping balls are arranged in the connecting shaft in a sliding mode, the clamping balls are connected with the contact blocks in a clamped mode, and the springs are connected between the clamping balls and the connecting shaft. The fixing sleeve is rotated reversely, the contact block extrudes the clamping ball again to move upwards, then the clamping ball and the contact block are extruded to be separated from clamping contact, then the fixing sleeve is pulled upwards, the propeller can be disassembled, and therefore the purpose of quick disassembly is achieved, and maintenance or replacement is facilitated.

Description

TECHNICAL FIELD

[0001] The utility model relates to unmanned aerial vehicle propeller technical field especially, it relates to a quick detach type unmanned aerial vehicle propeller. BACKGROUND

[0002] The unmanned aerial vehicle is also called unmanned plane or remote control plane, and is an aerial vehicle which can fly without the operation of the pilot on the plane.

[0003] The unmanned aerial vehicle propeller is one of the key components of the unmanned aerial vehicle, and is mainly used for generating lift and thrust to enable the unmanned aerial vehicle to fly in the air.

[0004] Therefore, a quick detach type unmanned aerial vehicle propeller is needed. UTILITY MODEL CONTENT

[0005] In order to overcome the defects that most of the unmanned aerial vehicle propellers in the prior art rely on screw or nut fixing mode for disassembly, which is too complex during disassembly and cannot realize quick disassembly, thereby increasing the time for maintenance or replacement, the utility model provides a quick detach type unmanned aerial vehicle propeller.

[0006] The technical scheme of the utility model is as follows: a quick detach type unmanned aerial vehicle propeller comprises a connecting plate, a motor, a connecting shaft, a fixing sleeve and helical blades, the top of the connecting plate is provided with the motor, the output shaft of the motor is connected with the connecting shaft through a shaft coupling, the top of the connecting shaft is covered with the fixing sleeve, the fixing sleeve is fixedly connected with the helical blades on the left and right sides, further comprises a contact block, a spring, a clamping ball and a rubber plate, the fixing sleeve is fixedly connected with the contact block on the left and right sides inside, two clamping balls are slidingly arranged in the connecting shaft, the clamping ball is clamped with the contact block, the spring is connected between the clamping ball and the connecting shaft, and two rubber plates are embedded in the connecting shaft.

[0007] In one embodiment, the connecting shaft is slidingly provided with a connecting block and a wedge block on the left and right sides of the lower end, the connecting block is fixedly connected with the wedge block on the inner side, the connecting shaft is slidingly provided with two clamping rods, the clamping rod is clamped with the contact block, the clamping rod is fixedly connected with a gravity plate at the bottom, and the gravity plate is tightly attached to the top of the wedge block.

[0008] In one embodiment, the connecting plate is clamped with two isolation plates on the outer side, the ventilation opening is formed in the middle of the outer side of the isolation plate, and the protection rod is fixedly connected to the upper part of the outer side of the isolation plate.

[0009] In one of the embodiments, the first magnetic block and the second magnetic block are further included, the first magnetic block is arranged inside the connecting shaft, and the second magnetic block is arranged on the top of the fixing sleeve.

[0010] In one of the embodiments, the anti-lost rope is further included, the anti-lost rope is connected to the front and rear sides of the connecting shaft, and the end of the anti-lost rope away from the connecting shaft is connected to the connecting block.

[0011] In one of the embodiments, the handle is further included, and the handle is fixedly connected to the outer side of the isolation plate.

[0012] Compared with the prior art, the utility model provides a quick release type unmanned aerial vehicle propeller, has the following beneficial effects: 1, by the reverse rotation fixed sleeve, make the contact block extrusion again and move upwards ball, and then, pull the fixed sleeve upwards, can complete the disassembly of propeller, to reach the purpose of quick release, and then convenient for maintenance or replacement.

[0013] 2, by the wedge-shaped block extrusion and move upwards the clamping rod, make the clamping rod and contact block contact, to further fix the fixed sleeve, ensure that the fixed sleeve does not fall off.

[0014] 3, by the isolation plate fixed, make the protection rod surround the spiral blade, when unmanned aerial vehicle is in the flight process, the protection rod effectively protects the spiral blade, avoids the spiral blade accidental touch the object of outside, ensures the safety and stability of flight. BRIEF DESCRIPTION OF DRAWINGS

[0015] Figure 1 It is the three-dimensional structure schematic diagram of the utility model.

[0016] Figure 2 It is the partial sectional view of connecting plate, motor and spiral blade and other parts of the utility model.

[0017] Figure 3 It is the partial sectional view of contact block, spring and rubber plate and other parts of the utility model.

[0018] Figure 4 It is the partial sectional view of connecting shaft, fixed sleeve and connecting block and other parts of the utility model.

[0019] Figure 5 It is the explosion view of wedge-shaped block, clamping rod and gravity plate and other parts of the utility model.

[0020] Figure 6 It is the partial sectional view of motor, isolation plate and protection rod and other parts of the utility model.

[0021] Figure 7The utility model discloses a partial sectional view of connecting plate, vent and handle and other parts.

[0022] Figure 8 The utility model discloses a partial sectional view of fixed sleeve, first magnetic block and second magnetic block and other parts.

[0023] Marked as: 1-connecting plate, 2-motor, 3-connecting shaft, 4-fixed sleeve, 5-spiral blade, 6-contact block, 7-spring, 8-ball, 9-rubber plate, 10-connecting block, 11-wedge block, 12-clamping rod, 13-gravity plate, 14-isolation plate, 15-vent, 16-protection rod, 17-first magnetic block, 18-second magnetic block, 19-anti-lost rope, 20-handle. DETAILED DESCRIPTION

[0024] The technical solutions in the embodiments of the utility model will be clearly and completely described below with reference to the drawings in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by those skilled in the art without creative labor fall within the scope of the utility model.

[0025] Embodiment 1: a quick-release type unmanned aerial vehicle propeller, please refer to Figure 1 、 Figure 2 、 Figure 3 、 Figure 4 、 Figure 6 、 Figure 7 And Figure 8 , including connecting plate 1, motor 2, connecting shaft 3, fixed sleeve 4 and spiral blade 5, the top of connecting plate 1 is installed with motor 2, the output shaft of motor 2 is connected with connecting shaft 3 through coupling, the top of connecting shaft 3 is covered with fixed sleeve 4, and the left and right sides of fixed sleeve 4 are fixedly connected with spiral blade 5, the left and right sides in fixed sleeve 4 are fixedly connected with contact block 6, two ball 8 are slidably arranged in connecting shaft 3, ball 8 is connected with contact block 6, spring 7 is connected between ball 8 and connecting shaft 3, two rubber plates 9 are embeddedly arranged in connecting shaft 3, rubber plate 9 increases the friction between contact block 6 and connecting shaft 3, avoids the rotation of fixed sleeve 4 due to external force factor, and then makes contact block 6 move, connecting shaft 3 is provided with first magnetic block 17, the inner top of fixed sleeve 4 is provided with second magnetic block 18, second magnetic block 18 adsorbs first magnetic block 17, thereby providing additional locking force, ensuring that fixed sleeve 4 does not accidentally loosen.

[0026] When installing the propeller, first, place the retaining sleeve 4 on top of the connecting shaft 3. Then, rotate the retaining sleeve 4 to cause the contact block 6 to press the retaining ball 8 upward. At this time, the spring 7 is compressed. Continue rotating the retaining sleeve 4 until the contact block 6 moves to the appropriate position. At this point, the retaining ball 8 is no longer compressed, and the spring 7 returns to its original state, pushing the retaining ball 8 downward so that the retaining ball 8 engages with the contact block 6, thus completing the propeller installation. When disassembling the propeller, rotate the retaining sleeve 4 in the opposite direction to cause the contact block 6 to press the retaining ball 8 again. At this time, the retaining ball 8 moves upward along the arc surface inside the contact block 6, thus disengaging the retaining ball 8 from the contact block 6. Then, pull the retaining sleeve 4 upward to complete the disassembly of the propeller, achieving quick disassembly and facilitating maintenance or replacement.

[0027] Example 2: Based on Example 1, please refer to... Figure 4 and Figure 5 Connecting blocks 10 are slidably installed on both the left and right sides of the lower end of the connecting shaft 3. A wedge block 11 is fixedly connected to the inner side of the connecting block 10. Two locking rods 12 are slidably installed inside the connecting shaft 3. The locking rods 12 are engaged with the contact block 6. A gravity plate 13 is fixedly connected to the bottom of the locking rod 12. The bottom of the gravity plate 13 is close to the top of the wedge block 11. Anti-loss ropes 19 are connected to both the front and rear sides of the connecting shaft 3. The end of the anti-loss rope 19 away from the connecting shaft 3 is connected to the connecting block 10 to prevent the connecting block 10 from being lost during the disassembly of the propeller.

[0028] After the propeller is installed, move the connecting block 10 to the left and right sides of the connecting shaft 3 and push the connecting block 10 inward so that the wedge block 11 is inserted into the connecting shaft 3. During this process, the wedge block 11 squeezes the locking rod 12 upward so that the locking rod 12 engages with the contact block 6, thereby further fixing the fixing sleeve 4 and ensuring that the fixing sleeve 4 will not fall off.

[0029] Please see Figure 1 , Figure 6 and Figure 7 Two isolation plates 14 are snapped onto the outside of the connecting plate 1. A ventilation opening 15 for heat dissipation is provided in the middle of the outer side of the isolation plate 14. A protective rod 16 is fixedly connected to the upper part of the outer side of the isolation plate 14. A handle 20 is fixedly connected to the outer side of the isolation plate 14, which makes it easy to pick up the isolation plate 14.

[0030] Before using the propeller, move the isolation plate 14 to the left and right sides of the connecting plate 1 and push the isolation plate 14 to engage with the connecting plate 1, thereby fixing the isolation plate 14 and allowing the protective rod 16 to surround the propeller blade 5. When the drone is in flight, the protective rod 16 effectively protects the propeller blade 5, preventing the propeller blade 5 from accidentally touching external objects and ensuring the safety and stability of the flight.

[0031] Although the embodiments of the present application have been shown and described, it is to be understood that various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the present application, the scope of which is defined by the appended claims and their equivalents.

Claims

1. Quick release unmanned aerial vehicle propeller, including connecting plate (1), motor (2), connecting shaft (3), fixed sleeve (4) and helical blade (5), the top of connecting plate (1) is provided with motor (2), the output shaft of motor (2) is connected with connecting shaft (3) through shaft coupling, the top of connecting shaft (3) is covered with fixed sleeve (4), and the left and right sides of fixed sleeve (4) are fixedly connected with helical blade (5), characterized in that: The contact block (6), the spring (7), the ball (8) and the rubber plate (9) are further included, the contact block (6) is fixedly connected to the inside of the fixed sleeve (4) left and right sides, two ball (8) are slidably arranged in the connecting shaft (3), the ball (8) is connected with the contact block (6), the spring (7) is connected between the ball (8) and the connecting shaft (3), two rubber plates (9) are embedded in the connecting shaft (3).

2. The quick release unmanned aerial vehicle propeller of claim 1, wherein: The connecting block (10), the wedge block (11), the clamping rod (12) and the gravity plate (13) are further included, the connecting block (10) is slidably arranged on the left and right sides of the lower end of the connecting shaft (3), the wedge block (11) is fixedly connected to the inner side of the connecting block (10), two clamping rods (12) are slidably arranged in the connecting shaft (3), the clamping rod (12) is connected with the contact block (6), the gravity plate (13) is fixedly connected to the bottom of the clamping rod (12), and the gravity plate (13) is tightly attached to the top of the wedge block (11).

3. The quick release unmanned aerial vehicle propeller of claim 2, wherein: The isolation plate (14) and the protection rod (16) are further included, two isolation plates (14) are connected to the outer side of the connecting plate (1), the ventilation opening (15) is formed in the middle of the outer side of the isolation plate (14), and the protection rod (16) is fixedly connected to the upper portion of the outer side of the isolation plate (14).

4. The quick release unmanned aerial vehicle propeller of claim 3, wherein: The first magnetic block (17) and the second magnetic block (18) are further included, the first magnetic block (17) is arranged in the connecting shaft (3), and the second magnetic block (18) is arranged at the top of the fixed sleeve (4).

5. The quick release unmanned aerial vehicle propeller of claim 4, wherein: The anti-lost rope (19) is further included, the anti-lost rope (19) is connected to the front and rear sides of the connecting shaft (3), and one end of the anti-lost rope (19) away from the connecting shaft (3) is connected with the connecting block (10).

6. The quick release unmanned aerial vehicle propeller of claim 5, wherein: The handle (20) is further included, and the handle (20) is fixedly connected to the outer side of the isolation plate (14).

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