Paddle protection structure of unmanned aerial vehicle

Abstract

The utility model discloses a blade protection structure of an unmanned aerial vehicle, and particularly relates to the unmanned aerial vehicle, which comprises a steering engine and a mounting seat of the steering engine, and further comprises a first plate and a second plate which are assembled in a sliding manner, the opposite ends of the first plate piece and the second plate piece are provided with lateral elastic pieces, and one ends of the lateral elastic pieces are connected with the outer wall of the outer protection ring piece. And one first plate piece and one second plate piece form a buffer group and are arranged in a circumferential array relative to the outer protection ring piece. A double-ring-shaped protection structure is adopted, and the outermost ring is designed to have an elastic buffering function, so that the anti-collision buffering capacity of the device is greatly improved.

Description

Technical Field

[0001] The utility model relates to an unmanned aerial vehicle, in particular to a blade protection structure of the unmanned aerial vehicle. Background Art

[0002] When a drone lands, the uneven ground or excessive side wind may cause the drone to tilt, causing the propeller blades on the operating servo to contact the ground and cause damage.

[0003] For this reason, a circular protective ring cover is added to the outer periphery of the drone's blades during design, which aims to protect the blades and also stabilize the airflow of the drone. However, when the protective ring cover comes into contact with the ground or hard objects, it will inevitably deform to a certain extent. If the deformation is severe, the blades will also scratch the inner wall of the protective ring cover. Utility Model Content

[0004] The utility model aims to provide a blade protection structure for a UAV, so as to solve the above-mentioned problem.

[0005] In order to achieve the above purpose, the utility model provides the following technical solutions:

[0006] A blade protection structure for a drone, comprising a steering gear and a mounting seat for the steering gear, an outer protection ring being arranged on the mounting seat, and a first plate and a second plate being slidably assembled, wherein opposite ends of the first plate and the second plate are respectively provided with lateral elastic members having one end connected to the outer wall of the outer protection ring;

[0007] And one of the first plate members and one of the second plate members form a buffer group, and are arranged in a circular array about the outer protective ring member.

[0008] Preferably, the buffer group is divided into an upper buffer group and a lower buffer group along the axial diameter direction of the outer protective ring, and a predetermined distance is maintained between the upper buffer group and the lower buffer group.

[0009] Preferably, the lateral elastic member is in the shape of an oblique broken line and has at least two vertices, and both of the two vertices are not in contact with the outer wall of the outer protective ring member.

[0010] Preferably, with respect to the horizontal plane, one end of the lateral elastic member is at a high position, and the other end is at a low position, and the low position is connected to the outer protective ring member.

[0011] Preferably, the second plate is provided with a notch and further comprises a U-shaped member, a first end of which is connected to the side wall of the first plate, and a second end of which is connected to an end of the first plate opposite to the notch.

[0012] Preferably, the bottom of the U-shaped member extends out from the notch and abuts against the side wall of the outer protective ring member.

[0013] Preferably, the mounting seat is located at the axis of the outer protective ring, and the two are connected by a plurality of round rods arranged in a circular array.

[0014] Preferably, the first plate component and the second plate component are both carbon fiber plates.

[0015] Preferably, the lateral elastic member is a carbon fiber plate.

[0016] In the above technical solution, the utility model provides a blade protection structure for a drone, which has the following beneficial effects: multiple modular buffer groups arranged in a circumferential array are assembled on the outer protective ring to provide a double protection effect. When a collision occurs, whether the first plate or the second plate is subjected to lateral or frontal force, the first plate and the second plate will shrink, and release the force and recover under the action of the lateral elastic member. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the drawings required for use in the embodiments will be briefly introduced below. Obviously, the drawings described below are only some embodiments recorded in the present utility model. For ordinary technicians in this field, other drawings can also be obtained based on these drawings.

[0018] Figure 1 The overall structural diagram provided for the embodiment of the utility model;

[0019] Figure 2 A schematic diagram of the sliding assembly structure of the first plate and the second plate provided in an embodiment of the utility model.

[0020] Description of reference numerals:

[0021] 1. Mounting seat; 2. External protective ring; 3. Lateral elastic member; 4. First plate member; 5. Second plate member; 51. Slot; 6. U-shaped member. DETAILED DESCRIPTION

[0022] In order to enable those skilled in the art to better understand the technical solution of the present invention, the present invention will be further described in detail below in conjunction with the accompanying drawings.

[0023] like Figure 1-2 As shown, a blade protection structure of a UAV includes a steering gear and a mounting seat 1 of the steering gear, an outer protective ring 2 is arranged on the mounting seat 1, and also includes a first plate 4 and a second plate 5 that are slidably assembled, and the first plate 4 and the second plate 5 are respectively provided with a lateral elastic member 3 at one end connected to the outer wall of the outer protective ring 2 at opposite ends;

[0024] A first plate member 4 and a second plate member 5 form a buffer group, and are arranged in a circular array about the outer protective ring member 2 .

[0025] Specifically, the mounting seat 1 is located at the axis of the outer protective ring 2, and the two are connected by a plurality of round rods arranged in a circumferential array, so that the mounting seat 1 is fixed. This is a conventional technology and will not be elaborated on.

[0026] Secondly, the lateral elastic member 3, the first plate member 4 and the second plate member 5 in the embodiment are all carbon fiber plates. Because the carbon fiber plates are relatively light and hard, they can be used in long-term collision environments.

[0027] In the above technology, multiple modular buffer groups arranged in a circumferential array are assembled on the outer anti-ring member 2 to provide a double protection effect. When a collision occurs, whether the first plate member 4 or the second plate member 5 is subjected to lateral or frontal force, the first plate member 4 and the second plate member 5 will shrink, and release the force and recover under the action of the lateral elastic member 3.

[0028] As an embodiment further provided by the present invention, the buffer group is divided into an upper buffer group and a lower buffer group along the axial direction of the outer anti-ring member 2, and a predetermined distance is maintained between the upper buffer group and the lower buffer group.

[0029] Specific, combined Figure 1 It can be known that the embodiment adopts the upper buffer group and the lower buffer group along the axial direction of the outer protective ring 2. The purpose is to make the first plate 4 and the second plate 5 be subjected to frontal force through the upper buffer group and the lower buffer group to divide the force, and the lateral force on the first plate 4 and the second plate 5 can also play a force dividing effect, thereby optimizing the buffering effect.

[0030] As another embodiment further provided by the present invention, the lateral elastic member 3 is in the shape of an oblique broken line and has at least two vertices, and both vertices are not in contact with the outer wall of the outer protective ring member 2 .

[0031] With respect to the horizontal plane, one end of the lateral elastic member 3 is at a high position, and the other end is at a low position, and the low position is connected to the outer protective ring member 2 .

[0032] Specifically, in the embodiment, when the first plate 4 and the second plate 5 are subjected to frontal force, during the deformation of the lateral elastic member 3, the two vertices may successively contact the outer protective ring member 2, thereby reducing the force applied to the first plate 4 and the second plate 5 to the outer protective ring member 2, thereby optimizing the buffering effect.

[0033] As another embodiment further provided by the utility model, the second plate 5 is provided with a notch 51 and further includes a U-shaped member 6, a first end of which is connected to the side wall of the first plate 4, and a second end of which is connected to an end of the first plate 4 opposite to the notch 51.

[0034] Furthermore, the bottom of the U-shaped member 6 extends out from the notch 51 and contacts the side wall of the outer protective ring member 2 .

[0035] Specifically, when the first plate member 4 or the second plate member 5 is subjected to force on either side, the U-shaped member 6 will also be squeezed and deformed, and at the same time, the force will be released and restored under the action of the lateral elastic member 3.

[0036] The above only describes some exemplary embodiments of the present invention by way of illustration. It is undoubted that those skilled in the art can modify the described embodiments in various ways without departing from the spirit and scope of the present invention. Therefore, the above drawings and descriptions are illustrative in nature and should not be construed as limiting the scope of protection of the claims of the present invention.

Claims

1. A blade protection structure for an unmanned aerial vehicle, comprising a steering gear and a mounting seat (1) thereof, characterized in that: The mounting seat (1) is provided with an outer anti-ring member (2), and further comprises a first plate member (4) and a second plate member (5) which are slidably assembled, and opposite ends of the first plate member (4) and the second plate member (5) are respectively provided with lateral elastic members (3) whose ends are connected to the outer wall of the outer anti-ring member (2); Furthermore, one of the first plate members (4) and one of the second plate members (5) form a buffer group and are arranged in a circular array about the outer protective ring member (2).

2. The blade protection structure of a drone according to claim 1, characterized in that: The buffer group is divided into an upper buffer group and a lower buffer group along the axial diameter direction of the outer anti-ring component (2), and a predetermined distance is maintained between the upper buffer group and the lower buffer group.

3. The blade protection structure of a drone according to claim 1, characterized in that: The lateral elastic member (3) is in the shape of an oblique broken line and has at least two vertices, and neither of the two vertices is in contact with the outer wall of the outer anti-ring member (2).

4. The blade protection structure of a drone according to claim 3, characterized in that: With respect to the horizontal plane, one end of the lateral elastic member (3) is at a high position and the other end is at a low position, and the low position is connected to the outer protective ring member (2).

5. The blade protection structure of a drone according to claim 1, characterized in that: The second plate member (5) is provided with a notch (51) and further comprises a U-shaped member (6), a first end of which is connected to the side wall of the first plate member (4) and a second end of which is connected to an end of the first plate member (4) opposite to the notch (51).

6. The blade protection structure of a drone according to claim 5, characterized in that: The bottom of the U-shaped part (6) extends out from the notch (51) and contacts the side wall of the outer protective ring part (2).

7. The blade protection structure of a drone according to claim 1, characterized in that: The mounting seat (1) is located at the axis of the outer protective ring (2), and the two are connected via a plurality of round bars arranged in a circumferential array.

8. The blade protection structure of a drone according to claim 1, characterized in that: The first plate component (4) and the second plate component (5) are both carbon fiber plates.

9. The blade protection structure of a drone according to claim 1, characterized in that: The lateral elastic member (3) is a carbon fiber plate.

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