CN205854470U - A kind of portable unmanned plane - Google Patents

Abstract

The utility model relates to the technical field of unmanned aerial vehicles, in particular to a portable unmanned aerial vehicle, comprising a fuselage, an arm, a motor, paddles and a tripod. A storage room is arranged around the fuselage; one end of the machine arm is slidably connected with the storage room; a motor is installed at the other end of the machine arm; two blades are installed on the motor; There is a groove at the bottom of the arm, the tripod is rotatably connected to one end of the groove, and a limit locking mechanism is set between the tripod and the groove; the tail end of the paddle is provided with a step and a circle Hole cylinder. The utility model can fold and shrink the machine arm, paddle and tripod into the body, and has the characteristics of simple operation, easy storage, and convenient portability. At the same time, the folded and contracted state can better protect the machine arm, paddle and tripod Protected from external damage.

Description

A portable drone

technical field

The utility model relates to the technical field of drones, in particular to a portable drone.

Background technique

Today, with the rapid development of the drone industry, drones will enter the daily life, entertainment and work of ordinary consumers. However, the existing quadrotor UAVs all have fixed arms, and the products are large in size and occupy a large space, which brings more and more inconveniences in transportation and carrying. In view of this, there is an urgent need for a drone that is easy to operate, easy to store, and easy to carry.

Contents of the invention

In order to make up for the deficiencies of the existing technology, the utility model provides a portable drone, which has the characteristics of simple operation, easy storage, and convenient portability. At the same time, the folded and contracted state can better protect the arms, blades and The tripod is protected from external forces.

The technical solution adopted by the utility model to solve its technical problems is: a portable unmanned aerial vehicle including a fuselage, an arm, a motor, blades, and a tripod; a storage room is arranged around the fuselage, and the storage room is used One end of the arm is slidably connected to the storage chamber; the other end of the arm is equipped with a motor; two blades are installed on the motor; a groove is provided at the bottom of the arm , the tripod is rotatably connected to one end of the groove, and a limit locking mechanism is arranged between the tripod and the groove, and the groove is used for storing the tripod.

A position-limited locking structure is provided at the contact between the machine arm and the storage chamber.

A cylinder with a step and a round hole is arranged at the tail end of the paddle.

The movable angle of the tripod is 0°-120°.

Described machine arm has 4, motor has 4, and blade has 4 pairs.

The beneficial effects of the utility model are: a portable unmanned aerial vehicle, the blades can be folded, the tripod can be folded into the groove in the arm, and the arm can be retracted into the body, which has the advantages of simple operation, easy storage, and convenient The characteristics of carrying, at the same time, the folded and contracted state can better protect the arms, blades and tripod from external forces.

Description of drawings

Below in conjunction with accompanying drawing and embodiment the utility model is further described.

Fig. 1 is a schematic diagram of the unfolded state of the utility model;

Fig. 2 is a schematic diagram of the contracted and folded state of the utility model;

Fig. 3 is a schematic diagram of the sliding direction of the machine arm and the rotating direction of the tripod of the utility model;

Fig. 4 is a bottom view schematic diagram of the utility model;

Fig. 5 is a partial schematic diagram of blade deployment and nut disassembly of the utility model;

In the figure: 1. Fuselage, 2. Arm, 3. Motor, 4. Propeller, 5. Tripod, 6. Nut, 7. Threaded column, 11. Storage room, 21. Groove, 41. Cylinder .

detailed description

In order to make the technical means, creative features, goals and effects achieved by the present invention easy to understand, the present invention will be further described below in conjunction with specific illustrations.

As shown in Figure 1, a portable unmanned aerial vehicle described in the utility model includes a fuselage 1, an arm 2, a motor 3, a paddle 4, and a tripod 5; it is characterized in that: the fuselage 1 Storage chamber 11 is arranged around, and the effect of storage chamber 11 is to be used for storing machine arm 2 and paddle 4, is convenient to carry, also can protect machine arm 2 and paddle 3 from the injury of external force; Said machine arm 2 one end It is slidingly connected with the storage chamber 11; the other end of the arm 2 is equipped with a motor 3; two blades 4 are installed on the motor 3; as shown in Figure 4, the bottom of the arm 2 is provided with a concave Slot 21, the tripod 5 is rotatably connected to one end of the groove 21, and a limit locking mechanism is arranged between the tripod 5 and the groove 21, the groove 21 is used to store the tripod; the arm There are 4 motors 2, 4 motors 3, and 4 pairs of blades 4; After the circular hole and the threaded column 7 are installed correspondingly, screw the fixed paddle 4 with the nut 6 .

As shown in Figures 2 and 3, one end of the machine arm 2 is slidingly connected to the storage chamber 11, and the contact between the machine arm 2 and the storage room 11 is provided with a limited locking structure, and only a certain force needs to be applied to the machine arm 2 It then slides in the direction of the force and stays firmly in place. It not only ensures the convenience of the user, but also ensures the stable flight of the product after unfolding and the minimum volume after folding. The movable angle of the tripod 5 is 0°-120°, and the span of the four tripods 5 can ensure a smooth landing when landing.

The basic principles, main features and advantages of the present utility model have been shown and described above. Those skilled in the industry should understand that the utility model is not limited by the above-mentioned embodiments. The above-mentioned embodiments and the description in the specification only illustrate the principle of the utility model. Without departing from the spirit and scope of the utility model, the utility model The utility model also has various changes and improvements, and these changes and improvements all fall within the scope of the claimed utility model. The scope of protection required by the utility model is defined by the appended claims and their equivalents.

Claims (5)

1. a portable unmanned aerial vehicle, is characterized in that: comprise fuselage (1), machine arm (2), motor (3), blade (4), tripod (5); Described fuselage ( 1) A storage chamber (11) is arranged around; one end of the machine arm (2) is slidably connected to the storage room; the other end of the machine arm (2) is equipped with a motor (3); the motor (3) Two blades (4) are installed on it; the bottom of the arm (2) is provided with a groove (21), and the tripod (5) is rotatably connected to one end of the groove (21), and A limit locking mechanism is arranged between the tripod (5) and the groove (21). 2. A portable drone according to claim 1, characterized in that: the contact between the arm (2) and the storage chamber is provided with a limit locking structure. 3. A portable drone according to claim 1, characterized in that: the tail end of the blade (4) is provided with a column (41) with steps and round holes. 4. A portable drone according to claim 1, characterized in that: the movable angle of the tripod (5) is 0°-120°. 5. A portable drone according to claim 1, characterized in that: there are four arms (2), four motors (3), and four pairs of blades (4).