Aircraft structure

Abstract

The utility model discloses an aircraft structure, which belongs to the technical field of aircrafts and comprises an aircraft body, a main motor and a circuit board are arranged in the aircraft body, the circuit board is connected with the main motor and a propeller, the propeller is arranged on the outer side of the aircraft body, and the output end of the main motor is connected with a transmission gear set which is connected with a light ring body. The light ring body is rotationally arranged on the machine body and comprises a lamp carrier and rotating pieces, the two sides of the lamp carrier are connected with the rotating pieces respectively, the two rotating pieces are connected through a connecting piece, a limiting piece is arranged at the end, close to the machine body, of each rotating piece, a limiting groove matched with the limiting piece is formed in the machine body, and an elastic piece is arranged on the connecting piece. The elastic piece is in contact connection with the metal column, the elastic piece is connected with the circuit board, the metal column is electrically connected with the lamp in the lamp carrier through the wire, the rotatable light ring body capable of emitting dazzle light is installed on the aircraft body of the aircraft structure, and playability and interestingness are increased.

Description

Technical Field

[0001] The utility model belongs to the technical field of aircraft, and more specifically, relates to an aircraft structure. Background Art

[0002] At present, the propellers on most multi-rotor aircraft are simple structures directly connected to the motor. The propellers are rotated by changing the speed of the motor to achieve lifting and lowering. The aircraft can only be controlled to rise and fall or fly left and right, which lacks playability and fun. Utility Model Content

[0003] The main purpose of the utility model is to provide an aircraft structure to overcome the deficiencies of the prior art.

[0004] According to the first aspect of the utility model, an aircraft structure is provided, including a fuselage, a main motor and a circuit board are arranged in the fuselage, the circuit board is connected to the main motor and a propeller, the propeller is arranged on the outside of the fuselage, the output end of the main motor is connected to a transmission gear set, the transmission gear set is connected to a halo body, the halo body is rotatably arranged on the fuselage, the halo body includes a lamp carrier and a rotating part, the two sides of the lamp carrier are respectively connected to the rotating parts, the two rotating parts are connected by a connecting part, a limit part is provided at one end of the rotating part close to the fuselage, a limit groove cooperating with the limit part is opened on the fuselage, an elastic part is provided on the connecting part, the elastic part is in contact with and connected to a metal column, the elastic part is connected to the circuit board, and the metal column is electrically connected to the lamp in the lamp carrier through a wire.

[0005] In a specific embodiment of the utility model, the transmission gear set includes a first gear and a second gear, the first gear is connected to the output end of the main motor, the second gear is sleeved on one side of the connecting member, and the first gear and the second gear are meshed with each other.

[0006] In a specific embodiment of the utility model, the interior of the connecting piece is a hollow structure, a through hole is opened in the middle of the connecting piece, the metal column is arranged in the connecting piece, one end of the metal column extends through the through hole and contacts with the elastic member, and the other end of the metal column extends to one side of the lamp carrier and is electrically connected to the lamp in the lamp carrier through a wire.

[0007] In a specific embodiment of the present invention, an LED light bar is arranged on the lamp carrier, and the LED light bar is electrically connected to the metal column through a wire.

[0008] In a specific embodiment of the utility model, the body has a mounting portion extending outwardly, a propeller motor is mounted on the mounting portion, the propeller motor is connected to the circuit board via a wire, and the propeller is mounted on the propeller motor.

[0009] In a specific embodiment of the utility model, the machine body includes an upper cover and a base, the main motor and the circuit board are both arranged on the base, and the upper cover and the base are buckled with each other.

[0010] In a specific embodiment of the present invention, a battery compartment is provided at the bottom of the base, a battery is detachably provided in the battery compartment, and the battery compartment is connected to the circuit board.

[0011] In a specific embodiment of the utility model, a positioning portion is provided on one end of the rotating member close to the body, a positioning groove matching with the positioning portion is provided on the body, and the positioning groove is provided on one side of the limiting groove.

[0012] One of the above technical solutions of the utility model has at least one of the following advantages or beneficial effects:

[0013] This aircraft structure has a main motor and propeller installed in the body, so that the body can be raised and lowered and moved normally. At the same time, the output end of the main motor drives the halo body set on the body to rotate through the transmission gear set. The halo body can also emit glare while rotating. The halo body provides electrical energy for light emission through the contact between elastic parts and metal columns, which increases playability and fun. BRIEF DESCRIPTION OF THE DRAWINGS

[0014] The utility model is further described below in conjunction with the accompanying drawings and embodiments;

[0015] Figure 1 It is a structural schematic diagram of an aircraft in one embodiment of the utility model;

[0016] Figure 2 It is a schematic diagram of the structure of an aircraft without an upper cover in one embodiment of the utility model;

[0017] Figure 3 It is a structural schematic diagram of a halo body in one embodiment of the utility model;

[0018] Figure 4 It is a structural schematic diagram of a base in one embodiment of the utility model. DETAILED DESCRIPTION

[0019] The embodiments of the present invention are described in detail below, and examples of the embodiments are shown in the accompanying drawings, wherein the same or similar reference numerals represent the same or similar elements or elements having the same or similar functions from beginning to end. The embodiments described below with reference to the accompanying drawings are exemplary and are only used to explain the present invention, and cannot be understood as limiting the present invention.

[0020] In the description of the present invention, it should be understood that descriptions involving orientation, such as up, down, front, back, left, right, etc., indicating orientations or positional relationships, are based on the orientations or positional relationships shown in the accompanying drawings, and are only for the convenience of describing the present invention and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as a limitation on the present invention.

[0021] In the description of the present utility model, "several" means one or more, "more" means more than two, "greater than", "less than", "exceed" etc. are understood to exclude the number itself, and "above", "below", "within" etc. are understood to include the number itself. If there is a description of "first" or "second", it is only used for the purpose of distinguishing the technical features, and cannot be understood as indicating or implying the relative importance or implicitly indicating the number of the indicated technical features or implicitly indicating the order of the indicated technical features.

[0022] In addition, the terms "first" and "second" are used for descriptive purposes only and should not be understood as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, the features defined as "first" and "second" may explicitly or implicitly include one or more features.

[0023] In the description of the present utility model, it should be noted that, unless otherwise clearly stipulated and limited, the term "connection" should be understood in a broad sense. For example, it can be a fixed connection or a movable connection, a detachable connection or a non-detachable connection, or an integral connection; it can be a mechanical connection, an electrical connection, or mutual communication; it can be a direct connection, or an indirect connection through an intermediate medium, and it can be internal connection between two elements, indirect connection, or an interactive relationship between two elements.

[0024] The following disclosure provides many different embodiments or examples for implementing different solutions of the present invention.

[0025] Reference Figures 1 to 4As shown, an aircraft structure is provided, including a body 1, the body 1 is formed by buckling an upper cover 13 and a base 14, an installation chamber for installing a main motor 2 is arranged in the base 14, a circuit board is installed on one side of the installation chamber, the circuit board connects the main motor 2 and a propeller 5, the propeller 5 is arranged around the outer side of the body 1, the output end of the main motor 2 is connected to a transmission gear set 3, so that the transmission gear set 3 drives a halo body 4 to rotate, the halo body 4 is arranged on the body 1 and can rotate freely, the halo body 4 is composed of a lamp carrier 41 and a rotating member 42, the two sides of the lamp carrier 41 are respectively connected to the rotating member 42, and the two rotating members 42 are connected by The connecting piece 43 is connected and arranged on the base 14, a limiting piece 44 is provided at one end of the rotating piece 42 close to the body 1, a limiting groove 11 cooperating with the limiting piece 44 is opened on the body 1, the limiting piece 44 is used to fix the halo body 4, but does not limit the rotation of the halo body 4, an elastic piece 7 is arranged on the connecting piece 43, the elastic piece 7 is in contact with the metal column 6, the elastic piece 7 is connected to the circuit board, the circuit board conducts electricity to the elastic piece 7, since the elastic piece 7 and the metal column 6 are in contact with each other, the metal column 6 is also charged, and the metal column 6 is electrically connected to the lamp in the lamp carrier 41 through a wire, so that the lamp in the lamp carrier 41 is energized and emits light.

[0026] In this embodiment, the halo body 4 is installed on the base 14, and the output end of the main motor 2 installed on the base 14 is connected to the transmission gear set 3 for rotation. The transmission gear set 3 drives the halo body 4 to rotate. An elastic member 7 is sleeved on the connecting member 43, and the elastic member 7 is connected to the circuit board. The elastic member 7 is also connected to the metal column 6. The metal column 6 is electrically connected to the lamp in the lamp carrier 41 by a wire. The aircraft is started, and the circuit board conducts electricity to the elastic member 7, and then to the metal column 6, and finally to the lamp in the lamp carrier 41 by a wire, so that it emits glare, so that the aircraft can not only fly and move, but also rotate the halo body 4 to rotate and emit glare, which increases playability and fun.

[0027] In one embodiment of the utility model, the transmission gear set 3 includes a first gear 31 and a second gear 32. The first gear 31 is connected to the output end of the main motor 2, and the second gear 32 is sleeved on one side of the connecting member 43. The first gear 31 and the second gear 32 are meshed with each other. When the main motor 2 is started, the first gear 31 connected to the output end is driven to rotate, and the first gear 31 drives the second gear 32 to rotate. The second gear 32 is sleeved on one side of the connecting member 43, and the second gear 32 drives the connecting member 43 to rotate, so that the rotating member 42 rotates and drives the lamp carrier 41 to rotate, so that the flight is realized while the halo body 4 is rotated, thereby increasing its playability and fun.

[0028] In one embodiment of the utility model, the interior of the connecting member 43 is hollow, a through hole 431 is opened in the middle position of the connecting member 43, a metal column 6 is arranged in the connecting member 43, one end of the metal column 6 extends toward the through hole 431 and passes through the through hole 431 to contact the elastic member 7, thereby conducting electricity and making the lamp in the lamp carrier 41 emit light, and the other end of the metal column 6 extends to one side of the lamp carrier 41 and is electrically connected to the lamp in the lamp carrier 41 through a wire.

[0029] In one embodiment of the utility model, an LED light bar is arranged in the lamp carrier 41, and lights of various colors are arranged on the LED light bar. The LED light bar is electrically connected to the metal column 6 through a wire, and can emit dazzling light after conduction.

[0030] In one embodiment of the utility model, a mounting portion 12 is extended outward from the body 1, and the mounting portion 12 is evenly distributed on the outer periphery of the body 1. A propeller motor 51 is fixedly mounted on the mounting portion 12. The propeller motor 51 is connected to the circuit board through a wire. The propeller 5 is mounted on the propeller motor 51. The speed of the propeller motor 51 is controlled, thereby controlling the speed of the propeller 5 to realize the lifting and lowering of the aircraft, and can also control its left and right movement.

[0031] In one embodiment of the utility model, a battery compartment is provided at the bottom of the base 14, and a battery is detachably installed in the battery compartment. By gently pressing the battery, the battery compartment can release the lock on the battery. When installing, put the battery into the battery compartment, and then gently press the battery, the battery compartment can lock the battery and fix it. After installation, the battery compartment cover is covered to prevent the battery from being exposed and affecting the appearance. The battery compartment is connected to the circuit board through a wire. The battery in the battery compartment provides electrical energy for other components of the aircraft and provides a source of kinetic energy for flight.

[0032] In one embodiment of the utility model, a positioning portion 421 is provided on one end of the rotating member 42 close to the body 1, and a positioning groove 15 matching the positioning portion 421 is provided on the body 1. The positioning portion 421 is first inserted into the positioning groove 15 to facilitate the installation of the rotating member 42. At the same time, the positioning portion 421 and the positioning groove 15 are clearance-matched, and the positioning portion 421 can rotate in the positioning groove 15. The positioning groove 15 is provided on one side of the limit groove 11.

[0033] Although the embodiments of the present invention have been shown and described, those skilled in the art will appreciate that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the claims and their equivalents.

Claims

1. An aircraft structure, comprising a body (1), characterized in that: A main motor (2) and a circuit board are arranged in the machine body (1); the circuit board is connected to the main motor (2) and a propeller (5); the propeller (5) is arranged outside the machine body (1); an output end of the main motor (2) is connected to a transmission gear set (3); the transmission gear set (3) is connected to a halo body (4); the halo body (4) is rotatably arranged on the machine body (1); the halo body (4) comprises a lamp carrier (41) and a rotating member (42); two sides of the lamp carrier (41) are respectively connected to the rotating member (42), the two rotating members (42) are connected via a connecting member (43), a limiting member (44) is provided at one end of the rotating member (42) close to the body (1), a limiting groove (11) cooperating with the limiting member (44) is provided on the body (1), an elastic member (7) is provided on the connecting member (43), the elastic member (7) is in contact with and connected to the metal column (6), the elastic member (7) is connected to the circuit board, and the metal column (6) is electrically connected to the lamp in the lamp carrier (41) via a wire.

2. The aircraft structure according to claim 1, characterized in that: The transmission gear set (3) comprises a first gear (31) and a second gear (32); the first gear (31) is connected to the output end of the main motor (2); the second gear (32) is sleeved on one side of the connecting member (43); the first gear (31) and the second gear (32) are meshed with each other.

3. The aircraft structure according to claim 1, characterized in that: The interior of the connecting piece (43) is a hollow structure, a through hole (431) is provided in the middle of the connecting piece (43), the metal column (6) is arranged in the connecting piece (43), one end of the metal column (6) extends through the through hole (431) and contacts the elastic piece (7), and the other end of the metal column (6) extends toward one side of the lamp carrier (41) and is electrically connected to the lamp in the lamp carrier (41) through a wire.

4. The aircraft structure according to claim 3, characterized in that: An LED light bar is arranged on the lamp carrier (41), and the LED light bar is electrically connected to the metal column (6) via a wire.

5. The aircraft structure according to claim 1, characterized in that: The machine body (1) has a mounting portion (12) extending outwardly, a propeller motor (51) is mounted on the mounting portion (12), the propeller motor (51) is connected to the circuit board via a wire, and the propeller (5) is mounted on the propeller motor (51).

6. The aircraft structure according to claim 1, characterized in that: The machine body (1) comprises an upper cover (13) and a base (14); the main motor (2) and the circuit board are both arranged on the base (14); and the upper cover (13) and the base (14) are buckled with each other.

7. The aircraft structure according to claim 6, characterized in that: A battery compartment is provided at the bottom of the base (14), a battery is detachably arranged in the battery compartment, and the battery compartment is connected to the circuit board.

8. The aircraft structure according to claim 1, characterized in that: A positioning portion (421) is provided on one end of the rotating member (42) close to the machine body (1), and a positioning groove (15) matching with the positioning portion (421) is provided on the machine body (1), and the positioning groove (15) is provided on one side of the limiting groove (11).

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