CN219928002U

CN219928002U - Modularized aircraft with detachable horn

Info

Publication number: CN219928002U
Application number: CN202321224966.4U
Authority: CN
Inventors: 刘军; 葛梓明
Original assignee: Dongguan Yinyan Electrical Technology Co ltd
Current assignee: Dongguan Yinyan Electrical Technology Co ltd
Priority date: 2023-05-19
Filing date: 2023-05-19
Publication date: 2023-10-31
Anticipated expiration: 2033-05-19

Abstract

The utility model discloses a modularized aircraft with a detachable horn, which comprises a horn lower clamping plate, a horn upper clamping plate, a 3.5-inch horn, a flight control chart transmission tower, an antenna, a receiver, a top carbon plate and a camera; the motor is fixed on the upper side of the corner of the 5-inch horn. Compared with the prior art, the method has the advantages that: according to the utility model, after the screws are disassembled, the original horn on the modularized aircraft can be removed, and then the horn with the 3.5-inch propeller or the horn with the 5-inch propeller can be replaced, so that the novel modular aircraft can be conveniently switched between the 3.5-inch modularized aircraft and the 5-inch modularized aircraft; and the loading and unloading operations of the 3.5-inch horn and the 5-inch horn are very convenient, so that the original horn can be replaced conveniently after being damaged.

Description

Modularized aircraft with detachable horn

Technical Field

The utility model relates to the technical field of unmanned aerial vehicles, in particular to a modularized aircraft with a detachable horn.

Background

At present, a part of 3.5 and 5 inch unmanned aerial vehicles (3.5 inch unmanned aerial vehicle fingers: the propeller on the horn of the unmanned aerial vehicle is 3.5 inch specification propeller; 5 inch unmanned aerial vehicle fingers: the propeller on the horn of the unmanned aerial vehicle is 5 inch specification propeller) on the market can only fix one size horn, so that the use limitation is relatively large, different horns can not be installed on the same unmanned aerial vehicle by replacing the 3.5 inch horn and the 5 inch horn, and the switching between the 3.5 inch unmanned aerial vehicle and the 5 inch unmanned aerial vehicle can not be realized by replacing the 3.5 inch horn and the 5 inch horn.

Here, in order to solve the above-mentioned problems, we propose a modular aircraft with a detachable horn.

Disclosure of Invention

The utility model aims to solve the technical problems and provide a modularized aircraft with a detachable horn, wherein the detachable horn can be switched between a 3.5-inch unmanned aerial vehicle and a 5-inch unmanned aerial vehicle by replacing the 3.5-inch horn and the 5-inch horn.

In order to solve the technical problems, the technical scheme provided by the utility model is as follows:

a modularized aircraft with a detachable horn comprises a horn lower clamping plate, a horn upper clamping plate, a 3.5-inch horn, a flight control chart tower, an antenna, a receiver, a top carbon plate and a camera;

a top carbon plate is fixedly arranged above the horn upper clamping plate, a flight control chart transmission tower is fixedly arranged between the horn upper clamping plate and the top carbon plate, an antenna is arranged at the tail part of the flight control chart transmission tower, a receiver is arranged at the upper side of the flight control chart transmission tower, a camera is fixedly arranged at the front side of the top carbon plate, a horn lower clamping plate is fixedly arranged at the lower side of the horn upper clamping plate, a pair of 3.5-inch horn are respectively and detachably arranged between the front part and the rear part of the horn lower clamping plate and the horn upper clamping plate in a front-back mirror image mode, a motor is fixedly arranged at the upper side of the corner of the 3.5-inch horn, and a propeller is fixedly arranged on an output shaft of the motor;

the motor is fixedly arranged on the upper side of the corner of the 5-inch horn, and a propeller is fixedly arranged on an output shaft of the motor.

As an improvement, an antenna bracket for placing an antenna is fixedly arranged on the lower side of the top carbon plate. For supporting the mounting antenna.

As an improvement, the support that is located the flight control diagram transmission tower front side is fixed with in top carbon sheet downside installation, and the installation of reversible about the camera sets up between two supports, and two still install the camera protection casing between the support, the camera protection casing cooperation is installed on the camera. The protective device is used for applying an effective protective effect to the camera.

Compared with the prior art, the utility model has the advantages that: according to the utility model, after the screws are disassembled, the original horn on the modularized aircraft can be removed, and then the horn with the 3.5-inch propeller or the horn with the 5-inch propeller (namely, the 3.5-inch horn or the 5-inch horn) can be replaced, so that the novel modular aircraft can be conveniently switched between the 3.5-inch modularized aircraft and the 5-inch modularized aircraft; and the loading and unloading operations of the 3.5-inch horn and the 5-inch horn are very convenient, so that the original horn can be replaced conveniently after being damaged.

Drawings

Fig. 1 is an exploded view of the present utility model.

Fig. 2 is a bottom view of the present utility model.

Fig. 3 is a top view of the present utility model.

Fig. 4 is a front view of the present utility model.

As shown in the figure: 1. a lower arm clamping plate; 2. a horn upper clamping plate; 3. 3.5 inch horn; 4. flight control chart tower transmission; 5. an antenna; 6. a receiver; 7. a top carbon plate; 8. a camera; 9. a motor; 10. a propeller; 11. a 5 inch horn; 12. an antenna support; 13. a support; 14. a camera protective cover.

Detailed Description

In the description of the present utility model, it should be understood that the terms "center," "lateral," "upper," "lower," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," and the like indicate or are based on the orientation or positional relationship shown in the drawings, merely to facilitate description of the utility model and simplify the description, and do not indicate or imply that the devices or elements referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus should not be construed as limiting the utility model. Furthermore, the terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defining "a first" or "a second" may explicitly or implicitly include one or more such feature. In the description of the present utility model, unless otherwise indicated, the meaning of "a plurality" is two or more. In addition, the term "include" and any variations thereof are intended to cover a non-exclusive inclusion.

The present utility model will be described in further detail with reference to the accompanying drawings.

A modularized aircraft with a detachable horn comprises a horn lower clamping plate 1, a horn upper clamping plate 2, a 3.5 inch horn 3, a flight control chart tower 4, a 2.4G antenna 5, a 2.4G receiver 6, a top carbon plate 7 and a camera 8;

a top carbon plate 7 is fixedly arranged above the horn upper clamping plate 2, a flight control image transmission tower 4 is fixedly arranged between the horn upper clamping plate 2 and the top carbon plate 7, an antenna 5 is arranged at the tail part of the flight control image transmission tower 4, a receiver 6 is arranged at the upper side, an antenna bracket 12 for placing 2.4G of the antenna 5 is fixedly arranged at the lower side of the top carbon plate 7, a pair of supports 13 positioned at the front side of the flight control image transmission tower 4 are fixedly arranged at the lower side of the top carbon plate 7, a camera 8 is vertically and rotatably arranged between the two supports 13, a camera protection cover 14 is also arranged between the two supports 13, and the camera protection cover 14 is cooperatively arranged on the camera 8;

the lower side of the horn upper clamping plate 2 is provided with a pair of horn lower clamping plates 1,3.5 inches horn 3, the front and back mirror image type horn lower clamping plates 1 and the horn upper clamping plates 2 are respectively detachably arranged between the front parts and the back parts, the upper side of the corner of the horn 3 with 3.5 inches is provided with a motor 9, and the output shaft of the motor 9 is provided with a propeller 10. Specifically, the upper arm clamping plate 2, the lower arm clamping plate 1 and the 3.5-inch arm 3 on the same side are fixed together through a pair of screws, and the upper arm clamping plate 2 is additionally fixedly connected with the 3.5-inch arm 3 through one screw;

the motor 9 is fixedly arranged on the upper side of the corner of the 5-inch horn 11, and the propeller 10 is fixedly arranged on the output shaft of the motor 9. Specifically, the upper arm clamping plate 2, the lower arm clamping plate 1 and the 5-inch arm 11 on the same side are fixed together through a pair of screws, and the upper arm clamping plate 2 is additionally fixedly connected with the 5-inch arm 11 through a screw.

So that the 3.5 inch horn 3 and the 5 inch horn 11 can be conveniently replaced on the modular aircraft.

The utility model and its embodiments have been described above with no limitation, and the actual construction is not limited to the embodiments of the utility model as shown in the drawings. In summary, if one of ordinary skill in the art is informed by this disclosure, a structural manner and an embodiment similar to the technical solution should not be creatively devised without departing from the gist of the present utility model.

Claims

1. A modular aircraft with a detachable horn, characterized in that: the device comprises a lower arm clamping plate (1), an upper arm clamping plate (2), a 3.5-inch arm (3), a flight control chart tower (4), an antenna (5), a receiver (6), a top carbon plate (7) and a camera (8);

a top carbon plate (7) is fixedly arranged above the horn upper clamping plate (2), a flight control chart transmission tower (4) is fixedly arranged between the horn upper clamping plate (2) and the top carbon plate (7), an antenna (5) is arranged at the tail of the flight control chart transmission tower (4), a receiver (6) is arranged at the upper side, a camera (8) is fixedly arranged at the front side of the top carbon plate (7), a horn lower clamping plate (1) is fixedly arranged at the lower side of the horn upper clamping plate (2), a pair of 3.5-inch horn (3) are respectively and detachably arranged between the front parts and the rear parts of the horn lower clamping plate (1) and the horn upper clamping plate (2) in a front-back mirror image mode, a motor (9) is fixedly arranged at the upper side of the corner of the 3.5-inch horn (3), and a propeller (10) is fixedly arranged on an output shaft of the motor (9);

the novel mechanical arm further comprises a 5-inch mechanical arm (11), the 5-inch mechanical arm (11) is a pair of front-back mirror type and is detachably arranged between the front parts and the rear parts of the mechanical arm lower clamping plate (1) and the mechanical arm upper clamping plate (2), a motor (9) is fixedly arranged on the upper side of the corner of the 5-inch mechanical arm (11), and a propeller (10) is fixedly arranged on an output shaft of the motor (9).

2. A modular aircraft with a detachable horn according to claim 1, wherein: the upper arm clamping plate (2), the lower arm clamping plate (1) and the 3.5-inch horn (3) on the same side are fixed together through a pair of screws, and the upper arm clamping plate (2) is additionally connected with the 3.5-inch horn (3) through a screw.

3. A modular aircraft with a detachable horn according to claim 1, wherein: the upper arm clamping plate (2), the lower arm clamping plate (1) and the 5-inch arm (11) on the same side are fixed together through a pair of screws, and the upper arm clamping plate (2) is additionally fixedly connected with the 5-inch arm (11) through one screw.

4. A modular aircraft with a detachable horn according to claim 1, wherein: an antenna bracket (12) for placing an antenna (5) is fixedly arranged on the lower side of the top carbon plate (7).

5. A modular aircraft with a detachable horn according to claim 1, wherein: the lower side of the top carbon plate (7) is fixedly provided with a pair of supports (13) positioned on the front side of the flight control chart transmission tower (4), and the camera (8) is arranged between the two supports (13) in an up-down reversible mode.

6. A modular aircraft with a detachable horn according to claim 5, wherein: a camera protection cover (14) is further arranged between the two supports (13), and the camera protection cover (14) is matched and arranged on the camera (8).