Controller of aircraft

Abstract

The utility model provides a controller of an aircraft, which belongs to the technical field of controllers and comprises a mounting plate, and the upper surface of the mounting plate is fixedly connected with a threaded cylinder. The controller main body is connected to the circumferential surface of the threaded cylinder in a sliding manner; the number of the supports is two, and the two supports are fixedly connected to the lower end of the mounting plate; the connecting block is fixedly connected to the surfaces of the two brackets; the rotating column is rotationally connected into the connecting block; by using the device, when the controller main body is not used, the controller main body is stored on the surface of the mounting plate, and at the moment, a user can conveniently carry out other operations.

Description

Technical Field

[0001] The utility model belongs to the technical field of controllers, and particularly relates to a controller for an aircraft. Background Art

[0002] The controller of an aircraft is a key component of an unmanned aerial vehicle (UAV) system, which allows an operator to remotely control the UAV to perform various flight tasks. The controller usually includes a handheld remote control and a ground control station. The handheld remote control is equipped with joysticks, switches and buttons for sending flight instructions such as forward, backward, up, down, roll and yaw. The ground control station is usually a computer system with a display screen for showing the status information, map, flight path and sensor data of the UAV. The controller communicates with the receiver on the UAV through wireless signals, which can be radio waves, Wi-Fi or satellite signals. Inside the controller, a signal processor converts the operator's instructions into electrical signals that the UAV can understand and sends them out through a modem. At the same time, the controller can also receive real-time data transmitted back from the UAV, such as battery status, flight speed and altitude, to ensure that the operator can monitor the status of the UAV and make corresponding adjustments. The controller design of an aircraft focuses on the user experience, aiming to be easy to operate, responsive, and equipped with various protection measures in terms of safety to prevent the UAV from getting out of control or flying into no-fly zones.

[0003] In the prior art, when using a controller to control an aircraft, the user needs to hold the controller by hand. When the controller is not in use, it still needs to be held by hand, resulting in inconvenience for the user to use one hand and making it difficult to perform other operations. Summary of the Utility Model

[0004] The purpose of the utility model is to provide a controller for an aircraft, aiming to solve the problem that when using a controller to control an aircraft in the prior art, the user needs to hold the controller by hand, and when the controller is not in use, it still needs to be held by hand, resulting in inconvenience for the user to use one hand and making it difficult to perform other operations.

[0005] To achieve the above purpose, the utility model provides the following technical solutions:

[0006] A controller for an aircraft, comprising:

[0007] A mounting plate, on the upper surface of which a threaded cylinder is fixedly connected;

[0008] A controller body, which is slidably connected to the circumferential surface of the threaded cylinder;

[0009] Two brackets, both of which are fixedly connected to the lower end of the mounting plate;

[0010] Connecting block, which is fixedly connected to the surfaces of two brackets;

[0011] Rotating column, which is rotatably connected within the connecting block;

[0012] Bottom block, which is fixedly connected to the lower end of the rotating column;

[0013] Arc surface clamping plates, there are two of them, and the two arc surface clamping plates are movably hinged to the lower end of the bottom block through a hinge shaft; and

[0014] Torque spring, which is fixedly connected within the hinge shaft, and the torque spring is fixed to the two arc surface clamping plates.

[0015] As a preferred solution of the present utility model, a positioning threaded block is threadedly connected within the threaded cylinder.

[0016] As a preferred solution of the present utility model, a plurality of limiting columns are fixedly connected to the lower end of the controller main body, a plurality of limiting holes are formed on the upper surface of the mounting plate, and the plurality of limiting columns are respectively slidably connected within the plurality of limiting holes.

[0017] As a preferred solution of the present utility model, two rotating blocks are fixedly connected to the surface of the controller main body, an antenna is rotatably connected within each of the two rotating blocks, and the two antennas are both signal-connected to the controller main body.

[0018] As a preferred solution of the present utility model, cushion pads are fixedly connected to the surfaces of the two arc surface clamping plates.

[0019] As a preferred solution of the present utility model, two ventilation holes are formed within each of the two arc surface clamping plates and the cushion pads.

[0020] Compared with the prior art, the beneficial effects of the present utility model are:

[0021] 1. In this solution, the controller main body is placed on the surface of the mounting plate, so that the limiting columns slide into the limiting holes. Subsequently, the positioning threaded block is threadedly connected to the threaded cylinder to fix the controller main body on the upper surface of the mounting plate, and the storage of the controller main body can be completed. By using this device, when the controller main body is not in use, the controller main body is stored on the surface of the mounting plate, which is convenient for the user to perform other operations at this time.

[0022] 2. In this solution, the cushion pads are used to improve the comfort of the arc surface clamping plates when clamping the user's arm, and the ventilation holes are used to improve the air permeability of the arc surface clamping plates when clamping the user's arm. Description of the Drawings

[0023] The accompanying drawings are used to provide a further understanding of the present utility model and form a part of the description. They are used together with the embodiments of the present utility model to explain the present utility model and do not constitute a limitation to the present utility model. In the accompanying drawings:

[0024] Figure 1 is the first perspective three-dimensional view of the present utility model;

[0025] Figure 2 is the second perspective three-dimensional view of the present utility model;

[0026] Figure 3 is the cross-sectional view of the present utility model.

[0027] In the figure: 1, mounting plate; 2, controller body; 3, threaded cylinder; 4, positioning threaded block; 5, rotating block; 6, antenna; 7, bracket; 8, connecting block; 9, rotating column; 10, bottom block; 11, hinge shaft; 12, torsion spring; 13, arc-shaped clamping plate; 14, cushion; 15, ventilation hole; 16, limiting column. Detailed implementation manners

[0028] Next, the technical solutions in the embodiments of the present utility model will be clearly and completely described in conjunction with the accompanying drawings in the embodiments of the present utility model. Obviously, the described embodiments are only a part of the embodiments of the present utility model, rather than all the embodiments. All other embodiments obtained by those of ordinary skill in the art based on the embodiments of the present utility model without creative efforts shall fall within the protection scope of the present utility model.

[0029] Embodiment

[0030] Please refer to Figures 1 - 3 , the present utility model provides the following technical solutions:

[0031] A controller for an aircraft, comprising:

[0032] A mounting plate 1, on the upper surface of which a threaded cylinder 3 is fixedly connected;

[0033] A controller body 2, which is slidably connected to the circumferential surface of the threaded cylinder 3;

[0034] Two brackets 7, both of which are fixedly connected to the lower end of the mounting plate 1;

[0035] A connecting block 8, which is fixedly connected to the surfaces of the two brackets 7;

[0036] A rotating column 9, which is rotatably connected to the connecting block 8;

[0037] A bottom block 10, which is fixedly connected to the lower end of the rotating column 9;

[0038] The arc-shaped clamping plates 13 are provided in two numbers, and the two arc-shaped clamping plates 13 are movably hinged to the lower end of the bottom block 10 through a hinge shaft 11; and

[0039] The torsion spring 12 is fixedly connected inside the hinge shaft 11, and the torsion spring 12 is fixed to the two arc-shaped clamping plates 13.

[0040] In a specific embodiment of the present utility model, the surface of the mounting plate 1 is used to place the controller body 2, the bracket 7 is used to connect the connecting block 8 and the mounting plate 1, the bottom block 10 is rotatably connected to the connecting block 8 through a rotating column 9, and there is a certain frictional force between the rotating column 9 and the connecting block 8. When rotating the connecting block 8, this frictional force needs to be overcome. Two arc-shaped clamping plates 13 are movably hinged inside the bottom block 10 through a hinge shaft 11, the arc-shaped clamping plates 13 are connected to the torsion spring 12, and the two arc-shaped clamping plates 13 cooperate to clamp at the user's arm. When the controller body 2 is not in use, the controller body 2 is placed on the surface of the mounting plate 1, and the positioning threaded block 4 is used to fix the controller body 2, without the need to hold the controller body 2 by hand. When the controller body 2 is not in use, both hands can be freed for other operations, which facilitates the storage and use of the controller body 2.

[0041] Specifically, please refer to Figures 1 - 3 , a positioning threaded block 4 is threadedly connected inside the threaded cylinder 3.

[0042] In this embodiment: The positioning threaded block 4 is threadedly connected to the threaded cylinder 3, and the positioning threaded block 4 is used to fix the controller body 2, which facilitates the storage of the controller body 2.

[0043] Specifically, please refer to Figures 1 - 3 , a plurality of limiting posts 16 are fixedly connected to the lower end of the controller body 2, and a plurality of limiting holes are formed in the upper surface of the mounting plate 1, and the plurality of limiting posts 16 are respectively slidably connected in the plurality of limiting holes.

[0044] In this embodiment: By connecting the limiting posts 16 with the limiting holes, the controller body 2 will not rotate when placed on the surface of the mounting plate 1, improving the stability of the storage of the controller body 2.

[0045] Specifically, please refer to Figures 1 - 3 , two rotating blocks 5 are fixedly connected to the surface of the controller body 2, and an antenna 6 is rotatably connected inside each of the two rotating blocks 5, and the two antennas 6 are both signal-connected to the controller body 2.

[0046] In this embodiment: An antenna 6 is rotatably connected inside the rotating block 5, and there is a certain frictional force at the connection between the rotating block 5 and the antenna 6. When rotating the antenna 6, this frictional force needs to be overcome.

[0047] Specifically, please refer to Figures 1 - 3 , cushion pads 14 are fixedly connected to the surfaces of the two arc-shaped clamping plates 13.

[0048] In this embodiment, the cushion 14 is used to improve the comfort of the arc-shaped splint 13 when clamping on the user's arm.

[0049] Specifically, please refer to Figures 1 - 3 , two ventilation holes 15 are opened in both of the two arc-shaped splints 13 and the cushion 14.

[0050] In this embodiment, the ventilation holes 15 are used to improve the breathability of the arc-shaped splint 13 when clamping the user's arm.

[0051] It should be noted that: The specific model of the controller body 2 and the antenna 6 to be used is selected by those skilled in the relevant art. And the above about the controller body 2 and the antenna 6, etc. all belong to the prior art, and this solution will not be elaborated here.

[0052] The working principle and usage process of the present utility model: When this device is in use, first use the controller body 2 to control the aircraft, and use the arc-shaped splint 13 to clamp on the user's arm through the elastic force of the torsion spring 12. When the controller body 2 is not in use, place the controller body 2 on the surface of the mounting plate 1, so that the limiting post 16 slides into the limiting hole, and then use the positioning threaded block 4 to be threadedly connected with the threaded cylinder 3 to fix the controller body 2 on the upper surface of the mounting plate 1, and the storage of the controller body 2 can be completed; by using this device, when the controller body 2 is not in use, the controller body 2 is stored on the surface of the mounting plate 1, and at this time it is convenient for the user to perform other operations.

[0053] Finally, it should be noted that: The above are only the preferred embodiments of the present utility model and are not used to limit the present utility model. Although the present utility model has been described in detail with reference to the foregoing embodiments, for those skilled in the art, they can still modify the technical solutions recorded in the foregoing embodiments, or perform equivalent replacements for some of the technical features. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present utility model shall be included within the protection scope of the present utility model.

Claims

1. A controller for an aircraft, characterized in that: include: A mounting plate (1), wherein a threaded barrel (3) is fixedly connected to the upper surface of the mounting plate (1); A controller body (2), wherein the controller body (2) is slidably connected to the circumferential surface of the threaded barrel (3); Two brackets (7) are provided, and both brackets (7) are fixedly connected to the lower end of the mounting plate (1); A connecting block (8), wherein the connecting block (8) is fixedly connected to the surfaces of the two brackets (7); A rotating column (9), wherein the rotating column (9) is rotatably connected in the connecting block (8); A bottom block (10), wherein the bottom block (10) is fixedly connected to the lower end of the rotating column (9); There are two curved surface clamping plates (13), and the two curved surface clamping plates (13) are movably hinged to the lower end of the bottom block (10) through a hinge shaft (11); and A torque spring (12), wherein the torque spring (12) is fixedly connected inside the hinge shaft (11), and the torque spring (12) is fixed to two curved surface clamping plates (13).

2. The aircraft controller according to claim 1, characterized in that: The threaded barrel (3) is internally threadedly connected to a positioning threaded block (4).

3. The aircraft controller according to claim 2, characterized in that: A plurality of limiting columns (16) are fixedly connected to the lower end of the controller body (2), a plurality of limiting holes are provided on the upper surface of the mounting plate (1), and the plurality of limiting columns (16) are respectively slidably connected to the plurality of limiting holes.

4. The aircraft controller according to claim 3, characterized in that: Two rotating blocks (5) are fixedly connected to the surface of the controller body (2), antennas (6) are rotatably connected inside the two rotating blocks (5), and the two antennas (6) are signal-connected to the controller body (2).

5. The aircraft controller according to claim 4, characterized in that: The surfaces of the two curved clamping plates (13) are both fixedly connected with protective pads (14).

6. The aircraft controller according to claim 5, characterized in that: Two ventilation holes (15) are provided in the two curved surface clamping plates (13) and the protective pad (14).

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