An integrated control cockpit for unmanned aerial vehicles

Abstract

The utility model discloses a kind of height integration control flight cabin suitable for unmanned aerial vehicle, including cabin table, display, throttle push rod, joystick, integrated control panel, display is installed on bracket, bracket is set in cabin table rear side;Throttle push rod, joystick and integrated control panel are all set in the top of cabin table, integrated control panel is set below display, throttle push rod and joystick are all located in the front side of cabin table.The technical effects reached are as follows: using integrated design, pilot completes relevant operation in a centralized control area, accelerates take-off preparation speed, improves flight efficiency.Each subsystem's operating state can be better monitored and managed through integrated design, reduce human error, centralized control interface can clearly present each key parameter and operation option, so that pilot will not miss important information due to frequent shift of sight between multiple instruments and control devices, ensure operation accuracy, so that it can better cope with flight condition.

Description

Technical Field

[0001] This utility model relates to the field of aircraft cockpit technology, specifically to a highly integrated control flight cockpit adapted for unmanned aerial vehicles (UAVs). Background Technology

[0002] With the rapid development of aviation technology, the complexity and functional diversity of aircraft control are constantly increasing. Traditional flight cockpits have many shortcomings. For example, various flight control switches, instruments, and displays are scattered, requiring pilots to frequently shift their gaze and attention during operation, which can easily lead to operational errors and reaction delays. Moreover, the information exchange between various systems is not efficient enough, making it difficult to achieve rapid and precise coordinated control. In addition, for some new types of aircraft, such as UAV swarm control and special mission aircraft, more convenient, efficient, and intelligent cockpit control solutions are needed. Utility Model Content

[0003] Therefore, this utility model provides a highly integrated control flight cockpit adapted to unmanned aerial vehicles (UAVs) to solve the above-mentioned problems in the prior art.

[0004] To achieve the above objectives, this utility model provides the following technical solution:

[0005] According to a first aspect of the present invention, a highly integrated control flight cockpit adapted for unmanned aerial vehicles includes a cockpit table, a display, a throttle lever, a joystick, and an integrated control panel, wherein the display is mounted on a bracket, and the bracket is disposed behind the cockpit table.

[0006] The throttle lever, the joystick, and the integrated control panel are all located on the top of the cockpit table. The integrated control panel is located below the display. The throttle lever and the joystick are both located on the front side of the cockpit table, and the throttle lever and the joystick are respectively located on the left and right sides.

[0007] The display, the throttle lever, and the joystick are all electrically connected to the integrated control panel.

[0008] Furthermore, the display includes multiple displays, each of which is set independently of the others.

[0009] Furthermore, it also includes an audible and visual alarm, which is mounted on the integrated control panel.

[0010] Furthermore, it also includes a multi-function socket, which is mounted on the cockpit table.

[0011] Furthermore, the multi-functional socket is a lift-type multi-functional socket.

[0012] Furthermore, it also includes multiple casters, all of which are located at the bottom of the cockpit table.

[0013] Furthermore, the number of the movable wheels is four, and the four movable wheels are arranged in a rectangular pattern.

[0014] Furthermore, the moving wheels are made of Fomas wheels.

[0015] Furthermore, the bracket is detachably connected to the cockpit table.

[0016] Furthermore, the support frame is height-adjustable.

[0017] This invention has the following advantages: The entire flight cockpit adopts an integrated design, allowing the pilot to complete relevant operations in a centralized control area, accelerating takeoff preparation and improving flight efficiency. The integrated design allows for better monitoring and management of the operational status of each subsystem, reducing human error. The centralized control interface clearly presents key parameters and operating options, preventing the pilot from missing important information due to frequent shifts in their gaze between multiple instruments and control devices, ensuring accurate operation and enabling better response to flight conditions. Attached Figure Description

[0018] To more clearly illustrate the embodiments of this utility model or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the drawings in the following description are merely exemplary, and those skilled in the art can derive other embodiments based on the provided drawings without creative effort.

[0019] The structures, proportions, sizes, etc. illustrated in this specification are only for the purpose of assisting those skilled in the art in understanding and reading the content disclosed herein, and are not intended to limit the implementation conditions of this utility model. Therefore, they have no substantial technical significance. Any modifications to the structure, changes in the proportional relationships, or adjustments to the size, without affecting the effects and purposes that this utility model can produce, should still fall within the scope of the technical content disclosed in this utility model.

[0020] Figure 1 This is a schematic diagram of the overall structure of a highly integrated control flight cockpit adapted for unmanned aerial vehicles (UAVs) provided for some embodiments of this utility model.

[0021] In the picture: 1. Cockpit table, 2. Casters, 3. Monitor, 4. Bracket, 5. Audible and visual alarm, 6. Throttle lever, 7. Joystick, 8. Integrated control panel, 9. Multi-function socket. Detailed Implementation

[0022] The following specific embodiments illustrate the implementation of this utility model. Those skilled in the art can easily understand other advantages and effects of this utility model from the content disclosed in this specification. Obviously, the described embodiments are only some, not all, of the embodiments of this utility model. Based on the embodiments of this utility model, all other embodiments obtained by those skilled in the art without creative effort are within the protection scope of this utility model.

[0023] Example 1

[0024] like Figure 1 As shown, a highly integrated control flight cockpit adapted to an unmanned aerial vehicle (UAV) according to the first aspect embodiment of the present invention includes a cockpit table 1, a display 3, a throttle lever 6, a joystick 7, and an integrated control panel 8. The display 3 is mounted on a bracket 4, and the bracket 4 is located behind the cockpit table 1.

[0025] Throttle lever 6, joystick 7 and integrated control panel 8 are all located on the top of cockpit table 1. Integrated control panel 8 is located below display 3. Throttle lever 6 and joystick 7 are both located on the front side of cockpit table 1, and throttle lever 6 and joystick 7 are respectively located on the left and right sides.

[0026] The display 3, throttle lever 6, and joystick 7 are all electrically connected to the integrated control panel 8. During use, commands are sent to the drone through the integrated control panel 8 to control it to perform corresponding actions.

[0027] In this embodiment, it should be noted that the entire flight cockpit needs to be equipped with a corresponding seat for use. The display 3 includes multiple screens, which can be used to display different system and instrument information. Each screen is set independently. The bracket 4 is detachably connected to the cockpit table 1. The bracket 4 is height-adjustable so that the display 3 can be adjusted to a suitable height during use.

[0028] The technical effects achieved by this embodiment are as follows: The entire flight cockpit adopts an integrated design, allowing the pilot to complete relevant operations in a centralized control area, accelerating takeoff preparation and improving flight efficiency. The integrated design enables better monitoring and management of the operational status of each subsystem, reducing human error. The centralized control interface clearly presents each key parameter and operation option, preventing the pilot from missing important information due to frequent shifts in their gaze between multiple instruments and control devices, ensuring accurate operation and enabling them to better respond to flight conditions.

[0029] Example 2

[0030] like Figure 1As shown in the figure, this embodiment provides another highly integrated control flight cockpit adapted to UAVs, the structure of which includes all the contents of embodiment 1. Only the different parts are described below.

[0031] In this embodiment, an audible and visual alarm 5 is also included. The audible and visual alarm 5 is installed on the integrated control panel 8. During flight, if a system malfunctions, the audible and visual alarm 5 will issue an audible and visual alarm to promptly remind the pilot.

[0032] In this embodiment, it should be noted that a multi-function socket 9 is also included. The multi-function socket 9 is installed on the cockpit table 1. The multi-function socket 9 is a liftable multi-function socket, which can be used for charging, connecting an external microphone, etc.

[0033] Example 3

[0034] like Figure 1 As shown in the figure, this embodiment provides another highly integrated control flight cockpit adapted to UAVs, the structure of which includes all the contents of embodiment 1. Only the different parts are described below.

[0035] In this embodiment, a plurality of casters 2 are also included, all of which are located at the bottom of the cockpit table 1.

[0036] In this embodiment, it should be noted that there are four movable wheels 2, which are arranged in a rectangular shape. The movable wheels 2 are made of fumarole, and the special bearing design of fumarole can keep them level on uneven ground, ensuring that the equipment remains stable on various terrains and surfaces.

[0037] The entire flight cockpit operates as follows: Before use, the cockpit table 1 can be quickly moved to a suitable position using the casters 2, depending on the usage scenario. Upon entering the cockpit, the system automatically performs a self-check. After the self-check, the pilot inputs flight plan information, such as the origin, destination, and waypoints, through the integrated control panel 8, and the planning results are displayed on the monitor 3. During flight, the pilot can control the aircraft via the touch-sensitive integrated control panel 8. Alternatively, the pilot can manually control the throttle stick 6 and joystick 7 to adjust the drone's speed and flight attitude. Simultaneously, the monitor 3 updates and displays changes in flight altitude and other relevant flight parameters in real time. If a system malfunctions during flight, the audible and visual alarm 5 will sound, and the pilot can take appropriate countermeasures based on the prompts. Additionally, the retractable multi-functional socket allows for charging and connecting an external microphone.

[0038] The technical effects achieved by this embodiment are as follows: it enables highly integrated control of the UAV, assisting the pilot in precise control; it has a reasonable structure, stable operation, and high adaptability. In terms of safety, integrated display of flight information reduces human error caused by viewing scattered instruments, and real-time monitoring and early warning of anomalies effectively prevent accidents. In terms of efficiency, it simplifies operation and optimizes flight paths to reduce energy consumption. In terms of user experience, centralized control facilitates operation and observation, reduces the pilot's workload, and comprehensive information display enhances situational awareness, enabling the pilot to better respond to flight conditions.

[0039] Although the present invention has been described in detail above with general descriptions and specific embodiments, some modifications or improvements can be made to it, which will be obvious to those skilled in the art. Therefore, all such modifications or improvements made without departing from the spirit of the present invention fall within the scope of protection claimed by the present invention.

[0040] The terms such as "upper," "lower," "left," "right," and "middle" used in this specification are merely for clarity of description and are not intended to limit the scope of implementation of this utility model. Any changes or adjustments to their relative relationships, without substantially altering the technical content, shall also be considered within the scope of implementation of this utility model.

Claims

1. A highly integrated control flight cockpit adapted for unmanned aerial vehicles (UAVs), characterized in that, Includes a cockpit table (1), a display (3), a throttle lever (6), a joystick (7), and an integrated control panel (8). The display (3) is mounted on a bracket (4), which is located behind the cockpit table (1). The throttle lever (6), the rocker arm (7) and the integrated control panel (8) are all located on the top of the cockpit table (1). The integrated control panel (8) is located below the display (3). The throttle lever (6) and the rocker arm (7) are both located on the front side of the cockpit table (1), and the throttle lever (6) and the rocker arm (7) are respectively located on the left and right sides. The display (3), the throttle lever (6), and the rocker arm (7) are all electrically connected to the integrated control panel (8).

2. The highly integrated control flight cockpit adapted for unmanned aerial vehicles according to claim 1, characterized in that, The display (3) includes multiple display screens, each of which is set independently of the others.

3. The highly integrated control flight cockpit adapted for unmanned aerial vehicles according to claim 1, characterized in that, It also includes an audible and visual alarm (5), which is mounted on the integrated control panel (8).

4. The highly integrated control flight cockpit adapted for unmanned aerial vehicles according to claim 1, characterized in that, It also includes a multi-function socket (9) which is located on the cockpit table (1).

5. A highly integrated control flight cockpit adapted for unmanned aerial vehicles according to claim 4, characterized in that, The multi-functional socket (9) is a lift-type multi-functional socket.

6. The highly integrated control flight cockpit adapted for unmanned aerial vehicles according to claim 1, characterized in that, It also includes multiple casters (2), all of which are located at the bottom of the cockpit table (1).

7. A highly integrated control flight cockpit adapted for unmanned aerial vehicles according to claim 6, characterized in that, The number of the moving wheels (2) is four, and the four moving wheels (2) are arranged in a rectangular shape.

8. A highly integrated control flight cockpit adapted for unmanned aerial vehicles according to claim 6, characterized in that, The moving wheel (2) is a Foma wheel.

9. A highly integrated control flight cockpit adapted for unmanned aerial vehicles according to claim 1, characterized in that, The bracket (4) is detachably connected to the cockpit table (1).

10. A highly integrated control flight cockpit adapted for unmanned aerial vehicles according to claim 9, characterized in that, The bracket (4) is height-adjustable.

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