Electric operating load device

By electrically manipulating the load device, a millisecond-level dynamic response is achieved using a brushless permanent magnet servo motor and a high-precision encoder. This solves the problems of response delay and force simulation distortion in traditional hydraulic systems, providing high-precision force feedback. It is suitable for flight simulators and industrial servo systems.

CN224020344UActive Publication Date: 2026-03-20EASY CONTROL INTELLIGENT TECHNOLOGY (TIANJIN) CO LTD
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Patent Information

Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2025-05-12
Publication Date
2026-03-20

AI Technical Summary

Technical Problem

Traditional hydraulic control load systems suffer from problems such as response delay, high energy consumption, complex maintenance, and distortion of force sensing simulation, making it difficult to meet the requirements for high-precision real-time force feedback and affecting the training effect of pilots.

Method used

It adopts an electrically operated load device, using a brushless permanent magnet servo motor and a high-precision encoder, combined with PWM modulation technology to achieve millisecond-level dynamic response. Through modular design, it can be adapted to different models, and the structure is lightweight and the rope and wheel transmission is optimized to reduce motion inertia.

Benefits of technology

It achieves high-precision, real-time force loading feedback, enabling pilots to perceive the stick force and displacement characteristics of real aircraft in a virtual environment, reducing training costs, and is suitable for flight simulators and industrial servo systems.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model provides an electric control load device, which comprises a mounting rack, two parallel cross beams and two parallel longitudinal beams, and the two cross beams are connected through the two longitudinal beams to form a frame structure; one end of the operating rod is connected with one end of one longitudinal beam; the transmission mechanism is parallel to the longitudinal beam, and one end of the transmission mechanism is connected with the operating rod; and the loading mechanism is connected with the mounting frame, and one end of the loading mechanism is connected with the other end of the transmission mechanism. The structure is light in weight and modularized, movement inertia is reduced, and meanwhile the requirement for quick replacement of operating devices of different models is met through detachable module design.
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Description

TECHNICAL FIELD

[0001] The utility model relates to operating load device technical field especially relates to a kind of electric operating load device. BACKGROUND

[0002] With the continuous development of China's aviation industry, the demand for pilots is increasing, and if real aircraft is used for training each time, not only the cost is high, but also it cannot be trained under extreme conditions, which greatly increases the cost of pilot training. The aircraft simulator can reflect the various conditions of the aircraft in the air in real time through specific simulation equipment, so that the pilot can complete various training on the ground, and can not be restricted by weather, environment and climate, greatly reducing the training cost and shortening the training cycle, while ensuring the safety of the pilot to the greatest extent during training. The operating load system is a key component of the simulator, which aims to provide the pilot with consistent operating feeling as the real aircraft, and its performance directly affects the user experience of the operator.

[0003] The technical bottleneck of traditional mechanical hydraulic system, traditional hydraulic operating load system relies on fluid transmission, and has problems such as response delay, high energy loss, complex maintenance, etc., which is difficult to meet the demand of high-precision real-time force feedback. The hydraulic system is sensitive to temperature and sealing, and is prone to performance degradation due to leakage or oil pollution, especially in harsh scenes such as aviation simulation, which has insufficient reliability. Force simulation distortion: mechanical structure friction, inertia force compensation is not sufficient, etc. cause the pilot to feel the deviation between the rod force in the simulator and the real aircraft, which affects the training effect. Therefore, an electric operating load device is urgently needed. UTILITY MODEL CONTENT

[0004] (I) Technical problem to be solved

[0005] Based on the above problems, the utility model provides an electric operating load device to alleviate the technical problems of insufficient dynamic response and poor environmental adaptability in the prior art.

[0006] (II) Technical scheme

[0007] The utility model provides an electric operating load device, comprising:

[0008] Mounting frame, with two parallel arranged cross beams and two parallel arranged longitudinal beams, two cross beams are connected to form a frame structure through two longitudinal beams;

[0009] Operating rod, one end is connected with one end of one longitudinal beam;

[0010] Transmission mechanism, parallel to the longitudinal beam, one end of the transmission mechanism is connected with the operating rod;

[0011] A load mechanism is connected with the mounting frame, and one end of the load mechanism is connected with the other end of the transmission mechanism.

[0012] In the embodiment of the utility model, the two cross beams of the mounting frame are all equipped with reinforcing plates at the connection with the two longitudinal beams.

[0013] In the embodiment of the utility model, the joystick is axially connected with the longitudinal beam through the mounting plate.

[0014] In the embodiment of the utility model, the transmission mechanism comprises:

[0015] The clamp block, the first connecting rod, the force sensor and the second connecting rod are sequentially connected, and the clamp block clamps the joystick and the joystick.

[0016] The clamp block, the first connecting rod, the force sensor and the second connecting rod are sequentially connected, and the clamp block clamps the joystick and the joystick.

[0017] In the embodiment of the utility model, the load mechanism comprises:

[0018] The fixed frame, the speed reducer, the servo motor and the rocker are connected.

[0019] The load mechanism is located at the other end of the longitudinal beam opposite to the one end of the longitudinal beam connected with the joystick.

[0020] The fixed frame is provided with a mounting hole, and the fixed frame is connected with the mounting frame.

[0021] The servo motor is connected with the fixed frame, and the servo motor has a rotating shaft, and the rotating shaft passes through the mounting hole.

[0022] One end of the rocker is fixedly connected with the rotating shaft, and the other end of the rocker is axially connected with the second connecting rod.

[0023] The servo motor is connected with the speed reducer.

[0024] In the embodiment of the utility model, the speed reducer is a planetary speed reducer.

[0025] In the embodiment of the utility model, the connection between the rocker and the rotating shaft is a key connection.

[0026] (Three) beneficial effects

[0027] From the above technical solution, the electrically operated load device has at least one or part of the following beneficial effects:

[0028] The structure is lightweight and modular, the motion inertia is reduced, and the quick replacement requirement of different models of operating devices is met through the detachable module design. BRIEF DESCRIPTION OF DRAWINGS

[0029] Figure 1 It is a structural schematic view of the electric operating load device of the embodiment of the utility model.

[0030] Figure 2 It is a structural schematic view of the mounting frame of the electric operating load device of the embodiment of the utility model.

[0031] Figure 3 It is a structural schematic view of the operating rod of the electric operating load device of the embodiment of the utility model.

[0032] Figure 4 It is a structural schematic view of the transmission mechanism of the electric operating load device of the embodiment of the utility model.

[0033] Figure 5 It is a structural schematic view of the load mechanism of the electric operating load device of the embodiment of the utility model.

[0034] Figure 6 It is a structural schematic view of the fixed frame of the electric operating load device of the embodiment of the utility model.

[0035]

Explanation of main elements symbol in the drawings of the embodiment of the utility model

[0036] 1 mounting frame

[0037] 11 crossbeam

[0038] 12 longitudinal beam

[0039] 13 reinforcing plate

[0040] 2 operating rod

[0041] 21 mounting plate

[0042] 3 transmission mechanism

[0043] 31 clamping block

[0044] 32 first connecting rod

[0045] 33 force sensor

[0046] 34 second connecting rod

[0047] 4 load mechanism

[0048] 41 fixed frame

[0049] 411 mounting hole

[0050] 42 speed reducer

[0051] 43 servo motor

[0052] 44 rocker DETAILED DESCRIPTION

[0053] The utility model provides a kind of electric control load device, the electric control load device adopts brushless permanent magnet servo motor and high-precision encoder, millisecond level dynamic response is realized by PWM modulation technique, and the real-time and smoothness of force loading are improved.Lightweight structure and modular design, optimize rope wheel transmission mechanism and steel wire rope layout, reduce the moment of inertia, simultaneously by detachable module design adaptation different model control device The quick replacement demand of device, the main shortcomings and deficiencies of existing control load device can be overcome.

[0054] To make the purpose, technical scheme and advantages of the utility model more clear and obvious, the following will be combined with specific embodiment, and referring to drawing, the utility model is further detailed.

[0055] In the utility model embodiment, a kind of electric control load device is provided, as shown in Figure 1 And Figure 2 Electric control load device, including: mounting bracket 1, with two parallelly arranged cross beams 11 and two parallelly arranged longitudinal beams 12, two cross beams 11 are connected to form frame structure by two longitudinal beams 12.Longitudinal lever 2, one end is connected with the one end of one longitudinal beam 12.Transmission mechanism 3, it is arranged in parallel with longitudinal beam 12, one end of transmission mechanism 3 is connected with longitudinal lever 2.Load mechanism 4 is connected with mounting bracket 1, one end of load mechanism 4 is connected with the other end of transmission mechanism 3.

[0056] In the utility model embodiment, as shown in Figure 2 Two cross beams 11 of mounting bracket and the connecting place of two longitudinal beams 12 are all equipped with reinforcing plate 13.

[0057] In the utility model embodiment, as shown in Figure 1 And Figure 3 Longitudinal lever 2 is connected with longitudinal beam by mounting plate 21.

[0058] In the utility model embodiment, as shown in Figure 4 Transmission mechanism 3 includes: clamp block 31, first connecting rod 32, force sensor 33 and second connecting rod 34.Clamp block 31, first connecting rod 32, force sensor 33 and second connecting rod 34 are sequentially connected, clamp block 31 clamps longitudinal lever 2 and is connected with longitudinal lever 2.

[0059] In the utility model embodiment, as shown in Figure 1 And Figure 5As shown, the load mechanism 4 comprises a fixed frame 41, a speed reducer 42, a servo motor 43 and a rocker 44. The load mechanism 4 is located at the other end of the longitudinal beam opposite to the longitudinal beam end connected with the operating rod 2. The fixed frame 41 is provided with a mounting hole 411, and the fixed frame 41 is connected with the mounting frame 1. The servo motor 43 is connected with the fixed frame 41, and the servo motor 43 has a rotating shaft penetrating through the mounting hole 411. One end of the rocker 44 is fixedly connected with the rotating shaft, and the other end of the rocker 44 is connected with the second connecting rod in a shaft connection mode. The servo motor 43 is connected with the speed reducer 42.

[0060] In the embodiment of the utility model, the speed reducer is planetary speed reducer.

[0061] In the embodiment of the utility model, the connection between the rocker and the rotating shaft is key connection.

[0062] Hereinbefore, the embodiment of the utility model has been described in detail in combination with the drawings. It should be noted that the implementation mode not shown or described in the drawings or the specification is the form known by the ordinary skilled in the art, and is not described in detail. In addition, the definition of the above-mentioned elements and methods is not limited to the various specific structures, shapes or modes mentioned in the embodiment, and the ordinary skilled in the art can make simple changes or replacements.

[0063] According to the above description, the skilled in the art should have a clear understanding of the electric load operating device.

[0064] In conclusion, the electric load operating device can be applied to aviation flight simulation training: providing high-fidelity operating force feeling for full-motion flight simulator, supporting pilots to perceive the lever force displacement characteristics of real aircraft in virtual environment. Industrial servo system test: adapting to dynamic load simulation of robot and electric vehicle driving motor. The electric load operating device replaces the traditional hydraulic system through electric driving technology, combines high-precision control algorithm and modular structure design, solves the dynamic response, and becomes the key technical carrier of high-end simulation training and industrial test.

[0065] It should be further noted that the directional phrases mentioned in the embodiment, such as "up", "down", "front", "back", "left", "right" and the like, are only the directions of the drawings, and are not used to limit the protection scope of the utility model. Throughout the drawings, the same elements are represented by the same or similar reference numerals. When it may cause confusion to the understanding of the utility model, the conventional structure or configuration will be omitted.

[0066] And the shape and size of each component in the figure do not reflect the true size and proportion, but only illustrate the content of the embodiment of the utility model. In addition, in the claims, any reference symbol located between parentheses should not be constructed as a limitation on the claims.

[0067] Unless otherwise indicated, the numerical parameters in the specification and attached claims are approximations. Depending upon the desired properties, the numerical parameters set forth in the specification and claims can vary somewhat. At the very least, each numerical parameter should be construed in light of the stated purpose of the implement the concepts disclosed and claimed herein. A person skilled in the art will recognize that many of the examples provided herein have a degree of operational flexibility, versatility, and / or equivalency that would be appreciated only by a person skilled in the art, and the scope of the application should be construed to cover any such alterations or modifications of the examples that have different step sequences and / or relative step importance assignments or uses of equivalent means.

[0068] Further, the word "comprise" or "comprising" does not exclude the presence of elements or steps other than those listed in a claim. The word "a" or "an" preceding an element does not exclude the presence of a plurality of such elements.

[0069] The use of the word "about" or "approximately" in relation to a numerical value refers to a value that is within 10% of the value, in some embodiments within 5% of the value, in some embodiments within 1% of the value, and in some embodiments within 0.1% of the value.

[0070] Furthermore, the order of steps or order for executing processing steps presented in the concepts claimed herein is not necessarily the same as that utilized in the example embodiments. Also, the individual steps can occur in any order or be executed in any sequence or in parallel, unless otherwise indicated, and are contingent on input available from any of the preceding or following steps in the state machine flow diagram. Furthermore, embodiments can be based on design choices and considerations of reliability, and can be mixed and matched with other embodiments, i.e. features of different embodiments can be freely combined in order to achieve yet further embodiments.

[0071] Those skilled in the art will appreciate that the modules in the apparatuses in the embodiments can be adapted and placed in one or more apparatuses other than the embodiments. The modules or units or components in the embodiments can be combined into one module or unit or component, and further can be divided into multiple sub-modules or sub-units or sub-components. In addition to the fact that at least some of such features and / or processes or units are mutually exclusive, all features disclosed in the specification (including the claims, abstract and drawings) and all processes or units of any method or apparatus disclosed thus can be combined in any combination. Unless explicitly stated otherwise, each feature disclosed in the specification (including the claims, abstract and drawings) can be replaced by an alternative feature providing the same, equivalent or similar purpose. Also, in unit claims that include several devices, several of those devices can be embodied by one and the same hardware item.

[0072] Similarly, it is to be understood that the brunt of the description of the exemplary embodiments of the present application above has sometimes grouped various features together in a single embodiment, figure, or description thereof for the purposes of streamlining the disclosure and aiding in the elucidation of one or more of the various disclosed aspects. However, one of ordinary skill in the art will understand that not all of the features and elements described above will necessarily be required in each and every instance of the application. In addition, while the above description has been made with regard to a number of embodiments, it is contemplated that various alterations, modifications, and improvements will readily occur to those skilled in the art. Accordingly, the application is intended to embrace all such alterations, modifications, and improvements as fall within the scope of the appended claims. In particular, with regard to the various functions performed by the above described components, devices, circuits, and systems, the terms (including a reference to a "means") used to describe such components are intended to correspond, unless otherwise indicated, to any component which performs the specified function of the described component (e.g., a "means for determining" can correspond to any of the components described above which is configured to perform the functions of the described means). In addition, the logics described herein can be embodied in various forms, including hardware, software, or any combination thereof. For example, the logics can be implemented in software as one or more instructions or code on a computer-readable medium, which is executed by a processor. From this code, the processor can directly or indirectly in response to the execution of the code, perform the functions and / or operations described herein. In another example, the logics can be implemented in hardware, which does not necessarily involve software.

[0073] The above description of the specific embodiments, the purpose, technical solutions and beneficial effects of the present application are further detailed, it should be understood that the above description is only the specific embodiments of the present application, and is not intended to limit the present application, any modification, equivalent replacement, improvement, etc. made within the spirit and principles of the present application should be included in the protection scope of the present application.

Claims

1. An electrically operated load control device, characterized in that, include: The mounting frame has two parallel crossbeams and two parallel longitudinal beams, and the two crossbeams are connected by the two longitudinal beams to form a frame structure; One end of the control lever is connected to one end of the longitudinal beam; A transmission mechanism is arranged parallel to the longitudinal beam, and one end of the transmission mechanism is connected to the control lever; A load mechanism is connected to the mounting bracket, and one end of the load mechanism is connected to the other end of the transmission mechanism.

2. The electrically operated load device according to claim 1, characterized in that, Reinforcing plates are installed at the joints between the two crossbeams and the two longitudinal beams of the mounting frame.

3. The electrically operated load device according to claim 1, characterized in that, The control lever is axially connected to the longitudinal beam via a mounting plate.

4. The electrically operated load device according to claim 1, characterized in that, The transmission mechanism includes: Clamping block, first connecting rod, force sensor and second connecting rod; The clamping block, the first connecting rod, the force sensor, and the second connecting rod are connected in sequence, and the clamping block holds the control lever and is connected to the control lever.

5. The electrically operated load device according to claim 4, characterized in that, The load mechanism includes: Mounting frame, speed reducer, servo motor and joystick; The load mechanism is located at the other end of the longitudinal beam opposite to one end of the longitudinal beam to which the control lever is connected; The fixing frame is provided with mounting holes, and the fixing frame is connected to the mounting frame; The servo motor is connected to the mounting bracket, and the servo motor has a rotating shaft that passes through the mounting hole; One end of the rocker arm is fixedly connected to the rotating shaft, and the other end of the rocker arm is connected to the second connecting rod as an axis. The servo motor is connected to the reducer.

6. The electrically operated load device according to claim 5, characterized in that, The speed reducer is a planetary speed reducer.

7. The electrically operated load device according to claim 5, characterized in that, The connection between the rocker arm and the rotating shaft is a keyed connection.