CN115132019A

CN115132019A - Simulated flight side operating rod assembly

Info

Publication number: CN115132019A
Application number: CN202210850104.6A
Authority: CN
Inventors: 王海飞; 徐伟松; 贾宇霖; 赵建刚; 段志平; 农金鹏
Original assignee: Shenzhen Silver Basis Technology Co Ltd
Current assignee: Shenzhen Silver Basis Technology Co Ltd
Priority date: 2022-07-19
Filing date: 2022-07-19
Publication date: 2022-09-30

Abstract

The application provides a simulated flight side operating rod assembly, which relates to the technical field of aviation simulation and comprises a base body, an operating handle, a universal transmission module, an angle detection module and an elastic piece, wherein an operating opening is formed in the base body; the operating handle is movably connected with the base body through the universal transmission module so that the operating handle can swing relative to the base body, and the angle detection module is used for detecting the swinging angle of the operating handle relative to the base body; the elastic piece is connected to the base body and the universal transmission module at the same time so as to provide damping for the operating handle when the operating handle swings relative to the base body; the elastic member is exposed in an area surrounded by the operation opening. The elastic part can provide the damping when the application of force is in operating handle, promotes the operation and feels, and the elastic part dismouting is convenient nimble, reduces maintenance cost.

Description

Simulated flight side operating rod assembly

Technical Field

The invention relates to the technical field of aviation simulation, in particular to a simulated flying side operating rod assembly.

Background

The flight simulator is a ground training operation device for training and training the flight driving technology of pilots, and is used for carrying out simulated flight operation technology similar to a real airplane by relying on computer hardware and software technology. The high simulation and the strong interactivity are the most remarkable characteristics of simulated flight, and the advanced simulator is adopted to ensure that a pilot is in a flight environment close to the real flight environment, namely cockpit arrangement, and the same instruments and equipment are used as the model of the pilot, so that the pilot just like a real airplane and can finish all flight comprehensive courseware on the simulator. The flight simulator takes a real-time simulation control computer as a core, simulates various elements encountered in real world flight, and is an optical, mechanical and electrical integrated system for simulating the flight state behaviors, flight environments and conditions of the airplane at various stages on the ground. In some projects, a side operating lever device of a civil aircraft cabin needs to be simulated, the side operating lever device comprises a handle and a bottom plate, the handle is installed on the bottom plate through a universal structure, and an angle sensing sensor is arranged on a universal transmission structure installed on the bottom plate; the handle is provided with an operation key, the signal is converted into a signal through digital-to-analog conversion and is sent to the storage unit, the signal is input to the core computer, the control surface of the airplane is driven in a simulation mode, pitching and rolling instructions of the airplane are simulated, and flight simulation training is achieved.

The inventor researches and finds that the existing side operating rod device has the following defects:

in the prior art, dampers are arranged on a roll control shaft and a pitch control shaft in a bottom plate of a side control lever device, belong to wearing parts, are difficult to maintain and have high cost.

Disclosure of Invention

The invention aims to provide a simulated flight side operating rod assembly, which can simplify a damping structure, reduce maintenance cost and reduce operation cost.

The embodiment of the invention is realized by the following steps:

the invention provides a simulated flight side lever assembly, comprising:

the device comprises a base body, an operating handle, a universal transmission module, an angle detection module and an elastic piece, wherein an operating opening is formed in the base body; the operating handle is movably connected with the base body through the universal transmission module so that the operating handle can swing relative to the base body, and the angle detection module is used for detecting the swinging angle of the operating handle relative to the base body; the elastic piece is connected to the base body and the universal transmission module at the same time so as to provide damping for the operating handle when the operating handle swings relative to the base body; the elastic piece is exposed in the area enclosed by the operation opening.

In an alternative embodiment, the elastic member is provided as a spring or a rubber member.

In an alternative embodiment, the base body includes a bottom plate and an adjusting assembly, the adjusting assembly is slidably connected to the bottom plate, the elastic member is connected to both the adjusting assembly and the universal transmission module, and the adjusting assembly is used for adjusting the expansion amount of the elastic member so as to adjust the elastic force of the elastic member.

In an optional embodiment, the adjusting assembly includes a first nut, an adjusting screw, a second nut and a first universal joint, the adjusting screw is disposed on the bottom plate, the first nut and the second nut are both screwed outside the adjusting screw, and the bottom plate is located between the first nut and the second nut; the first universal joint is connected with the adjusting screw rod, and the elastic piece is connected with the first universal joint.

In an alternative embodiment, the adjusting screw is provided with graduation marks.

In an alternative embodiment, the universal transmission module comprises a transmission part, a first rotating shaft and a second rotating shaft, the operating handle is connected with the transmission part, the transmission part is rotatably connected with the first rotating shaft around the axis of the first rotating shaft, the first rotating shaft is perpendicular to and fixedly connected with the second rotating shaft, and the second rotating shaft is rotatably connected with the base body around the axis of the base body;

the elastic piece is connected with the transmission piece through a second universal joint.

In an alternative embodiment, the angle detection module comprises a first angle sensing sensor and a second angle sensing sensor, the first angle sensing sensor is used for detecting the rotation angle of the transmission piece around the axis of the first rotation shaft; the second angle induction sensor is used for detecting the rotation angle of the transmission piece around the axis of the second rotating shaft.

In an optional embodiment, a first tooth structure arranged coaxially with the first rotating shaft is arranged on the transmission member, a positioning plate is arranged on the first rotating shaft, the first angle induction sensor is rotatably connected with the positioning plate around an axis parallel to the first rotating shaft, a second tooth structure is arranged on the first angle induction sensor, and the first tooth structure is meshed with the second tooth structure.

In an optional embodiment, a third tooth structure is sleeved outside the second rotating shaft, the second angle sensing sensor and the transmission member are rotatably connected around an axis parallel to the second rotating shaft, a fourth tooth structure is arranged on the second angle sensing sensor, and the third tooth structure is meshed with the fourth tooth structure.

In an optional implementation manner, the operating handle comprises a holding part, a connecting rod and a folding cover, the holding part is connected with the connecting rod, the connecting rod is connected with the universal transmission module, the folding cover is connected with the holding part and the base body at the same time, and the folding cover can swing relative to the base body at the holding part to adjust the folding state in a self-adaptive manner.

The embodiment of the invention has the beneficial effects that:

in conclusion, the simulation flight side action bars subassembly that this embodiment provided is provided with the elastic component between universal drive module and base member, and the application of force is in operating handle's in-process, and operating handle's motion transmits to universal drive module, then transmits to the elastic component through universal drive module, and the elastic component can produce certain damping to provide the corresponding feedback force of operator, improve the operation and feel, simulation effect is good. And, the elastic component is located between universal drive module and the base member, is not integrated in the axis of rotation of universal drive module and the base member, and directly exposes in the region that the operation mouth on the base member enclosed, when the elastic component damages to need to be changed or when maintaining, directly from operation mouth department to the elastic component carry out corresponding operation can, easy dismounting, cost of maintenance is low, the running cost is low.

Drawings

In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings needed to be used in the embodiments will be briefly described below, it should be understood that the following drawings only illustrate some embodiments of the present invention and therefore should not be considered as limiting the scope, and for those skilled in the art, other related drawings can be obtained according to the drawings without inventive efforts.

FIG. 1 is a schematic structural view of a simulated flight side lever assembly according to an embodiment of the present invention;

FIG. 2 is a schematic diagram of a portion of a simulated flight side lever assembly according to an embodiment of the invention;

FIG. 3 is a schematic structural diagram of a substrate according to an embodiment of the present invention;

FIG. 4 is a schematic structural diagram of a universal transmission module according to an embodiment of the invention;

FIG. 5 is a schematic structural diagram of a universal transmission module and an angle detection module according to an embodiment of the present invention;

fig. 6 is a schematic structural view of an operating handle according to an embodiment of the present invention.

Icon:

001-first direction; 002-a second direction; 003-third direction; 100-a substrate; 110-a top plate; 120-a backplane; 130-a first side panel; 131-a first locating hole; 132-a second positioning hole; 140-a second side panel; 141-a third positioning hole; 150-an operation port; 160-an adjustment assembly; 161-adjusting screw; 162-a first nut; 163-a second nut; 164-first gimbal; 200-operating handle; 210-a grip portion; 220-a connecting rod; 230-a folding cover; 300-universal drive module; 310-a transmission member; 311-a first plate body; 312-a second plate; 313-a third plate body; 314-a fourth plate body; 315-first fixation hole; 316-a second fixing hole; 317-a fourth positioning hole; 318-fifth location hole; 319-a second gimbal; 320-a first rotation axis; 321-a first tooth structure; 330-a second axis of rotation; 340-a third tooth structure; 350-a connecting plate; 400-a first angle sensing sensor; 410-a second tooth structure; 500-a second angle sensing sensor; 510-a fourth tooth structure; 600-an elastic member; 610-hook.

Detailed Description

In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are some, but not all, embodiments of the present invention. The components of embodiments of the present invention generally described and illustrated in the figures herein may be arranged and designed in a wide variety of different configurations.

Thus, the following detailed description of the embodiments of the present invention, presented in the figures, is not intended to limit the scope of the invention, as claimed, but is merely representative of selected embodiments of the invention. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

It should be noted that: like reference numbers and letters refer to like items in the following figures, and thus, once an item is defined in one figure, it need not be further defined and explained in subsequent figures.

In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc. indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings or the orientations or positional relationships that the products of the present invention are conventionally placed in use, and are only used for convenience in describing the present invention and simplifying the description, but 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 present invention. Furthermore, the terms "first," "second," "third," and the like are used solely to distinguish one from another, and are not to be construed as indicating or implying relative importance.

Furthermore, the terms "horizontal", "vertical" and the like do not imply that the components are required to be absolutely horizontal or pendant, but rather may be slightly inclined. For example, "horizontal" merely means that the direction is more horizontal than "vertical" and does not mean that the structure must be perfectly horizontal, but may be slightly inclined.

In the description of the present invention, it should also be noted that, unless otherwise explicitly specified or limited, the terms "disposed," "mounted," "connected," and "connected" are to be construed broadly and may, for example, be fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in a specific case to those of ordinary skill in the art.

At present, when a pilot simulates flight, a simulator is used, and the pilot can finish all flight comprehensive courseware on the simulator. The flight simulator takes a real-time simulation control computer as a core, simulates various elements encountered in real world flight, and is an optical, mechanical and electrical integrated system for simulating the flight state behaviors, flight environments and conditions of the airplane at various stages on the ground. The side operating rod simulation piece arranged in the cockpit is mainly used for simulating a control surface of a driving airplane and pitching and rolling instructions of the airplane so as to realize flight simulation training. Among the prior art, in order to improve the feel of side action bars, need set up damping structure on side action bars usually, damping structure integration is loaded down with trivial details in the axis of rotation of side action bars or in the base of side action bars, and damping structure dismouting is maintained and is overhauld inconveniently. And the damping structure is a quick-wear part, the replacement and overhaul frequency is high, and the design of the damping structure in the prior art leads to the increase of the later maintenance cost.

With reference to fig. 1 to 6, in view of this, a designer designs a simulated flight side operation rod assembly, which can reduce the difficulty of assembling and disassembling the damping structure and reduce the maintenance cost.

Referring to fig. 1, fig. 2 and fig. 5, in the present embodiment, the simulated flying side joystick assembly includes a base 100, an operating handle 200, a universal transmission module 300, an angle detection module and an elastic member 600, wherein the base 100 is provided with an operating opening 150; the operating handle 200 is movably connected with the base body 100 through the universal transmission module 300 so that the operating handle 200 can swing relative to the base body 100, and the angle detection module is used for detecting the swinging angle of the operating handle 200 relative to the base body 100; the elastic member 600 is connected to both the base 100 and the universal transmission module 300 to provide damping to the manipulation handle 200 when the manipulation handle 200 swings with respect to the base 100; the elastic member 600 is exposed to the area surrounded by the operation opening 150.

The working principle of the simulated flight side operating rod assembly provided by the embodiment is as follows:

when performing the simulation training, the operator holds the operation handle 200, and can press the function button on the operation handle 200 to output the instruction. Furthermore, various actions of the aircraft during flight can be simulated by shaking the operating handle 200. In the process of shaking the operating handle 200, the operating handle 200 swings relative to the base 100, and the operating handle 200 is connected with the base 100 through the universal transmission module 300, so that the operating handle 200 can swing relative to the base 100 within a range of 360 degrees, and the operation is flexible. Simultaneously, when the operator application of force drove its motion in operating handle 200, elastic component 600 can provide a power that hinders the motion of universal drive module 300, and this power passes through universal drive module 300 and transmits to operating handle 200, makes the operator receive the feedback force, promotes to experience and feels, appears controlling the excessive risk when avoiding novice driver simulation. The elastic member 600 is exposed at the operation opening 150 on the base body 100, so that the elastic member 600 can be directly overhauled or replaced and other related operations from the operation opening 150, the operation is convenient and flexible, the operation difficulty is reduced, and the maintenance cost is reduced.

It should be noted that the functional button may be designed with reference to a button on a handle of an existing real aircraft, and the structural design of the functional button may adopt an existing known structure, which is not specifically described in this embodiment.

Referring to fig. 3, in the present embodiment, the base 100 optionally includes a top plate 110, a bottom plate 120, a first side plate 130, and a second side plate 140. The top plate 110 and the bottom plate 120 are arranged in parallel at intervals in a first direction 001, the first side plate 130 and the second side plate 140 are located between the top plate 110 and the bottom plate 120, the first side plate 130 and the second side plate 140 are fixedly connected with the top plate 110 and the bottom plate 120 through screws and other structures, and the first side plate 130 and the second side plate 140 are arranged in parallel at intervals in a second direction 002 perpendicular to the first direction 001. Thus, the top plate 110, the bottom plate 120, the first side plate 130 and the second side plate 140 jointly define a through hole, both open ends of the through hole are the operation openings 150, that is, the base body 100 has two operation openings 150, and operations such as disassembling and assembling of the elastic member 600 can be performed from at least one of the two operation openings 150 as required, which is flexible and convenient.

Optionally, the first side plate 130 is provided with a first positioning hole 131 and a second positioning hole 132. The first positioning hole 131 and the second positioning hole 132 are cylindrical through holes, axes of the first positioning hole 131 and the second positioning hole 132 extend in the second direction 002, the first positioning hole 131 and the second positioning hole 132 are arranged at intervals in the first direction 001, and the first positioning hole 131 is located on one side of the second positioning hole 132 close to the top plate 110. Meanwhile, a third positioning hole 141 is provided on the second side plate 140, the third positioning hole 141 is a cylindrical through hole, and the third positioning hole 141 and the first positioning hole 131 are coaxially disposed. Bearings may be disposed in the first positioning hole 131, the second positioning hole 132, and the third positioning hole 141.

Further, the base 100 further includes an adjustment assembly 160. The adjusting assembly 160 is slidably connected to the base 100 in a first direction 001, wherein the first direction 001 is an arrangement direction of the top plate 110 and the bottom plate 120, and the first side plate 130 and the second side plate 140 are arranged at intervals in a second direction 002 perpendicular to the first direction 001. Optionally, the adjustment assembly 160 includes an adjustment screw 161, a first nut 162, a second nut 163, and a first gimbal 164. The middle position of the bottom plate 120 is provided with an assembly through hole which is a cylindrical hole, the adjusting screw 161 is inserted into the assembly through hole, the first nut 162 and the second nut 163 are both screwed outside the adjusting screw 161, and the bottom plate 120 is clamped between the first nut 162 and the second nut 163. One end of the adjusting screw 161 close to the top plate 110 is provided with a first universal joint 164, and the first universal joint 164 is used for connecting with the elastic member 600. By means of the design, the position of the first universal joint 164 can be adjusted by adjusting the distance between one end, close to the top plate 110, of the adjusting screw 161 and the bottom plate 120, so that the stretching length of the elastic piece 600 is changed, the initial elastic force of the elastic piece 600 is adjusted, the damping adjusting function is achieved, and the operation habits of different operators are adapted. In a specific operation, by screwing the first nut 162 and the second nut 163, the positions of the first nut 162 and the second nut 163 on the adjusting screw 161 can be adjusted, and the length of the adjusting screw 161 extending between the bottom plate 120 and the top plate 110 can be changed by clamping the bottom plate 120 through the first nut 162 and the second nut 163.

It should be understood that the adjusting assembly 160 may also be other structures that can slide relative to the base plate 120, such as a telescopic cylinder, a lead screw transmission structure, and an electric push rod, which are not listed in this embodiment.

Furthermore, in order to improve the accuracy of the position of the adjusting screw 161 and facilitate the position adjustment of an operator, scale marks are arranged on the adjusting screw 161, and the numerical values shown by the scale marks are used as references during adjustment, so that the adjustment is convenient and reliable, the adjustment time is shortened, and the efficiency is improved.

Referring to fig. 2, fig. 4 and fig. 5, in the present embodiment, the universal transmission module 300 optionally includes a transmission member 310, a first rotating shaft 320 and a second rotating shaft 330. The transmission part 310 is arranged in a rectangular frame structure, the transmission part 310 comprises a first plate body 311, a second plate body 312, a third plate body 313 and a fourth plate body 314 which are sequentially connected end to end, the first plate body 311 and the third plate body 313 are arranged in the first direction 001 at parallel intervals, the second plate body 312 and the fourth plate body 314 are arranged in the third direction 003 at parallel intervals, and the first direction 001, the second direction 002 and the third direction 003 are pairwise perpendicular. First plate 311 is provided with first fixing hole 315, third plate 313 is provided with second fixing hole 316, and first fixing hole 315 and second fixing hole 316 are coaxially disposed. A fourth positioning hole 317 is disposed on the second plate 312, a fifth positioning hole 318 is disposed on the fourth plate 314, the fourth positioning hole 317 and the fifth positioning hole 318 are coaxially disposed, and bearings may be disposed in both the fourth positioning hole 317 and the fifth positioning hole 318. The two ends of the first rotating shaft 320 are respectively inserted into the bearings in the first positioning hole 131 and the third positioning hole 141, and are rotatably connected with the base 100 around the axis thereof. The two ends of the second rotating shaft 330 are inserted into the bearings in the fourth positioning hole 317 and the fifth positioning hole 318, respectively, and are rotatably connected with the transmission member 310 around the axis thereof. The first rotating shaft 320 and the second rotating shaft 330 are perpendicularly crossed and fixedly connected, for example, the first rotating shaft 320 may be sleeved outside the second rotating shaft 330 and fixedly connected by a bolt. In this way, the transmission member 310 and the second rotating shaft 330 can rotate around the axis of the first rotating shaft 320 relative to the base 100 under the driving of the first rotating shaft 320, and the transmission member 310 can also rotate relative to the second rotating shaft 330 alone. Through the cooperation of the first rotating shaft 320 and the second rotating shaft 330, the transmission member 310 can be freely swung within a range of 360 °. Meanwhile, the operating handle 200 is connected to the transmission member 310, so that the operating handle 200 can be arbitrarily swung within a range of 360 °.

Further, a second universal joint 319 is disposed in the second fixing hole 316 of the third plate body 313, and an end of the elastic member 600 away from the first universal joint 164 is connected to the second universal joint 319, and in an initial state, the elastic member 600 is in a stretched state, so that the transmission member 310 receives a force from the top plate 110 to the bottom plate 120. By the engagement of the first and second

universal joints

164 and 319, the elastic force of the elastic member 600 can be divided into the second direction 002 and the third direction 003, and when the operator applies force to the operation handle 200 to swing with respect to the base 100, the operator receives the force fed back by the elastic member 600, thereby generating a damping effect.

Further, a first tooth structure 321 is sleeved on the first rotating shaft 320, and the first tooth structure 321 is a sector gear. The first tooth structure 321 and the first rotating shaft 320 are relatively fixed in the circumferential direction of the first rotating shaft 320, and the first tooth structure 321 is located on one side of the first side plate 130 away from the second side plate 140, that is, the first tooth structure 321 is located outside the base 100, so that the assembly and disassembly are facilitated. Correspondingly, the angle detection module comprises a first angle induction sensor 400 and a second angle induction sensor 500, wherein the first angle induction sensor 400 is used for detecting the rotation angle of the transmission member 310 around the axis of the first rotation shaft 320; the second angle sensing sensor is used to detect the angle of rotation of the transmission member 310 about the axis of the second rotating shaft 330. First angle-sensitive sensor 400 is located on first curb plate 130, first angle-sensitive sensor 400 disposes second tooth structure 410, second tooth structure 410 rotationally connects with second locating hole 132 to first tooth structure 321 and the meshing of second tooth structure 410, when operating handle 200 so transmitted the moment of torsion to universal transmission and made it rotate around the axis of first axis of rotation 320, first tooth structure 321 drove second tooth structure 410 and rotates, second tooth structure 410 pivoted angle acquires through first angle-sensitive sensor 400. Meanwhile, a third tooth structure 340 is disposed on the second plate 312, a connecting plate 350 is fixed outside the second rotating shaft 330, the second angle sensor 500 is disposed on the connecting plate 350, the second angle sensor 500 is configured with a fourth tooth structure 510, and the fourth tooth structure 510 is engaged with the third tooth structure 340. When the transmission member 310 is driven by the operation handle 200 to rotate around the second rotation axis 330, the third tooth structure 340 transmits the torque to the fourth tooth structure 510, so as to obtain the angle parameter of the fourth tooth structure 510 through the second angle-sensing sensor 500.

Referring to fig. 1, in the present embodiment, optionally, the operating handle 200 includes a holding portion 210, a connecting rod 220 and a folding cover 230, the holding portion 210 is connected to the connecting rod 220, the connecting rod 220 is inserted into the first fixing hole 315 and fixedly connected to the first plate 311, the folding cover 230 is simultaneously connected to the holding portion 210 and the top plate 110 of the base 100, and the folding cover 230 can swing relative to the base 100 at the holding portion 210 to adaptively adjust a folded state. It should be understood that the folding cover 230 may be a rubber member, and may adopt any known structure, which can accommodate the movement of the grip portion 210 relative to the base 100, and always keep the gap between the grip portion 210 and the base 100 closed, and has high sealing performance.

In this embodiment, the elastic member 600 may be a spring, a rubber member, or the like. For example, in this embodiment, the elastic member 600 is a tension spring, the two ends of the elastic member 600 are both provided with the hooks 610, and the hooks 610 are respectively connected with the first gimbal 164 and the second gimbal 319, so that the assembly and disassembly are convenient and fast.

The embodiment provides a simulated flying side operating rod assembly, damping received when the elastic piece 600 is used for simulating the movement of the operating handle 200, the elastic piece 600 is convenient to disassemble and assemble, and the maintenance cost is reduced. Meanwhile, the initial elasticity of the elastic member 600 can be adjusted as needed, thereby adapting to the requirements of different operators for damping.

The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention, and various modifications and changes may be made by those skilled in the art. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims

1. A simulated flight side lever assembly, comprising:

2. The simulated flight-side lever assembly of claim 1, wherein:

the elastic piece is set to be a spring or a rubber piece.

3. The simulated flight-side lever assembly of claim 1, wherein:

the base member includes bottom plate and adjusting part, adjusting part with bottom plate slidable connects, the elastic component connect simultaneously in adjusting part with the universal drive module, adjusting part is used for adjusting the flexible volume of elastic component, in order to adjust the elasticity of elastic component.

4. The simulated flight-side lever assembly of claim 3, wherein:

the adjusting assembly comprises a first nut, an adjusting screw rod, a second nut and a first universal joint, the adjusting screw rod penetrates through the bottom plate, the first nut and the second nut are both screwed outside the adjusting screw rod, and the bottom plate is located between the first nut and the second nut; the first universal joint is connected with the adjusting screw rod, and the elastic piece is connected with the first universal joint.

5. The simulated flight-side lever assembly of claim 4, wherein:

and the adjusting screw rod is provided with scale marks.

6. The simulated flight-side lever assembly of claim 1, wherein:

the universal transmission module comprises a transmission part, a first rotating shaft and a second rotating shaft, the operating handle is connected with the transmission part, the transmission part and the first rotating shaft are rotatably connected around the axis of the first rotating shaft, the first rotating shaft and the second rotating shaft are vertically arranged and fixedly connected, and the second rotating shaft and the base body are rotatably connected around the axis of the base body;

7. The simulated flight-side lever assembly of claim 6, wherein:

the angle detection module comprises a first angle induction sensor and a second angle induction sensor, and the first angle induction sensor is used for detecting the rotation angle of the transmission piece around the axis of the first rotating shaft; the second angle induction sensor is used for detecting the rotation angle of the transmission piece around the axis of the second rotating shaft.

8. The simulated flight side lever assembly of claim 7, wherein:

the transmission part is provided with a first tooth structure coaxially arranged with the first rotating shaft, the first rotating shaft is provided with a positioning plate, the first angle induction sensor and the positioning plate are rotatably connected around an axis parallel to the first rotating shaft, the first angle induction sensor is provided with a second tooth structure, and the first tooth structure is meshed with the second tooth structure.

9. The simulated flight-side lever assembly of claim 7, wherein:

the second angle sensing sensor is connected with the transmission piece in a rotating mode around an axis parallel to the second rotating shaft, and is provided with a fourth tooth structure meshed with the third tooth structure.

10. The simulated flight side lever assembly of claim 1, wherein:

the operating handle comprises a holding part, a connecting rod and a folding cover, the holding part is connected with the connecting rod, the connecting rod is connected with the universal transmission module, the folding cover is connected with the holding part and the base body at the same time, and the folding cover can enable the holding part to self-adaptively adjust the folding state relative to the base body in a swinging mode.