Simulation type aircraft flight simulation training cabin

Abstract

The invention discloses a simulation type aircraft flight simulation training cabin. The cabin comprises a cabin main body; an instrument, an electric switch and an illuminating lamp are arranged on the instrument panel; the control board is provided with an undercarriage control assembly, an engine switch, a cold air switch, an oil injector, an accelerator assembly, an elevator adjusting assembly and a flap control assembly; the seat is arranged on the inner bottom surface of the cabin main body; a steering column; a pedal; and the operation indication unit is used for generating indication information for manipulating or checking each device in the cabin main body. The instrument, the electrical switch, the illuminating lamp, the undercarriage control assembly, the engine switch, the cold air switch, the oil injector, the accelerator assembly, the elevator adjusting assembly, the flap control assembly, the seat, the steering column and the pedal are arranged in the cabin main body, so that the real layout in the aircraft cabin is greatly restored; therefore, a pilot can train in a highly restored cockpit, and the training quality is greatly improved.

Description

Technical Field

[0001] The present application relates to the technical field of aircraft simulation training equipment, and in particular to a simulated aircraft flight simulation training cockpit. Background Art

[0002] Simulation training is a necessary process for pilots before formal flight. Through simulation training, pilots can gradually become familiar with and understand the driving of the aircraft, so as to reach the level of being able to fly a real aircraft alone.

[0003] Simulated driving is currently divided into two main methods: one is training through virtual scenes and virtual operating platforms, and the other is training through virtual scenes and real operating platforms. Although the former has the advantage of low cost, it cannot make pilots feel the real operating environment, while the latter makes up for this shortcoming. Pilots can deepen their memory of operations through highly simulated operating platforms, thereby laying a solid foundation for improving their driving ability.

[0004] However, most of the current simulation operating platforms are just simple simulations of the real cockpit, which only simulate the main instruments and equipment such as joysticks and instruments. The degree of restoration of the real cockpit is not high, which greatly reduces the training effect. Summary of the invention

[0005] The embodiment of the present application provides a simulated aircraft flight simulation training cockpit to solve the problem of low degree of cockpit restoration in the prior art.

[0006] On the one hand, an embodiment of the present application provides a simulated aircraft flight simulation training cockpit, comprising:

[0007] Cockpit body;

[0008] The instrument panel is arranged on the inner bottom surface of the cockpit body and is provided with instruments, electrical switches and lighting lamps;

[0009] A control panel is arranged on the inner bottom surface of the cockpit body, and is provided with a landing gear control assembly, an engine switch, a cold air switch, an oiler, a throttle assembly, an elevator adjustment assembly and a flap control assembly;

[0010] A seat, arranged on the inner bottom surface of the cockpit body;

[0011] A control stick, arranged on the inner bottom surface of the cockpit body;

[0012] Footrests, arranged on the inner bottom surface of the cockpit body;

[0013] The operation indication unit is arranged inside the cockpit body and is used to generate indication information for operating or viewing instruments, electrical switches, lighting, landing gear control components, engine switches, air conditioning switches, oilers, throttle components, elevator adjustment components, flap control components, joysticks and pedals.

[0014] The simulated aircraft flight simulation training cockpit in this application has the following advantages:

[0015] By setting instruments, electrical switches, lighting, landing gear control components, engine switches, air conditioning switches, oilers, throttle components, elevator adjustment components, flap control components, seats, joysticks and pedals inside the main body of the cockpit, the actual layout of the aircraft cockpit is greatly restored, allowing pilots to train in a highly restored cockpit, greatly improving the quality of training. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the drawings required for use in the embodiments or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of the present application. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative work.

[0017] Figure 1 A schematic diagram of the external structure of a simulated aircraft flight simulation training cockpit provided in an embodiment of the present application;

[0018] Figure 2 A schematic diagram of the structure of the dashboard provided in the embodiment of the present application;

[0019] Figure 3 A schematic diagram of the structure of the left control panel provided in an embodiment of the present application;

[0020] Figure 4 A schematic diagram of the structure of the right console provided in an embodiment of the present application;

[0021] Figure 5 A schematic diagram of the structure of a cockpit door provided in an embodiment of the present application;

[0022] Figure 6 A schematic diagram of the structure of a landing gear control assembly provided in an embodiment of the present application;

[0023] Figure 7 A schematic diagram of the structure of an engine switch provided in an embodiment of the present application;

[0024] Figure 8 A schematic diagram of the structure of the oiler provided in the embodiment of the present application;

[0025] Fig. 9 A schematic diagram of the structure of an elevator adjustment assembly provided in an embodiment of the present application;

[0026] Fig.10 A schematic diagram of the structure of a flap control assembly provided in an embodiment of the present application.

[0027] Description of reference numerals: 100 - cockpit body, 200 - instrument panel, 300 - left control panel, 310 - right control panel, 400 - door panel, 410 - rotation mechanism, 420 - locking mechanism, 430 - seat, 440 - cushion, 500 - landing gear control housing, 510 - landing gear control handle, 520 - landing gear control synchronizing wheel, 530 - landing gear control sensor, 600 - engine control panel, 610 - engine control damper, 620 - engine control sensor, 630 - engine control pointer , 700-oiler control lever, 710-oiler control frame, 720-oiler control limit lever, 730-oiler control sensor, 740-oiler rebound unit, 800-elevator adjustment plate, 810-elevator adjustment damper, 820-intermediate transmission assembly, 821-elevator adjustment limit lever, 830-elevator adjustment sensor, 840-elevator adjustment limit block, 900-flap control housing, 910-flap control lever, 920-flap control synchronization wheel, 930-flap control sensor. DETAILED DESCRIPTION

[0028] The following will be combined with the drawings in the embodiments of the present application to clearly and completely describe the technical solutions in the embodiments of the present application. Obviously, the described embodiments are only part of the embodiments of the present application, not all of the embodiments. Based on the embodiments in the present application, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of this application.

[0029] Figure 1-10 The present invention provides a structural diagram of a simulated aircraft flight simulation training cockpit. The present invention provides a simulated aircraft flight simulation training cockpit, including:

[0030] Cockpit body 100;

[0031] The instrument panel 200 is arranged on the inner bottom surface of the cockpit body 100, and the instrument panel 200 is provided with instruments, electrical switches and lighting lamps;

[0032] A control panel is arranged on the inner bottom surface of the cockpit body 100, and a landing gear control assembly, an engine switch, a cold air switch, an oiler, a throttle assembly, an elevator adjustment assembly and a flap control assembly are arranged on the control panel;

[0033] A seat 430 is provided on the inner bottom surface of the cabin body 100;

[0034] A control column, arranged on the inner bottom surface of the cockpit body 100;

[0035] Footrests, arranged on the inner bottom surface of the cabin body 100;

[0036] The operation instruction unit is arranged inside the cockpit body 100, and is used to generate instruction information for operating or viewing instruments, electrical switches, lighting, landing gear control components, engine switches, air conditioning switches, oilers, throttle components, elevator adjustment components, flap control components, joysticks and pedals.

[0037] For example, the cockpit body 100 can be installed in a place that can simulate flight scenes, for example, in conjunction with display devices such as a projector or a display screen, to simulate flight scenes through virtual images. At the same time, the cockpit body 100 can also be connected to the ground or other fixed objects using a multi-degree-of-freedom activity mechanism, so that the cockpit body 100 can simulate the activity state in a real driving scene through multi-degree-of-freedom activities.

[0038] In the embodiment of the present application, the cabin body 100 includes a main frame and a skin arranged on the outer side of the main frame. Specifically, the main frame can be formed by welding galvanized steel pipes and angle steels, and the skin can be formed by processing galvanized sheets. After the skin is processed, it can be fixed to the main frame by riveting.

[0039] The instrument panel can be processed into the required shape by cold-rolled sheet, and then laser cut to form openings for the installation of instruments, electrical switches and lighting. The control panel can also be processed into the required shape by cold-rolled sheet, and then laser cut to form openings for the installation of various instruments and equipment.

[0040] In an embodiment of the present application, the control panel includes a left control panel 300 and a right control panel 310, which are respectively installed on the left and right sides of the inner bottom surface of the cockpit body 100, and the landing gear control assembly, engine switch, air conditioning switch, oiler, throttle assembly, elevator adjustment assembly, flap control assembly and other instruments and equipment can be arranged on the corresponding control panels according to the layout of the real aircraft cockpit.

[0041] Furthermore, a vibration unit is provided on the inner bottom surface of the cabin body 100, and when the vibration unit is in operation, it is used to simulate the vibration when the aircraft engine is started.

[0042] Instruments arranged on the instrument panel 200 include an altimeter, an airspeed indicator, a vertical rate indicator, an attitude indicator, a turn and slip indicator, a gyromagnetic compass, a water compass, a radio compass, a volt-ampere meter, a tachometer, an intake pressure gauge, a fuel gauge, an engine multimeter, a cylinder head temperature gauge, an air conditioning pressure gauge, an angle of attack indicator, and an aviation clock, and these instruments are arranged on the instrument panel 200 according to the layout in a real aircraft cockpit. At the same time, the electrical switches and lighting lamps arranged on the instrument panel 200 also use real parts and are arranged at the same position as in a real cockpit.

[0043] Furthermore, the indicator lights include in-cabin indicator lights and out-cabin lighting lights. The in-cabin indicator lights include the adjustment plate neutral position signal light, the generator fault indicator light, the left fuel tank remaining oil 10 liters signal light, the right fuel tank remaining oil 10 liters signal light, and the landing gear indicator light. The out-cabin lighting lights include the cockpit lights, the left fluorescent lamps, and the right fluorescent lamps.

[0044] After adopting the above-mentioned training cockpit layout, the training cockpit will have the same layout as the real cockpit, which will result in multiple devices in the training cockpit that need to be operated or viewed. For pilots with little experience, although they have learned theoretical knowledge before training, they are unable to accurately and quickly apply the theoretical knowledge in the training cockpit in actual operation, resulting in the pilot being unable to operate or view the correct equipment according to the correct steps. In order to solve this problem, the present application sets an operation instruction unit inside the cockpit body 100, which can issue instruction information to each corresponding device in the correct order. The pilot can respond quickly after viewing the instruction information, and after multiple prompts, the pilot can form a memory of the location and function of each device in the training cockpit, thereby helping the pilot to get started quickly.

[0045] Specifically, the operation instruction unit can adopt various devices with display effects, such as display screens or projectors. If a display screen is adopted, it is necessary to set mounting holes near each device, and then install the display screens on the corresponding mounting holes. Each display screen can display the instruction information for each device in sequence under the control of the central controller. When a projector is adopted, it can be set on the top surface of the cockpit body 100 to ensure that the projection range of the projector can cover all devices. When displaying the instruction information, the projector controls the projection content according to the position of each device, so that the instruction information corresponding to each device is projected near the corresponding device. Regardless of the form of the operation instruction unit adopted, when the pilot needs to operate or view a device, the instruction information such as "Please operate (view) xxx here" can be displayed to the device, and the instruction information such as "Please operate (view) xxx on the right (left, front, bottom)" can be displayed to other devices, so that the pilot can accurately and quickly find the device that needs to be operated or viewed.

[0046] In a possible embodiment, one side of the cabin body 100 is open, and a door panel 400 is hinged on the opening. The door panel 400 contacts the seat 430 when closed.

[0047] For example, the door panel 400 can be hinged to the opening of the cabin body through at least one rotating mechanism 410, and the size and shape of the door panel 400 need to match the opening so that the opening can be completely closed after the door panel 400 is closed. The rotating mechanism 410 can be a pin or a hinge.

[0048] In an embodiment of the present application, a locking mechanism 420 can also be provided on the inner side of the door panel 400, that is, on the edge of one side close to the seat 430. The locking mechanism 420 can adopt a latch, and the latch can be provided with an elastic member so that the insertion rod of the latch can automatically rebound after being pulled out, so that it can be automatically plugged into the socket provided on the edge of the cabin body 100.

[0049] Furthermore, the door panel 400 is provided with a cushion 440 on the side facing the seat 430. The cushion 440 and the seat 430 may both be wrapped with a leather surface layer, and the leather surface layer may be imitation leather or genuine leather, so as to improve the pilot's riding comfort. When the door panel 400 is closed, the cushion 440 is located above the seat 430, and the pilot can lean on the cushion 440 when sitting on the seat 430, which greatly improves the pilot's comfort during training.

[0050] In a possible embodiment, the landing gear control assembly includes: a landing gear control housing 500; a landing gear control handle 510, which is rotatably set on the landing gear control housing 500; and a landing gear control sensor 530, which is transmission-connected to the landing gear control handle 510, and the landing gear control sensor 530 is used to detect the rotation angle of the landing gear control handle 510.

[0051] Exemplarily, the landing gear control housing 500 is a hollow box body with openings at two opposite ends. One end of the landing gear control handle 510 is inserted into the landing gear control housing 500 and is rotatably connected to the inside of the landing gear control housing 500 through a rotating shaft, while the other end of the landing gear control handle 510 is located outside the landing gear control housing 500 and a ball is provided at its end for easy operation. The rotating shaft for rotating the landing gear control handle 510 is provided with a landing gear control synchronous wheel 520 on the outer side of the landing gear control housing 500. The landing gear control synchronous wheel 520 rotates coaxially with the rotating shaft, and a landing gear control driven wheel is also rotatably provided on the outer side of the landing gear control housing 500. The landing gear control driven wheel is connected to the landing gear control synchronous wheel 520 by transmission, and specifically can be driven by gear or belt. The landing gear control sensor 530 is connected to the landing gear control synchronous wheel 520, so that the landing gear control sensor 530 rotates with the landing gear control driven wheel, thereby playing a role in detecting the rotation angle of the landing gear control handle 510. After detecting the data of the rotation angle, the landing gear control sensor 530 will transmit the data to the simulation software through the UDP user datagram protocol communication.

[0052] In an embodiment of the present application, a front landing gear indicator rod can also be provided on the front top of the cockpit body 100. The front landing gear indicator rod is movably connected to the cockpit body 100 through an electric push rod, and the electric push rod works under the control of the simulation software, thereby pushing the front landing gear indicator rod to move forward and backward, so as to achieve the effect of showing the status of the front landing gear to the pilot.

[0053] In a possible embodiment, the engine switch includes: an engine control panel 600; an engine control damper 610, which is rotationally connected to the engine control panel 600, and the engine control damper 610 is used to provide resistance to the engine control panel 600 during rotation; an engine control sensor 620, which is connected to the engine control panel 600, and the engine control sensor 620 is used to detect the rotation angle of the engine control panel 600.

[0054] For example, the engine switch adopts a fish scale switch, and its specific installation position and shape are the same as those of the engine switch on the real aircraft. The engine control panel 600 is coaxially fixedly connected with the rotating shaft, and the rotating shaft passes through the engine control damper 610 and is connected to the engine control sensor 620, so that the engine control sensor 620 can detect the rotation angle of the engine control panel 600, and the detected rotation angle will be transmitted to the simulation software through UDP communication.

[0055] The engine control damper 610 can provide rotation damping for the engine control dial 600 , simulating the rotation texture of a real engine switch while also preventing the engine control dial 600 from being misoperated.

[0056] In an embodiment of the present application, the engine control pointer 630 can be fixedly connected to the rotating shaft, and a dial matching the engine control pointer 630 can also be set at the position where the engine switch is installed on the console. When the engine control pointer 630 rotates synchronously with the rotating shaft, the real-time rotation angle of the engine control pointer 630 can be understood in real time through the dial.

[0057] In a possible embodiment, the lubricator includes: a lubricator operating rod 700; a lubricator operating frame 710, on which the lubricator operating rod 700 is axially slidably inserted; a lubricator operating sensor 730, which is connected to the lubricator operating rod 700, and the lubricator operating sensor 730 is used to detect the displacement of the lubricator operating rod 700; and a lubricator rebound unit 740, which is arranged at the end of the lubricator operating rod 700, and the lubricator rebound unit 740 is used to provide elastic force to the lubricator operating rod 700 after being pressed.

[0058] For example, a handle for convenient operation may be provided at the end of the lubricator lever 700, and the lubricator rebound unit 740 includes a rebound rod and an elastic member, the rebound rod may be fixedly provided on the control console, and the end of the rebound rod is coaxially slidably connected with the end of the lubricator lever 700, so that the lubricator 700 can move along the axial direction of the lubricator lever 700 under the pressure of the pilot. The elastic member may be provided between the end of the rebound rod and the end of the lubricator lever 700, and when the lubricator lever 700 is pressed down, the elastic member will be compressed to provide a rebound elastic force to the lubricator lever 700.

[0059] The lubricator operating frame 710 can be fixedly installed on the operating table and slidably connected to the lubricator operating rod 700. The lubricator limiting rod 720 can be set on the outer surface of the lubricator operating rod 700. When the lubricator operating rod 700 moves to the lowest position, the lubricator limiting rod 720 will contact the lubricator operating frame 710, thereby limiting the displacement of the lubricator operating rod 700.

[0060] In an embodiment of the present application, the lubricator operating sensor 730 may include a conductive rod and two conductive probes. The conductive rod may be arranged on the side of the lubricator operating lever 700, and the two conductive probes need to be fixed on the lubricator operating frame 710. When the lubricator operating lever 700 moves to the lowest position, the conductive rod just contacts the two conductive probes, thereby turning on the two conductive probes. The conduction signal will be transmitted to the simulation software via UDP communication.

[0061] In a possible embodiment, the elevator adjustment assembly includes: an elevator adjustment disk 800; an elevator adjustment damper 810 connected to the elevator adjustment disk 800, and the elevator adjustment damper 810 is used to provide resistance when the elevator adjustment disk 800 rotates; an elevator adjustment sensor 830 is transmission-connected to the elevator adjustment disk 800, and the elevator adjustment sensor 830 is used to detect the rotation angle of the elevator adjustment disk 800.

[0062] Exemplarily, the elevator adjustment disk 800 is coaxially connected to the rotating shaft, and the end of the rotating shaft is connected to the elevator adjustment damper 810. The elevator adjustment damper 810 provides rotational damping to the elevator adjustment disk 800, which can simulate the rotation texture of a real elevator adjustment component while preventing the elevator adjustment disk 800 from being operated incorrectly.

[0063] In the embodiment of the present application, a first driving wheel can be arranged on the rotating shaft, and an intermediate transmission component 820 parallel to the rotating shaft and rotatable is arranged inside the control panel. The intermediate transmission component 820 is preferably a rod-shaped structure, on which a first driven wheel and a second driving wheel need to be arranged. The first driven wheel and the first driving wheel can be connected by gear transmission or belt transmission, so that the rotating shaft drives the intermediate transmission component 820 to rotate. At the same time, a terminal driving rod parallel to the intermediate transmission component 820 can also be arranged inside the control panel, and a second driven wheel can be arranged on the terminal driving rod, and the second driven wheel is connected by gear transmission or belt transmission. The elevator adjustment sensor 830 is connected to the end of the terminal driving rod. After the rotation speed of the elevator adjustment disk 800 is reduced by the first driving wheel, the first driven wheel, the second driving wheel and the second driven wheel, the elevator adjustment sensor 830 can detect the rotation angle of the elevator adjustment disk 800 at a certain ratio, and the detected rotation angle will also be transmitted to the simulation software through UDP communication.

[0064] Furthermore, an elevator adjustment limit rod 821 may be provided at the end of the intermediate transmission assembly 820, and an elevator adjustment limit block 840 may be fixedly provided within the rotation range of the elevator adjustment limit rod 821 on the control panel. When the elevator adjustment limit rod 821 rotates together with the intermediate transmission assembly 820, after rotating to a certain angle, the elevator adjustment limit block 840 will contact the elevator adjustment limit rod 821 and limit the rotation of the elevator adjustment limit rod 821, thereby limiting the rotation angle of the elevator adjustment plate 800.

[0065] In a possible embodiment, the flap control assembly includes: a flap control housing 900; a flap control rod 910, which is rotatably disposed on the flap control housing 900; and a flap control sensor 930, which is transmission-connected to the flap control rod 910, and the flap control sensor 930 is used to detect the rotation angle of the flap control rod 910.

[0066] Exemplarily, the flap control housing 900 is a hollow box body with openings at two opposite ends. After one end of the flap control rod 910 is inserted into the flap control housing 900, it is rotatably connected to the inside of the flap control housing 900 through a rotating shaft, while the other end of the flap control rod 910 is located outside the flap control housing 900 and a ball for convenient operation is also arranged at its end. The rotating shaft for rotating the flap control rod 910 is provided with a flap control synchronous wheel 920 on the outer side of the flap control housing 900, and the flap control synchronous wheel 920 rotates coaxially with the rotating shaft, and a flap control driven wheel is also rotatably arranged on the outer side of the flap control housing 900, and the flap control driven wheel is transmission-connected with the flap control synchronous wheel 920, which can be specifically gear transmission or belt transmission, and the flap control sensor 930 is connected with the flap control synchronous wheel 920, so that the flap control sensor 930 rotates with the flap control driven wheel, thereby playing a role in detecting the rotation angle of the flap control rod 910. After detecting the rotation angle data, the flap control sensor 930 will transmit the data to the simulation software via UDP communication.

[0067] Although the preferred embodiments of the present application have been described, those skilled in the art may make additional changes and modifications to these embodiments once they have learned the basic creative concept. Therefore, the appended claims are intended to be interpreted as including the preferred embodiments and all changes and modifications falling within the scope of the present application.

[0068] Obviously, those skilled in the art can make various changes and modifications to the present application without departing from the spirit and scope of the present application. Thus, if these modifications and variations of the present application fall within the scope of the claims of the present application and their equivalents, the present application is also intended to include these modifications and variations.

Claims

1. A simulated aircraft flight simulation training cockpit, characterized in that: include: Cockpit body (100); A dashboard (200) is arranged on the inner bottom surface of the cockpit body (100), and the dashboard (200) is provided with instruments, electrical switches and lighting lamps; A control panel is arranged on the inner bottom surface of the cockpit body (100), and is provided with a landing gear control assembly, an engine switch, a cold air switch, an oiler, a throttle assembly, an elevator adjustment assembly and a flap control assembly; A seat (430) arranged on the inner bottom surface of the cabin body (100); A control column, arranged on the inner bottom surface of the cockpit body (100); Footrests, arranged on the inner bottom surface of the cabin body (100); An operation instruction unit is arranged inside the cockpit body (100), and is used to generate instruction information for operating or viewing the instrument, electrical switch, lighting, landing gear control assembly, engine switch, air conditioner switch, oiler, throttle assembly, elevator adjustment assembly, flap control assembly, joystick and pedals.

2. The simulated aircraft flight simulation training cockpit according to claim 1, characterized in that: The cabin body (100) comprises a main frame and a skin arranged on the outer side of the main frame.

3. The simulated aircraft flight simulation training cockpit according to claim 2, characterized in that: A vibration unit is arranged on the inner bottom surface of the cabin body (100), and when the vibration unit is in operation, the vibration is used to simulate the vibration when the aircraft engine is started.

4. The simulated aircraft flight simulation training cockpit according to claim 1, characterized in that: The instruments arranged on the instrument panel (200) include an altimeter, an airspeed indicator, a vertical rate indicator, an attitude indicator, a turn and slip indicator, a gyromagnetic compass, a water compass, a radio compass, a volt-ampere meter, a tachometer, an intake pressure gauge, a fuel gauge, an engine multimeter, a cylinder head temperature gauge, a cold air pressure gauge, an angle of attack indicator and an aviation clock.

5. The simulated aircraft flight simulation training cockpit according to claim 1, characterized in that: One side of the cabin body (100) is open, and a door panel (400) is hinged on the opening; the door panel (400) contacts the seat (430) when closed.

6. The simulated aircraft flight simulation training cockpit according to claim 1, characterized in that: The landing gear control assembly comprises: Landing gear control housing (500); A landing gear control handle (510), rotatably disposed on the landing gear control housing (500); A landing gear control sensor (530) is in transmission connection with the landing gear control handle (510), and the landing gear control sensor (530) is used to detect the rotation angle of the landing gear control handle (510).

7. The simulated aircraft flight simulation training cockpit according to claim 1, characterized in that: The engine switch comprises: Engine control panel (600); An engine control damper (610) is rotatably connected to the engine control plate (600), and the engine control damper (610) is used to provide resistance to the engine control plate (600) during rotation; An engine control sensor (620) is connected to the engine control panel (600), and the engine control sensor (620) is used to detect the rotation angle of the engine control panel (600).

8. The simulated aircraft flight simulation training cockpit according to claim 1, characterized in that: The oil injector comprises: Oiler operating lever (700); An oiler operating frame (710), on which the oiler operating rod (700) is inserted and slidably connected in the axial direction; A lubricator operating sensor (730) connected to the lubricator operating rod (700), the lubricator operating sensor (730) being used to detect the displacement of the lubricator operating rod (700); The lubricator rebound unit (740) is arranged at the end of the lubricator operating rod (700), and the lubricator rebound unit (740) is used to provide elastic force to the lubricator operating rod (700) after being pressed.

9. The simulated aircraft flight simulation training cockpit according to claim 1, characterized in that: The elevator adjustment assembly comprises: Elevator adjustment plate (800); an elevator adjustment damper (810), connected to the elevator adjustment disk (800), the elevator adjustment damper (810) being used to provide resistance when the elevator adjustment disk (800) rotates; An elevator adjustment sensor (830) is transmission-connected to the elevator adjustment disk (800), and the elevator adjustment sensor (830) is used to detect the rotation angle of the elevator adjustment disk (800).

10. The simulated aircraft flight simulation training cockpit according to claim 1, characterized in that: The flap control assembly comprises: flap control housing (900); A flap control rod (910) is rotatably disposed on the flap control housing (900); A flap control sensor (930) is transmission-connected to the flap control rod (910), and the flap control sensor (930) is used to detect the rotation angle of the flap control rod (910).

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