A pilot health index real-time monitoring device

By installing a health monitoring device with a camera and a rotating drive mechanism on the aircraft, the problems of helmet weight and visual obstruction in existing technologies are solved, achieving high-accuracy pilot health monitoring that is burden-free and unobstructed.

CN119723797BActive Publication Date: 2026-07-24CIVIL AVIATION FLIGHT UNIV OF CHINA
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Patent Information

Application Number
CN202411575827.5
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2024-11-06
Publication Date
2026-07-24
Estimated Expiration
2044-11-06

AI Technical Summary

Technical Problem

Existing pilot health monitoring devices increase helmet weight, causing discomfort to pilots and posing a safety hazard of visual obstruction.

Method used

Design a real-time health index monitoring device to be installed in an appropriate location on an aircraft. Use two cameras to capture images of the pilot's eye area in real time, analyze and judge the health index through a central processor, adjust the position of the cameras by rotating a drive mechanism to ensure clear images, and set an alarm to provide timely warnings.

Benefits of technology

It enables health monitoring without additional burden, avoids obstruction of vision, and improves monitoring accuracy and safety.

✦ Generated by Eureka AI based on patent content.

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Abstract

The application discloses a kind of pilot health index real-time monitoring device, belong to monitoring technical field, including: shell, mounting block, rotating mouth, camera, rotating drive mechanism, central processing unit, alarm;The device of the application is installed in the adaptive position of aircraft, will not increase any burden in the flight process of pilot, at the same time, also will not cause the occlusion of the line of sight in the flight process of pilot, improve the use safety of device.
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Description

Technical Field

[0001] This invention belongs to the field of monitoring technology, specifically relating to a real-time monitoring device for pilot health index. Background Technology

[0002] As the core of air transport, the physical health of pilots is directly related to flight safety and the operational quality of airlines. With increasingly heavy flight missions and longer flight times, pilots' physical fitness and health are facing severe challenges. Therefore, real-time monitoring of pilots' health indices and timely detection and intervention of potential health problems are of great significance for ensuring flight safety.

[0003] Chinese patent application number 202111392482.6 discloses a helmet for comprehensive monitoring of pilot health status. The helmet includes an ultra-fine elastic conductive bristle bundle, a blood flow detection mechanism, and a facial color detection mechanism. When the helmet is in use, the ultra-fine elastic conductive bristle bundle collects the pilot's electroencephalogram (EEG) signals, the blood flow detection mechanism detects the pilot's blood condition, and the facial color detection mechanism detects the pilot's facial color. Based on the pilot's EEG signals, blood condition, and facial color, the pilot's health index is determined, achieving real-time monitoring.

[0004] The above technology has the following problems: The ultra-fine elastic conductive bristle bundle, blood flow detection mechanism and facial color detection mechanism of the above structure are all integrated into the helmet. Although it can monitor the pilot's health index in real time, it increases the weight of the helmet, that is, increases the burden on the pilot's head during flight. If the flight time is long, it is easy to cause discomfort to the pilot. At the same time, the integration of the structure can easily cause visual obstruction for the pilot, which may pose a safety hazard.

[0005] Therefore, a real-time monitoring device for pilot health index is designed to solve the above problems. Summary of the Invention

[0006] To address the problems mentioned in the background section, this invention provides a real-time pilot health index monitoring device that does not increase the pilot's workload during flight, nor does it obstruct the pilot's view, thus improving the device's safety.

[0007] To achieve the above objectives, the present invention provides the following technical solution: a real-time monitoring device for pilot health index, comprising:

[0008] The outer casing, used to mount the various structures of the device;

[0009] There are two mounting blocks, which are symmetrically fixed in the middle of the mounting sides at the top and bottom of the outer shell, and are used to fix the outer shell to the fitting position on the aircraft.

[0010] There are two rotating openings, located on the camera side of the outer casing, for mounting the camera structure of the device and for allowing the camera structure to be rotated and adjusted.

[0011] There are two cameras, located inside two rotating ports, used to capture images of the pilot's eye area;

[0012] A rotation drive mechanism, fitted between the housing and the two cameras, is used to drive the two cameras to rotate and adjust their positions so that the two cameras can capture images of the pilot's eye area.

[0013] The central processing unit, fixed to the top of the outer casing, is used to receive images of the pilot's eye area captured by two cameras, process and analyze them, determine whether there are any abnormal conditions, including fatigue and pain, and send alarm commands when there are abnormal conditions.

[0014] The alarm, fixed to the top of the casing, is used to receive alarm commands from the central processing unit and provide audible and visual alarms to serve as a warning.

[0015] Furthermore, the rotation drive mechanism includes:

[0016] The first rotating shaft is rotatably connected to the inside of the outer casing at one end via a bearing, and is used to support rotation.

[0017] Two circular plates are provided. One circular plate is fixed at one end to the other end of the first rotating shaft, and the other circular plate is located inside the outer shell on the other side for mounting the rotation drive mechanism structure.

[0018] A drive mechanism, assembled between the outer casing and another circular plate, is used to drive the other circular plate to rotate;

[0019] A fixed shaft is attached to the two circular plates near the rotating opening. It is used to install the rotation drive mechanism structure and allows the circular plates to rotate along with it.

[0020] There are two fixed blocks, symmetrically fixed to the fixed shaft, used to install the rotation drive mechanism structure;

[0021] A double-ended screw is rotatably connected to two circular plates away from the fixed axis via bearings, and is used to install a rotary drive mechanism structure.

[0022] A follower mechanism is assembled between the outer casing and the double-ended screw to enable the double-ended screw to rotate accordingly.

[0023] There are two movable blocks, which are symmetrically connected to the double-ended screw through a transmission nut, and are used to move in the opposite direction when the double-ended screw rotates;

[0024] Two movable frames are provided, located on the same side outside the fixed block and the movable block, and are fixedly connected to the two cameras to drive the two cameras to rotate.

[0025] The first movable opening is provided in four pairs, symmetrically opened on the two movable frames. The two fixed blocks and the two movable blocks are located in the four first movable openings respectively, so that the two movable frames can be fitted over the two fixed blocks and the two movable blocks through the four first movable openings.

[0026] The second rotating shaft has eight shafts, which are symmetrically connected to the top and bottom of the two fixed blocks and the two movable blocks by bearings, and are used to move with the two movable blocks.

[0027] The second movable opening is provided in eight symmetrically arranged in four groups on the two movable frames. The other end of each of the eight second rotating shafts extends into the eight second movable openings, which are used to drive the two movable frames to move as the eight second rotating shafts move.

[0028] Furthermore, the drive mechanism includes:

[0029] The motor is fixed to the outer wall of the housing and is used to provide rotational driving force;

[0030] The drive shaft, with one end connected to the motor output via a coupling, is used to transmit rotational driving force;

[0031] The third rotating shaft is fixed to the side wall of another circular plate and is used to drive the connected circular plate to rotate.

[0032] The first adsorption mechanism is assembled between the drive shaft and the third rotating shaft. It is used to adsorb and connect the drive shaft and the third rotating shaft so that the drive shaft drives the third rotating shaft to rotate, thereby driving the connected circular plate to rotate.

[0033] Furthermore, the first adsorption mechanism includes:

[0034] An electromagnet is fixed to the drive shaft away from the motor end wall to generate electromagnetic attraction.

[0035] The connecting block is sleeved on the outside of the third rotating shaft. Two limiting strips are symmetrically fixed to the outer wall of the third rotating shaft. Two limiting grooves are symmetrically opened on the inner wall of the connecting block. The two limiting strips are placed in the two limiting grooves and are used to slide on the third rotating shaft and connect with the electromagnet when the electromagnet is energized.

[0036] A connecting spring is sleeved outside the third rotating shaft, with its two ends fixed to the connecting block and the circular plate close to each other on the side walls, and is used to automatically reset when the electromagnet is de-energized.

[0037] Furthermore, the follower mechanism includes:

[0038] The first gear is fixedly sleeved on the drive shaft and is used to generate driving force;

[0039] The bracket is fixed to the side wall of the circular plate near the first gear and is used to install the follower mechanism structure.

[0040] The follower shaft is rotatably connected to the bracket via bearings and is used to transmit the follower driving force;

[0041] The second adsorption mechanism is assembled between the follower shaft and the double-ended screw, and is used to adsorb and connect the follower shaft and the double-ended screw so that the follower shaft drives the double-ended screw to rotate.

[0042] The second gear is fixedly sleeved on the follower shaft near the end wall of the first gear and meshes with the first gear to generate follower driving force.

[0043] Furthermore, the second adsorption mechanism has the same structure as the first adsorption mechanism.

[0044] Compared with the prior art, the beneficial effects of the present invention are:

[0045] 1. The device of the present invention is installed in a suitable position on the aircraft, which will not increase any burden on the pilot during flight, nor will it obstruct the pilot's line of sight during flight, thus improving the safety of the device.

[0046] 2. This invention uses two cameras to capture images of the pilot's two eye areas in real time during flight. The central processing unit processes and analyzes these images in real time to determine the pilot's eye condition and then their health index. Based on the pilot's health index, relevant operations are performed. Compared with existing technologies, this dual discrimination based on images of two eye areas can improve the monitoring accuracy of the device.

[0047] 3. The present invention is equipped with a rotation drive mechanism, which enables two cameras to track the pilot's eyes in real time, thereby capturing eye area images that better express the pilot's eye state and improving the monitoring accuracy of the device. Attached Figure Description

[0048] Figure 1 This is a perspective view of the present invention;

[0049] Figure 2 This is a cross-sectional view of the present invention;

[0050] Figure 3 For the present invention Figure 2 Enlarged view of point A in the middle;

[0051] In the diagram: 1. Outer casing; 2. Central processing unit; 3. Alarm; 4. Mounting block; 5. Rotating port; 6. Camera;

[0052] 101. Circular plate; 102. Fixing block; 103. Fixing shaft; 104. First rotating shaft; 105. Double-ended screw; 106. Movable frame; 107. Movable block; 108. Second rotating shaft; 109. First movable opening; 110. Second movable opening;

[0053] 201. Motor; 202. Drive shaft; 203. Third rotating shaft;

[0054] 301. Electromagnet; 302. Connecting spring; 303. Connecting block;

[0055] 401, First gear; 402, Support; 403, Follower shaft; 404, Second gear. Detailed Implementation

[0056] The technical solutions of the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of the present invention, and not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of the present invention.

[0057] A real-time pilot health index monitoring device, comprising:

[0058] The outer casing 1 is used to install the various structures of the device;

[0059] Mounting blocks 4 are provided in two, symmetrically fixed in the middle of the mounting sides at the top and bottom of the outer shell 1, for fixing the outer shell 1 to the fitting position on the aircraft.

[0060] There are two rotating ports 5, which are located on the camera side of the outer casing 1. They are used to install the camera structure of the device and also allow for the rotation and adjustment of the camera structure.

[0061] Camera 6, there are two of them, set in two rotating ports 5, for capturing images of the pilot's eye area;

[0062] A rotation drive mechanism is fitted between the outer casing 1 and the two cameras 6, and is used to drive the two cameras 6 to rotate and adjust their positions so that the two cameras 6 can capture images of the pilot's eye area.

[0063] The central processing unit 2, fixed to the top of the outer casing 1, is used to receive images of the pilot's eye area captured by the two cameras 6, process and analyze them, determine whether there are any abnormal conditions including fatigue and pain, and send an alarm command when there are abnormal conditions.

[0064] Alarm 3 is fixed to the top of the outer casing 1 and is used to receive alarm commands from the central processing unit 2 and provide audible and visual alarms to serve as a warning.

[0065] The central processing unit 2 is electrically connected to the camera 6, the rotation drive mechanism, and the alarm 3.

[0066] In this embodiment, please refer to the appendix. Figure 1-2 Before the device is used, the two mounting blocks 4 are fixed to the adapter position on the aircraft with screws, that is, the device is fixed to the adapter position on the aircraft.

[0067] When the device is in use, the central processing unit 2 controls the two cameras 6 to start, capture images, and transmit them to the central processing unit 2 for processing and analysis. If the central processing unit 2 determines that the two images do not represent the pilot's eye area, it controls the rotation drive mechanism to start, which drives the two cameras 6 to rotate. During this process, the two cameras 6 continue to capture images until the central processing unit 2 determines that the two images represent the pilot's eye area and stops. During the pilot's flight, the two cameras 6 continuously capture images and transmit them to the central processing unit 2 for processing and analysis. If the central processing unit 2 determines that the pilot's eye condition is fatigued or in pain, it sends an alarm command, and the alarm 3 sounds, so that timely action can be taken. If the central processing unit 2 determines that the results of the two images are different, it receives the two images from the next moment for reprocessing and analysis. During this process, if the pilot's eye area moves, the above correction work of the two cameras 6 is repeated to achieve real-time monitoring of the pilot's health index.

[0068] Specifically, the rotation drive mechanism includes:

[0069] The first rotating shaft 104 is rotatably connected to the inside of the outer shell 1 through a bearing at one end, and is used to support rotation.

[0070] Two circular plates 101 are provided. One circular plate 101 is fixedly connected to the other end of the first rotating shaft 104 at one end, and the other circular plate 101 is provided on the other side inside the outer shell 1 for mounting the rotation drive mechanism structure.

[0071] A drive mechanism is assembled between the outer casing 1 and another circular plate 101 for driving the other circular plate 101 to rotate.

[0072] The fixed shaft 103 is fixedly connected to the two circular plates 101 on the side near the rotating opening 5, and is used to install the rotation drive mechanism structure, and at the same time, it can rotate along with the circular plates 101 when they rotate.

[0073] Two fixed blocks 102 are provided and symmetrically fixed to the fixed shaft 103 for mounting the rotation drive mechanism structure;

[0074] The double-ended screw 105 is rotatably connected to the two circular plates 101 on the side away from the fixed shaft 103 via bearings, and is used to install the rotation drive mechanism structure.

[0075] A follower mechanism is assembled between the outer casing 1 and the double-ended screw 105 to enable the double-ended screw 105 to rotate accordingly.

[0076] Two movable blocks 107 are provided and are symmetrically connected to the double-ended screw 105 via transmission nuts, and are used to move in the opposite direction when the double-ended screw 105 rotates;

[0077] Two movable frames 106 are provided, which are located outside the fixed block 102 and movable block 107 on the same side and are fixedly connected to the two cameras 6 to drive the two cameras 6 to rotate.

[0078] The first movable opening 109 is provided in four pairs, symmetrically opened on the two movable frames 106. The two fixed blocks 102 and the two movable blocks 107 are respectively located in the four first movable openings 109, so that the two movable frames 106 can be fitted over the two fixed blocks 102 and the two movable blocks 107 through the four first movable openings 109.

[0079] The second rotating shaft 108 is provided in eight parts, which are symmetrically connected to the top and bottom of the two fixed blocks 102 and the two movable blocks 107 by bearings, and are used to move with the two movable blocks 107.

[0080] The second movable opening 110 is provided in eight symmetrically arranged on the two movable frames 106. The other ends of the eight second rotating shafts 108 extend into the eight second movable openings 110 respectively, and are used to drive the two movable frames 106 to move with the movement of the eight second rotating shafts 108.

[0081] The central processing unit 2 is electrically connected to the drive mechanism.

[0082] In this embodiment, please refer to the appendix. Figure 2The rotation drive mechanism drives the connected circular plate 101 to rotate. The connected circular plate 101 drives the fixed shaft 103, the double-ended screw 105, and the follower mechanism to rotate. The fixed shaft 103 and the double-ended screw 105 respectively drive the connected fixed block 102 and the movable block 107 to rotate. The connected fixed block 102 and the movable block 107 respectively drive the connected second rotating shaft 108 to rotate. The connected second rotating shaft 108 drives the connected movable frame 106 to rotate. The connected movable frame 106 drives the connected camera 6 to rotate up and down in the corresponding rotating port 5. When the image captured by the camera 6 during this process contains the pilot's eye area but is not located in the center, the rotation of the circular plate 101 stops. The drive mechanism drives the follower mechanism to rotate, which in turn drives the double-headed screw 105 to rotate. During the rotation of the double-headed screw 105, the two movable blocks 107 move in opposite directions on the double-headed screw 105. The two movable blocks 107 drive the connected second rotating shaft 108 to move in the same direction. During the movement of the connected second rotating shaft 108, it moves within the corresponding second movable opening 110, which drives the two movable frames 106 to move left and right. The two movable frames 106 drive the two cameras 6 to rotate left and right within the corresponding rotating opening 5 until the image captured by the camera 6 during this process contains the pilot's eye area and is located in the center, thus realizing the drive for the two cameras 6 to rotate and adjust their positions.

[0083] Specifically, the drive mechanism includes:

[0084] Motor 201 is fixed to the outer wall of housing 1 and is used to provide rotational driving force;

[0085] The drive shaft 202 is connected at one end to the output end of the motor 201 via a coupling, and is used to transmit rotational driving force.

[0086] The third rotating shaft 203 is fixed to the side wall of another circular plate 101 and is used to drive the connected circular plate 101 to rotate.

[0087] The first adsorption mechanism is assembled between the drive shaft 202 and the third rotating shaft 203, and is used to adsorb and connect the drive shaft 202 and the third rotating shaft 203 so that the drive shaft 202 drives the third rotating shaft 203 to rotate, thereby driving the connected circular plate 101 to rotate.

[0088] The central processing unit 2 is electrically connected to the motor 201 and the first adsorption mechanism.

[0089] In this embodiment, please refer to the appendix. Figure 3 The drive mechanism is controlled by the central processing unit 2 to start the motor 201. The motor 201 drives the output shaft to rotate, the output shaft of the motor 201 drives the drive shaft 202 to rotate, the drive shaft 202 drives the first adsorption mechanism to rotate, and the first adsorption mechanism drives the connected circular plate 101 to rotate, so as to realize the rotation drive of the connected circular plate 101.

[0090] Specifically, the first adsorption mechanism includes:

[0091] Electromagnet 301 is fixed to the end wall of drive shaft 202 away from motor 201 to generate electromagnetic attraction;

[0092] The connecting block 303 is sleeved on the outside of the third rotating shaft 203. Two limiting strips are symmetrically fixed to the outer wall of the third rotating shaft 203. Two limiting grooves are symmetrically opened on the inner wall of the connecting block 303. The two limiting strips are placed in the two limiting grooves and are used to slide on the third rotating shaft 203 and connect with the electromagnet 301 when the electromagnet 301 is energized.

[0093] The connecting spring 302 is sleeved outside the third rotating shaft 203, and its two ends are respectively fixed to the connecting block 303 and the circular plate 101 close to each other's side walls, so as to automatically reset when the electromagnet 301 is de-energized.

[0094] The central processing unit 2 is electrically connected to the electromagnet 301.

[0095] In this embodiment, please refer to the appendix. Figure 3 The first adsorption mechanism is controlled by the central processing unit 2 to energize the electromagnet 301, which in turn adsorbs the connecting block 303, so that the electromagnet 301, the connecting block 303 and the third rotating shaft 203 are in a connected state. At this time, the drive shaft 202 drives the electromagnet 301 to rotate, the electromagnet 301 drives the connecting block 303 to rotate, the connecting block 303 drives the third rotating shaft 203 to rotate, and the third rotating shaft 203 drives the connected circular plate 101 to rotate, so as to realize the adsorption connection drive between the drive shaft 202 and the third rotating shaft 203.

[0096] Specifically, the follow-up mechanism includes:

[0097] The first gear 401 is fixedly sleeved on the drive shaft 202 and is used to generate driving force;

[0098] The bracket 402 is fixedly connected to the side wall of the circular plate 101 near the first gear 401 and is used to install the follower mechanism structure.

[0099] The follower shaft 403 is rotatably connected to the bracket 402 via a bearing and is used to transmit the follower driving force;

[0100] The second adsorption mechanism is assembled between the follower shaft 403 and the double-ended screw 105, and is used to adsorb and connect the follower shaft 403 and the double-ended screw 105 so that the follower shaft 403 drives the double-ended screw 105 to rotate.

[0101] The second gear 404 is fixedly sleeved on the end wall of the follower shaft 403 near the first gear 401 and meshes with the first gear 401 to generate follower driving force.

[0102] The central processing unit 2 is electrically connected to the second adsorption mechanism.

[0103] In this embodiment, please refer to the appendix. Figure 3 When the follower mechanism moves, the central processing unit 2 controls the electromagnet 301 connected to the drive shaft 202 to be de-energized, the electromagnet 301 separates from the connecting block 303, and the connecting block 303 resets under the reset force of the connecting spring 302. At this time, it will not drive the connected circular plate 101 to rotate. The drive shaft 202 drives the first gear 401 to rotate, the first gear 401 drives the meshed second gear 404 to rotate, the second gear 404 drives the connected follower shaft 403 to rotate, the follower shaft 403 drives the second adsorption mechanism to rotate, and the second adsorption mechanism drives the double-headed screw 105 to rotate, so as to realize the follower rotation drive of the double-headed screw 105.

[0104] Specifically, the second adsorption mechanism has the same structure as the first adsorption mechanism.

[0105] In this implementation, please refer to the appendix. Figure 3 The adsorption rotation principle of the second adsorption mechanism is the same as that of the first adsorption mechanism.

[0106] Although embodiments of the invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the invention, the scope of which is defined by the appended claims and their equivalents.

Claims

1. A real-time monitoring device for pilot health index, characterized in that, include: Outer shell (1); There are two mounting blocks (4), which are symmetrically fixed to the middle of the mounting sides at the top and bottom of the outer shell (1); There are two rotating ports (5), which are located on the camera side of the outer casing (1); There are two cameras (6), which are set inside the two rotating ports (5); A rotation drive mechanism is assembled between the outer casing (1) and the two cameras (6); The rotary drive mechanism includes: The first rotating shaft (104) is rotatably connected at one end to the inside of the outer shell (1) via a bearing; Two circular plates (101) are provided. One circular plate (101) is fixed at one end to the other end of the first rotating shaft (104), and the other circular plate (101) is provided on the other side inside the outer shell (1). The drive mechanism is assembled between the outer casing (1) and another circular plate (101); The drive mechanism includes: The motor (201) is fixed to the outer wall of the outer casing (1); The drive shaft (202) is connected at one end to the output end of the motor (201) via a coupling; The third rotating shaft (203) is fixed to the side wall of another circular plate (101); The first adsorption mechanism is assembled between the drive shaft (202) and the third rotating shaft (203); The first adsorption mechanism includes: An electromagnet (301) is fixed to the end wall of the drive shaft (202) away from the motor (201); The connecting block (303) is sleeved outside the third rotating shaft (203). Two limiting strips are symmetrically fixed to the outer wall of the third rotating shaft (203). Two limiting grooves are symmetrically opened on the inner wall of the connecting block (303), and the two limiting strips are placed in the two limiting grooves. The connecting spring (302) is sleeved outside the third rotating shaft (203), and its two ends are fixed to the connecting block (303) and the circular plate (101) close to each other on the side wall, respectively; A fixed shaft (103) is fixed to the two circular plates (101) near the rotating opening (5); There are two fixing blocks (102), which are symmetrically fixed to the fixing shaft (103); The double-ended screw (105) is rotatably connected to the two circular plates (101) on the side away from the fixed shaft (103) via bearings; The follower mechanism is assembled between the outer shell (1) and the double-headed screw (105); The follower mechanism includes: The first gear (401) is fixedly sleeved on the drive shaft (202); The bracket (402) is fixed to the side wall of the circular plate (101) near the first gear (401); The follower shaft (403) is rotatably connected to the bracket (402) via a bearing; The second adsorption mechanism is assembled between the follower shaft (403) and the double-headed screw (105); The second adsorption mechanism has the same structure as the first adsorption mechanism; The second gear (404) is fixedly sleeved on the end wall of the follower shaft (403) near the first gear (401) and meshes with the first gear (401); Two movable blocks (107) are provided, which are symmetrically connected to the double-ended screw (105) through transmission nuts; Two movable frames (106) are provided, located outside the fixed block (102) and movable block (107) on the same side, and are fixedly connected to the two cameras (6); The first movable opening (109) is provided in four pairs, symmetrically opened on two movable frames (106), and two fixed blocks (102) and two movable blocks (107) are respectively located in the four first movable openings (109); The second rotating shaft (108) has eight shafts, which are symmetrically connected to the top and bottom of the two fixed blocks (102) and the two movable blocks (107) by bearings. There are eight second movable openings (110), which are symmetrically arranged on two movable frames (106) in a four-by-four configuration. The other ends of the eight second rotating shafts (108) extend into the eight second movable openings (110). The central processing unit (2) is fixed to the top of the outer casing (1); The alarm (3) is fixed to the top of the outer casing (1).

Citation Information

Patent Citations

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    CN114224357A

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