CN219207976U - Pilot brain fatigue countermeasure system - Google Patents

Pilot brain fatigue countermeasure system Download PDF

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Publication number
CN219207976U
CN219207976U CN202320088870.3U CN202320088870U CN219207976U CN 219207976 U CN219207976 U CN 219207976U CN 202320088870 U CN202320088870 U CN 202320088870U CN 219207976 U CN219207976 U CN 219207976U
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module
pilot
seat
brain
rotating shaft
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林榕
杨柳
刘娟
熊端琴
张焱
廖扬
张宜爽
朱煜阳
杜健
戈含笑
刘昕
韩梦霏
胡译文
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Air Force Specialty Medical Center of PLA
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Air Force Specialty Medical Center of PLA
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Abstract

The utility model discloses a brain fatigue resistance system for a pilot, which is designed to quickly recover the brain and physical ability of the pilot, so that the mental energy can be effectively recovered in a shorter time, and the fatigue state is recovered to the vitality state. The pilot brain fatigue countermeasure system comprises a seat function module and an operation module; the seat functional module comprises a blood pressure acquisition circuit, an electrocardio acquisition circuit, a seat angle sensor, a gyroscope, a linear motor, a vibration massage module, a neuromuscular electric stimulation module, an infrared heating module and a music playing module; the operation module comprises a data acquisition module, a control module, a wireless transmission module and a display interface. The utility model can quickly restore the vitality of the brain and the neuromuscular of the pilot through various stimulations; the angle and the body position can be conveniently and quickly adjusted, so that blood can be quickly transferred from the lower limb to the upper body by the static force, and the brain activity can be recovered; the brain recovery process is conveniently adjusted through circuit control and state display.

Description

Pilot brain fatigue countermeasure system
Technical Field
The utility model relates to pilot training auxiliary equipment, in particular to a pilot brain fatigue countermeasure system.
Background
Flight fatigue has been a subject of great concern for many years. However, at present, no exact standard exists for research and quantitative evaluation of the occurrence mechanism of the flight fatigue at home and abroad. Fatigue is known to be a group of phenomena involving efficiency and skill damage or loss. As a complaint, it may include sleep insufficiency, interruption or deprivation due to long-term work, increased subjective tiredness, short-time loss of attention, and possibly decreased mental exercise ability. Flight fatigue can be defined as a phenomenon in which flight personnel's flight work ability is lowered, flight operation errors and the probability of occurrence of accidents are increased during the work.
Research shows that the reasons for inducing flight fatigue mainly comprise: intensity of work and duration of flight, physical quality, method of work and proficiency, degree of matching of tool equipment to people, environmental conditions, sleep, psychological burden, nutritional status, and the like. The occurrence mechanism of the flight fatigue is complex, and the flight fatigue can be considered to be the phenomenon that the flight operation capability is reduced due to continuous or repeated tasks and the physical, physiological or psychological stress aggravates the flight fatigue by combining the induction factors of the flight fatigue. While Russian specialists consider that flight fatigue is generated in the professional activities, and the flight fatigue is characterized by fatigue feeling, physiological function change and moderate reduction of the normal function state of pilots.
The causes of flight fatigue of pilots are roughly of the following three types: (1) The strength and load capacity of pilot load, the strength and duration of the workload during flight, duty and ground preparation; (2) The effect of flight stress factors, which in some cases may be the main factor in causing fatigue; (3) Individual factors such as violations of the regimen, dietary regimen, long flight interval, early stage of disease, bad habit, etc. The occurrence mechanism of flight fatigue can be understood from the following three aspects: (1) Effects of flight tasks and biorhythms on sleep arousal function. From a human perspective, flight fatigue is mainly related to the following factors: sleep deprivation or sleep insufficiency, circadian rhythm disturbances of sleep arousal, influence of flight tasks on sleep and circadian rhythms. (2) The effects of sustained flight tasks on brain function and other physiological functions. The basic characteristics of the flying labor are mental labor mainly based on multi-task comprehensive decision, long-time continuous operation can cause brain function fatigue and influence other related physiological and psychological functions, subjective fatigue feeling, especially mental fatigue feeling, is obviously increased, objective cognitive work performance is obviously reduced, and objective index change with larger difficulty is more obvious. (3) Aviation stress factors cause flight personnel to often receive continuous dynamic loads and other stress stimuli, and sports, circulation, respiration and other functional systems continuously respond to the stress factors, so that physical fatigue of the flight personnel is easily caused.
Classification and characteristics of fatigue of the body and the mind of long-endurance flying. According to the occurrence mechanism analysis of the long-endurance flight physical and mental fatigue, the flight fatigue is divided into the following main categories: global fatigue, local fatigue, physiological fatigue, and psychological fatigue. From the viewpoint of service support, it is generally classified into acute fatigue, chronic fatigue and overfatigue according to the occurrence course of flight fatigue.
Acute fatigue is caused by short but intense flight activities. The appearance of the pilot is gait swaying, action misalignment, retardation, pale or reddish skin, dyspnea, excessive perspiration and the like; objectively expressed as an increase in heart rate and respiration volume, unstable pulse and arterial pressure, and a decrease in work performance index.
Chronic fatigue may also be referred to as cumulative fatigue, due to the pilot receiving heavy workload multiple times. The subjective feeling of the pilot is tired before and during flight, weak feeling, headache, insomnia and the like, objective indexes are represented by reduced muscle strength and endurance, reduced visual sensitivity and critical flicker fusion frequency, obviously slowed down working operation and increased false action.
Overfatigue is a state of a pilot's pathological function due to a workload of great intensity over time, characterized by a significant change in physiological function and a drastic decrease in activity efficiency. The objective index of the heart rate is accelerated, the attention and the memory are reduced, pains such as neck, shoulder, waist and the like sometimes occur, the adaptability of the cardiovascular system to physical load is reduced, and the electrocardiogram is characterized by coronary insufficiency and reduces the overload endurance.
From the generation mechanism of flight fatigue and the analysis of the existing state of the flight fatigue, a comprehensive countermeasure device for the physical and mental fatigue of the pilot in long voyage needs to be designed so as to solve the following problems:
(1) After long, high load flights, blood accumulates in the lower extremities, causing hydrostatic transfer of blood from the lower body to the upper body. There are two methods currently in use: in the first method, the sitting position is taken, the two arms are lifted and put down periodically, and the duration of each posture is 8-10 s. At this point, the zero level hydrostatic pressure in the cardiovascular system moves up or down, which is associated with filling and regurgitating a certain amount of blood into the head vessels and reversing phase into the leg vessels, which helps "lavage" the organs. After a large overload flight, the pilot should lift up his hands and maintain this attitude for 8s to 10s. During this time, the heart rhythm automation completes an autoregulation cycle starting from the carotid sinus. In the second method, the prone position is taken, the knee joint is bent by 90 degrees, and the feet are lifted and put down. Taking the lying position for not less than 5min before lifting feet, taking the lying position for not less than 10min after operation, and taking the foot lifting time within 10min. With this approach, blood is redistributed from the lower limb to the head. At this point, the cerebral vessels contract, wherein blood flow is enhanced and blood filling is increased. The lying position allows maximum relaxation of the antigravity muscles subject to overload.
(2) The greater sustained flight trick acceleration effects can cause impaired activity in the neuromuscular, central nervous, cardiovascular and respiratory systems of the body, as well as in visual analyzers. Specific methods should be employed to normalize the reflex responses of the central nervous and neuromuscular systems, eliminate lower body congestion, accelerate the flow of muscle blood that is maximally loaded by static load, and minimize energy consumption to prevent fatigue. These special methods are mainly: electrophysiological methods, neuromuscular device electrical stimulation relaxation, cutaneous biological activity point axon reflex action, pulsed low frequency physiotherapy, central electrical analgesia, biological resonance energy information therapy, and the like; psychological methods, mental self-regulation, autogenous exercise, flight mental therapy on flight exercises, rational mental therapy, hypnotic cues, functional music, etc.
Therefore, there is a need to design a device that can quickly recover the mental, psychological and physical fatigue of a pilot, in conjunction with efficient completion of pilot training and flight tasks, and quick brain recovery.
The information disclosed in this background section is only for enhancement of understanding of the general background of the utility model and should not be taken as an acknowledgement or any form of suggestion that this information forms the prior art already known to a person of ordinary skill in the art.
Disclosure of Invention
The utility model aims to provide a brain fatigue resistance system for a pilot, which can realize multiple stimulation of electric, optical, acoustic and mechanical massage by utilizing an electromechanical structure and quickly recover the vitality of the brain and neuromuscular of the pilot; the angle and the body position can be conveniently adjusted, so that blood can be quickly transferred from lower limbs to upper body blood static force, brain blood can be recovered, brain can be quickly recovered, and limb muscles can be relaxed, so that the aim of quickly recovering from a fatigue state can be fulfilled; through circuit control and state display, the physiological parameters of a pilot can be mastered in real time by operating personnel, and the brain recovery process is conveniently and quickly adjusted.
In order to achieve the above object, the present utility model provides a pilot brain fatigue resistance system including a seat function module provided on a seat and an operation module outside the seat;
the seat functional module comprises a blood pressure acquisition circuit, an electrocardio acquisition circuit, a seat angle sensor, a gyroscope, a linear motor, a vibration massage module, a neuromuscular electric stimulation module, an infrared heating module, a music playing module and an expansion interface; the various modules realize corresponding functions, can stimulate nerves and muscles in multiple aspects, enable brain bodies to be quickly recovered, improve recovery effect and efficiency, and meet pilot training requirements.
The operation module comprises a data acquisition module, a control module, a wireless transmission module and a display interface; the data acquisition module is respectively connected with the blood pressure acquisition circuit, the electrocardio acquisition circuit, the seat angle sensor and the gyroscope through signal lines; the control module is respectively connected with the linear motor, the vibration massage module, the neuromuscular electric stimulation module, the infrared heating module, the music playing module and the expansion interface through signal lines;
the data acquisition module is connected with the control module through a signal line, the control module is connected with the wireless transmission module through a signal line, and the wireless transmission module is connected with the display interface through a wireless signal. The display interface can display the brain recovery state and physiological parameters of the pilot in real time, so that an operator can conveniently adjust the recovery process.
In one or more embodiments, the seat structure of the pilot brain fatigue resistance system includes: the right side of the seat surface is rotationally connected with the lower end of the chair back through a first rotating shaft, the left side of the seat surface is rotationally connected with the upper end of the lower leg plate through a second rotating shaft, and the lower end of the lower leg plate is rotationally connected with the upper end of the foot plate through a third rotating shaft; the rotation of the three rotating shafts can adjust the angle posture, so that a pilot can quickly relax and recover the brain under different posture positions;
the front side surface of the upper part of the backrest and the front side surface of the lower part of the backrest are respectively provided with a vibration massage module, and the vibration massage modules can enable muscles of the head and neck parts and the waist of a pilot to quickly recover physical strength through knocking and massage operation, so that the body and mind of the pilot are relaxed; the middle part of the upper side surface of the chair surface is provided with a first thigh clamp and a second thigh clamp which are transversely arranged; the upper side surface of the middle part of the shank plate is provided with a shank clamp; an infrared heating module is arranged on the upper side surface of the foot plate; the infrared heating device can heat feet, promote blood circulation of a human body, quickly recover blood supply of the brain and accelerate recovery speed of the brain;
the front and back sides of the middle part of the chair surface are respectively provided with an armrest.
In one or more embodiments, the blood pressure acquisition circuit is disposed at an armrest of the seat for measuring pilot blood pressure in real time; the acquisition head of the electrocardio acquisition circuit is arranged at the chair back and is used for being attached to the chest of a pilot to carry out electrocardio monitoring; the seat angle sensor comprises three seat angle sensors respectively arranged on the first rotating shaft, the second rotating shaft and the third rotating shaft; the gyroscope comprises three gyroscopes which are respectively arranged in the chair back, the chair surface and the lower leg plate. Therefore, the body position of the pilot can be conveniently adjusted, blood backflow to the brain is promoted, and the physiological state is monitored in real time, so that the aim of rapid recovery is fulfilled.
In one or more embodiments, the vibration massage module comprises a linear motor and a massage roller, wherein the linear motor drives the massage roller to reciprocate through reciprocating motion so as to perform massage operation on the body of a pilot; the beating frequency of the massage roller is 200 times/min-600 times/min, and the kneading frequency is 20 revolutions/min-60 revolutions/min. The vibration massage module can promote the relaxation of lower limb muscles and the blood reflux, thereby promoting the cerebral blood return.
In one or more embodiments, the infrared heating module includes infrared heating circuitry disposed within the foot plate, the calf plate, the seat and the backrest. The infrared heating of a plurality of positions not only can relax the mind and body, but also can make the blood circulate fast and accelerate the recovery efficiency of the brain.
In one or more embodiments, the neuromuscular electrical stimulation module includes neuromuscular electrical stimulation probes disposed on foot plates, calf plates, seat backs, and armrests, the neuromuscular electrical stimulation probes being attached to the pilot's body surface in patches for electrical current stimulation; the current stimulation adopts low-frequency pulse current with the pulse frequency of 0.5 Hz-5 Hz and lower than 50 mA. The neuromuscular electrical stimulation module can perform electrical stimulation on corresponding acupoints and muscles, so that the human body can quickly recover the mental and physical activities.
In one or more embodiments, the music playing module is disposed in the chair back, and the music playing module includes an external speaker and an audio earphone interface. The music playing module can play the soothing music, and further relax psychologically so as to quickly restore the vitality of the brain.
In one or more embodiments, the expansion interface includes a universal serial bus, IEEE 1394, RS232, GPIB, ethernet interface.
In one or more embodiments, the angle of the included angle alpha between the chair back and the horizontal plane, the included angle beta between the chair surface and the horizontal plane and the included angle gamma between the chair surface and the lower leg plate can be respectively adjusted through the first rotating shaft, the bracket and the second rotating shaft; the included angle between the foot plate and the lower leg plate is adjusted through the rotation of the third rotating shaft;
drive motors for adjusting the rotation angles are respectively arranged on the first rotating shaft, the second rotating shaft and the third rotating shaft; the bracket is provided with a driving motor for adjusting the angle between the chair surface and the horizontal angle.
In one or more embodiments, the vibration massage module includes an air bladder in communication with an air pump via a conduit.
Compared with the prior art, the brain fatigue countermeasure system for the pilot is convenient for operators to master physiological parameters of the pilot in real time through circuit control and state display, and the brain recovery process is convenient and rapid to adjust; the comprehensive multiple stimulations are adopted to realize the recovery of nerves, muscles and brains, and the neuromuscular electrical stimulation method is adopted to relieve the muscle tension of limbs and the relaxation of nerves and simultaneously relax the mental and psychological activities; the massage head is adopted, and the muscles and nerves are relaxed through vibration massage; the angle and the body position of the body are adjusted, thighs are lifted up on the fatigue countermeasure device to form a certain angle with the trunk, so that blood accumulated on lower limbs can circulate well, cerebral blood supply is recovered, and the cerebral blood supply is recovered quickly, so that the brain can be recovered quickly; the music playing module is used for playing the relaxed music, so that the effect of psychological relaxation is achieved, and the psychological and mental relaxation is recovered rapidly; the foot sole is adopted for heating, so that the blood circulation is promoted, the physical fatigue is relieved, the mind and the body are relaxed, and the recovery of the mind and the mind is realized; the angle and the body position of the trunk can be conveniently adjusted, and the angle meeting the requirements of specific personnel can be adjusted according to different fatigue states and characteristics so as to meet the demands of different groups and different degrees of mental, psychological and physical fatigue countermeasures and recovery.
Drawings
FIG. 1 is a schematic circuit diagram of a pilot brain fatigue resistance system according to an embodiment of the present utility model.
Fig. 2 is a schematic perspective view of a pilot brain fatigue countermeasure system according to an embodiment of the utility model.
The main reference numerals illustrate:
the seat comprises a seat back, a 2-vibration massage module, a 3-vibration massage module, a 4-seat, a 5-second thigh clamp, a 6-handrail, a 7-shank clamp, an 8-foot plate, a 9-third rotating shaft, a 10-second rotating shaft, a 11-base, a 12-first rotating shaft, a 13-bracket and a 14-display interface.
Detailed Description
The following detailed description of embodiments of the utility model is, therefore, to be taken in conjunction with the accompanying drawings, and it is to be understood that the scope of the utility model is not limited to the specific embodiments.
Throughout the specification and claims, unless explicitly stated otherwise, the term "comprise" or variations thereof such as "comprises" or "comprising", etc. will be understood to include the stated element or component without excluding other elements or components.
As shown in fig. 1, a pilot brain fatigue resistance system according to an embodiment of the present utility model includes a seat function module provided on a seat and an out-of-seat operation module; the seat functional module comprises a blood pressure acquisition circuit, an electrocardio acquisition circuit, a seat angle sensor, a gyroscope, a linear motor, a vibration massage module, a neuromuscular electric stimulation module, an infrared heating module, a music playing module and an expansion interface, wherein the circuit of the seat functional module realizes functions of photoelectric and heating stimulation, seat position adjustment, music playing and the like, and comprehensively realizes rapid relaxation and recovery of brain and physical strength of a pilot; the operation module comprises a data acquisition module, a control module, a wireless transmission module and a display interface; the data acquisition module is respectively connected with the blood pressure acquisition circuit, the electrocardio acquisition circuit, the seat angle sensor and the gyroscope through signal lines, and the four devices respectively acquire physiological data and seat position data of a pilot, so that a basis is provided for efficient brain recovery, and the recovery condition is convenient to observe and the recovery operation is convenient to adjust; the control module is respectively connected with the linear motor, the vibration massage module, the neuromuscular electric stimulation module, the infrared heating module, the music playing module and the expansion interface through signal lines, and the control module sends out control signals to regulate and control the working state of the equipment; the data acquisition module is connected with the control module through a signal line, the control module is connected with the wireless transmission module through a signal line, the wireless transmission module is connected with the display interface through wireless signals, the display interface can conveniently display various physiological states and system states, and corresponding operation can be carried out on the display interface to send out control signals to reach the control module and then regulate and control corresponding recovery processes and parameters.
As shown in fig. 2, the seat structure of the pilot brain fatigue countermeasure system includes: the right side of the seat 4 is rotationally connected with the lower end of the chair back 1 through a first rotating shaft 12, the left side of the seat 4 is rotationally connected with the upper end of a lower leg plate through a second rotating shaft 10, and the lower end of the lower leg plate is rotationally connected with the upper end of a foot plate 8 through a third rotating shaft 9;
the front side surface of the upper part of the backrest and the front side surface of the lower part of the backrest are both provided with vibration massage modules 2; the middle part of the upper side surface of the chair surface 4 is provided with a first thigh clamp and a second thigh clamp 5 which are transversely arranged; the upper side surface of the middle part of the shank plate is provided with a shank clamp 7; an infrared heating module is arranged on the upper side surface of the foot plate 8;
the front and back sides of the middle part of the chair surface 4 are respectively provided with an armrest 6.
Preferably, the blood pressure acquisition circuit is arranged at the armrest 6 of the seat and is used for measuring the blood pressure of a pilot in real time; the acquisition head of the electrocardio acquisition circuit is arranged at the chair back 1 and is used for being attached to the chest of a pilot for electrocardio monitoring; the seat angle sensor comprises three seat angle sensors respectively arranged on the first rotating shaft 12, the second rotating shaft 10 and the third rotating shaft 9; the gyroscope comprises three gyroscopes respectively arranged in the chair back 1, the chair surface 4 and the lower leg plate.
Preferably, the vibration massage module 2 comprises a linear motor and a massage roller, and the linear motor drives the massage roller to reciprocate through reciprocating motion so as to massage the body of the pilot; the beating frequency of the massage roller is 200 times/min-600 times/min, and the kneading frequency is 20 revolutions/min-60 revolutions/min. The vibration massage module can promote the relaxation of lower limb muscles and the blood reflux, thereby promoting the cerebral blood return.
Preferably, the infrared heating module includes infrared heating circuits disposed within the foot plate 8, the calf plate, the seat 4 and the backrest. Infrared heating is carried out on the sole of the foot to promote the blood to flow back from the lower limb; through various stimulation modes, the nerve relaxation of the pilot is realized, so that the mental and psychological of the pilot is relaxed and quickly recovered.
Preferably, the neuromuscular electrical stimulation module comprises neuromuscular electrical stimulation probes arranged on the foot plate 8, the lower leg plate, the chair surface 4, the backrest and the armrest 6, wherein the neuromuscular electrical stimulation probes are attached to the body surface of a pilot in a patch form for current stimulation; the current stimulation adopts low-frequency pulse current with the pulse frequency of 0.5 Hz-5 Hz and lower than 50 mA. So as to achieve the purposes of promoting blood circulation and relaxing neuromuscular, thereby leading the mind and the mind to relax and recover simultaneously.
Preferably, the music playing module is arranged in the chair back 1, and the music playing module comprises an externally-placed loudspeaker and an audio earphone interface. The music playing module can play the soothing music, and further relax psychologically so as to quickly restore the vitality of the brain.
Preferably, the expansion interface includes universal serial bus, IEEE 1394, RS232, GPIB, ethernet interface. The various interfaces can be conveniently connected with different kinds of external equipment, and different functions are expanded.
Preferably, the angle α between the chair back 1 and the horizontal plane, the angle β between the chair surface 4 and the horizontal plane, and the angle γ between the chair surface 4 and the lower leg plate are respectively adjustable by the first rotating shaft 12, the bracket 13 and the second rotating shaft 10; the included angle between the foot plate 8 and the lower leg plate is adjusted by the rotation of the third rotating shaft 9; the included angle alpha is in the range of-15 to 90 degrees, the included angle beta is in the range of 15 to 105 degrees, and the included angle gamma is in the range of 90 to 180 degrees. When the angle alpha takes a negative value, the height of the head is lower than the height of the thigh of the chair surface 4, so that the blood of the lower limb can flow back upwards, the blood of the brain can be recovered, and the brain can be recovered quickly.
Driving motors for adjusting the rotation angles are respectively arranged on the first rotating shaft 12, the second rotating shaft 10 and the third rotating shaft 9; the bracket 13 is provided with a driving motor for adjusting the angle between the chair surface 4 and the horizontal. Driving motors for adjusting the rotation angles are respectively arranged on the first rotating shaft 12, the second rotating shaft 10 and the third rotating shaft 9; the bracket 13 is provided with a driving motor for adjusting the angle between the chair surface 4 and the horizontal. The driving motor adopts a stepping motor, the output shaft of the stepping motor is provided with a reduction gear mechanism, and the output gear of the reduction gear mechanism is matched with the gear on the circumferential side surface of the rotating shaft, so that the driving motor can be conveniently adjusted and the purpose of position locking can be achieved; the stepping motor is matched with a stepping motor driver to adjust the rotation of the stepping motor, so that the angle and the body position of the brain fatigue resisting device of the pilot are adjusted.
Preferably, the vibration massage module 2 comprises an air bag, and the air bag is communicated with the air pump through a pipeline. The air pump inflates the air bag, so that the air bag filling degree is adjusted, and the relaxation requirement of a pilot is met.
The foregoing descriptions of specific exemplary embodiments of the present utility model are presented for purposes of illustration and description. It is not intended to limit the utility model to the precise form disclosed, and obviously many modifications and variations are possible in light of the above teaching. The exemplary embodiments were chosen and described in order to explain the specific principles of the utility model and its practical application to thereby enable one skilled in the art to make and utilize the utility model in various exemplary embodiments and with various modifications as are suited to the particular use contemplated. It is intended that the scope of the utility model be defined by the claims and their equivalents.

Claims (10)

1. A pilot brain fatigue countermeasure system, characterized in that the pilot brain fatigue countermeasure system comprises a seat function module arranged on a seat and an operation module outside the seat;
the seat functional module comprises a blood pressure acquisition circuit, an electrocardio acquisition circuit, a seat angle sensor, a gyroscope, a linear motor, a vibration massage module, a neuromuscular electric stimulation module, an infrared heating module, a music playing module and an expansion interface;
the operation module comprises a data acquisition module, a control module, a wireless transmission module and a display interface; the data acquisition module is respectively connected with the blood pressure acquisition circuit, the electrocardio acquisition circuit, the seat angle sensor and the gyroscope through signal lines; the control module is respectively connected with the linear motor, the vibration massage module, the neuromuscular electric stimulation module, the infrared heating module, the music playing module and the expansion interface through signal lines;
the data acquisition module is connected with the control module through a signal line, the control module is connected with the wireless transmission module through a signal line, and the wireless transmission module is connected with the display interface through a wireless signal.
2. The pilot brain fatigue resistance system of claim 1, wherein the seat structure of the pilot brain fatigue resistance system comprises: the right side of the seat surface is rotationally connected with the lower end of the chair back through a first rotating shaft, the left side of the seat surface is rotationally connected with the upper end of the lower leg plate through a second rotating shaft, and the lower end of the lower leg plate is rotationally connected with the upper end of the foot plate through a third rotating shaft;
the front side surface of the upper part of the backrest and the front side surface of the lower part of the backrest are respectively provided with a vibration massage module; the middle part of the upper side surface of the chair surface is provided with a first thigh clamp and a second thigh clamp which are transversely arranged; the upper side surface of the middle part of the shank plate is provided with a shank clamp; an infrared heating module is arranged on the upper side surface of the foot plate;
the front and back sides of the middle part of the chair surface are respectively provided with an armrest.
3. The pilot brain fatigue countermeasure system of claim 2, wherein the blood pressure acquisition circuit is disposed at an armrest of the seat for measuring pilot blood pressure in real time; the acquisition head of the electrocardio acquisition circuit is arranged at the chair back and is used for being attached to the chest of a pilot to carry out electrocardio monitoring; the seat angle sensor comprises three seat angle sensors respectively arranged on the first rotating shaft, the second rotating shaft and the third rotating shaft; the gyroscope comprises three gyroscopes which are respectively arranged in the chair back, the chair surface and the lower leg plate.
4. The brain fatigue countermeasure system for pilots of claim 2, wherein the vibration massage module comprises a linear motor and a massage roller, the linear motor driving the massage roller to reciprocate by reciprocating motion, and performing massage operation on the pilot's body; the beating frequency of the massage roller is 200 times/min-600 times/min, and the kneading frequency is 20 revolutions/min-60 revolutions/min.
5. The pilot brain fatigue resistance system according to claim 2, wherein the infrared heating module includes infrared heating circuitry disposed within the foot plate, the lower leg plate, the seat and the back rest.
6. The pilot brain fatigue countermeasure system of claim 2, wherein the neuromuscular electrical stimulation module includes neuromuscular electrical stimulation probes provided on foot plates, lower leg plates, seating surfaces, backrests and armrests, the neuromuscular electrical stimulation probes being attached to the pilot's body surface in patches for electrical current stimulation; the current stimulation adopts low-frequency pulse current with the pulse frequency of 0.5 Hz-5 Hz and lower than 50 mA.
7. The pilot brain fatigue countermeasure system of claim 2, wherein the music playing module is disposed within the seat back, the music playing module including a loud speaker and an audio headset interface.
8. The pilot brain fatigue counter system according to claim 2, wherein the expansion interface comprises a universal serial bus, IEEE 1394, RS232, GPIB, ethernet interface.
9. The pilot brain fatigue countermeasure system of claim 2, wherein the angles of the angle α of the back to the horizontal plane, the angle β of the seat to the horizontal plane, and the angle γ of the seat to the lower leg plate are adjustable by the first rotation axis, the bracket, and the second rotation axis, respectively; the included angle between the foot plate and the lower leg plate is adjusted through the rotation of the third rotating shaft;
drive motors for adjusting the rotation angles are respectively arranged on the first rotating shaft, the second rotating shaft and the third rotating shaft; the bracket is provided with a driving motor for adjusting the angle between the chair surface and the horizontal angle.
10. The pilot brain fatigue countermeasure system of claim 4, wherein the vibration massage module includes an air bladder in communication with the air pump via a conduit.
CN202320088870.3U 2023-01-31 2023-01-31 Pilot brain fatigue countermeasure system Active CN219207976U (en)

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Application Number Priority Date Filing Date Title
CN202320088870.3U CN219207976U (en) 2023-01-31 2023-01-31 Pilot brain fatigue countermeasure system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202320088870.3U CN219207976U (en) 2023-01-31 2023-01-31 Pilot brain fatigue countermeasure system

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CN219207976U true CN219207976U (en) 2023-06-20

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