CN112218459B - Civil aviation operation data monitoring equipment and monitoring method thereof - Google Patents
Civil aviation operation data monitoring equipment and monitoring method thereof Download PDFInfo
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- CN112218459B CN112218459B CN202011079118.XA CN202011079118A CN112218459B CN 112218459 B CN112218459 B CN 112218459B CN 202011079118 A CN202011079118 A CN 202011079118A CN 112218459 B CN112218459 B CN 112218459B
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- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K5/00—Casings, cabinets or drawers for electric apparatus
- H05K5/02—Details
- H05K5/0217—Mechanical details of casings
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
- G01K1/00—Details of thermometers not specially adapted for particular types of thermometer
- G01K1/02—Means for indicating or recording specially adapted for thermometers
- G01K1/024—Means for indicating or recording specially adapted for thermometers for remote indication
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
- G01K1/00—Details of thermometers not specially adapted for particular types of thermometer
- G01K1/14—Supports; Fastening devices; Arrangements for mounting thermometers in particular locations
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
- G01K13/00—Thermometers specially adapted for specific purposes
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- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K7/00—Constructional details common to different types of electric apparatus
- H05K7/20—Modifications to facilitate cooling, ventilating, or heating
- H05K7/20009—Modifications to facilitate cooling, ventilating, or heating using a gaseous coolant in electronic enclosures
- H05K7/20136—Forced ventilation, e.g. by fans
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Abstract
The invention relates to the technical field of aviation, and discloses civil aviation operation data monitoring equipment which comprises an organism, wherein a cavity is formed in the bottom of the organism, a warning lamp is arranged at the top of the organism, a handle is fixedly connected to the rear side of the top of the organism, an installation block is slidably connected to the interior of the cavity, moving grooves are formed in the inner walls of the left side and the right side of the cavity, and racks are fixedly connected to the inner walls of the two groups of moving grooves on the opposite sides. This civilian aviation operation data monitoring facilities, through setting up the mobile device, and then make the installation piece drive the temperature sensor probe and remove after opening the mobile device to make the position of temperature sensor probe no longer fixed, made things convenient for the pencil of temperature sensor probe to different positions to respond to, reduced the cost of monitoring pencil temperature data, and make operating personnel's work become convenient, reduce operating personnel's the work degree of difficulty, suitable popularization.
Description
Technical Field
The invention relates to the technical field of aviation, in particular to civil aviation operation data monitoring equipment and a monitoring method thereof.
Background
Aviation, a complex and strategic human activity, refers to the flying (sailing) activity of an aircraft in the earth's atmosphere (air space), and many fields related thereto, such as scientific research and education, industrial manufacturing, public transportation, professional work, aviation movement, national defense and military, government management, etc., by utilizing the air space and the aircraft (aircraft), the aviation activity can be subdivided into many independent industries and fields, typically, such as aviation manufacturing, civil aviation, etc., it is often seen that people use this term from their respective fields, the content is rich and varied, the aircraft engaged in flying activity, also called aircraft, is divided into two types, i.e., lighter-than-air aircraft and heavier-air aircraft, the former relying on the static buoyancy of air to lift off, such as balloons, airship, etc., and the latter relying on the aerodynamic lift-off generated by the relative movement with air, for example, airplanes, helicopters and the like can be divided into a man-machine and an unmanned machine according to whether people are carried, and the mankind has a strong desire to fly in the air in the last day, for example, Chang ' e in China runs for the moon mythology legend and kite, in the 19 th century, many people manufacture gliders without engines to fly, the gradual use of hot balloons and airships, in 1903, America Laite brothers invented airplanes and successfully tried to fly, but somebody thinks that Klawn and Ader are true airplane inventors, China ' ancient father of aviation ' Von is also a pioneer in the world aviation history, the history of human aviation is long, even rocks and spears for people, mechanical pigeons manufactured by ancient Aristota in Greece, travelers far to Australia, Kongming lantern and kites in China have relations, and as for true flying, Yikalo in ancient Hitaco is a person capable of flying, China Yuanhuang, European parachute and a Muslim abas Kaschim Eben Franas gliding flight, are all the expressions that people want to fly, and by the 15 th century, Daphnqi servants made flapping-wing aircraft with simulated bird wings to do flight tests, but not only can fly away but also break one leg, the English aviation term is from Latin bird (avia) or air (aero), the aircraft engaged in flight activities is also called aircraft, and the aircraft is divided into two types of lighter-than-air aircraft and heavier-than-air aircraft, the former is such as balloon, airship and the like, and the air static buoyancy is used for lifting air; the latter is like the plane, the helicopter, etc., and the lift-off by using the aerodynamic force (English: Aviation) refers to the navigation activity of a manned or unmanned aircraft in the atmosphere in narrow sense, the wide sense of Aviation, the aeronautical research, aeronautical manufacturing, air transportation, etc. and many fields related to Aviation, and the human will like birds to fly the sky since ancient times, but the manned hot air balloon is realized firstly until the lift-off of Europe in the later 18 th century, the human Aviation industry is developed rapidly along with the technological progress brought by the industrial revolution in the beginning of 20 th century, the Latet brother of 12.12.12.s.17.21. America successfully tries to fly the aircraft which is mainly heavier than air, has power, is controlled and can be continuously emptied, a new era of modern Aviation is opened, the Aviation is the scientific and technical field with the most active and most influential power in 21 st century, and the important achievement of the field marks the development level of human civilization, also embody the state of the national force of a country and the level of science and technology, the aircraft indicates that the power device that has one or more engines produces the thrust or pulling force that advances, produce the lift by the fixed wing of fuselage, the aircraft of being heavier than the air that flies in the atmosphere, along with electric circuit interconnected system (EWIS) more and more receives attention, civil aircraft pencil monitoring and early warning device also need further development urgently, at present, pencil data monitoring equipment is mostly the temperature that uses temperature sensor to monitor the pencil in current aviation operation, temperature sensor's position is mostly fixed, so can only monitor the pencil of single position, thereby need set up multiunit temperature sensor or need the frequent mobile sensor of operating personnel, thereby bring very big inconvenience for operating personnel's work.
Disclosure of Invention
Technical problem to be solved
Aiming at the defects of the prior art, the invention provides the civil aviation operation data monitoring equipment and the monitoring method thereof, which have the advantages that the wire harnesses at different positions can be monitored by a single temperature sensor, and the like, and the problem that the wire harnesses at the single position can only be monitored by the single sensor is solved.
(II) technical scheme
In order to realize the purpose that the wire harnesses at different positions can be monitored by the single temperature sensor, the invention provides the following technical scheme: the civil aviation operation data monitoring equipment comprises an engine body, wherein a cavity is formed in the bottom of the engine body, a warning lamp is arranged on the top of the engine body, a handle is fixedly connected to the rear side of the top of the engine body, an installation block is slidably connected to the interior of the cavity, moving grooves are formed in the left inner wall and the right inner wall of the cavity, racks are fixedly connected to the inner walls of two opposite sides of the moving grooves, moving devices are fixedly connected to the left side and the right side of the installation block and extend into the moving grooves and are meshed with the racks, movable cavities are formed in the top inner wall and the bottom inner wall of the moving grooves, the top and the bottom of each moving device are slidably connected into the movable cavities, a temperature sensor probe is arranged at the bottom of the installation block, a central processing unit is arranged in the installation block, and a fixing device is fixedly connected to the rear side of the installation block, one side sliding connection of fixing device is in the sliding tray, and one side card of fixing device goes into in the fixed orifices, the sliding tray has been seted up to cavity top inner wall, has seted up the multiunit fixed orifices at sliding tray top inner wall, central processing unit's output is connected with the input electricity of warning light, the output of temperature sensor probe is connected with central processing unit's input electricity.
Preferably, the mobile device includes the fixed block, the fixed block is with the outside fixed connection of installation piece, fixed block sliding connection is in the shifting chute, the equal fixedly connected with backup pad in top and the bottom of fixed block, backup pad sliding connection is in the activity intracavity, the standing groove has been seted up to the inside of fixed block, standing groove bottom inner wall fixedly connected with motor, the output of motor and the bottom fixed connection of dwang, the top of dwang and the middle part fixed connection of bearing, the top and the standing groove top inner wall fixed connection of bearing, the outside fixed connection and the gear of dwang, wheel and rack toothing, the recess has been seted up to the inside of backup pad, the inner wall fixedly connected with center pin of recess, the gyro wheel has been cup jointed in the outside of center pin.
Preferably, the fixing device comprises a connecting plate, the front side of the connecting plate is fixedly connected with the rear side of the mounting block, the rear side of the connecting plate is fixedly connected with a clamping block, the clamping block is slidably connected in the sliding groove, the inner cavity of the clamping block is fixedly connected with a fixing plate, the middle part of the fixing plate is inserted with a clamping rod, the top end of the clamping rod penetrates through the clamping block and is clamped in the fixing hole, the top end of the clamping rod penetrates through the fixing plate and is fixedly connected with the top of the movable plate, the top of the movable plate is fixedly connected with the bottom end of a spring, the top end of the spring is fixedly connected with the bottom of the fixing plate, the spring is positioned on the outer side of the clamping rod, the top of the connecting plate is fixedly connected with a rotating motor, the output end of the rotating motor is fixedly connected with the bottom end of the movable column, the outer side of the movable column is fixedly connected with a turntable, and the inside of the turntable is fixedly connected with a connecting rope, one end of the connecting rope, which is far away from the rotary table, extends into the inner cavity of the clamping block and is fixedly connected with the bottom of the movable plate.
Preferably, the outer side of the central shaft is fixedly connected with two sets of anti-falling blocks, the two sets of anti-falling blocks are respectively positioned at the left side and the right side of the roller, the width of the supporting plate is matched with the width of the inner wall of the movable cavity, and the height of the supporting plate is matched with the height of the inner wall of the movable cavity.
Preferably, the balancing tank has all been seted up to the left side inner wall and the right side inner wall of cavity bottom, the inside sliding connection of balancing tank has the balancing plate, one side that the balancing tank was kept away from to the balancing plate runs through the balancing tank and extends to in the cavity, one side that the balancing tank was kept away from to the balancing plate and the outside fixed connection of installation piece, the high looks adaptation with the height of balancing tank inner wall of balancing plate, the length of balancing plate is less than the length of balancing tank inner wall, the height that highly is greater than the balancing tank inner wall of installation piece.
Preferably, the left side and the right side of the rack are both fixedly connected with blocking blocks, and the height of each blocking block is larger than that of the rack.
Preferably, the inner cavity of the clamping block is fixedly connected with a guide rod, and the outer side of the guide rod is in contact with the outer side of the connecting rope.
Preferably, four groups of sliding wheels are fixedly connected to the bottom of the machine body and are respectively positioned at four corners of the bottom of the machine body.
Preferably, the central processing unit is internally provided with: a heat dissipation fan and a controller;
the heat radiation fan is used for performing heat radiation treatment on the interior of the central processing unit;
the controller is connected with the radiating fan, calculates the internal temperature of the central processing unit, judges whether the internal temperature of the central processing unit is greater than a preset temperature value or not, and controls the radiating fan to start to radiate when the internal temperature of the central processing unit is determined to be greater than the preset temperature value;
the calculating the internal temperature of the central processing unit comprises the following steps:
step a1, calculating the thermal conductivity according to the following formula:
wherein mu represents the thermal conductivity coefficient, pi represents the natural constant, lambda represents the relative electrical constant of the material, LoRepresents the length of the CPU, LiRepresents the inner diameter of the cpu;
step A2, calculating the internal temperature of the CPU according to the following formula:
wherein T represents the CPU internal temperature, v represents the heat transfer rate, ρ1Represents the density of the material, beta represents the specific heat capacity, p2Represents the heat flow density, t represents the working time, and γ represents the prandtl number.
Another technical problem to be solved by the present invention is to provide a monitoring method for civil aviation operation data monitoring equipment, comprising the following steps:
the method comprises the following steps that firstly, starting power-on, pushing a civil aviation operation data monitoring device to the upper part of a wire harness, enabling the civil aviation operation data monitoring device to be electrically connected with external commercial power, and pressing a power switch to prepare operation;
step two, monitoring, namely starting a temperature sensor probe, transmitting the wire harness temperature data obtained by the temperature sensor probe to a central processing unit, judging whether the data is normal by the central processing unit, and controlling a warning lamp to be started by the central processing unit if the data is abnormal;
adjusting the position of a probe of the temperature sensor, adjusting the position of the mounting block, rotating the turntable to enable the clamping rod to be separated from the fixing hole, controlling the gear to rotate to enable the mounting block to transversely displace, reversely rotating the turntable to enable the clamping rod to be clamped into the fixing hole, and changing the position of the probe of the temperature sensor;
and step four, the rotary table is rotated to enable the clamping rod to be separated from the fixing hole, the mounting block is returned to the cavity by reversely rotating the gear, the rotary table is rotated again to enable the clamping rod to enter the fixing hole, and the power supply is turned off.
(III) advantageous effects
Compared with the prior art, the invention provides civil aviation operation data monitoring equipment and a monitoring method thereof, and the monitoring equipment has the following beneficial effects:
1. this civilian aviation operation data monitoring facilities, through setting up the mobile device, and then make the installation piece drive the temperature sensor probe and remove after opening the mobile device to make the position of temperature sensor probe no longer fixed, made things convenient for the pencil of temperature sensor probe to different positions to respond to, reduced the cost of monitoring pencil temperature data, and make operating personnel's work become convenient, reduce operating personnel's the work degree of difficulty, suitable popularization.
2. This civilian aviation operation data monitoring facilities through setting up backup pad and gyro wheel sliding connection in the activity intracavity, and then the gyro wheel makes mobile device's removal become smooth and easy, simultaneously because of the width of backup pad and the width looks adaptation of activity intracavity wall, so the setting up of backup pad makes mobile device 3 can not appear the condition that the dislocation leads to the device to become invalid in the removal, has ensured mobile device's normal removal.
3. This civilian aviation operation data monitoring facilities, through setting up fixing device, and then before removing the installation piece, open fixing device and make the installation piece no longer fixed to the installation piece can remove the position that changes the temperature sensor probe, and when the position of needs fixed temperature sensor probe, opens fixing device once more and can make the installation piece fix at the current position, thereby fixed the position of temperature sensor probe.
4. This civilian aviation operation data monitoring facilities, through setting up temperature sensor probe, central processing unit and warning light, and then the temperature data of pencil can be gathered to the temperature sensor probe, and the data transmission after the collection gives central processing unit, then judges whether data is normal by central processing unit, if have abnormal data central processing unit will control the warning light and open to warn peripheral staff, reduced dangerous emergence.
Drawings
Fig. 1 is a schematic structural diagram of a civil aviation operation data monitoring device provided by the invention;
FIG. 2 is a schematic diagram of a civil aviation operation data monitoring device mounting block structure according to the present invention;
fig. 3 is a sectional view of a civil aviation operation data monitoring device body structure according to the present invention;
fig. 4 is a structural sectional view of a mobile device of a civil aviation operation data monitoring device according to the present invention;
FIG. 5 is a sectional view of a civil aviation operation data monitoring device fixing device according to the present invention;
fig. 6 is a structural sectional view of a civil aviation operation data monitoring device body and a mounting block according to the present invention.
In the figure: 1. a body; 2. mounting blocks; 3. a mobile device; 301. a fixed block; 302. a placement groove; 303. a motor; 304. rotating the rod; 305. a gear; 306. a bearing; 307. a support plate; 308. a groove; 309. a roller; 310. an anti-drop block; 311. a central shaft; 4. a fixing device; 401. a connecting plate; 402. a rotating electric machine; 403. a turntable; 404. a movable post; 405. a guide bar; 406. a clamping block; 407. connecting ropes; 408. a movable plate; 409. clamping a stick; 410. a spring; 411. a fixing plate; 5. a sliding wheel; 6. a cavity; 7. a balancing tank; 8. a movable cavity; 9. a blocking block; 10. a warning light; 11. a handle; 12. a rack; 13. a moving groove; 14. a temperature sensor probe; 15. a sliding groove; 16. a fixing hole; 17. a balance plate; 18. a central processing unit.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-6, the present invention provides a technical solution: a civil aviation operation data monitoring device comprises a machine body 1, a cavity 6 is formed in the bottom of the machine body 1, a warning lamp 10 is arranged on the top of the machine body 1, a handle 11 is fixedly connected to the rear side of the top of the machine body 1, an installation block 2 is slidably connected to the interior of the cavity 6, moving grooves 13 are formed in the left inner wall and the right inner wall of the cavity 6, racks 12 are fixedly connected to the inner walls of the two opposite sides of the moving grooves 13, moving devices 3 are fixedly connected to the left side and the right side of the installation block 2, the installation block 2 drives a temperature sensor probe 14 to move after the moving devices 3 are started, so that the position of the temperature sensor probe 14 is not fixed, the temperature sensor probe 14 can conveniently sense wire harnesses at different positions, the cost for monitoring temperature data of the wire harnesses is reduced, and the work of operators is facilitated, the working difficulty of operators is reduced, the device is suitable for popularization, the mobile device 3 extends into the mobile groove 13 and is meshed with the rack 12, the inner wall of the top and the inner wall of the bottom of the mobile groove 13 are respectively provided with a movable cavity 8, the top and the bottom of the mobile device 3 are both connected in the movable cavities 8 in a sliding manner, the bottom of the mounting block 2 is provided with a temperature sensor probe 14, the inside of the mounting block 2 is provided with a central processing unit 18, the rear side of the mounting block 2 is fixedly connected with a fixing device 4, the fixing device 4 is arranged, then the mounting block 2 is not fixed before the mounting block 2 is moved, so that the mounting block 2 can be moved to change the position of the temperature sensor probe 14, when the position of the temperature sensor probe 14 needs to be fixed, the fixing device 4 is opened again to fix the mounting block 2 at the current position, so that the position of the temperature sensor probe 14 is fixed, one side sliding connection of fixing device 4 is in sliding tray 15, and one side card of fixing device 4 is gone into in fixed orifices 16, sliding tray 15 has been seted up to cavity 6 top inner wall, multiunit fixed orifices 16 have been seted up at sliding tray 15 top inner wall, central processing unit 18's output is connected with the input electricity of warning light 10, the output of temperature sensor probe 14 is connected with central processing unit 18's input electricity, through setting up temperature sensor probe 14, central processing unit 18 and warning light 10, and then temperature sensor probe 14 can gather the temperature data of pencil, the data transmission after the collection is for central processing unit 18, then judge whether data is normal by central processing unit 18, if abnormal data central processing unit 18 will control warning light 10 and open, thereby warn peripheral staff, dangerous emergence has been reduced.
In the invention, in order to conveniently adjust the position of the temperature sensor probe 14, the moving device 3 is arranged, the moving device 3 comprises a fixed block 301, the fixed block 301 is fixedly connected with the outer side of the mounting block 2, the fixed block 301 is slidably connected in a moving groove 13, the top and the bottom of the fixed block 301 are fixedly connected with supporting plates 307, the supporting plates 307 are slidably connected in a movable cavity 8, the supporting plates 307 are slidably connected in the movable cavity 8 through arranging the supporting plates 307 and rollers 309, and the rollers 309 enable the moving of the moving device 3 to be smooth, meanwhile, the arrangement of the supporting plates 307 enables the moving device 3 not to be out of work due to dislocation in the moving process because the width of the supporting plates 307 is matched with the width of the inner wall of the movable cavity 8, the normal moving of the moving device 3 is ensured, a placing groove 302 is arranged in the fixed block 301, and a motor 303 is fixedly connected to the inner wall of the bottom of the placing groove 302, the output of motor 303 and the bottom fixed connection of dwang 304, the top of dwang 304 and the middle part fixed connection of bearing 306, the top and the standing groove 302 top inner wall fixed connection of bearing 306, the outside fixed connection and the gear 305 of dwang 304, gear 305 and rack 12 meshing, recess 308 has been seted up to the inside of backup pad 307, the inner wall fixedly connected with center pin 311 of recess 308, gyro wheel 309 has been cup jointed in the outside of center pin 311, open behind the motor 303 rotation of gear 305 will and the mutual cooperation between rack 12, thereby make installation piece 2 remove, and the removal of installation piece 2 will drive temperature sensor probe 14 and remove, thereby the position of regulation temperature sensor probe 14 that can be convenient.
In the invention, in order to fix the position of the temperature sensor probe 14 and prevent the temperature sensor probe from shaking, a fixing device 4 is provided, the fixing device 4 comprises a connecting plate 401, the front side of the connecting plate 401 is fixedly connected with the rear side of the mounting block 2, the rear side of the connecting plate 401 is fixedly connected with a fixture block 406, the fixture block 406 is slidably connected in the sliding groove 15, the inner cavity of the fixture block 406 is fixedly connected with a fixing plate 411, the middle part of the fixing plate 411 is inserted with a fixture rod 409, the top end of the fixture rod 409 penetrates through the fixture block 406 and is clamped in the fixing hole 16, the top end of the fixture rod 409 penetrates through the fixing plate 411 and is fixedly connected with the top of the movable plate 408, the top of the movable plate 408 is fixedly connected with the bottom end of a spring 410, the top end of the spring 410 is fixedly connected with the bottom of the fixing plate 411, the spring 410 is positioned at the outer side of the fixture rod 409, the top of the connecting plate 401 is fixedly connected with a rotating motor 402, the output end of the rotating motor 402 is fixedly connected with the bottom end of the movable column 404, the outer side fixedly connected with carousel 403 of activity post 404, the inside fixedly connected with of carousel 403 connects rope 407, connects the one end that rope 407 kept away from carousel 403 and stretches into fixture block 406 inner chamber and with the bottom fixed connection of fly leaf 408, can the position of fixed mounting piece 2 after the card rod 409 card goes into fixed orifices 16 from this, the fixed position that can fix temperature sensor probe 14 of installation piece 2 prevents it to rock.
In the present invention, in order to prevent the roller 309 from being displaced, two sets of anti-slip blocks 310 are fixedly connected to the outside of the central shaft 311, and the two sets of anti-slip blocks 310 are respectively located on the left and right sides of the roller 309, so that the roller 309 can be received by the anti-slip blocks 310.
In the invention, in order to prevent the mounting block 2 from being misplaced in the movement, the left inner wall and the right inner wall of the bottom of the cavity 6 are both provided with the balance groove 7, the balance plate 17 is slidably connected inside the balance groove 7, one side of the balance plate 17, which is far away from the balance groove 7, penetrates through the balance groove 7 and extends into the cavity 6, one side of the balance plate 17, which is far away from the balance groove 7, is fixedly connected with the outer side of the mounting block 2, the height of the balance plate 17 is matched with the height of the inner wall of the balance groove 7, the length of the balance plate 17 is smaller than that of the inner wall of the balance groove 7, and the height of the mounting block 2 is larger than that of the inner wall of the balance groove 7, so that the mounting block 2 can be prevented from being misplaced in the movement through the balance plate 17.
In the present invention, in order to prevent the gear 305 from being separated from the rack 12, the stoppers 9 are fixedly connected to both left and right sides of the rack 12, and the height of the stopper 9 is greater than that of the rack 12, so that the gear 305 can be stopped by the stopper 9.
In the present invention, in order to prevent the connection cord 407 from being cut, the guide rod 405 is fixedly coupled to the inner cavity of the latch 406, and the outer side of the guide rod 405 is in contact with the outer side of the connection cord 407, thereby preventing the connection cord 407 from being cut by the guide rod 405.
In the present invention, in order to smoothly move the supporting plate 307, the width of the supporting plate 307 is adapted to the width of the inner wall of the movable chamber 8, and the height of the supporting plate 307 is adapted to the height of the inner wall of the movable chamber 8, so that the supporting plate 307 can smoothly move.
In the invention, in order to move the device conveniently, four sets of sliding wheels 5 are fixedly connected to the bottom of the machine body 1, and the four sets of sliding wheels 5 are respectively positioned at four corners of the bottom of the machine body 1, so that the device can be moved conveniently through the sliding wheels 5.
When the temperature sensor probe 14 is used, the temperature sensor probe is started to collect temperature data of a wire harness, the collected data is transmitted to the central processing unit 18, whether the data is normal or not is judged by the central processing unit 18, if the data is abnormal, the central processing unit 18 controls the warning lamp 10 to be started, thereby warning surrounding workers, and reducing the occurrence of danger, if other positions of the wire harness need to be monitored, the rotating motor 402 is controlled to rotate, so that the rotating disc 403 rotates to stretch the connecting rope 407, the connecting rope 407 pulls the movable plate 408 to move downwards, the movable plate 408 moves downwards to drive the clamping rod 409 to be separated from the currently clamped fixing hole 16, then the motor 303 is started, so that the output end of the motor 303 drives the gear 305 to rotate, the gear 305 forms dislocation of teeth with the rack 12 during rotation, so as to generate reverse motion, and the rotation of the gear 305 drives the mounting block 2 to move, the movement of the mounting block 2 can drive the temperature sensor probe 14 to move, so that the temperature sensor probe 14 can rapidly monitor other positions of the wiring harness, the position of the temperature sensor probe 14 needs to be fixed, the movement of the mounting block 2 is controlled to enable the clamping rod 409 to coincide with the fixing hole 16 closest to the current position, then the output end of the rotating motor 402 is controlled to rotate reversely, the spring 410 is further used for bouncing the movable plate 408 to ascend, the clamping rod 409 is clamped into the fixing hole 16, the mounting block 2 is fixed at the current position, and the fixing of the mounting block 2 enables the temperature sensor probe 14 to be fixed at the current position.
In conclusion, this civilian aviation operation data monitoring facilities through setting up mobile device 3, and then makes installation piece 2 drive temperature sensor probe 14 and remove after opening mobile device 3 to make temperature sensor probe 14's position no longer fixed, made things convenient for temperature sensor probe 14 to respond to the pencil of different positions, reduced the cost of monitoring pencil temperature data, and make operating personnel's work become convenient, reduced operating personnel's the work degree of difficulty, suitable popularization.
This civilian aviation operation data monitoring facilities through setting up backup pad 307 and gyro wheel 309 sliding connection in activity chamber 8, and then gyro wheel 309 makes mobile device 3's removal become smooth and easy, simultaneously because of the width of backup pad 307 and the width looks adaptation of activity chamber 8 inner wall, so the setting up of backup pad 307 makes mobile device 3 can not appear the condition that the dislocation leads to the device to become invalid in the removal, has ensured mobile device 3's normal removal.
This civilian aviation operation data monitoring facilities, through setting up fixing device 4, and then before removing installation piece 2, open fixing device 4 and make installation piece 2 no longer fixed to installation piece 2 can move the position that changes temperature sensor probe 14, and when the position of need fixed temperature sensor probe 14, open fixing device 4 once more and can make installation piece 2 fix current position, thereby fixed temperature sensor probe 14's position.
This civilian aviation operation data monitoring facilities through setting up temperature sensor probe 14, central processing unit 18 and warning light 10, and then the temperature data of pencil can be gathered to temperature sensor probe 14, and the data transmission after the collection gives central processing unit 18, then judges by central processing unit 18 whether data is normal, and if having unusual data central processing unit 18 to control warning light 10 and open to warn peripheral staff, reduced dangerous emergence.
In the present invention, in order to prevent the temperature inside the cpu 18 from being too high, the cpu 18 is provided with: a heat dissipation fan and a controller;
a heat radiation fan for performing heat radiation processing on the inside of the central processing unit 1;
the controller is connected with the heat radiation fan, calculates the internal temperature of the central processing unit, judges whether the internal temperature of the central processing unit 18 is greater than a preset temperature value or not, and controls the heat radiation fan to start to radiate heat when the internal temperature of the central processing unit 18 is determined to be greater than the preset temperature value;
the calculation of the temperature inside the central processor 18 includes:
step a1, calculating the thermal conductivity according to the following formula:
wherein mu represents the thermal conductivity coefficient, pi represents the natural constant, lambda represents the relative electrical constant of the material, LoRepresents the length, L, of the CPU 18iRepresents the internal workings of the central processor 18;
step a2, calculating the internal temperature of the cpu 18 according to the following formula:
where T represents the CPU 18 internal temperature, v represents the heat transfer rate, ρ1Represents the density of the material, beta represents the specific heat capacity, p2Represents the heat flow density, t represents the working time, and γ represents the prandtl number.
Has the advantages that: through the technical scheme, the central controller 18 is provided with the cooling fan for cooling the interior of the central processor 18, the controller is connected with the cooling fan, calculates the temperature of the interior of the central processor and judges whether the temperature of the interior of the central processor 18 is greater than a preset temperature value or not, when the temperature of the interior of the central processor 18 is determined to be greater than the preset temperature value, the controller controls the cooling fan to be started for cooling, the factors such as heat conduction coefficient, heat transfer rate, material density, specific heat capacity, heat flow density and working time are considered when the temperature of the interior of the central processor 18 is calculated by the algorithm, so that the calculated result is more accurate, the accuracy of judging whether the temperature of the interior of the central processor 18 is greater than the preset temperature value by the controller is improved, the cooling fan is limited to be started to cool the interior of the central processor 18, thereby greatly improving the working efficiency of the central processing unit 18, avoiding the fault of the central processing unit 18 caused by overhigh temperature and further prolonging the service life of the central processing unit 18.
In another aspect, a monitoring method for civil aviation operation data monitoring equipment is provided, which includes the following steps:
the method comprises the following steps that firstly, starting power-on, pushing a civil aviation operation data monitoring device to the upper part of a wire harness, enabling the civil aviation operation data monitoring device to be electrically connected with external commercial power, and pressing a power switch to prepare operation;
monitoring, namely starting the temperature sensor probe 14, transmitting the wire harness temperature data obtained by the temperature sensor probe 14 to the central processing unit 18, judging whether the data is normal by the central processing unit 18, and controlling the warning lamp 10 to be started by the central processing unit 18 if the data is abnormal;
thirdly, adjusting the position of the temperature sensor probe 14, adjusting the position of the mounting block 2, rotating the turntable 403 to enable the clamping rod 409 to be separated from the fixing hole 16, controlling the gear 305 to rotate to enable the mounting block 2 to transversely displace, reversely rotating the turntable 403 to enable the clamping rod 409 to be clamped in the fixing hole 16, and changing the position of the temperature sensor probe 14;
and step four, rotating the turntable 403 to enable the clamping rod 409 to be separated from the fixing hole 16, reversely rotating the gear 305 to enable the mounting block 2 to return to the cavity 6, rotating the turntable 403 again to enable the clamping rod 409 to enter the fixing hole 16, and turning off the power supply.
The electrical components presented in the document are all electrically connected with an external master controller and 220V mains, and the master controller can be a conventional known device controlled by a computer or the like.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Also in the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", and the like, indicate orientations and positional relationships based on those shown in the drawings, and are used only for convenience of description and simplicity of description, and do not indicate or imply that the equipment or element so referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be considered as limiting the present invention. In the drawings of the present invention, the filling pattern is only for distinguishing the layers, and is not limited to any other way.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (8)
1. A civil aviation operation data monitoring device, includes organism (1), its characterized in that: the temperature sensor is characterized in that a cavity (6) is formed in the bottom of the machine body (1), warning lamps (10) are arranged at the top of the machine body (1), a handle (11) is fixedly connected to the rear side of the top of the machine body (1), an installation block (2) is connected to the inside of the cavity (6) in a sliding manner, moving grooves (13) are formed in the left inner wall and the right inner wall of the cavity (6), racks (12) are fixedly connected to the inner walls of two opposite sides of the moving grooves (13), moving devices (3) are fixedly connected to the left side and the right side of the installation block (2), the moving devices (3) extend into the moving grooves (13) and are meshed with the racks (12), movable cavities (8) are formed in the inner walls of the top and the bottom of the moving grooves (13), the top and the bottom of the moving devices (3) are slidably connected into the movable cavities (8), temperature sensor probes (14) are arranged at the bottom of the installation block (2), a central processing unit (18) is arranged in the mounting block (2), a fixing device (4) is fixedly connected to the rear side of the mounting block (2), one side of the fixing device (4) is connected in a sliding groove (15) in a sliding mode, one side of the fixing device (4) is clamped in a fixing hole (16), the sliding groove (15) is formed in the inner wall of the top of the cavity (6), a plurality of groups of fixing holes (16) are formed in the inner wall of the top of the sliding groove (15), the output end of the central processing unit (18) is electrically connected with the input end of the warning lamp (10), and the output end of the temperature sensor probe (14) is electrically connected with the input end of the central processing unit (18);
the moving device (3) comprises a fixed block (301), the fixed block (301) is fixedly connected with the outer side of the installation block (2), the fixed block (301) is connected in a moving groove (13) in a sliding manner, the top and the bottom of the fixed block (301) are fixedly connected with a supporting plate (307), the supporting plate (307) is connected in a movable cavity (8) in a sliding manner, a placing groove (302) is formed in the fixed block (301), a motor (303) is fixedly connected to the inner wall of the bottom of the placing groove (302), the output end of the motor (303) is fixedly connected with the bottom of a rotating rod (304), the top end of the rotating rod (304) is fixedly connected with the middle of a bearing (306), the top of the bearing (306) is fixedly connected with the inner wall of the top of the placing groove (302), the outer side of the rotating rod (304) is fixedly connected with a gear (305), and the gear (305) is meshed with a rack (12), a groove (308) is formed in the supporting plate (307), the inner wall of the groove (308) is fixedly connected with a central shaft (311), and the outer side of the central shaft (311) is sleeved with a roller (309);
the fixing device (4) comprises a connecting plate (401), the front side of the connecting plate (401) is fixedly connected with the rear side of the mounting block (2), the rear side of the connecting plate (401) is fixedly connected with a clamping block (406), the clamping block (406) is slidably connected in a sliding groove (15), an inner cavity of the clamping block (406) is fixedly connected with a fixing plate (411), a clamping roller (409) is inserted in the middle of the fixing plate (411), the top end of the clamping roller (409) penetrates through the clamping block (406) and is clamped in a fixing hole (16), the top end of the clamping roller (409) penetrates through the fixing plate (411) and is fixedly connected with the top of the movable plate (408), the top of the movable plate (408) is fixedly connected with the bottom end of the spring (410), the top end of the spring (410) is fixedly connected with the bottom of the fixing plate (411), and the spring (410) is located on the outer side of the clamping roller (409), the top fixedly connected with rotating electrical machines (402) of connecting plate (401), the output of rotating electrical machines (402) and the bottom fixed connection of activity post (404), the outside fixedly connected with carousel (403) of activity post (404), the inside fixedly connected with of carousel (403) connects rope (407), connect rope (407) keep away from the one end of carousel (403) stretch into fixture block (406) inner chamber and with the bottom fixed connection of fly leaf (408).
2. Civil aviation operation data monitoring device according to claim 1, characterized in that: the outside fixedly connected with two sets of anticreep pieces (310) of center pin (311), it is two sets of anticreep piece (310) are located the left and right sides of gyro wheel (309) respectively, the width of backup pad (307) and the width looks adaptation of activity chamber (8) inner wall, and the height looks adaptation of backup pad (307) and activity chamber (8) inner wall.
3. Civil aviation operation data monitoring device according to claim 1, characterized in that: balancing tank (7) have all been seted up to the left side inner wall and the right side inner wall of cavity (6) bottom, the inside sliding connection of balancing tank (7) has balancing plate (17), one side that balancing tank (7) were kept away from in balancing plate (17) runs through balancing tank (7) and extends to cavity (6), one side that balancing tank (7) were kept away from in balancing plate (17) and the outside fixed connection of installation piece (2), the height of balancing plate (17) and the high looks adaptation of balancing tank (7) inner wall, the length of balancing plate (17) is less than the length of balancing tank (7) inner wall, the height that highly is greater than balancing tank (7) inner wall of installation piece (2).
4. Civil aviation operation data monitoring device according to claim 1, characterized in that: the left side and the right side of the rack (12) are fixedly connected with blocking blocks (9), and the height of each blocking block (9) is larger than that of the rack (12).
5. Civil aviation operation data monitoring device according to claim 1, characterized in that: the inner cavity of the clamping block (406) is fixedly connected with a guide rod (405), and the outer side of the guide rod (405) is in contact with the outer side of the connecting rope (407).
6. Civil aviation operation data monitoring device according to claim 1, characterized in that: the bottom of the machine body (1) is fixedly connected with four groups of sliding wheels (5), and the four groups of sliding wheels (5) are respectively positioned at four corners of the bottom of the machine body (1).
7. Civil aviation operation data monitoring device according to claim 1, characterized in that: the central processing unit (18) is internally provided with: a heat dissipation fan and a controller;
the heat radiation fan is used for performing heat radiation treatment on the interior of the central processing unit (18);
the controller is connected with the heat radiation fan, calculates the internal temperature of the central processing unit (18), judges whether the internal temperature of the central processing unit (18) is greater than a preset temperature value or not, and controls the heat radiation fan to start to radiate heat when the internal temperature of the central processing unit (18) is determined to be greater than the preset temperature value;
the calculation of the internal temperature of the central processing unit (18) comprises:
step a1, calculating the thermal conductivity according to the following formula:
wherein mu represents the thermal conductivity coefficient, pi represents the natural constant, lambda represents the relative electrical constant of the material, LoRepresents the length of the CPU, LiRepresents the internal direct of the central processor (18);
step A2, calculating the internal temperature of the central processing unit (18) according to the following formula:
wherein T represents the internal temperature of the CPU (18), v represents the heat transfer rate, p1Represents the density of the material, beta represents the specific heat capacity, p2Represents the heat flow density, t represents the working time, and γ represents the prandtl number.
8. A monitoring method of civil aviation operation data monitoring equipment is characterized by comprising the following steps:
starting, namely starting power-on, pushing the civil aviation operation data monitoring equipment as claimed in any one of claims 1 to 7 to the upper part of a wire harness, electrically connecting the civil aviation operation data monitoring equipment as claimed in any one of claims 1 to 7 with external commercial power, and pressing a power switch to prepare operation;
monitoring, namely starting a temperature sensor probe (14), transmitting the wire harness temperature data obtained by the temperature sensor probe (14) to a central processing unit (18), judging whether the data is normal or not by the central processing unit (18), and controlling the warning lamp (10) to be started by the central processing unit (18) if the data is abnormal;
thirdly, adjusting the position of the temperature sensor probe (14), adjusting the position of the mounting block (2), rotating the turntable (403) to enable the clamping rod (409) to be separated from the fixing hole (16), controlling the gear (305) to rotate to enable the mounting block (2) to be transversely displaced, reversely rotating the turntable (403) to enable the clamping rod (409) to be clamped in the fixing hole (16), and changing the position of the temperature sensor probe (14);
and step four, rotating the turntable (403) to enable the clamping roller (409) to be separated from the fixing hole (16), reversely rotating the gear (305) to enable the mounting block (2) to return to the cavity (6), rotating the turntable (403) again to enable the clamping roller (409) to enter the fixing hole (16), and turning off the power supply.
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| CN114216039A (en) * | 2021-12-20 | 2022-03-22 | 罗益机械制造(苏州)有限公司 | Adjustable temperature sensor support mounting frame structure |
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