CN107416216A - A kind of aircraft drunk-driving prevention intelligent monitor system - Google Patents
A kind of aircraft drunk-driving prevention intelligent monitor system Download PDFInfo
- Publication number
- CN107416216A CN107416216A CN201710317362.7A CN201710317362A CN107416216A CN 107416216 A CN107416216 A CN 107416216A CN 201710317362 A CN201710317362 A CN 201710317362A CN 107416216 A CN107416216 A CN 107416216A
- Authority
- CN
- China
- Prior art keywords
- aircraft
- drunk
- intelligent monitor
- driving prevention
- amplifier
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 230000002265 prevention Effects 0.000 title claims abstract description 16
- 238000004891 communication Methods 0.000 claims abstract description 15
- 239000004973 liquid crystal related substance Substances 0.000 claims abstract description 12
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 abstract description 21
- 210000001124 body fluid Anatomy 0.000 abstract description 12
- 239000010839 body fluid Substances 0.000 abstract description 12
- 238000001514 detection method Methods 0.000 abstract description 5
- 230000035622 drinking Effects 0.000 abstract description 4
- 238000012360 testing method Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 238000009434 installation Methods 0.000 description 2
- 206010039203 Road traffic accident Diseases 0.000 description 1
- 150000001298 alcohols Chemical class 0.000 description 1
- 230000003321 amplification Effects 0.000 description 1
- 238000007405 data analysis Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000004927 fusion Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000003199 nucleic acid amplification method Methods 0.000 description 1
- 230000029058 respiratory gaseous exchange Effects 0.000 description 1
- 238000005070 sampling Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D43/00—Arrangements or adaptations of instruments
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
- B60K28/00—Safety devices for propulsion-unit control, specially adapted for, or arranged in, vehicles, e.g. preventing fuel supply or ignition in the event of potentially dangerous conditions
- B60K28/02—Safety devices for propulsion-unit control, specially adapted for, or arranged in, vehicles, e.g. preventing fuel supply or ignition in the event of potentially dangerous conditions responsive to conditions relating to the driver
- B60K28/06—Safety devices for propulsion-unit control, specially adapted for, or arranged in, vehicles, e.g. preventing fuel supply or ignition in the event of potentially dangerous conditions responsive to conditions relating to the driver responsive to incapacity of driver
- B60K28/063—Safety devices for propulsion-unit control, specially adapted for, or arranged in, vehicles, e.g. preventing fuel supply or ignition in the event of potentially dangerous conditions responsive to conditions relating to the driver responsive to incapacity of driver preventing starting of vehicles
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Auxiliary Drives, Propulsion Controls, And Safety Devices (AREA)
- Investigating Or Analysing Biological Materials (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
Abstract
A kind of aircraft drunk-driving prevention intelligent monitor system.It includes three skin sensors, amplifier, A/D converter, single-chip computer control system, GPS positioning system, gsm wireless communication system, relay, alarm system, liquid crystal display systems and power supply.Advantage of the present invention：Using three skin sensors, the alcohol concentration in captain and copilot body fluid can be detected respectively, the just automatic start relative program when detecting that alcohol concentration is exceeded in any human body fluid, prevents from flying after drinking, effectively reduce persons on board's life and property loss.The alcohol concentration in captain and copilot body fluid can be detected effectively in real time, overcome artificial selective examination incomprehensive, improved flight safety.Be advantageous to aircraft safety as intelligent control center, accuracy and data transfer using single-chip microcomputer and detect to completely electronic era development.Using skin sensor, aircrew effectively reduces relevant staff's workload by contacting alcohol concentration in skin sensor automatic detection body fluid.
Description
Technical field
The invention belongs to aircraft field of intelligent control technology, more particularly to a kind of aircraft drunk-driving prevention intelligent monitor system.
Background technology
Nowadays traffic accident is of common occurrence, causes substantial amounts of property and human loss.Drive when intoxicated is to trigger traffic thing
One of therefore the main reason for, whether after drinking domestic public security traffic control department mainly detects driver using portable type of respiration alcohol tester
Drive, but this alcohol content tester must can only be directed to Some vehicles sampling inspection by law enfrocement official to driver's compulsory test
Survey, driver can not be monitored in real time and driven when intoxicated situation, efficiency is low and has a strong impact on normal traffic.
Existing vehicle-mounted alcohol test system uses single sensor more, it is impossible to takes into full account in-car air-flow actual conditions, does
Disturb big and be difficult to promote very well.As multisensor Data Fusion technology develops, a kind of vehicle-mounted alcohol test system is designed,
In-car many places, which are layouted, gathers information, by the way that multiple alcohol sensor alcohol concentration information are merged, provides driver's prompting
And warning, but this system is relative complex, and data analysis is lost precisely.
For the airport of security incident zero tolerance, in the improper security incident of aircraft pilot's drunk driving be also reason it
One, extremely serious life and property loss caused by meeting.Pilot receives alcohol concentration selective examination before performing aerial mission, and selective examination is real
It is narrow to apply face, it is impossible to carry out absoluteness control to flying after drinking.
The content of the invention
In order to solve the above problems, it is an object of the invention to provide a kind of aircraft drunk-driving prevention intelligent monitor system.
In order to achieve the above object, aircraft drunk-driving prevention intelligent monitor system provided by the invention includes：Three skin sensings
Device, amplifier, A/D converter, single-chip computer control system, GPS positioning system, gsm wireless communication system, relay, dangerous report
Alert system, liquid crystal display systems and power supply, wherein：Three skin sensors are connected with amplifier respectively, and amplifier is turned by A/D
Parallel operation is connected with single-chip computer control system, single-chip computer control system respectively with gsm wireless communication system, relay, danger warning
System is connected with liquid crystal display systems, and GPS positioning system is connected with single-chip computer control system and gsm wireless communication system respectively,
Power supply is connected with each consuming parts in the system.
Described relay is connected with aircraft engine starting-up later time.
Three described skin sensors are separately mounted on throttle lever and control stick；Liquid crystal display systems is mounted on
In the cabin on the pilot crown, it is attached that anticollision beacon and stroboscopic lamp in alarm system are arranged on the outer fuselage receiver J-Horner of aircraft
Closely；Amplifier, A/D converter, single-chip computer control system, GPS positioning system, gsm wireless communication system, relay and power supply peace
In airframe.
Aircraft drunk-driving prevention intelligent monitor system provided by the invention compared with the prior art the advantages of：
1st, the present invention uses three skin sensors, can accurately detect out the wine in captain and copilot body fluid respectively
Smart concentration, the just automatic start relative program when detecting that alcohol concentration is exceeded in any human body fluid, prevents from flying after drinking, can have
Effect reduces persons on board's life and property loss.
2nd, the present invention can detect the alcohol concentration in captain and copilot body fluid effectively in real time, overcome artificial selective examination
It is incomprehensive, can effectively control drunk driving, improve flight safety.
3rd, the present invention is advantageous to aircraft safety detection using single-chip microcomputer as intelligent control center, accuracy and data transfer
To completely electronic era development.
4th, the present invention is using the alcohol concentration in skin sensor detection aircrew's body fluid, and the vehicle-mounted expiration alcohol of tradition
Detector is compared, and is reduced the influence of space air humidity, temperature to testing result, can be improved detection accuracy.
5th, the present invention uses skin sensor, and aircrew is by contacting the alcohol in skin sensor automatic detection body fluid
Concentration, it can effectively reduce relevant staff's workload.
Brief description of the drawings
Fig. 1 is that aircraft drunk-driving prevention intelligent monitor system provided by the invention forms schematic diagram.
Fig. 2 is skin sensor installation site in the aircraft drunk-driving prevention intelligent monitor system provided by the invention on throttle lever
Schematic diagram.
Fig. 3 is skin sensor installation site in the aircraft drunk-driving prevention intelligent monitor system provided by the invention on control stick
Schematic diagram.
Embodiment
Aircraft drunk-driving prevention intelligent monitor system provided by the invention is carried out with specific embodiment below in conjunction with the accompanying drawings detailed
Explanation.
As shown in figure 1, aircraft drunk-driving prevention intelligent monitor system provided by the invention includes：
Three skin sensors 1, amplifier 2, A/D converter 3, single-chip computer control system 4, GPS positioning system 5, GSM without
Line communication system 6, relay 7, alarm system 8, liquid crystal display systems 9 and power supply 10, wherein：Three skin sensors 1
It is connected respectively with amplifier 2, amplifier 2 is connected by A/D converter 3 with single-chip computer control system 4, single-chip computer control system 4
It is connected respectively with gsm wireless communication system 6, relay 7, alarm system 8 and liquid crystal display systems 9, GPS positioning system 5
It is connected respectively with single-chip computer control system 4 and gsm wireless communication system 6, power supply 10 is connected with each consuming parts in the system.
Described power supply 10 is used for powering to each consuming parts；Three skin sensors 1 are respectively intended to detect captain and pair
The alcohol concentration signal in body fluid is driven, the alcohol concentration analog signal that amplifier 2 detects skin sensor 1 is amplified, A/D
Alcohol concentration analog signal after amplifier 2 amplifies is changed into data signal and is transmitted to single-chip microcomputer control system by converter 3
System 4, single-chip computer control system 4 is handled the alcohol concentration data signal after amplification, and is contrasted with the standard value of storage, when
When testing result is exceeded, single-chip computer control system 4 is respectively to relay 7, alarm system 8, liquid crystal display systems 9 and GSM
Wireless communication system 6 sends control instruction；GPS positioning system 5 be used for aircraft carry out precise positioning, alarm system 8 by
Anticollision beacon and stroboscopic lamp, buzzer composition, after being connected to the control instruction of single-chip computer control system 4, anticollision beacon and stroboscopic lamp are opened,
To cause ground crewmember attention, while buzzer sends alarm：" please the life of all personnel, property on machine are responsible for,
You are drunk to fly ".Liquid crystal display systems 9 then shows the alcohol concentration in pilot's body fluid, gsm wireless communication system
6 receive GPS positioning system 5 to after the positioning signal of aircraft single-chip computer control system 4 control under from trend control tower work people
Member's alarm, there is provided pilot's information and aircraft position, model, order of classes or grades at school.Relay 7 is connected with aircraft engine starting-up later time,
The lower relay 7 of the control of single-chip computer control system 4 remains open, to prevent aircraft engine from starting.
As shown in Figure 2 and Figure 3, three described skin sensors 1 are separately mounted on throttle lever 11 and control stick 12, when
Captain and copilot grasp throttle lever 11 and when control stick 12 are operated, and skin sensor 1 can be with captain and the passenger side
The hand skin sailed is in contact, therefore can detect the alcohol concentration in captain and copilot body fluid, and liquid crystal display systems 9 is installed
In the cabin positioned at the pilot crown, anticollision beacon and stroboscopic lamp in alarm system 8 are arranged on the outer fuselage earphone of aircraft
Near socket, amplifier 2, A/D converter 3, single-chip computer control system 4, GPS positioning system 5, gsm wireless communication system 6, after
Electrical equipment 7 and power supply 10 are arranged in airframe.
Claims (3)
- A kind of 1. aircraft drunk-driving prevention intelligent monitor system, it is characterised in that：Described aircraft drunk-driving prevention intelligent monitor system includes：Three skin sensors (1), amplifier (2), A/D converter (3), single-chip computer control system (4), GPS positioning system (5), gsm wireless communication system (6), relay (7), alarm system (8), liquid crystal display systems (9) and power supply (10), its In：Three skin sensors (1) are connected with amplifier (2) respectively, and amplifier (2) is controlled by A/D converter (3) and single-chip microcomputer System (4) connect, single-chip computer control system (4) respectively with gsm wireless communication system (6), relay (7), alarm system (8) with liquid crystal display systems (9) connect, GPS positioning system (5) respectively with single-chip computer control system (4) and gsm wireless communication system System (6) connection, power supply (10) are connected with each consuming parts in the system.
- 2. aircraft drunk-driving prevention intelligent monitor system according to claim 1, it is characterised in that：Described relay (7) with Aircraft engine starting-up later time connects.
- 3. aircraft drunk-driving prevention intelligent monitor system according to claim 1, it is characterised in that：Described three skins sensing Device (1) is separately mounted on throttle lever (11) and control stick (12)；Liquid crystal display systems (9) is mounted on the pilot crown In cabin, anticollision beacon and stroboscopic lamp in alarm system (8) are arranged near the outer fuselage receiver J-Horner of aircraft；Amplifier (2), A/D converter (3), single-chip computer control system (4), GPS positioning system (5), gsm wireless communication system (6), relay (7) it is arranged on power supply (10) in airframe.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710317362.7A CN107416216A (en) | 2017-05-08 | 2017-05-08 | A kind of aircraft drunk-driving prevention intelligent monitor system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710317362.7A CN107416216A (en) | 2017-05-08 | 2017-05-08 | A kind of aircraft drunk-driving prevention intelligent monitor system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107416216A true CN107416216A (en) | 2017-12-01 |
Family
ID=60424512
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710317362.7A Pending CN107416216A (en) | 2017-05-08 | 2017-05-08 | A kind of aircraft drunk-driving prevention intelligent monitor system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107416216A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102642467A (en) * | 2011-12-12 | 2012-08-22 | 浙江吉利汽车研究院有限公司 | Drunk driving prevention processing system for automobile and control method |
| CN203142402U (en) * | 2013-01-16 | 2013-08-21 | 华南理工大学广州学院 | Humanized vehicle-mounted safe driving system |
| CN203528310U (en) * | 2013-09-17 | 2014-04-09 | 黄军友 | Intelligent automobile drunk driving identification and control system |
| CN103818257A (en) * | 2014-01-08 | 2014-05-28 | 吉林大学 | Vehicle-mounted drunk driving initiative response system |
| CN105667312A (en) * | 2016-04-15 | 2016-06-15 | 吉林大学 | Intelligent drunk driving prevention and control system based on vehicle |
-
2017
- 2017-05-08 CN CN201710317362.7A patent/CN107416216A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102642467A (en) * | 2011-12-12 | 2012-08-22 | 浙江吉利汽车研究院有限公司 | Drunk driving prevention processing system for automobile and control method |
| CN203142402U (en) * | 2013-01-16 | 2013-08-21 | 华南理工大学广州学院 | Humanized vehicle-mounted safe driving system |
| CN203528310U (en) * | 2013-09-17 | 2014-04-09 | 黄军友 | Intelligent automobile drunk driving identification and control system |
| CN103818257A (en) * | 2014-01-08 | 2014-05-28 | 吉林大学 | Vehicle-mounted drunk driving initiative response system |
| CN105667312A (en) * | 2016-04-15 | 2016-06-15 | 吉林大学 | Intelligent drunk driving prevention and control system based on vehicle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN205405811U (en) | Vehicle status monitored control system | |
| US20140257603A1 (en) | Aircraft braking early warning system | |
| CN104217539B (en) | Taxi personnel's real-time monitoring platform | |
| CN106843046B (en) | Artificial precipitation aircraft detection operation system | |
| CN107856537A (en) | One kind prevents drunk driving, prevents fatigue driving system | |
| CN202853646U (en) | Multi-type sensor testing device | |
| CN201566837U (en) | Configuration of sensor for aircraft icing | |
| CN201777145U (en) | Non-contact vehicle-mounted alcohol detection and drunk driving control system | |
| US7714743B1 (en) | Aircraft lightning strike detector | |
| CN109733626B (en) | Amphibious aircraft cabin door alarm and indication system | |
| CN109552661A (en) | Machine docking system is leaned on a kind of airport | |
| CN107416216A (en) | A kind of aircraft drunk-driving prevention intelligent monitor system | |
| CN104240440A (en) | Method for monitoring personnel in taxi in real time | |
| CN103335774A (en) | Intelligent airplane tire pressure detector | |
| CN203282981U (en) | Intelligentized aircraft tire pressure detector | |
| CN106153104A (en) | A kind of intelligent link system | |
| CN104898121A (en) | Runway collision avoidance system based on ranging mode and method thereof | |
| CN105361863B (en) | Aircraft captain's physiological parameter monitoring system | |
| CN205388695U (en) | Ordnance equipment transports whole monitored control system | |
| CN209684026U (en) | Machine docking system is leaned on a kind of airport | |
| CN203773689U (en) | Marine engineer inspection alarm apparatus | |
| CN107132807A (en) | A kind of passive inflammable volatile matter monitoring device and remote supervision system | |
| EP1980489A3 (en) | Aircraft security | |
| CN207059777U (en) | A kind of active safety early warning system | |
| CN206544512U (en) | A kind of offline secure warning system in traffic monitoring |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20171201 |
|
| WD01 | Invention patent application deemed withdrawn after publication |