CN103950545B - Airplane black box position apprizing and route tracking system - Google Patents
Airplane black box position apprizing and route tracking system Download PDFInfo
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- CN103950545B CN103950545B CN201410133960.5A CN201410133960A CN103950545B CN 103950545 B CN103950545 B CN 103950545B CN 201410133960 A CN201410133960 A CN 201410133960A CN 103950545 B CN103950545 B CN 103950545B
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Abstract
The invention discloses an airplane black box position apprizing and route tracking system, which comprises a main black box for the existing airplane, and a shell of the main black box is internally provided with a flight recorder, a voice recorder and a storage system for storing the recorders. The airplane black box position apprizing and route tracking system is characterized by also comprising a Beidou transmission device and an auxiliary black box which are arranged in a passenger compartment, wherein the auxiliary black box is internally provided with Beidou satellite transmission equipment which can be monitored and tracked by an air traffic control center in real time, as well as a backup device connected with the storage system in the main black box. The airplane black box position apprizing and route tracking system is mature in technology, can be realized by adopting an existing technology and plays a significant role in monitoring the navigation safety of airplanes.
Description
Technical field
The present invention designs aircraft navigation alignment system, specifically, relates to a kind of aircraft black box position reporting and system is followed the tracks of in course line.
Background technology
Black box formal name used at school is " flight recorder " (Flight Recorder).The flight recorder that on passenger plane, black box is installed has 2, and one is aeroplane data recorder (FDR), be responsible for the record-setting flight time, speed, highly, the data such as the aircraft rudder surface degree of bias, engine speed；Another is cockpit voice recorder (CVR), is responsible on logging machine the call with ground on the dialogue of aircrew, machine, and the various sound in cabin.Black box is the firmest, is resistant to fiercely impact and high temperature hot flame during air crash.
Radio transmission apparatus is not had, the luminous zone by land if air crash, on the bright shell of simply its salmon pink that black box prompting people note and shell on black box.
Black box uniquely can externally send the parts of signal and be called subsea beacon (ULB), and subsea beacon starts after meeting water, and a per second secondary frequencies is the acoustic signals (attention is acoustic signals) of 37.5KHz, sustainable work 30 days.
The acoustic signals that black box sends under water can only be detected in water by sonar, but owing to the subsea beacon volume of black box is little, power is the least, generally, shipboard sonar maximum about can receive the black box acoustic signals within several kilometer range, and the effective scope of detection of small handheld sonar then only has hundreds of meters.Investigative range less than several kilometers is relative to boundless sea, strong the most not how many than " looking for a needle in a haystack ".
In existing black box, the flying quality of record, has more than 700 flying quality, uninterrupted recording during flight.Data volume is the least, and engineering all can periodically be taken CD to go on aircraft and download.Also have cockpit voice recording, originally only record 30 minutes, it can be understood as a continual satellite phone adds real-time recording if present real time record.This cost performance is the highest, and cost is too big, and this expense can not improve safety.Transmit this kind of data also likely require anti-interference by force, strong security, this technology satellite to be used, if out of question if military, if involving civilian, or problem short of money.Additionally relating to pilot's right of privacy, real time communication, all of dialogue the most inside, ground can be monitored at any time, it is possible to can invade pilot's privacy.
Additionally, " horse boat event " is learnt, existing aircraft tracking performance is poor, and black box is difficult to found, and this is accomplished by utilizing autonomous Big Dipper technology to solve the problems referred to above.
Summary of the invention
The present invention is directed to black box present in existing aircraft to sink under water with accident aircraft, be difficult to found, course line and be difficult to tracked defect, it is provided that system is followed the tracks of to solve the problems referred to above in a kind of aircraft black box position reporting and course line.
The solution of the present invention is by being achieved in that: system is followed the tracks of in a kind of aircraft black box position reporting of structure and course line, including the main black box of existing machine, flight recorder and voice recording instrument it is provided with in main black box housing, and store the stocking system of above-mentioned monitor, also include Big Dipper transmitting device and the pair black box being arranged in cabin, be provided with, in described secondary black box, the big-dipper satellite signalling device that tracking can be monitored by air traffic control centre in real time
, and the back-up device being connected with stocking system in main black box；
It is additionally provided with stand-by power supply in described secondary black box；
Described secondary black box is arranged on ejectable and goes out the position of airframe, it is provided with catapult-launching gear bottom described secondary black box, with accident, described catapult-launching gear judges that sensor is connected, after accident judges sensor-triggered, catapult-launching gear starts and can be ejected outside body by secondary black box；
Described secondary black box is provided with air bag, and when can floating on the water surface by fully wrapped around for secondary black box after airbag inflation, described airbag inflation is triggered by catapult-launching gear.
The general plotting of the present invention is: set up a Big Dipper transmitting device the most aboard, thus when aircraft is at normal flight, the Big Dipper can be the positional information that blank pipe mechanism offer aircraft is real-time；Additionally, on the basis of original main black box, set up a secondary black box that can share and store main black box information, when unusual condition occurs in aircraft, accident judges that sensor sensing judges when aircraft is in abnormal condition, then start catapult-launching gear, pair black box is ejected outside airframe, now, after air bag in secondary black box is launched out, automatic inflating can be realized so that when black box is just in case falling on the water surface, can be the most floating.Meanwhile, the Big Dipper utilizes the big-dipper satellite signalling device in secondary black box to position, thus obtains the location information of secondary black box.
In the present invention, the above accident judges that sensor includes acceleration induction module, vibration induction module, highly induction module and sea water induction module.Above-mentioned module may determine that aircraft acceleration, vibration, residing height whether exception or is in air crash state, it addition, sea water induction module can sense whether touches sea water.Above-mentioned module, all can use existing technology to realize.
In the present invention, as further improving, described Big Dipper signalling device includes BeiDou-I satellite alignment system.By number alignment system of the Big Dipper in a device, it is simple to locking aircraft accident position rapidly, in order to rapid deployment is searched and rescued.
In the present invention, as improving further, described Big Dipper signalling device includes BeiDou-I satellite alignment system, the Big Dipper/GPS dual-mode alignment system, radio signals discharger and communication control unit.By number alignment system of the Big Dipper in a device, it is simple to locking aircraft accident position rapidly, in order to rapid deployment is searched and rescued；And the Big Dipper/GPS dual-mode alignment system can pass through radio signals discharger, transmit signals to the rescue worker of periphery；Communication control unit can control the Big Dipper one and radio station transmitting time interval, avoid the two electromagnetic interference, blank pipe department can also be made by part critical data in the secondary black box of communication controler reading, it is sent directly to air traffic control centre by big-dipper satellite, air crash is easy to higher level and quickly works out rescue plan.
In the present invention, preferably, power launched by described radio signals discharger is 400-600mW.
Have prominent actual features and the marked improvement of the present invention be:
1. the present invention can effectively follow the trail of airplane information by arranging Big Dipper transmitting device, thus avoids aircraft to occur and situation about being lost contact by blank pipe mechanism at the normal Intermediate Course that travels.
2. in the present invention, the addition pair black box of novelty, so that secondary black box is when running into emergency situations, can eject cabin the very first time, thus avoid valuable information destroyed.
3. it addition, secondary black box have employed autoprotection device, by arranging air bag so that it can be floating when falling into the water surface, it is to avoid falls into seabed and cannot be searched.
4. the technology of the present invention is ripe, existing technology can be used to realize, and aircraft navigation security monitoring is had great effect.
Accompanying drawing explanation
Fig. 1 is the structural representation of the embodiment of the present invention 1；
Fig. 2 is the structural representation of the embodiment of the present invention 2.
Detailed description of the invention
Describing the present invention below in conjunction with drawings and Examples, following example explain with invention optimal effectiveness.
Embodiment 1:
As shown in Figure 1, system is followed the tracks of in this aircraft black box position reporting and course line, including the main black box of existing machine, flight recorder and voice recording instrument it is provided with in main black box housing, and storing the stocking system of above-mentioned monitor, above equipment is all identical with existing black box equipment, also includes the Big Dipper transmitting device being arranged in cabin in this system, this device can be connected with big-dipper satellite, so that blank pipe mechanism can understand aircraft navigation position in real time；In addition, this system also includes secondary black box, it is provided with, in secondary black box, the Big Dipper signalling device that tracking can be monitored by air traffic control centre in real time, this equipment is provided with BeiDou-I satellite alignment system, being provided with, in secondary black box, the back-up device being connected with stocking system in main black box, its connected mode can use wireless communication technology to realize, such as, the existing communication modes such as bluetooth realize, and are additionally provided with stand-by power supply in secondary black box.
Secondary black box is arranged on ejectable and goes out the position of airframe, such as, cabin afterbody or side locations, being provided with catapult-launching gear bottom secondary black box, this catapult-launching gear can take various forms, such as, conventional chemical explosion formula catapult-launching gear, or mechanical ejection device all can realize；With accident, catapult-launching gear judges that sensor is connected, after accident judges sensor-triggered, catapult-launching gear starts and can be ejected outside body by secondary black box；This accident judges that sensor includes acceleration induction module, vibration induction module, highly induction module and sea water induction module, above-mentioned induction module, in existing technology the most on the books, and sea water induction module, function can be realized by sea water electric conductivity, from prior art, we learn, logical conventional sign σ in sea electrical conductivity of water (inverse of resistivity) represents, typically at 3-5 Europe/rice.During temperature 17 DEG C, the electrical conductivity of Copenhagen water is 4.54-4.81 Europe/rice, is 10-7 times of copper, 1012 times of glass.Lake water that the Conductivity Ratio of sea water is general, more than big thousand times of river, therefore can constantly detect self-conductive rate by above-mentioned concept by sea water induction module, make it possible to generation when running into sea water, send the function of induced signal.In secondary black box, it is additionally provided with air bag, when can be by fully wrapped around for secondary black box after airbag inflation, described airbag inflation is triggered by catapult-launching gear, such as, if this airbag inflation can be by chemistry catapult-launching gear, realize, when chemistry ejection mechanism blast sends impulse force, chemical gas can be filled with air bag so that airbag inflation；And the airing form of other similar automotive airbags, it is also possible to use in the present invention.
Embodiment 2:
As in figure 2 it is shown, difference from Example 1 is, the Big Dipper signalling device in secondary black box includes BeiDou-I satellite alignment system, the Big Dipper/GPS dual-mode alignment system, radio signals discharger and communication control unit.Power launched by radio signals discharger is 400-600mW, it is preferably 500mW, communication control unit can control the Big Dipper one and radio station transmitting time interval, avoid the two electromagnetic interference, blank pipe department can also be made by part critical data in the secondary black box of communication controler reading, it is sent directly to air traffic control centre by big-dipper satellite, in air crash, it is easy to higher level quickly works out rescue plan, this communication control unit is general control structure, all can realize with the above-mentioned interval function of straight line and information read functions, belong to existing technology.
Although in the above-described embodiments, concrete technology for some electronics or induction module is not described in detail, but, the utilization of these building block techniques can realize, and the process that the present invention mainly realizes mainly is arranged by the Nomenclature Composition and Structure of Complexes of this technology, it is therefore not necessary to repeat the technology of some maturations at this.
Last it is noted that obviously, above-described embodiment is only used to example of the present invention is clearly described, and not to the restriction implemented.For the those of ordinary skill in described field, can also make other changes in different forms on the basis of the above description.Here without also cannot be to all of embodiment party's formula with exhaustive.And the obvious change thus amplified out or variation still in protection scope of the present invention among.
Claims (4)
1. a system is followed the tracks of, including the main black box of existing machine, in main black box housing in aircraft black box position reporting and course line
It is provided with flight recorder and voice recording instrument, and stores above-mentioned flight recorder and the storage system of voice recording instrument internal data
System, it is characterised in that: also including Big Dipper transmitting device and the pair black box being arranged in cabin, being provided with in described secondary black box can
To be monitored the big-dipper satellite signalling device of tracking in real time by air traffic control centre, and the backup being connected with stocking system in main black box
Device；
It is additionally provided with stand-by power supply in described secondary black box；
Described secondary black box is arranged on ejectable and goes out the position of airframe, is provided with catapult-launching gear bottom described secondary black box, described
With accident, catapult-launching gear judges that sensor is connected, after accident judges sensor-triggered, catapult-launching gear startup can be by secondary black box bullet
Ejaculator is external；
Described secondary black box is provided with air bag, when can floating on the water surface by fully wrapped around for secondary black box after airbag inflation, described
Airbag inflation is triggered by catapult-launching gear,
Described accident judges that sensor includes acceleration induction module, vibration induction module, highly induction module and sea water sensing mould
Block.
2. follow the tracks of system according to the aircraft black box position reporting described in claim 1 and course line, it is characterised in that: the described Big Dipper
Signalling device includes BeiDou-I satellite alignment system.
3. follow the tracks of system according to the aircraft black box position reporting described in claim 1 and course line, it is characterised in that: the described Big Dipper
Signalling device includes BeiDou-I satellite alignment system, the Big Dipper/GPS dual-mode alignment system, radio signals discharger and the control that communicates
Device processed.
4. follow the tracks of system according to the aircraft black box position reporting described in claim 3 and course line, it is characterised in that: described radio station is believed
Power launched by number discharger is 400-600mW.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410133960.5A CN103950545B (en) | 2014-04-01 | 2014-04-01 | Airplane black box position apprizing and route tracking system |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201410133960.5A CN103950545B (en) | 2014-04-01 | 2014-04-01 | Airplane black box position apprizing and route tracking system |
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| Publication Number | Publication Date |
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| CN103950545A CN103950545A (en) | 2014-07-30 |
| CN103950545B true CN103950545B (en) | 2017-01-11 |
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| CN201410133960.5A Expired - Fee Related CN103950545B (en) | 2014-04-01 | 2014-04-01 | Airplane black box position apprizing and route tracking system |
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Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105139480A (en) * | 2015-08-10 | 2015-12-09 | 昆明五威科工贸有限公司 | Positioning method of black box system |
| CN105253306A (en) * | 2015-11-09 | 2016-01-20 | 杨珊珊 | UAV (Unmanned aerial vehicle) provided with falling guard device and falling guard method thereof |
| RU2630272C2 (en) * | 2015-12-30 | 2017-09-06 | Виктор Иванович Дикарев | System for determining location of crashed aircraft |
| WO2018041253A1 (en) * | 2016-09-01 | 2018-03-08 | 梁泰然 | Black box control method and system |
| CN106842180B (en) * | 2017-01-19 | 2018-02-02 | 王惟滨 | A kind of overboard aircraft black box search and rescue system based on GPS information carrier wave |
| CN111806704B (en) * | 2020-07-23 | 2021-10-12 | 南京航空航天大学 | A helicopter air-separated emergency flight data recording system |
| CN116482723A (en) * | 2023-06-25 | 2023-07-25 | 成都星历科技有限公司 | Multipurpose beacon module |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6009356A (en) * | 1996-10-11 | 1999-12-28 | Raytheon Ti Systems | Wireless transducer data capture and retrieval system for aircraft |
| CN101817403A (en) * | 2009-06-30 | 2010-09-01 | 廖大中 | Floatable black box with emergency gas bag |
| CN201703564U (en) * | 2010-02-01 | 2011-01-12 | 上海东方久乐汽车安全气囊有限公司 | Black box protector |
| CN102360220A (en) * | 2011-05-31 | 2012-02-22 | 江汉大学 | Device and method for searching aviation recorder on seabed |
| CN204197305U (en) * | 2014-04-01 | 2015-03-11 | 柳州治业科技有限公司 | Aircraft black box position reporting and course line track channel |
-
2014
- 2014-04-01 CN CN201410133960.5A patent/CN103950545B/en not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6009356A (en) * | 1996-10-11 | 1999-12-28 | Raytheon Ti Systems | Wireless transducer data capture and retrieval system for aircraft |
| CN101817403A (en) * | 2009-06-30 | 2010-09-01 | 廖大中 | Floatable black box with emergency gas bag |
| CN201703564U (en) * | 2010-02-01 | 2011-01-12 | 上海东方久乐汽车安全气囊有限公司 | Black box protector |
| CN102360220A (en) * | 2011-05-31 | 2012-02-22 | 江汉大学 | Device and method for searching aviation recorder on seabed |
| CN204197305U (en) * | 2014-04-01 | 2015-03-11 | 柳州治业科技有限公司 | Aircraft black box position reporting and course line track channel |
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| CN103950545A (en) | 2014-07-30 |
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