CN106143929A - A kind of throwing is put formula black box and is launched control method, system and airborne vehicle - Google Patents
A kind of throwing is put formula black box and is launched control method, system and airborne vehicle Download PDFInfo
- Publication number
- CN106143929A CN106143929A CN201610744646.XA CN201610744646A CN106143929A CN 106143929 A CN106143929 A CN 106143929A CN 201610744646 A CN201610744646 A CN 201610744646A CN 106143929 A CN106143929 A CN 106143929A
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- Prior art keywords
- black box
- throwing
- aircraft
- accident signal
- aviation
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- 238000000034 method Methods 0.000 title claims abstract description 15
- 230000006698 induction Effects 0.000 claims description 5
- 230000002159 abnormal effect Effects 0.000 abstract description 3
- 239000000463 material Substances 0.000 description 2
- 230000001133 acceleration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 230000007274 generation of a signal involved in cell-cell signaling Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 239000003208 petroleum Substances 0.000 description 1
- 239000013535 sea water Substances 0.000 description 1
- 206010042772 syncope Diseases 0.000 description 1
- 238000002604 ultrasonography Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 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
- 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
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
-
- 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
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D2045/0065—Black boxes, devices automatically broadcasting distress signals
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The present invention relates to aviation field, put formula black box particularly to one throwing and launch control method, system and airborne vehicle.Method comprises the following steps: generate aviation accident signal；The instrumental panel of aircraft shows aviation accident signal；If aviation accident signal is not cancelled in Preset Time, then automatically formula black box is put in throwing and launch away from aircraft.The present invention can be when detecting that aircraft travels abnormal possible accident, produce aviation accident signal and driver is proposed warning, if it is normal that driver judges that aircraft travels, manually release described aviation accident signal, if described aviation accident signal is not released from Preset Time, illustrate that aircraft will have an accident, the most in advance black box is ejected from aircraft, conveniently black box is searched.
Description
Technical field
The present invention relates to aviation field, put formula black box particularly to one throwing and launch control method, system and airborne vehicle.
Background technology
Black box, is one of special electronic recording equipment of aircraft, and aircraft each machinery position and electronic instrument are all
Being attached thereto equipped with sensor, it can quit work aircraft or have an accident the flying of halfhour voice dialogue and two hours before crashing
Line height, speed, course, the climb rate, rate of descent, acceleration situation and aircraft system working condition and engine operating parameter etc.
Flight parameter is all recorded, and is used for flight experiment, accident analysis.But once aviation accident, especially aircraft is at the water surface
Or midair disintegration, when black box sinks to deep-sea, the search to black box is extremely difficult, because what black box carried
Underwater Navigation beacon the degree of depth of about 6000 meters can only send ultrasound wave, ultrasonic in the range of distance beacon 1800～3600 meters
Ripple can be detected by instrument, simultaneously the state of sea water, ship, marine animal, petroleum pipeline and other factors of surrounding
The ambient noise caused all can affect the detected scope of beacon.The most currently designed go out a kind of throwing put formula black box, pass through
Catapult-launching gear is set bottom black box, when determining aircraft and being overboard, black box can be launched away, make black box float over
On sea, conveniently black box is searched.But it is in the case of disintegrating after aircraft the most aloft disintegrates but be overboard, black
Case is together with substantial amounts of the wreckage of an plane, and catapult-launching gear is difficult to make black box depart from the wreckage of an plane, is the most still difficult to search.
Summary of the invention
The invention provides a kind of throwing to put formula black box and launch control method, system and airborne vehicle, solve the above
Technical problem.
The technical scheme is that
According to one aspect of the present invention, it is provided that a kind of throwing is put formula black box and launched control method, comprises the following steps:
Step 1, generates aviation accident signal；
Step 2, shows described aviation accident signal on the instrumental panel of aircraft；
Step 3, if described aviation accident signal is not cancelled in Preset Time, then automatically throwing is put formula black box from
Launch away on aircraft.
According to another aspect of the present invention, it is provided that a kind of throwing is put formula black box and launched control system, including accident letter
Number generation module, display module, judge module and control module,
Described accident signal generator module is used for generating aviation accident signal；
Described display module is for showing described aviation accident signal on the instrumental panel of aircraft；
Described judge module is for judging whether described aviation accident signal is cancelled in Preset Time；
Throwing, for when aviation accident signal described in Preset Time is not cancelled, is put by described control module automatically
Formula black box launches away from aircraft.
In order to solve the technical problem of the present invention, additionally provide a kind of airborne vehicle, put formula black box bullet including described throwing
Penetrate control system.
The invention has the beneficial effects as follows: the invention provides a kind of formula black box of throwing being put and eject the side of wrecked aircraft
Method, system and airborne vehicle, when detecting that aircraft travels abnormal possible accident, produce aviation accident signal and also carry driver
Go out warning, if driver judges that aircraft travels normally, manually release described aviation accident signal, if described in Preset Time
Aviation accident signal is not released from, and illustrates that aircraft will have an accident, is ejected by black box the most in advance from aircraft, convenient to black box
Son is searched.
Accompanying drawing explanation
Fig. 1 is that embodiment 1 is thrown and put formula black box and launch the schematic flow sheet of control method；
Fig. 2 is that embodiment 2 is thrown and put formula black box and launch the structural representation of control system；
Fig. 3 is the structural representation of embodiment 3 airborne vehicle.
Detailed description of the invention
Being described principle and the feature of the present invention below in conjunction with accompanying drawing, example is served only for explaining the present invention, and
Non-for limiting the scope of the present invention.
As it is shown in figure 1, put formula black box for embodiment 1 throwing to launch the schematic flow sheet of control method, comprise the following steps:
Step 1, generates aviation accident signal；
Step 2, shows described aviation accident signal on the instrumental panel of aircraft；
Step 3, if described aviation accident signal is not cancelled in Preset Time, then automatically throwing is put formula black box from
Launching away on aircraft, in the present embodiment, described Preset Time is 1～5 minute.
In the present embodiment, generate aviation accident signal, employing sound according to flight speed, flying height and/or flight attitude
Light type of alarm shows described aviation accident signal on the instrumental panel of aircraft.The present embodiment is by air speed, flight height
The factors such as degree and flight attitude consider, it is judged that whether aircraft will have an accident, and produces aviation accident signal to driving
Member sounds a warning, if driver's judgement is to detect wrong and aircraft travels normal, then manually releases described aviation accident signal,
If described aviation accident signal is not released from Preset Time, illustrating that aircraft will have an accident, driver is likely not to have the time
Or having no ability to release aviation accident signal because fainting, both can avoid launching the situation of error, again can be in advance by black
Case ejects from aircraft, so that black box departs from the wreckage of an plane, conveniently searches black box.
As in figure 2 it is shown, put formula black box for embodiment 2 throwing to launch the structural representation of control system, including accident signal
Generation module, display module, judge module and control module,
Described accident signal generator module is used for generating aviation accident signal；
Described display module is for showing described aviation accident signal on the instrumental panel of aircraft；
Described judge module is for judging whether described aviation accident signal is cancelled in Preset Time；
Throwing, for when aviation accident signal described in Preset Time is not cancelled, is put by described control module automatically
Formula black box launches away from aircraft.
In the present embodiment, described accident signal generator module connection accident judges that sensor, described accident judge sensor
Including flight speed induction module, flying height induction module and/or flight attitude induction module, thus by aircraft speed
The factors such as degree, flying height and flight attitude consider, it is judged that whether aircraft will have an accident.
In the present embodiment, described throwing is put formula black box and is arranged on ejectable and goes out the position of airframe, and it is black that formula is put in described throwing
It is provided with for described throwing being put the catapult-launching gear that formula black box ejects from aircraft bottom case, described catapult-launching gear and described control
Molding block is connected, thus conveniently described black box is ejected aircraft in due course.
As it is shown on figure 3, be the structural representation of embodiment 3 airborne vehicle, put formula black box including above-described throwing and launch
Control system.
The invention provides a kind of formula black box of throwing being put and eject the method for wrecked aircraft, system and airborne vehicle, work as inspection
When measuring the abnormal possible accident of aircraft traveling, produce aviation accident signal and also driver is proposed warning, if driver's judgement
Aircraft travels the normal then described aviation accident signal of manual releasing, if described aviation accident signal is not solved in Preset Time
Remove, illustrate that aircraft will have an accident, the most in advance black box is ejected from aircraft, conveniently black box is searched.
In describing the invention, it is to be understood that term " first ", " second " are only used for describing purpose, and can not
It is interpreted as instruction or hint relative importance or the implicit quantity indicating indicated technical characteristic.Thus, define " the
One ", the feature of " second " can express or implicitly include at least one this feature.In describing the invention, " multiple "
It is meant that at least two, such as two, three etc., unless otherwise expressly limited specifically.
In the description of this specification, reference term " embodiment ", " some embodiments ", " example ", " specifically show
Example " or the description of " some examples " etc. means to combine this embodiment or example describes specific features, structure, material or spy
Point is contained at least one embodiment or the example of the present invention.In this manual, to the schematic representation of above-mentioned term not
Identical embodiment or example must be directed to.And, the specific features of description, structure, material or feature can be in office
One or more embodiments or example combine in an appropriate manner.Additionally, in the case of the most conflicting, the skill of this area
The feature of the different embodiments described in this specification or example and different embodiment or example can be tied by art personnel
Close and combination.
Although above it has been shown and described that embodiments of the invention, it is to be understood that above-described embodiment is example
Property, it is impossible to being interpreted as limitation of the present invention, those of ordinary skill in the art within the scope of the invention can be to above-mentioned
Embodiment is changed, revises, replaces and modification.
Claims (8)
1. a throwing is put formula black box and is launched control method, it is characterised in that comprise the following steps:
Step 1, generates aviation accident signal；
Step 2, shows described aviation accident signal on the instrumental panel of aircraft；
Step 3, if described aviation accident signal is not cancelled in Preset Time, then puts formula black box from aircraft by throwing automatically
On launch away.
Throwing the most according to claim 1 is put formula black box and is launched control method, it is characterised in that step 2, uses acousto-optic report
Police's formula shows described aviation accident signal on the instrumental panel of aircraft.
Throwing the most according to claim 1 is put formula black box and is launched control method, it is characterised in that described Preset Time is 1
～5 minutes.
4. put formula black box according to the arbitrary described throwing of claims 1 to 3 and launch control method, it is characterised in that in step 1,
Aviation accident signal is generated according to flight speed, flying height and/or flight attitude.
5. a throwing is put formula black box and is launched control system, it is characterised in that the signal generator module that includes having an accident, display module,
Judge module and control module,
Described accident signal generator module is used for generating aviation accident signal；
Described display module is for showing described aviation accident signal on the instrumental panel of aircraft；
Described judge module is for judging whether described aviation accident signal is cancelled in Preset Time；
Throwing, for when aviation accident signal described in Preset Time is not cancelled, is put formula black by described control module automatically
Case launches away from aircraft.
Throwing the most according to claim 5 is put formula black box and is launched control system, it is characterised in that described accident signal produces
Module connection accident judges that sensor, described accident judge that sensor includes that flight speed induction module, flying height sense mould
Block and/or flight attitude induction module.
7. put formula black box according to the throwing described in claim 5 or 6 and launch control system, it is characterised in that it is black that formula is put in described throwing
Case is arranged on ejectable and goes out the position of airframe, and described throwing is put and is provided with bottom formula black box for described throwing is put formula black box
The catapult-launching gear that son ejects from aircraft, described catapult-launching gear is connected with described control module.
8. an airborne vehicle, it is characterised in that include that the arbitrary described throwing of claim 5～7 is put formula black box and launched control system
System.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610744646.XA CN106143929A (en) | 2016-08-28 | 2016-08-28 | A kind of throwing is put formula black box and is launched control method, system and airborne vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610744646.XA CN106143929A (en) | 2016-08-28 | 2016-08-28 | A kind of throwing is put formula black box and is launched control method, system and airborne vehicle |
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| Publication Number | Publication Date |
|---|---|
| CN106143929A true CN106143929A (en) | 2016-11-23 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610744646.XA Pending CN106143929A (en) | 2016-08-28 | 2016-08-28 | A kind of throwing is put formula black box and is launched control method, system and airborne vehicle |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107948963A (en) * | 2017-11-17 | 2018-04-20 | 广州杰赛科技股份有限公司 | Aircraft emergency communication apparatus and method |
| CN111498113A (en) * | 2020-05-06 | 2020-08-07 | 中国商用飞机有限责任公司 | Jettisoning type flight recorder system and control method |
| CN111907707A (en) * | 2020-06-15 | 2020-11-10 | 哈尔滨工业大学 | Electromagnetic drive's black box throwing machine constructs |
| CN112874795A (en) * | 2021-01-21 | 2021-06-01 | 北京京东乾石科技有限公司 | Throwing device, unmanned aerial vehicle, control method, control device and storage medium |
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| CN2601938Y (en) * | 2002-10-15 | 2004-02-04 | 宝鸡市公安局交通警察支队 | Black box for defence |
| CN1600642A (en) * | 2003-09-24 | 2005-03-30 | 高忠民 | Method for saving oneself of aircraft and all occupants in air accident, |
| CN201566840U (en) * | 2009-12-30 | 2010-09-01 | 陕西飞机工业（集团）有限公司 | Aircraft alarm signal integrating and alarming device |
| CN103065372A (en) * | 2012-12-07 | 2013-04-24 | 陕西千山航空电子有限责任公司 | Aviation recorder and automatic positioning method |
| CN103209895A (en) * | 2010-06-08 | 2013-07-17 | 佩尼贾尔斯航空航天有限公司 | Flight recorder |
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| DE102014005878A1 (en) * | 2014-04-16 | 2015-10-22 | Hans-Joachim Lange | Device for finding a black box |
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- 2016-08-28 CN CN201610744646.XA patent/CN106143929A/en active Pending
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|---|---|---|---|---|
| CN2601938Y (en) * | 2002-10-15 | 2004-02-04 | 宝鸡市公安局交通警察支队 | Black box for defence |
| CN1600642A (en) * | 2003-09-24 | 2005-03-30 | 高忠民 | Method for saving oneself of aircraft and all occupants in air accident, |
| CN201566840U (en) * | 2009-12-30 | 2010-09-01 | 陕西飞机工业（集团）有限公司 | Aircraft alarm signal integrating and alarming device |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107948963A (en) * | 2017-11-17 | 2018-04-20 | 广州杰赛科技股份有限公司 | Aircraft emergency communication apparatus and method |
| CN111498113A (en) * | 2020-05-06 | 2020-08-07 | 中国商用飞机有限责任公司 | Jettisoning type flight recorder system and control method |
| CN111907707A (en) * | 2020-06-15 | 2020-11-10 | 哈尔滨工业大学 | Electromagnetic drive's black box throwing machine constructs |
| CN111907707B (en) * | 2020-06-15 | 2021-09-07 | 哈尔滨工业大学 | Electromagnetic drive's black box throwing machine constructs |
| CN112874795A (en) * | 2021-01-21 | 2021-06-01 | 北京京东乾石科技有限公司 | Throwing device, unmanned aerial vehicle, control method, control device and storage medium |
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Application publication date: 20161123 |