CN106965947A - Aircraft fall into the sea positioning signal show system - Google Patents
Aircraft fall into the sea positioning signal show system Download PDFInfo
- Publication number
- CN106965947A CN106965947A CN201610021330.8A CN201610021330A CN106965947A CN 106965947 A CN106965947 A CN 106965947A CN 201610021330 A CN201610021330 A CN 201610021330A CN 106965947 A CN106965947 A CN 106965947A
- Authority
- CN
- China
- Prior art keywords
- aircraft
- sea
- water
- door
- positioning signal
- 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
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 26
- 239000000843 powder Substances 0.000 claims abstract description 20
- 238000006243 chemical reaction Methods 0.000 claims abstract description 11
- 239000000443 aerosol Substances 0.000 claims abstract description 4
- 230000008961 swelling Effects 0.000 claims description 4
- 230000009977 dual effect Effects 0.000 claims description 2
- 230000005484 gravity Effects 0.000 claims description 2
- 238000007667 floating Methods 0.000 abstract description 8
- 238000005516 engineering process Methods 0.000 abstract description 3
- 210000000056 organ Anatomy 0.000 abstract description 3
- 230000005540 biological transmission Effects 0.000 abstract description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 28
- 229910052742 iron Inorganic materials 0.000 description 14
- 239000013535 sea water Substances 0.000 description 5
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 4
- 239000004020 conductor Substances 0.000 description 4
- 229910052802 copper Inorganic materials 0.000 description 4
- 239000010949 copper Substances 0.000 description 4
- 230000005611 electricity Effects 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 230000002633 protecting effect Effects 0.000 description 3
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 2
- 229910052744 lithium Inorganic materials 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 241001074085 Scophthalmus aquosus Species 0.000 description 1
- 238000005842 biochemical reaction Methods 0.000 description 1
- 230000000368 destabilizing effect Effects 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 239000002984 plastic foam Substances 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 238000007665 sagging Methods 0.000 description 1
- 238000005303 weighing 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
- B64D47/00—Equipment not otherwise provided for
- B64D47/02—Arrangements or adaptations of signal or lighting devices
- B64D47/06—Arrangements or adaptations of signal or lighting devices for indicating aircraft presence
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
Abstract
Aircraft fall into the sea positioning signal show system major function, be after being hit the drink for aircraft in a flash, the full-automatic accurate location opened in time when positioning overboard, " floating object " Zhong Nei departments and organs automatically turn on sends and receives signal to satellite, gives people searching and falls into the sea aircraft there is provided accurate location.When aircraft falls into the sea in a flash, this technology does the principle of transmission power lead using water, is directed at storehouse interior power open circuit, promotes " machine-operated in storehouse " interlocking linkage reaction.This technology meets the chemical reaction for becoming aerosol after water-soluble conjunction using dry powder, automatic " stingy " move " trigger " after " in storehouse machine-operated " proportion is unbalance, and the aircraft positioning signal display system that falls into the sea is launched into export, the water surface is swum in, the overboard accurate location of aircraft is shown to satellite in time, signal is simultaneously emitted by.
Description
Technical field
Aircraft fall into the sea positioning signal show system be installed in tail appropriate location, beIt is independentOffice, the not commander by pilot and manipulation.Simply " seat " aircraft and performs task.When aircraft falls into the sea in a flash, power lead is done using seawater, it is directed at the open circuit of " storehouse " interior power, electric power disconnection is directed at electromagnet and loses suction, after the spring lock of left and right door is opened, after pressure door in seawater is opened, after being intake in warehouse, fused with the dry powder that is placed in storehouse, dry powder meets the biochemical reaction of aquatic products and becomes in aerosol, storehouse office because interlocking linkage reaction occurs for weightlessness by object, positioning signal is shown into system ejection export, seawater face is floated on, signal, accurate location when display aircraft falls into the sea is sent to satellite in time.
Background technology
Using Malaysian lost contact flight AM370 passenger planes on March 18th, 2013 as background, chemically reactive thing is Technical Reference after falling into the sea chance water using aircraft, it is also contemplated that by being placed in aircraft, should possess pollution-free, free from extraneous odour article of fine qualities, it is secondary Alarm finally to select dry powder.The built-in dry powder thing of dry powder-fire extinguisher, hangs upside down fire extinguisher during fire extinguishing, deposited in dry powder and fire extinguisher it is water-soluble close chemical reaction, the unbalance principle of aerosol is become by object.Once alarm is to be installed in positive and negative electrode power supply before and after tail outer periphery (upside of this contact point of power source 1/2 is by dress protective cover), when aircraft falls into the sea into water in a flash, front and rear positive and negative power supply makees wire with water, electric power disconnection, door spring lock tapered end loses electromagnetic force unlocking, the power-assisted sunk by heavy iron (heavy iron sinks like people with pulling power), substantial amounts of water is poured in after door is opened by hydraulic pressure again, meet dry powder fused rear weightless, automatic " stingy " trigger action of office's interlocking linkage in storehouse, will《Aircraft fall into the sea positioning signal show system》Launch export.The water surface is swum in, to satellite display location signal.
The content of the invention
The aircraft positioning signal that falls into the sea shows that the problem of system is most basic allows for aircraft and fallen into the water in a flash, and water runs into the problem of what thing could play interlocking linkage weightless reaction.One, which allows for electricity, meets after water, and water can play electric action.Two be that the one kilogram of dry powder filled inside dry powder extinguisher when recalling fire extinguishing, fire extinguisher is met after water-soluble conjunction, and carves generation chemical reaction, weightless by thing change gas.It is main body by electricity and dry powder, it is conductive using water when aircraft falls into the water in a flash, promote storehouse interior power open circuit,《Aircraft fall into the sea positioning signal show system》Door lock lose power supply, be equal to lose electromagnetic attraction, storehouse door-lock opening, by the pressure of seawater, dry powder, which is met, after door is opened, in swelling warehouse entry produces chemical reaction after water-soluble conjunction, weightless by thing change gas, office is unbalance in storehouse, drives interlocking linkage to start trigger, will《Aircraft fall into the sea positioning signal show system》Export is launched, the water surface is swum in, sends the particular location signal that aircraft has fallen into the water to satellite in time.To be on the safe side, electricity meets water after water and does power conductor, electric power disconnection is opened after door, if in being put in storage without substantial amounts of swelling, meeting dry powder and fusing, positioning signal shows that system will not launch export.The present invention, which considers to meet, rains, avenges wet weather, and positioning signal shows the dual fail-safe of system destabilizing factor.
Embodiment
1st, aircraft fall into the sea positioning signal show system be a body structure, collectively referred to as " storehouse ".Warehouse traverse is installed in appropriate location inside tail, is fixed according to the fixed mount span inside tail.The long 2400mm in storehouse, width 2300mm, high 900mm, storehouse plate thickness 10mm, (tentative need firmly light material).(the built-in lithium battery of warehouse fixes tentatively mono- group of direct current 36V)
2nd, channel-section steel (long 2400mm, width 60mm, high 1300mm) is separately fixed at warehouse upper face two ends, recess correspondence wide vertical with storehouse.For protecting " floating object " body (being that built-in positioning signal shows system).Triangle launching cradle (1600mm, each long 900mm in upper both sides, high 30mm are put centered on warehouse face 1/2.Launching cradle tip hangs 100 kilograms of extension springs (tentative), extension spring stroke 1000mm, the launching cradle bottom long 1600mm of dress angle bar, width 130mm × 130mm, thickness 5mm
3rd, the centre drill away from left part 300mm 1/2 at the top of warehouse-rectangular skylight (long 41mm, width 21mm) this skylight is to place ejection control trigger, the thickness of trigger is 40mm × 20mm) this skylight be place ejection control trigger, the thickness of trigger is the equilateral right angles of the high 30mm of 40mm × 20mm.
4th, aircraft fall into the sea positioning signal show system be made up of 3 parts：(1) warehouse office, (2) afterbody office, (3) aircraft positioning signal that falls into the sea of automatically opening the door show that system referred to as " floating object " Wai Nei departments and organs are set.
(1) warehouse office：The hard material of plate face is fixed in following part by dress width 200mm, high 800mm thickness 10mm on the outside of from skylight, away from skylight central right bottom dress width 200mm, high 800mm, thickness 10mm fixed plate facestock matter, away from one diametric hole of brill (41mm) at skylight central right bottom 200mm, place long 860mm, diameter 40mm rotating shafts, with respect to part 800mm by filling high 900mm supports and silo roof interior contact and fixation.A bore dia 16mm is bored at 1/2430mm away from rotating shaft overall length, long 600mm diameters 15mm drive links are placed, 1/2 does oblique drive link, and 1/2 does oblique drive link, drive link top fills the circle roller of a long 600mm diameters 105mm, iron ball tentative 5 kilograms the inside dress diameter 100mm.Upper oblique drive link top is connected with the roller on underdrive bar top, and the high 400mm of roller, bottom fills-sunk iron (weighing 10 kilograms), it is parallel with right side drive link away from bore diameter 16mm at the power transmission shaft 20mm under skylight, fill a drive link, drive link long 200mm, diameter 15mm and fixation.Drive link top bore diameter 4mm puts draw ring, and draw ring is connected (8 slide fasteners) zipper length 400mm, 40 kilograms of dry powder of dress (tentative) totally with bottom dress dry powder box
(2) afterbody automatically opens the door office：
The long 2600mm of the lateral incision of drive end unit appropriate location two × high 1300mm window,《Aircraft fall into the sea positioning signal show system》Roman loads and fixed.Copper round diameter 10mm protrusion 10mm electric leads are respectively set in tail external windows at two 45 degree of angle 30mm, insulation measures are carried out with fuselage, the top of copper coin shape electric conductor 1/2 is covered with rain cover, and copper round conductor connects power supply in fuselage, and front portion is that positive pole, rear portion are negative pole.Magnet coil is filled on window at the 1/2 of minister 2600mm, the iron that the rectangle of 5 kilograms (tentative) can be sunk is held, heavy iron is connected with window spring lock head (by stainless ironwork) bottom, the thickness middle level portion of door adds one layer of stainless iron sheet, door is held when closing door with electromagnet to close suddenly, door spring lock is locked a door.When two copper coin shape electric conductors meet water conduction, all electric power disconnections in storehouse, door nose electromagnetism loses suction, now inhale the heavy iron on door nose and lose suction and fall down, the suitable people of pulling force fallen down wrenches tapered end with hand and opened the door equally, door-lock opening, by the pressure of seawater, door is opened and intake, water is met after dry powder fuses and loses weight, the heavy iron (tentative 10 kilograms) of upper oblique drive link bottom starts to sink, the moment of sinking drives middle rotating shaft, rotating shaft drives trigger rod (it is the same that trigger rod scratches trigger action equivalent to the finger of people) to be rotated to trigger direction, (5 kilograms) of the iron ball now filled above oblique drive link in roller starts with oblique on the gravity of heavy iron, it is upper tiltedly to start to tilt to the heavy side of iron one when 10 degree of angles, finally roll into the heavy side of iron one, and heavy iron is pounded suddenly, also the dynamic trigger bar of violent speed belt pounds weight trigger suddenly, trigger is sagging, launching cradle is out of control, launching cradle is wrenched by the extension spring of 100 kilograms (tentative), by aircraft fall into the sea positioning signal show system eject fuselage, the water surface is floated on to start to show signal to satellite.
(3), aircraft falls into the sea positioning signal display system referred to as " floating object ", and Wai Nei departments and organs are set：White " floating object " is that square body (2200mm × 2200mm) center section is made up of white plastic foam; upper following peripheral net metal hard material catch net (tentative); Zhou Biankuan 100mm plastic-steels protect-ing frame structure (the thick built-in direct current 12V lithium batteries of 100mm); the 1/2 coil component spring power switch that has a protrusion 10mm of the protect-ing frame structure away from thickness at anterior 300mm; coil component spring power switch withstands (recessed) launching cradle crossbeam to close " floating object " internal electric source, and indicator lamp sends out a warning display.When being ejected " storehouse " and leaving firing mount crossbeam, coil component spring power switch protrusion, " floating object " internal electric source is connected, to open, indicator lamp bright green.Internal signal is opened to satellite display location simultaneously.The square object colleague of " floating object " of white (tentative) is shown on the water surface, and accurate target is provided to satellite and search aircraft.
Claims (4)
1. aircraft falls into the sea, positioning signal shows that system is installed in airplane tail group appropriate location or aircraft a part appropriate location, is independent " office ", not the manipulation by interior of aircraft personnel and commander." office " is set, positioning signal is shown system ejection export by full-automatic interlocking linkage.
2. the present invention does the principle of power lead using water, when aircraft falls into the water in a flash, external fuselage positive and negative electrode power supply is installed in the electric action of water, and storehouse interior power all open circuits, electromagnetism loses magnetic force, and door is opened.
After 3. door spring lock is unlocked, the pressure of water is recycled to be intake after door is opened, after water chance dry powder (a kind of dry powder used in fire extinguisher) is fused, chemically reactive, dry powder becomes aerosol and weightless by object, office's interlocking linkage reaction is caused in storehouse, the aircraft positioning signal that falls into the sea finally is shown system ejection export, to satellite or the aircraft display location signal of search.
4. of the invention be provided with dual safety, one is that electric power disconnection opens door, and this is the first insurance, and two are opened after door, in being put in storage without substantial amounts of swelling, it is impossible to which interlocking linkage reaction will not be produced by meeting office in weightlessness after dry powder dissolving, storehouse.Only possess this two conditions, one is that electric power disconnection is opened after door, two be large batch of swelling enter to meet produce chemical reaction after dry powder dissolving after lose center of gravity, could start interlocking linkage reaction, the aircraft positioning signal display system that falls into the sea is launched into export.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610021330.8A CN106965947A (en) | 2016-01-14 | 2016-01-14 | Aircraft fall into the sea positioning signal show system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610021330.8A CN106965947A (en) | 2016-01-14 | 2016-01-14 | Aircraft fall into the sea positioning signal show system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106965947A true CN106965947A (en) | 2017-07-21 |
Family
ID=59334626
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610021330.8A Pending CN106965947A (en) | 2016-01-14 | 2016-01-14 | Aircraft fall into the sea positioning signal show system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106965947A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111186586A (en) * | 2019-12-11 | 2020-05-22 | 贵州电网有限责任公司 | Smog emission device suitable for unmanned aerial vehicle |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101450707A (en) * | 2008-12-31 | 2009-06-10 | 西安四方航空科技有限公司 | Backpack type electric life saving system for pilot |
| CN201914465U (en) * | 2010-12-31 | 2011-08-03 | 航宇救生装备有限公司 | Safeguard station swim bladder |
| FR2960517A1 (en) * | 2010-05-27 | 2011-12-02 | Pierre Bansard | Device for ejection of data recorder e.g. flight voice recorder, of aircraft, has flotation device placed in enclosure in fuselage of aircraft, where enclosure is provided with closure flap and electro-magnetic devices |
| CN102658859A (en) * | 2012-05-18 | 2012-09-12 | 苏州金纳信息技术有限公司 | Cabin supplementary restraint system realizing device |
| FR2983833A1 (en) * | 2011-12-08 | 2013-06-14 | Amatec | Emergency beacon device i.e. emergency locator transmitter, for use in on-board equipment of e.g. aircraft, has beacon presenting structure ensuring floating orientation of beacon in water such that part of case remains emerged |
| CN104007451A (en) * | 2014-05-27 | 2014-08-27 | 曹宇 | Wrecking position recording reporting device |
| CN104751601A (en) * | 2013-12-27 | 2015-07-01 | 北京尚乘亿邦信息技术有限公司 | Maritime emergency rescue system |
| CN105197201A (en) * | 2015-10-13 | 2015-12-30 | 成都九十度工业产品设计有限公司 | Lifesaving device and lifesaving method with triggering type positioning launching |
-
2016
- 2016-01-14 CN CN201610021330.8A patent/CN106965947A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101450707A (en) * | 2008-12-31 | 2009-06-10 | 西安四方航空科技有限公司 | Backpack type electric life saving system for pilot |
| FR2960517A1 (en) * | 2010-05-27 | 2011-12-02 | Pierre Bansard | Device for ejection of data recorder e.g. flight voice recorder, of aircraft, has flotation device placed in enclosure in fuselage of aircraft, where enclosure is provided with closure flap and electro-magnetic devices |
| CN201914465U (en) * | 2010-12-31 | 2011-08-03 | 航宇救生装备有限公司 | Safeguard station swim bladder |
| FR2983833A1 (en) * | 2011-12-08 | 2013-06-14 | Amatec | Emergency beacon device i.e. emergency locator transmitter, for use in on-board equipment of e.g. aircraft, has beacon presenting structure ensuring floating orientation of beacon in water such that part of case remains emerged |
| CN102658859A (en) * | 2012-05-18 | 2012-09-12 | 苏州金纳信息技术有限公司 | Cabin supplementary restraint system realizing device |
| CN104751601A (en) * | 2013-12-27 | 2015-07-01 | 北京尚乘亿邦信息技术有限公司 | Maritime emergency rescue system |
| CN104007451A (en) * | 2014-05-27 | 2014-08-27 | 曹宇 | Wrecking position recording reporting device |
| CN105197201A (en) * | 2015-10-13 | 2015-12-30 | 成都九十度工业产品设计有限公司 | Lifesaving device and lifesaving method with triggering type positioning launching |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111186586A (en) * | 2019-12-11 | 2020-05-22 | 贵州电网有限责任公司 | Smog emission device suitable for unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170721 |
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| WD01 | Invention patent application deemed withdrawn after publication |