CN1459402A - Safety aircraft - Google Patents
Safety aircraft Download PDFInfo
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- CN1459402A CN1459402A CN 02115874 CN02115874A CN1459402A CN 1459402 A CN1459402 A CN 1459402A CN 02115874 CN02115874 CN 02115874 CN 02115874 A CN02115874 A CN 02115874A CN 1459402 A CN1459402 A CN 1459402A
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- aerocraft
- box
- parachute
- airbag
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Abstract
A high-safety aerial craft features that a huge parachutes, a lifesaving cabin, a multifunctional record box, hydrogen gas generator, an oil tank ejector, an automatic fire extinguisher, and an equipment for automatically regulating the inclination of aerial craft are equipped to the aerial craft. When an accident occurs, they can slow down the dropping speed for successful landing and automatically show the landing place.
Description
Involved in the present invention is safety aircraft, is to have the very aerocraft of high safety performance.Huge parachute, lifesaving Security Module, multifunctional record box, hydrogen gas generator, fuel tank ejector, automatic sprinkler, automatic compensation aerocraft heeling angle device etc. are housed on aerocraft, when aerocraft major failure took place aloft, this aerocraft had very strong self-saving ability.
For a long time, aviation is clamored, aerocraft such as aircarrier aircraft, fighter plane particularly, in case major failure aloft takes place, will become and be all in vain difficultly, cause numerous personal casualty and enormous economic loss, and victim's corpse, the wreckage of an plane, black box etc. all are difficult to seek, some temporary transient survivor is died because of can not in time rescuing, and accident causation also is difficult to forensics analysis.
Task of the present invention provides has the very aerocraft of high safety performance, when aerocraft generation major failure, a whole set of safety apparatus can slow down the descending speed of aerocraft greatly, for rescuing the people and rushing to repair aerocraft and striven for valuable time, best situation is during this period of time to rob to fix machine, pull through, recover normal flight, another kind of situation is to allow the occupant take advantage of Security Module to break away from aerocraft rapidly, safe falling, simultaneously the automatic device for ejecting of the fuel tank fuel tank that can will catch fire ejects aerocraft, fire extinguisher begins fire extinguishing automatically, equipment such as huge parachute and automatic compensation aerocraft heeling angle device can make aerocraft more successfully land, the multifunctional record box in high-altitude can be from aerial shooting aerocraft scene at this moment on the bullet, can clearly demonstrate the accurate position of the aerocraft and the manned Security Module of landing, so that rescue in time.
Solution of the present invention is: several huge parachutes are set on aerocraft, but the Security Module of several safety landing, also be provided with fuel tank ejector and automatic sprinkler, be provided with the recording box that several have hydrogen balloon, airbag, band keyboard, pick up camera, transmitting set, be provided with storage battery, transmitting set, and aerocraft come-up airbag, also have the equipment and the articles for use of a whole set of and their adapteds.
The invention will be further described below in conjunction with accompanying drawing.
Fig. 1: the front view of safety aircraft
Fig. 2: huge parachute figure
Fig. 8: multifunctional record box outside drawing
Fig. 4: a kind of Security Module outside drawing
Fig. 5: a kind of Security Module outside drawing
Fig. 6: inflation necklace outside drawing
Among the figure: 1. airborne vehicle 2. huge parachute ejector 3. hydrogen generators 4. flexible pipes, 5. huge parachute 6. umbrella cloths, 7. woven wires 8. Pneumatic rubber rings, 9. drogue-parachutes 10. hydrogen balloons, 11. multifunctional record boxes 12. recorders, 13. video cameras 14. elongate strands, 15. recording box ejectors 16. compressed air cylinders, 17. umbrella ropes 18. fuel tanks, 19. fuel tank ejectors 20. Automatic Fire Extinguishers, 21. Security Module pushers 22. Security Modules, 23. pneumatic boats 24. snifters, 25. automatic adjustment airborne vehicle heeling angle device 26. airbag boxes, 27. large airbag 28. battery 29. transmitting sets, 30. one-way air inlet element 31. accident pattern keyboards, 32. thin metal sealing boxes or foamed plastics 33. are struck and are starched 34. large-scale parachute 35. hard base plates 36. inflation necklaces 37. containment pockets 38. pulling ropes
Fig. 1, chief component of the present invention: several huge parachute ejectors 2 are equipped with at each position before, during and after aerocraft 1, huge parachute 5 is housed in the ejector 2, when aerocraft 1 runs into major failure, ejector 2 can launch huge umbrella 5 in the air, can slow down the descending speed of aerocraft 1 greatly, strive for valuable time for rescuing the people and rescuing machine.
The hydrogen balloon 10 that the useful elongate strands 14 in each position is tacked before, during and after aerocraft 1 is when aerocraft 1 drops in the water.Hydrogen balloon 10 can be suspended in aerial work sign and use.
Fig. 2, the another kind of form of huge parachute 5 is: by leak free umbrella cloth 6 around two-layer, wire gauze 7, umbrella rope 17, inflation glue ring 8, compressed air tank 16 compositions such as grade, in umbrella cloth central authorities of lower floor unidirectional air inlet element 30 is housed, air inlet element 30 has the pressure limiting function, between upper strata umbrella cloth and the lower floor's umbrella cloth very large space is arranged, and be sealing state, after parachute opens, powerful wind enters in the Sealed sandwich of two-layer umbrella cloth 6 from air inlet element 30, become an air-bag type parachute, like this, parachute 5 aloft can pop-up aerocraft 1, the aerocraft 1 that in water, can float, the middle body between the two-layer umbrella cloth up and down also the pulling rope 37 of useful certain-length link to each other, in order to avoid the umbrella cloth of lower floor protrudes downwards.
Fig. 1: clamor in aviation and recording box ejector 15 to be housed on 1, several multifunctional record boxes 11 are housed in the ejector 15, press ejector 15 with hand and recording box 11 can be launched in the air.Just in case blast in the aerocraft 1, then recording box 11 can be while making a video recording from moving to the high-altitude.
Fig. 2: recording box 11 has fire prevention, explosion-proof, functions such as waterproof, pick up camera 13 also is housed on the recording box 11, audifier recorder 12, accident type keyboard 31, transmitting set 29, hydrogen gas generator 3, hydrogen balloon 10, drogue-parachute 9, when major failure appears in aerocraft 1, ejector 15 can hold note in box 11 and launch in the air, drogue-parachute 9 opens, hydrogen gas generator 3 is started working, the hydrogen full balloon 10 that produces, recording box 11 is suspended in the air, take from the high-altitude to the scene of the accident of following aerocraft 1, distress signal takes place in the transmitting set 29 on the recording box 11, and demonstrate oneself longitude and latitude, the recording box 11 in directive high-altitude has an elongated rope 14 of high strength to link to each other with aerocraft 1, front portion at aerocraft 1, the middle part, the rear portion also is installed with several recording box 11, also have the recording box 11 of some activities can be connected on thin metallic seal box or the plastic foam, in water, can float to the water surface automatically.In accident type keyboard 31, predeterminable several frequently seen accident type number when fault just begins to take place, is pressed keyboard 31 fast, and the fastest available speed is represented this aerocraft type of et out of order at the moment.
Fig. 1, when determine that must man-machine separation the time, available several be equipped with the Security Module 22 of large-scale parachute 34, and occupant on the machine is sent from aerocraft in batches, the occupant takes advantage of Security Module 22, pushes away aircraft by pusher 21, but safe falling is to ground.Security Module pusher 21 can also allow large-scale parachute open rapidly, propelling unit 21 can be located at the last hatch door of aerocraft, following hatch door or side hatch door, can avoid airstream eddy current and flame zone, in the decline process, the rubber boat 23 of Security Module 22 bottoms can charge into air, if drop to the land, rubber boat can surpass the bumper and absorbing shock effect, if drop on the water surface, rubber boat then can float on the surface.On the Security Module 22 useful elongate strands be hydrogen balloon 10 be suspended in the air, make the emergency sign, find target as early as possible for rescue aircraft, ship.Transmitting set 29 is housed on the Security Module 22, the necessitys such as slurry 32, food, potable water, medicine of striking.
Fig. 4 and Fig. 5 are that two kinds of forms of Security Module 22 are given an example.
Fig. 4: Security Module 22 is the basket bodies that are made of light material high-intensity, that fold by force and thick cloth, hard base plate 35 is arranged at the bottom, rubber boat 23 and slurry 33 are arranged below, large-scale parachute 34, hydrogen gas generator 3, hydrogen balloon 10, inflation glue ring 8 are arranged above, inflation glue ring 3 is arranged around the umbrella cloth of big parachute 34, can be beneficial to umbrella and open rapidly earlier to 8 inflations of inflation glue ring before the landing, big parachute 34 is two, and wherein one is auxiliary parachute.
Fig. 5: with Fig. 4 difference be that high-intensity, the folding wire gauze of Security Module 22 usefulness and thick cloth constitute, be a bag shape, remainder is identical with Fig. 4, big parachute 34 is two, wherein a handle is an auxiliary parachute.
Fig. 1: fuel tank ejector 19, automatic sprinkler 20 are equipped with in the side of the fuel tank of aerocraft 1, when Mars appearred in fuel tank 18, automatic sprinkler 20 was the self-opening fire extinguishing, when naked light occurring, fuel tank ejector 19 automatically with fuel tank 18 bullets from aerocraft, with the harm that prevents that fire from stretching.
Fig. 1: automatic compensation aerocraft heeling angle device 25 is housed on the aerocraft 1, when aerocraft before last resort enters in the water, automatic compensation angle device 25 can transfer to the leaning angle of aerocraft entry the best angle that pre-sets, avoid aerocraft to rupture, but this install also manual adjustment angle because of the bump water surface as far as possible.
Fig. 1: several levitating devices are housed on aerocraft 1.Before aerocraft 1, in, each position, back is provided with several airbag boxes 26, folding big airbag 27 all is housed in the airbag box 26, hydrogen balloon 10, hydrogen gas generator 3 immersion back airbag boxes 26 are opened automatically, 3 pairs of big airbags 27 of hydrogen gas generator and hydrogen balloon 10 fill hydrogen, the atmosphere bag is long-pending to be increased gradually, can aerocraft 1 is floating to the water surface, hydrogen balloon 10 usefulness elongate strands are connected with aerocraft 1, hydrogen balloon 10 can emerge, and be suspended in the air, as distinctive marks, the maximum gas production rate of hydrogen gas generator 3 is controlled at optimum value, airbag box 26 1 sides are equipped with self-filler 24 in aerocraft 1 storehouse, the wind-force that produces when utilizing aerocraft to descend is filled air with on-board atmosphere bag 27, still can float after aerocraft 1 is fallen into water.Big airbag 27 is equipped with unidirectional air inlet element 30, and unidirectional air inlet element 30 is a kind of unidirectional pressure limiting air inlet valves.Hydrogen balloon 10 can be made rubber balloon, thin metal hollow ball, hollow box.Levitating devices such as hydrogen clamors 3, hydrogen balloon 10, big airbag 27, aerator 23 except can be used on the aerocraft, also can be contained on ship, warship, the Submarine etc.
Fig. 1 is equipped with storage battery 28 in the driving compartment, for transmitting set 29 is transmitted messages and illumination provides emergency source of electrical power, in case cut off the power supply because of the rear deck electrical generator has a power failure.Can send the emergency electric wave signal, this moment such as light distress signal etc. in the same old way.
Fig. 6: each passenger issues inflation necklace 36, can be worn over neck, inflatable in the inflation necklace 36, on the inflation necklace 36 salable pocket 37 is arranged, pack into be marked with the card of passenger's name, sex, identification card number, home address, telephone number and aerial sign after, be sealing state, can be used as souvenir and use.
Modern design of the present invention, the safety performance height, when aerocraft runs into major failure aloft, has good self-saving ability, particularly can with occupant safety deliver to ground, the aviation landing of clamoring can be more successfully allowed, the landing place that personnel and aviation are clamored can be reported timely and accurately, so that aircraft and ship come to the rescue.
The present invention has great social value and economic value.
Claims (9)
1, a kind of safety aircraft, it is characterized in that: huge parachute ejector 2, Security Module 22, airbag box 26, recording box ejector 15 more than one are housed being equipped with the position before, during and after the aerocraft, the aviation heeling automatic compensation angle device 25 of clamoring is installed in the cockpit of aerocraft 1, and fuel tank ejector 19 and automatic sprinkler 20 are equipped with in the side of fuel tank in aerocraft 1;
2, the huge parachute ejector 2 of safety aircraft as claimed in claim 1, it is characterized in that: huge parachute 5 is housed in the ejector 2, when aerocraft runs into major failure, ejector 2 can launch huge parachute 5 in the air, huge parachute 5 aloft opens, one end of umbrella rope 17 is fixed on the aerocraft, the umbrella cloth 6 of huge parachute 5 is to make with one deck to two-layer high-intensity cloth, appearance scribbles luminescent coating and various color pigment, inflation glue ring 8 is arranged in the garden week of umbrella cloth 6, appearance also can add layer of metal silk screen 7, hydrogen gas generator 3 and compressed air tank 16 are housed on the umbrella rope, compressed air tank 16 can be inflated 8 inflations of glue ring from trend, but self-opening and produce a large amount of hydrogen when hydrogen gas generator 3 immerses in the water, between the two-layer umbrella cloth 6 of leak free, huge parachute 5 has just become the airbag that is full of hydrogen to hydrogen, on the huge parachute 5 multifunctional record box 11 is housed around flexible pipe 4 enters;
3, the huge parachute 5 of safety aircraft as claimed in claim 2, it is characterized in that: form by leak free umbrella cloth 6, wire gauze 7 and umbrella rope 17, inflation glue ring 8 etc. around two-layer, unidirectional air inlet element 30 is equipped with in umbrella cloth central authorities of lower floor, air inlet element 30 is unidirectional pressure limiting air inlet valves, between upper strata umbrella cloth and the lower floor's umbrella cloth very large space is arranged, and be sealing state, after huge umbrella 5 opens, powerful wind enters in the Sealed sandwich of umbrella cloth 6 from air inlet element 30, becomes an air-bag type parachute.Link to each other at the pulling rope 37 that also has certain-length up and down between the two-layer umbrella cloth, in order to avoid the umbrella cloth of lower floor protrudes downwards;
4, safety aircraft recording box ejector 15 as claimed in claim 1, it is characterized in that: an above multifunctional record box 11 is housed in the ejector 15, pressing ejector 15 with hand can launch recording box 11 in the air, recording box 11 has recording, shooting, fire prevention, explosion-proof, functions such as waterproof, also has accident type keyboard 31, transmitting set 29, hydrogen gas generator 3, hydrogen balloon 10, drogue-parachute 9, the aerial elongated rope 14 of high strength of recording box 11 usefulness of directive is connected with aerocraft 1, hydrogen balloon 10 and drogue-parachute 9 can allow recording box 11 be suspended in the air, pick up camera 13 on the recording box 11 can be taken following in the air from height, front portion at aerocraft 1, the middle part, the rear portion also is installed with several recording box 11, also have some mobile recording box 11 can be connected on thin metallic seal box or the foamed plastic, in water, can float automatically to the water surface, in accident type keyboard 31, predeterminable several frequently seen accident type, just in case there is the blast situation to take place in the aerocraft 1, recording box 11 can be while making a video recording from moving to the high-altitude;
5, safety aircraft Security Module 22 as claimed in claim 1, it is characterized in that: have large-scale parachute 34 on the Security Module 22, the bottom of Security Module 22 has rubber boat 23 to be attached thereto, transmitting set 29 is housed on the Security Module 22, strike and starch 33, food, potable water, necessitys such as medicine, with the hydrogen balloon 10 that is attached thereto with elongate strands 14, Security Module 22 is the basket bodies that constitute with folding light material of high strength and thick cloth, or make folding metal filament mesh bag shape, hard base plate 35 is arranged at the bottom, Security Module 22 also can be sent aerocraft by pusher 21, all parachutes of the present invention comprise huge parachute 5, large-scale parachute 34, the circumference of umbrella all has a circle inflation glue ring 8, compressed air tank 16, compressed air tank 16 impels parachute to open rapidly from 8 inflations of trend inflation glue ring;
6, safety aircraft heeling automatic compensation angle device 25 as claimed in claim 1 is characterized in that: device 25 also available manual operationss;
7, safety aircraft airbag box 26 as claimed in claim 1, it is characterized in that: folding big airbag 27 is housed in the airbag box 26, hydrogen balloon 10 and hydrogen gas generator 3, immersion back airbag box 26 is opened automatically, hydrogen gas generator 3 is automatically to airbag 27 inflations, hydrogen balloon 10 can be made rubber balloon, thin metal hollow ball, hollow box, and ball 10 is linked to each other with aerocraft 1 with elongate strands 14, hydrogen balloon 10 can emerge, and be suspended in aerial, the maximum gas production rate of hydrogen gas generator 3 is controlled at optimum value, and above-mentioned hydrogen gas generator 3 and big airbag 27 levitating devices such as grade also can be installed in steamer, warship, on the Submarine etc.;
8, safety aircraft airbag box 26 as claimed in claim 7, it is characterized in that: airbag box 26 1 sides are equipped with self-filler 24, and the wind-force that produces when utilizing aerocraft to descend is filled air with big airbag 27, and big airbag 27 is equipped with unidirectional air inlet element 30;
9, safety aircraft as claimed in claim 1 is characterized in that: be furnished with several inflation necklaces 36 in aerocraft 1 storehouse, can charge into gas, can be worn over people's neck, on the inflation necklace 36 salable pocket 37 is arranged, be sealing state behind the card of packing into.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 02115874 CN1459402A (en) | 2002-05-19 | 2002-05-19 | Safety aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN 02115874 CN1459402A (en) | 2002-05-19 | 2002-05-19 | Safety aircraft |
Publications (1)
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CN1459402A true CN1459402A (en) | 2003-12-03 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN 02115874 Pending CN1459402A (en) | 2002-05-19 | 2002-05-19 | Safety aircraft |
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Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101941525A (en) * | 2010-09-30 | 2011-01-12 | 中北大学 | Parachuting device for recorder recovery |
CN102360220A (en) * | 2011-05-31 | 2012-02-22 | 江汉大学 | Device and method for searching aviation recorder on seabed |
CN102476709A (en) * | 2010-11-25 | 2012-05-30 | 吴佑之 | Escape cabin |
CN102673790A (en) * | 2012-06-12 | 2012-09-19 | 河南师范大学 | Escape device |
CN102005066B (en) * | 2009-09-03 | 2013-04-03 | 杨东宁 | Aircraft emergency information system |
CN105752336A (en) * | 2016-02-26 | 2016-07-13 | 舟山巨洋技术开发有限公司 | Multipurpose large-sized unmanned aerial vehicle |
WO2018188472A1 (en) * | 2017-04-12 | 2018-10-18 | 王树强 | High-efficiency device for generating controllable lifting force for gear lifting parachutes and use method |
CN110107457A (en) * | 2019-05-06 | 2019-08-09 | 龚水明 | A kind of balloon suspension formula air compression plant and wind generator system |
CN111295334A (en) * | 2017-08-24 | 2020-06-16 | 日本化药株式会社 | Safety device for aircraft and aircraft |
-
2002
- 2002-05-19 CN CN 02115874 patent/CN1459402A/en active Pending
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102005066B (en) * | 2009-09-03 | 2013-04-03 | 杨东宁 | Aircraft emergency information system |
CN101941525A (en) * | 2010-09-30 | 2011-01-12 | 中北大学 | Parachuting device for recorder recovery |
CN101941525B (en) * | 2010-09-30 | 2013-03-20 | 中北大学 | Parachuting device for recorder recovery |
CN102476709A (en) * | 2010-11-25 | 2012-05-30 | 吴佑之 | Escape cabin |
CN102360220A (en) * | 2011-05-31 | 2012-02-22 | 江汉大学 | Device and method for searching aviation recorder on seabed |
CN102360220B (en) * | 2011-05-31 | 2013-06-12 | 江汉大学 | Device and method for searching aviation recorder on seabed |
CN102673790A (en) * | 2012-06-12 | 2012-09-19 | 河南师范大学 | Escape device |
CN105752336A (en) * | 2016-02-26 | 2016-07-13 | 舟山巨洋技术开发有限公司 | Multipurpose large-sized unmanned aerial vehicle |
WO2018188472A1 (en) * | 2017-04-12 | 2018-10-18 | 王树强 | High-efficiency device for generating controllable lifting force for gear lifting parachutes and use method |
CN111295334A (en) * | 2017-08-24 | 2020-06-16 | 日本化药株式会社 | Safety device for aircraft and aircraft |
CN111295334B (en) * | 2017-08-24 | 2024-06-07 | 日本化药株式会社 | Safety device for flying body and flying body |
CN110107457A (en) * | 2019-05-06 | 2019-08-09 | 龚水明 | A kind of balloon suspension formula air compression plant and wind generator system |
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C06 | Publication | ||
PB01 | Publication | ||
C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
WD01 | Invention patent application deemed withdrawn after publication |