CN205239938U - Difficult anti - safety coefficient that hijacks a plane of airdreadnought air defense - Google Patents
Difficult anti - safety coefficient that hijacks a plane of airdreadnought air defense Download PDFInfo
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- CN205239938U CN205239938U CN201520927029.4U CN201520927029U CN205239938U CN 205239938 U CN205239938 U CN 205239938U CN 201520927029 U CN201520927029 U CN 201520927029U CN 205239938 U CN205239938 U CN 205239938U
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- hatch door
- parachute
- airdreadnought
- door plate
- cabin
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Abstract
The utility model relates to a difficult anti - safety coefficient that hijacks a plane of airdreadnought air defense belongs to aviation machinery. A difficult anti - safety coefficient that hijacks a plane of airdreadnought air defense, includes organism, wing, the both sides at the organism are connected to the wing, the organism includes outer cabin and independent cabin, outer cabin's upper portion opening part is provided with the hatch door headstock gear, independent cabin set up in outer cabin's inside, a plurality of independent cabin detachable are formed by connecting in order, independent under -deck is provided with safety device and the anti - water -spraying system of airplane hijacking, the top in independent cabin is provided with the parachute device, at every the both ends in independent cabin all be provided with adjacent two independent cabin pull separator. The utility model provides a difficult anti - safety coefficient that hijacks a plane of airdreadnought air defense, this safety coefficient can make things convenient for effectual prevention or limit emergent events, personal security in the protection airdreadnought.
Description
Technical field
The present invention is specifically related to the anti-airplane crash Convention for the Suppression of Unlawful Seizure of Aircraft of a kind of airdreadnought security system, belongs to aviation machine field.
Background technology
Though compared with automobile, railroad accident rate, the accident rate of aircraft is minimum. Once but have an accident, fly the probability that Passenger On Board survives almost nil. Therefore,, from aircraft birth, " airplane crash " is the shade that aircraft industry be can't get rid of all the time. Once large airplane crash, hundreds of fresh and alive life pop-offs, this is to one family, and a country even of airline, is all a huge disaster. In recent years, aircraft industry makes the matter worse, and " airplane hijacking " event is frequent. " mistakenly hit " event is continuous. Allow people produce distrust to aircraft industry, aircraft industry has been received huge impact and influence. The existing aircraft with anti-airplane crash Convention for the Suppression of Unlawful Seizure of Aircraft, its function is comprehensive not, the defence deficiency playing.
Summary of the invention
In order to solve the problems of the technologies described above, the invention provides the anti-airplane crash Convention for the Suppression of Unlawful Seizure of Aircraft of a kind of airdreadnought security system, the prevention that this security system can be easily and effectively or restriction accident, personal security in protection airdreadnought.
Technical scheme of the present invention is as follows:
The anti-airplane crash Convention for the Suppression of Unlawful Seizure of Aircraft of a kind of airdreadnought security system, comprises body, wing; Described wing is connected to the both sides of body, and described body comprises outer cabin and independent tank; The upper opening place in described outer cabin is provided with hatch door headstock gear, described independent tank is arranged at the inside in described outer cabin, multiple independent tanks are dismountable to be formed by connecting in turn, in described independent tank, be provided with safety device and Convention for the Suppression of Unlawful Seizure of Aircraft spraying system, on the top of described independent tank, be provided with parachute assembly; Be provided with the traction separator of the independent tank described in adjacent two at the two ends of each described independent tank.
Wherein, described hatch door headstock gear includes the first hatch door plate, the second hatch door plate, the 3rd hatch door plate, extensible member, first connecting rod and second connecting rod; Described the first hatch door plate is hinged at the first tie point place and outer cabin opening part; Described the second hatch door plate and described the first hatch door plate are hinged; Described the 3rd hatch door plate and described the second hatch door plate are hinged; Described first connecting rod and described the first hatch door plate and the 3rd hatch door plate are hinged; Described second connecting rod one end and described the second hatch door plate are hinged, and the other end and outer cabin are hinged; Yu Wai cabin, described extensible member one end is hinged, and the other end and described the first hatch door plate are hinged.
Wherein, each described independent tank is a complete unit that works alone, and each independent tank comprises: a section structure; One is arranged at the hermatic door that makes the airtight safe Waiting space of the interior formation one of this section structure on this section structure, and wherein sealing door comprises emergency exits and observation window; And be arranged at the cabin body internal unit in this section structure; Described independent tank also includes one and makes the axle mechanism that this section structure can be mobile in orbit, and this axle mechanism is to be directly arranged on the bottom surface of this section structure outside.
Wherein, described traction separator comprises body, one end of described body is provided with two sections of screw thread inner push-rods that are step-like, and wherein: major diameter screw thread inner push-rod is connected with outer journal stirrup threaded engagement, minor diameter screw thread inner push-rod is joined merga pass separation nut screw-threaded coupling with interior journal stirrup suit and is connected; The arranged outside of described separation nut has platen, and described platen is fixedly connected with described interior journal stirrup by screw, in the toroidal cavity between described separation nut and described platen, is provided with buffer gasket; On described buffer gasket, edge is circumferentially distributed with eight grooves.
Wherein, described safety device includes air cleaning system, apparatus of oxygen supply, gps satellite positioner, thermostat, seat and storage tank; Described section structure comprises metal framework, and described metal framework outer surface is surrounded with shell, and described metal framework inner surface is surrounded with inner bag, is provided with heat-insulating flame-retardant layer and spring between described inner bag and shell; Described metal framework adopts netted structure; Described shell is box structure, adopts fire prevention shell steel plate; Described inner bag adopts corrosion resistant plate material, and the turning in described inner bag is arc-shaped transition, without corner angle, and described inner bag surface is provided with flexible material layer; Described heat-insulating flame-retardant layer comprises the heat insulating coatings layer that is coated in inner surface of outer cover; Spring between described inner bag and shell is to group stage clip; Described independent tank bottom is provided with fixed castor and universal castor; Described chair mounted is in the bottom of inner bag inside, and described seat front lower place is provided with footmuff, and seat both sides are provided with safety belt, on described inner bag inwall, is provided with handle; Described air cleaning system comprises the air hole with window being arranged on section structure, and described air hole place is provided with ventilation fan, and the air inlet of described ventilation fan is provided with air filter; Described apparatus of oxygen supply is chemical oxygen self-rescuer; Described thermostat comprises eight incubators that are contained in described inner bag, is provided with insulation powder in described incubator; Described gps satellite positioner is arranged in seat, and the holding wire that connects GPS locator is outside section structure.
Wherein, described Convention for the Suppression of Unlawful Seizure of Aircraft spraying system comprises the spray tank, control device and the spray pipe that are communicated with successively.
Wherein, described parachute assembly comprises parachute housing, parachute cloth structure, hawser, gas muscle, parachute upper cover, compressed air pipe joint, spring sealing hook and electronic control dop; Described parachute housing is flat configuration, and described parachute cloth structure is stacked in parachute housing; The core of described parachute cloth structure is dome, surrounding is box-shaped frame, described hawser involves mutually with the periphery of described parachute cloth structure, described hawser has 12, every three hawser lower ends are provided with a link, and four described links articulate with four described spring sealing hooks respectively mutually through four eyelets of described parachute housing bottom surface respectively; Described gas muscle has five, wherein one communicates with the core dome of described parachute cloth structure, all the other four communicate with the surrounding box-shaped frame of described parachute cloth structure, described five gas muscle lower ends are connected with compressed air pipe joint jointly, and described compressed air pipe joint is connected with compressed air line through the centre bore of parachute housing bottom surface; The edge of healing up mutually up and down at described parachute housing and described parachute upper cover is provided with electronic control dop.
The present invention has following beneficial effect:
1, the setting of parachute assembly of the present invention and independent tank can ensure better passenger safety in the time there is crisis situation.
2, the present invention is provided with Convention for the Suppression of Unlawful Seizure of Aircraft spraying system; as required ruffian place independent tank is discharged to anesthesia spraying; not injuring under the prerequisite of personnel in passenger and cabin; prevention that can be easily and effectively or restriction accident; personal security in protection airdreadnought, thus Flight Safety ensured.
3, the present invention is provided with safety device, can be shellproof, explosion-proof, heat resistanceheat resistant and shock resistance, can, in clutch support personnel safety, ensure supply and the required existence necessity of oxygen, and time delay life, waits for rescue.
Brief description of the drawings
Fig. 1 is overall schematic of the present invention;
Fig. 2 is the structural representation of hatch door headstock gear deployed condition of the present invention;
Fig. 3 is the structural representation of hatch door headstock gear folded state of the present invention;
Fig. 4 is independent tank structural representation of the present invention;
Fig. 5 is traction separator structural representation of the present invention;
Fig. 6 is the structural representation of buffer gasket of the present invention;
Fig. 7 is safety device schematic diagram of the present invention;
Fig. 8 is the schematic diagram of Convention for the Suppression of Unlawful Seizure of Aircraft spraying system of the present invention at body section;
Fig. 9 is the structural representation under parachute assembly open mode of the present invention;
Figure 10 is the not structural representation under open mode of parachute assembly of the present invention.
In figure, Reference numeral is expressed as:
1-body, 2-wing, the outer cabin of 3-, 4-independent tank, 41-section structure, 42-hermatic door, 421-emergency exits, 422-observation window, 43-axle mechanism, 5-hatch door headstock gear, 51-the first hatch door plate, 52-the second hatch door plate, 53-the 3rd hatch door plate, 54-extensible member, 55-first connecting rod, 56-second connecting rod, 6-safety device, 61-air cleaning system, 62-apparatus of oxygen supply, 63-GPS satellite positioning device, 64-thermostat, 65-seat, 66-storage tank, 67-metal framework, 68-shell, 69-inner bag, 601-heat-insulating flame-retardant layer, 602-spring, the fixed castor of 603-, 604-universal castor, 611-air hole, 612-ventilation fan, 613-air filter, 7-Convention for the Suppression of Unlawful Seizure of Aircraft spraying system, 71-spray tank, 72-control device, 73-spray pipe, 8-parachute assembly, 81-housing, 82-parachute cloth structure, 83-hawser, 84-gas muscle, 85-parachute upper cover, 86-compressed air pipe joint, 87-spring sealing hook, the electronic control dop of 88-, 801-link, 9-draws separator, 91-body, 92-major diameter screw thread inner push-rod, 93-minor diameter screw thread inner push-rod, the outer journal stirrup of 94-, journal stirrup in 95-, 96-separation nut, 97-platen, 98-screw, 99-buffer gasket, 901-groove.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments, the present invention will be described in detail.
Referring to Fig. 1-10, the anti-airplane crash Convention for the Suppression of Unlawful Seizure of Aircraft of a kind of airdreadnought security system, comprises body 1, wing 2; Described wing 2 is connected to the both sides of body 1, and described body 1 comprises outer cabin 3 and independent tank 4; The upper opening place in described outer cabin 3 is provided with hatch door headstock gear 5, described independent tank 4 is arranged at the inside in described outer cabin 3, multiple independent tanks 4 are dismountable to be formed by connecting in turn, in described independent tank 4, be provided with safety device 6 and Convention for the Suppression of Unlawful Seizure of Aircraft spraying system 7, on the top of described independent tank 4, be provided with parachute assembly 8; Be provided with the traction separator 9 of the independent tank described in adjacent two at the two ends of each described independent tank 4.
Described hatch door headstock gear 5 includes the first hatch door plate 51, the second hatch door plate 52, the 3rd hatch door plate 53, extensible member 54, first connecting rod 55 and second connecting rod 56; Described the first hatch door plate 52 is hinged at the first tie point place and outer cabin 3 opening parts; Described the second hatch door plate 52 is hinged with described the first hatch door plate 51; Described the 3rd hatch door plate 53 is hinged with described the second hatch door plate 52; Described first connecting rod 55 is hinged with described the first hatch door plate 51 and the 3rd hatch door plate 53; Described second connecting rod 56 one end and described the second hatch door plate 52 are hinged, and the other end and outer cabin 3 are hinged; Described extensible member 54 Yu Wai cabins 3, one end are hinged, and the other end and described the first hatch door plate 51 are hinged.
Each described independent tank 4 is the complete unit that work alone, and each independent tank 4 comprises: a section structure 41; One is arranged at the hermatic door 42 that makes the airtight safe Waiting space of the interior formation one of this section structure 41 on this section structure 41, and wherein sealing door 42 comprises emergency exits 421 and observation window 422; And be arranged at the cabin body internal unit in this section structure 41; Described independent tank 4 also includes one and makes the axle mechanism 43 that this section structure 41 can be mobile in orbit, and this axle mechanism 43 is to be directly arranged on the bottom surface of these section structure 41 outsides.
Described traction separator 9 comprises body 91, one end of described body 91 is provided with the two sections of screw thread inner push-rods 92,93 that are step-like, wherein: major diameter screw thread inner push-rod 92 is connected with outer journal stirrup 94 threaded engagement, minor diameter screw thread inner push-rod 93 is joined merga pass separation nut 96 screw-threaded couplings with interior journal stirrup 95 suits and is connected; The arranged outside of described separation nut 96 has platen 97, and described platen 97 is fixedly connected with described interior journal stirrup 95 by screw 98, in the toroidal cavity between described separation nut 96 and described platen 97, is provided with buffer gasket 99; On described buffer gasket 99, edge is circumferentially distributed with eight grooves 901.
Described safety device 6 includes air cleaning system 61, apparatus of oxygen supply 62, gps satellite positioner 63, thermostat 64, seat 65 and storage tank 66; Described section structure 41 comprises metal framework 67, and described metal framework 67 outer surfaces are surrounded with shell 68, and described metal framework 67 inner surfaces are surrounded with inner bag 69, are provided with heat-insulating flame-retardant layer 601 and spring 602 between described inner bag 69 and shell 68; Described metal framework 67 adopts netted structure; Described shell 68 is box structure, adopts fire prevention shell steel plate; Described inner bag 69 adopts corrosion resistant plate material, and the turning in described inner bag 69 is arc-shaped transition, without corner angle, and described inner bag 69 surfaces are provided with flexible material layer; Described heat-insulating flame-retardant layer 601 comprises the heat insulating coatings layer that is coated in shell 68 inner surfaces; Spring 602 between described inner bag 69 and shell 68 is to group stage clip; Described independent tank 4 bottoms are provided with fixed castor 603 and universal castor 604; Described seat 65 is arranged on the bottom of inner bag 69 inside, and described seat 65 front lower places are provided with footmuff, and seat 65 both sides are provided with safety belt, on described inner bag 69 inwalls, is provided with handle; Described storage tank 66 can be put first-aid medicine, food, water and instrument etc.; Described air cleaning system 61 comprises the air hole 611 with window being arranged on section structure 41, and described air hole 611 places are provided with ventilation fan 612, and the air inlet of described ventilation fan 612 is provided with air filter 613; Described apparatus of oxygen supply 62 is chemical oxygen self-rescuer; Described thermostat 64 comprises eight incubators that are contained in described inner bag 69, is provided with insulation powder in described incubator; Described gps satellite positioner 63 is arranged in seat 65, and the holding wire that connects GPS locator is outside section structure 41.
Described Convention for the Suppression of Unlawful Seizure of Aircraft spraying system 7 comprises the spray tank 71, control device 72 and the spray pipe 73 that are communicated with successively.
Described parachute assembly 8 comprises parachute housing 81, parachute cloth structure 82, hawser 83, gas muscle 84, parachute upper cover 85, compressed air pipe joint 86, spring sealing hook 87 and electronic control dop 88; Described parachute housing 81 is flat configuration, and described parachute cloth structure 82 is stacked in parachute housing 81; The core of described parachute cloth structure 82 is dome, surrounding is box-shaped frame, described hawser 83 involves mutually with the periphery of described parachute cloth structure 82, described hawser 83 has 12, every three hawser 83 lower ends are provided with 801, four described links 801 of a link and articulate mutually with four described spring sealing hooks 87 respectively through four eyelets of described parachute housing 81 bottom surfaces respectively again; Described gas muscle 84 has five, wherein one communicates with the core dome of described parachute cloth structure 82, all the other four communicate with the surrounding box-shaped frame of described parachute cloth structure 82, described five gas muscle 84 lower ends are connected with compressed air pipe joint 86 jointly, and described compressed air pipe joint 86 is connected with compressed air line through the centre bore of parachute housing 81 bottom surfaces; The edge of healing up mutually up and down at described parachute housing 81 and described parachute upper cover 85 is provided with electronic control dop 88.
The foregoing is only embodiments of the invention; not thereby limit the scope of the claims of the present invention; every equivalent structure or conversion of equivalent flow process that utilizes description of the present invention and accompanying drawing content to do; or be directly or indirectly used in other relevant technical fields, be all in like manner included in scope of patent protection of the present invention.
Claims (7)
1. the anti-airplane crash Convention for the Suppression of Unlawful Seizure of Aircraft of an airdreadnought security system, is characterized in that: comprise body (1), wing (2); Described wing (2) is connected to the both sides of body (1), and described body (1) comprises outer cabin (3) and independent tank (4); The upper opening place in described outer cabin (3) is provided with hatch door headstock gear (5), described independent tank (4) is arranged at the inside in described outer cabin (3), multiple independent tanks (4) are dismountable to be formed by connecting in turn, in described independent tank (4), be provided with safety device (6) and Convention for the Suppression of Unlawful Seizure of Aircraft spraying system (7), on the top of described independent tank (4), be provided with parachute assembly (8); Be provided with the traction separator (9) of the independent tank described in adjacent two at the two ends of each described independent tank (4).
2. the anti-airplane crash Convention for the Suppression of Unlawful Seizure of Aircraft of a kind of airdreadnought according to claim 1 security system, is characterized in that: described hatch door headstock gear (5) includes the first hatch door plate (51), the second hatch door plate (52), the 3rd hatch door plate (53), extensible member (54), first connecting rod (55) and second connecting rod (56); Described the first hatch door plate (52) is hinged at the first tie point place and outer cabin (3) opening part; Described the second hatch door plate (52) is hinged with described the first hatch door plate (51); Described the 3rd hatch door plate (53) is hinged with described the second hatch door plate (52); Described first connecting rod (55) is hinged with described the first hatch door plate (51) and the 3rd hatch door plate (53); Described second connecting rod (56) one end and described the second hatch door plate (52) are hinged, and the other end and outer cabin (3) are hinged; Yu Wai cabin, described extensible member (54) one end (3) is hinged, and the other end and described the first hatch door plate (51) are hinged.
3. the anti-airplane crash Convention for the Suppression of Unlawful Seizure of Aircraft of a kind of airdreadnought according to claim 1 security system, it is characterized in that: each described independent tank (4) is a complete unit that works alone, and each independent tank (4) comprising: a section structure (41); One is arranged at the hermatic door (42) that makes the airtight safe Waiting space of the interior formation one of this section structure (41) on this section structure (41), and wherein sealing door (42) comprises emergency exits (421) and observation window (422); And be arranged at the cabin body internal unit in this section structure (41); Described independent tank (4) also includes one and makes the axle mechanism (43) that this section structure (41) can be mobile in orbit, and this axle mechanism (43) is to be directly arranged on the outside bottom surface of this section structure (41).
4. the anti-airplane crash Convention for the Suppression of Unlawful Seizure of Aircraft of a kind of airdreadnought according to claim 1 security system, it is characterized in that: described traction separator (9) comprises body (91), one end of described body (91) is provided with two sections of screw thread inner push-rods (92 that are step-like, 93), wherein: major diameter screw thread inner push-rod (92) is connected with outer journal stirrup (94) threaded engagement, minor diameter screw thread inner push-rod (93) and interior journal stirrup (95) suit is joined merga pass separation nut (96) screw-threaded coupling and is connected; The arranged outside of described separation nut (96) has platen (97), described platen (97) is fixedly connected with described interior journal stirrup (95) by screw (98), in the toroidal cavity between described separation nut (96) and described platen (97), is provided with buffer gasket (99); Described buffer gasket (99) is upper along being circumferentially distributed with eight grooves (901).
5. the anti-airplane crash Convention for the Suppression of Unlawful Seizure of Aircraft of a kind of airdreadnought according to claim 3 security system, is characterized in that: described safety device (6) includes air cleaning system (61), apparatus of oxygen supply (62), gps satellite positioner (63), thermostat (64), seat (65) and storage tank (66); Described section structure (41) comprises metal framework (67), described metal framework (67) outer surface is surrounded with shell (68), described metal framework (67) inner surface is surrounded with inner bag (69), is provided with heat-insulating flame-retardant layer (601) and spring (602) between described inner bag (69) and shell (68); Described metal framework (67) adopts netted structure; Described shell (68) is box structure, adopts fire prevention shell steel plate; Described inner bag (69) adopts corrosion resistant plate material, and the turning in described inner bag (69) is arc-shaped transition, without corner angle, and described inner bag (69) surface is provided with flexible material layer; Described heat-insulating flame-retardant layer (601) comprises the heat insulating coatings layer that is coated in shell (68) inner surface; Spring (602) between described inner bag (69) and shell (68) is to group stage clip; Described independent tank (4) bottom is provided with fixed castor (603) and universal castor (604); Described seat (65) is arranged on the inner bottom of inner bag (69), described seat (65) front lower place is provided with footmuff, seat (65) both sides are provided with safety belt, on described inner bag (69) inwall, are provided with handle; Described air cleaning system (61) comprises the air hole with window (611) being arranged on section structure (41), described air hole (611) locates to be provided with ventilation fan (612), and the air inlet of described ventilation fan (612) is provided with air filter (613); Described apparatus of oxygen supply (62) is chemical oxygen self-rescuer; Described thermostat (64) comprises eight incubators that are contained in described inner bag (69), is provided with insulation powder in described incubator; Described gps satellite positioner (63) is arranged in seat (65), and the holding wire that connects GPS locator is outside section structure (41).
6. the anti-airplane crash Convention for the Suppression of Unlawful Seizure of Aircraft of a kind of airdreadnought according to claim 1 security system, is characterized in that: described Convention for the Suppression of Unlawful Seizure of Aircraft spraying system (7) comprises the spray tank (71), control device (72) and the spray pipe (73) that are communicated with successively.
7. the anti-airplane crash Convention for the Suppression of Unlawful Seizure of Aircraft of a kind of airdreadnought according to claim 1 security system, is characterized in that: described parachute assembly (8) comprises parachute housing (81), parachute cloth structure (82), hawser (83), gas muscle (84), parachute upper cover (85), compressed air pipe joint (86), spring sealing hook (87) and electronic control dop (88); Described parachute housing (81) is flat configuration, and described parachute cloth structure (82) is stacked in parachute housing (81); The core of described parachute cloth structure (82) is dome, surrounding is box-shaped frame, described hawser (83) involves mutually with the periphery of described parachute cloth structure (82), described hawser (83) has 12, every three hawsers (83) lower end is provided with a link (801), and four described links (801) articulate with four described spring sealing hooks (87) respectively mutually through four eyelets of described parachute housing (81) bottom surface respectively; Described gas muscle (84) has five, wherein one communicates with the core dome of described parachute cloth structure (82), all the other four communicate with the surrounding box-shaped frame of described parachute cloth structure (82), described five gas muscle (84) lower end is connected with compressed air pipe joint (86) jointly, and described compressed air pipe joint (86) is connected with compressed air line through the centre bore of parachute housing (81) bottom surface; The edge of healing up mutually up and down at described parachute housing (81) and described parachute upper cover (85) is provided with electronic control dop (88).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520927029.4U CN205239938U (en) | 2015-11-19 | 2015-11-19 | Difficult anti - safety coefficient that hijacks a plane of airdreadnought air defense |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520927029.4U CN205239938U (en) | 2015-11-19 | 2015-11-19 | Difficult anti - safety coefficient that hijacks a plane of airdreadnought air defense |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205239938U true CN205239938U (en) | 2016-05-18 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520927029.4U Expired - Fee Related CN205239938U (en) | 2015-11-19 | 2015-11-19 | Difficult anti - safety coefficient that hijacks a plane of airdreadnought air defense |
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| Country | Link |
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| CN (1) | CN205239938U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105292496A (en) * | 2015-11-19 | 2016-02-03 | 郑启凡 | Air disaster prevention and anti-hijacking safety system of large-scale aircraft |
-
2015
- 2015-11-19 CN CN201520927029.4U patent/CN205239938U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105292496A (en) * | 2015-11-19 | 2016-02-03 | 郑启凡 | Air disaster prevention and anti-hijacking safety system of large-scale aircraft |
| CN105292496B (en) * | 2015-11-19 | 2018-03-23 | 郑启凡 | A kind of anti-airplane crash Convention for the Suppression of Unlawful Seizure of Aircraft security system of airdreadnought |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160518 Termination date: 20181119 |
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| CF01 | Termination of patent right due to non-payment of annual fee |