CN204776064U - Carrier -borne aircraft descending electromagnetic damping system - Google Patents
Carrier -borne aircraft descending electromagnetic damping system Download PDFInfo
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- CN204776064U CN204776064U CN201520407600.XU CN201520407600U CN204776064U CN 204776064 U CN204776064 U CN 204776064U CN 201520407600 U CN201520407600 U CN 201520407600U CN 204776064 U CN204776064 U CN 204776064U
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- carrier
- aircraft
- borne aircraft
- electromagnetic damping
- borne
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- 238000013016 damping Methods 0.000 title claims abstract description 28
- 230000005294 ferromagnetic effect Effects 0.000 claims description 9
- 238000001179 sorption measurement Methods 0.000 abstract description 2
- 238000010521 absorption reaction Methods 0.000 abstract 1
- 230000005291 magnetic effect Effects 0.000 description 12
- IWEDIXLBFLAXBO-UHFFFAOYSA-N dicamba Chemical compound COC1=C(Cl)C=CC(Cl)=C1C(O)=O IWEDIXLBFLAXBO-UHFFFAOYSA-N 0.000 description 8
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 208000027418 Wounds and injury Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 208000014674 injury Diseases 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
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Abstract
The utility model discloses a carrier -borne aircraft descending electromagnetic damping system belongs to large ship technical field. The carrier -borne aircraft afterbody be equipped with can and the aircraft carrier deck between produce to adsorb and form fricative electromagnetic damping piece, the electromagnetic damping piece passes through the rope and is connected with the carrier -borne aircraft. Pass through the electromagnetic damping piece and produce absorption with the aircraft carrier deck when the warship to the carrier -borne aircraft, increase carrier -borne aircraft and the friction of aircraft carrier deck, slow down the inertia of carrier -borne aircraft, realize the carrier -borne aircraft speed reduction and stop, improving the carrier -borne aircraft greatly and warship stability, reducing warship accident probability. Electro -magnet opposite poles attract through on aircraft carrier on -board electromagnetism strip and the carrier -borne aircraft can further promote adsorption affinity and friction for the carrier -borne aircraft stops.
Description
Technical field
The utility model relates to a kind of carrier-borne aircraft damping system, is specifically a kind of carrier-borne aircraft landing electromagnetic damping system, belongs to large ship technical field.
Background technology
Carrier landing damper is the important equipment on aircraft carrier, is mainly used in the slow down warship of carrier-borne aircraft in type aircraft carrier deck.In prior art, most of aircraft carrier adopts cable type stopping device to slow down facing to warship aircraft, it is in use easy can cause certain injury to carrier-borne aircraft, it warship poor stability simultaneously, cable type stopping device easily produces fracture in Long-Time Service process, cause carrier landing failure, cause heavy economic losses.
Utility model content
Technical problem to be solved in the utility model is to overcome prior art defect, provides a kind of carrier-borne aircraft landing electromagnetic damping system that effectively can improve warship stability.
In order to solve the problems of the technologies described above, the carrier-borne aircraft landing electromagnetic damping system that the utility model provides, comprise be arranged on carrier-borne aircraft afterbody can and type aircraft carrier deck between produce and adsorb and form the electromagnetic damping block rubbed, described electromagnetic damping block is connected with carrier-borne aircraft by rope.
In the utility model, described electromagnetic damping block is electromagnet, and described electromagnet connects carrier-borne aircraft power supply.
In the utility model, described type aircraft carrier deck is provided with electromagnetism bar, and described electromagnetism bar connects power supply, and the electromagnet polarity on described electromagnetism bar and carrier-borne aircraft is different.
In the utility model, described electromagnetic damping block is ferromagnetic plate.
In the utility model, described type aircraft carrier deck is provided with electromagnetism bar, and described electromagnetism bar connects power supply.
The beneficial effects of the utility model are: (1), produced adsorb when carrier landing by electromagnetic damping block and type aircraft carrier deck, increase carrier-borne aircraft and type aircraft carrier deck friction, slow down the inertia of carrier-borne aircraft, realize carrier-borne aircraft slow down and stop, greatly improve carrier landing stability, reduce warship accident probability; (2) there is a natural attraction between the sexes for the electromagnet, by type aircraft carrier deck powered on magnetic stripe and carrier-borne aircraft, can promote adsorption affinity and mutual friction further, accelerates the stopping speed of carrier-borne aircraft; (3), the utility model is safe and reliable, is easy to processing and installs and uses, assembling easy to maintenance, be applicable to various aircraft carrier platform.
Accompanying drawing explanation
Fig. 1 is the utility model carrier-borne aircraft landing electromagnetic damping system architecture schematic diagram;
Fig. 2 is the utility model carrier-borne aircraft landing electromagnetic damping system one example structure schematic diagram.
Fig. 3 is another example structure schematic diagram 2 of the utility model carrier-borne aircraft landing electromagnetic damping system.
Detailed description of the invention
Below in conjunction with accompanying drawing, the utility model is described in further detail.
As shown in Figure 1, the utility model carrier-borne aircraft landing electromagnetic damping system, comprises carrier-borne aircraft 1, electromagnet 2, rope 3 and type aircraft carrier deck 4.Electromagnet 2 is connected by the afterbody of rope 3 with carrier-borne aircraft 1, and electromagnet 2 can be placed in the afterbody accepting rack of carrier-borne aircraft 1.Electromagnet 2 is connected with the power supply of carrier-borne aircraft 1 simultaneously, and power control switch is arranged in driving compartment, is controlled by aviator.In carrier landing process, when it aligns with type aircraft carrier deck 4, aviator controls to put down electromagnet 2, open the power supply of electromagnet 2 simultaneously, now electromagnet 2 produces very strong magnetic force, make it tightly be adsorbed in type aircraft carrier deck 4, make carrier-borne aircraft 1 slow down and stop rapidly by the magnetic force between electromagnet 1 and type aircraft carrier deck 4 and friction force.After carrier-borne aircraft 1 stops, disconnecting electromagnet 2 power supply by carrier-borne aircraft 1 aviator, the magnetic force between battery iron 2 and type aircraft carrier deck 2 will disappear, and then be put back in the afterbody accepting rack of carrier-borne aircraft 1 by electromagnet 2 by ground crew.
As shown in Figure 2, in one embodiment, electromagnet 2 changes ferromagnetic plate 6 into, and ferromagnetic plate 6 is connected by the afterbody of rope 3 with carrier-borne aircraft 1, and can be rotated in the afterbody accepting rack of carrier-borne aircraft 1, controls it by aviator.The type aircraft carrier deck 4 in carrier landing region is provided with electromagnetism bar 5, and electromagnetism bar 5 connects power supply.In carrier landing process, when it aligns with type aircraft carrier deck 4, aviator controls to put down ferromagnetic plate 6, ground crew opens the power supply of electromagnetism bar 5 simultaneously, now electromagnetism bar 5 produces very strong magnetic force, it is made tightly to adsorb ferromagnetic plate 6, carrier-borne aircraft 1 is made to slow down and stop rapidly by the magnetic force between ferromagnetic plate 6 and electromagnetism bar 5 and friction force, carrier-borne aircraft 1 disconnects electromagnetism bar 5 power supply by ground crew after stopping, magnetic force between battery iron 5 and ferromagnetic plate 6 will disappear, and then be put back in the afterbody accepting rack of carrier-borne aircraft 1 by ferromagnetic plate 6 by ground crew.
As shown in Figure 3, in another embodiment, electromagnet 2 is connected by the afterbody of rope 3 with carrier-borne aircraft 1, and can be placed in the afterbody accepting rack of carrier-borne aircraft 1, electromagnet 2 is connected with the power supply of carrier-borne aircraft 1 simultaneously, and power control switch is arranged in driving compartment, is controlled by aviator.The type aircraft carrier deck 4 in carrier landing region is provided with electromagnetism bar 5, and electromagnetism bar 5 connects power supply, and the electromagnet 2 be arranged on carrier-borne aircraft 1 is contrary with the polarity that type aircraft carrier deck 4 electromagnetism bar 5 produces.In carrier landing process, when it aligns with type aircraft carrier deck 4, aviator controls to put down electromagnet 2 and the power supply opening electromagnet 2, and now electromagnet 2 produces magnetic force; Meanwhile, ground crew opens the power supply of electromagnetism bar 5, and now electromagnetism bar 5 produces magnetic force, and there is a natural attraction between the sexes with electromagnetism bar 5 for electromagnet 2, and generation magnetic force and friction force make carrier-borne aircraft 1 slow down and stop rapidly.After carrier-borne aircraft 1 stops, disconnecting electromagnet 2 power supply by carrier-borne aircraft 1 aviator, disconnect electromagnetism bar 5 power supply by ground crew, the magnetic force between electromagnetism bar 5 and electromagnet 2 will disappear, and then be put back in the afterbody accepting rack of carrier-borne aircraft 1 by electromagnet 2 by ground crew.
In the various embodiments described above, by changing electromagnet 2 and electromagnetism bar 5 power supply voltage and electric current, the adjustment of magnetic force size can be realized, to meet different warship needs.
The above is only preferred implementation of the present utility model; should be understood that; for those skilled in the art, can also make some improvement under the prerequisite not departing from the utility model principle, these improvement also should be considered as protection domain of the present utility model.
Claims (5)
1. a carrier-borne aircraft landing electromagnetic damping system, is characterized in that: comprise be arranged on carrier-borne aircraft afterbody can and type aircraft carrier deck between produce and adsorb and form the electromagnetic damping block rubbed, described electromagnetic damping block is connected with carrier-borne aircraft by rope.
2. carrier-borne aircraft landing electromagnetic damping system according to claim 1, it is characterized in that, described electromagnetic damping block is electromagnet, and described electromagnet connects carrier-borne aircraft power supply.
3. carrier-borne aircraft according to claim 2 landing electromagnetic damping system, it is characterized in that: described type aircraft carrier deck is provided with electromagnetism bar, described electromagnetism bar connects power supply, and the electromagnet polarity on described electromagnetism bar and carrier-borne aircraft is different.
4. a kind of carrier-borne aircraft landing electromagnetic damping system according to claim 1, is characterized in that: described electromagnetic damping block is ferromagnetic plate.
5. carrier-borne aircraft landing electromagnetic damping system according to claim 4, it is characterized in that: described type aircraft carrier deck is provided with electromagnetism bar, described electromagnetism bar connects power supply.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520407600.XU CN204776064U (en) | 2015-06-15 | 2015-06-15 | Carrier -borne aircraft descending electromagnetic damping system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520407600.XU CN204776064U (en) | 2015-06-15 | 2015-06-15 | Carrier -borne aircraft descending electromagnetic damping system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204776064U true CN204776064U (en) | 2015-11-18 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520407600.XU Expired - Fee Related CN204776064U (en) | 2015-06-15 | 2015-06-15 | Carrier -borne aircraft descending electromagnetic damping system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204776064U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104960671A (en) * | 2015-06-15 | 2015-10-07 | 南京航空航天大学 | Landing electromagnetic damping system for shipboard aircraft |
| CN106043727A (en) * | 2016-06-17 | 2016-10-26 | 哈尔滨工业大学 | Linear electromagnetic arresting device for aircraft carrier landing or aircraft landing |
-
2015
- 2015-06-15 CN CN201520407600.XU patent/CN204776064U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104960671A (en) * | 2015-06-15 | 2015-10-07 | 南京航空航天大学 | Landing electromagnetic damping system for shipboard aircraft |
| CN106043727A (en) * | 2016-06-17 | 2016-10-26 | 哈尔滨工业大学 | Linear electromagnetic arresting device for aircraft carrier landing or aircraft landing |
| CN106043727B (en) * | 2016-06-17 | 2018-03-16 | 哈尔滨工业大学 | Aircraft warship or landing linear electromagnetic arresting gear |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 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: 20151118 Termination date: 20180615 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |