CN218600400U - Ice breaking bomb used for emergency rescue and capable of being carried by unmanned aerial vehicle - Google Patents
Ice breaking bomb used for emergency rescue and capable of being carried by unmanned aerial vehicle Download PDFInfo
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- CN218600400U CN218600400U CN202222961495.7U CN202222961495U CN218600400U CN 218600400 U CN218600400 U CN 218600400U CN 202222961495 U CN202222961495 U CN 202222961495U CN 218600400 U CN218600400 U CN 218600400U
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Abstract
The utility model provides an ice breaking bomb that is used for emergency rescue can unmanned aerial vehicle to carry on relates to an emergency rescue relief technical field. The utility model discloses an including the warhead, projectile shell and afterbody structure, be provided with CO2 liquid storage pot and ignition on the projectile shell, the CO2 liquid storage pot sets up the inside at the projectile shell, ignition sets up the top at the projectile shell, and ignition is including filling the dress head, the heating tube, the electron fuze, cut the section and let out the ability strip, heating tube and electron fuze set up in CO2 liquid storage pot, and the electron fuze sets up the bottom at the heating tube, fill the dress head setting on the top of projectile shell, it is provided with the resistance core on the dress head to fill, be provided with the let out ability strip on the CO2 liquid storage pot, it cuts the section to be provided with on the projectile shell. The utility model discloses the phenomenon of icing appears in the harbour sea water winter, when leading to the unable trip of boats and ships, controls unmanned aerial vehicle and carry on the shell that opens ice, opens ice through gravity action shell that opens ice invasion ice sheet, improves the security and also pollution abatement.
Description
Technical Field
The utility model relates to an emergency rescue and disaster relief technical field especially relates to an ice breaking bullet that can unmanned aerial vehicle carry on for emergency rescue.
Background
The phenomenon of freezing of large-scale sea ice occurs in coastal ports of Liaoning province every winter, so that ships cannot go out, and huge economic loss is caused. At the present stage, modes such as an ice melting method, an icebreaker ice breaking method, a missile ice breaking method, an explosion ice breaking method and the like are adopted to solve the problem of sea ice freezing, and the ice melting method has advantages and disadvantages and easily causes environmental pollution; the icebreaker is limited by terrain factors for ice breaking, and the operation safety factor is low; the aerobomb ice breaking method has high cost and is not beneficial to large-scale application; the blasting ice breaking cost is low, the operation is flexible, but the safety is low due to the fact that the blasting ice breaking cost is too close to a building when sea ice at a port is processed.
According to the limitation of above-mentioned traditional ice breaking mode, propose and utilize unmanned aerial vehicle to carry on icebreaking shell and carry out the bullet and open ice. Liquid CO is filled in the ice breaking bomb 2 The heating tube is electrified through remote control to release a large amount of heat energy, and liquid CO is utilized 2 The shock wave generated instantaneously by the phase-change explosion can quickly break ice, and the flying pieces and CO generated by the explosion of ice-breaking bomb 2 The environmental pollution caused by the release of the active carbon is in a controllable state. Unmanned aerial vehicle has the characteristics that suitability and flexibility are stronger, and the image technique cooperation that its machine carried opens ice bullet and carries out the operation, information such as the freezing scope of distinguishable coastal harbor department and protected building, arranges the scheme of throwing the bullet and opening ice fast, can solve that the danger coefficient of opening ice is big, topography and weather are limited and practical problems such as environmental pollution, high-efficient CO that utilizes 2 To carry out emergencyAnd (5) rescue operation.
SUMMERY OF THE UTILITY MODEL
To the weak point that exists in the above-mentioned problem, the utility model provides a but ice breaking bullet that unmanned aerial vehicle carried on for emergency rescue makes it appear icing phenomenon in port sea water winter, when leading to the unable trip of boats and ships, controls unmanned aerial vehicle and carries on ice breaking bullet, opens ice through the ice breaking bullet invasion ice sheet of action of gravity, improves the security and also pollution abatement.
In order to solve the problem, the utility model provides a but ice breaking bullet that unmanned aerial vehicle carried on for emergency rescue, including warhead, projectile body shell and afterbody structure, the bottom of projectile body shell sets up the warhead, the top of projectile body shell is provided with the afterbody structure, wherein, be provided with CO on the projectile body shell 2 A liquid storage tank and an igniter, the CO 2 The liquid storage pot sets up the inside of projectile body shell, ignition sets up the top of projectile body shell, and ignition includes filling head, heating tube, electron detonator, shear slice and earial drainage strip, the heating tube with the electron detonator setting is in CO 2 In the liquid storage tank, the electronic fuse is arranged at the bottom end of the heating tube, the filling head is arranged at the top end of the shell, a resistor core is arranged on the filling head, and the CO is 2 An energy release strip is arranged on the liquid storage tank, and a shear slice is arranged on the shell of the bullet body.
Preferably, the energy release strip comprises a first energy release strip and a second energy release strip, and the first energy release strip is arranged on the CO 2 The left side of the liquid storage tank, the second energy release strip is arranged on the CO 2 The right side of liquid storage pot, it includes first shearing section and second shearing section to cut the section, first shearing section sets up the left side of projectile body shell, the second shearing section sets up the right side of projectile body shell, first shearing section with first earning strip corresponds the setting, the second shearing section with second earning strip corresponds the setting.
Preferably, still include sealed the pad, sealed pad includes first sealed pad and second sealed pad, first shearing piece passes through first sealed pad with the elastomer housing is connected, second shearing piece passes through the second sealed pad with the elastomer housing is connected.
Preferably, the tail structure is a tail fin for stabilizing the flight of the projectile body, the tail fin comprises a first tail fin, a second tail fin, a third tail fin and a fourth tail fin, and the first tail fin, the second tail fin, the third tail fin and the fourth tail fin are vertical structures.
Compared with the prior art, the utility model has the advantages of it is following:
1. the utility model provides an utilize unmanned aerial vehicle to carry on emergency rescue equipment and application method of icebreaking bullet, the coastal harbour all can appear extensive sea ice every winter and freeze the phenomenon, control unmanned aerial vehicle and carry on icebreaking bullet, through the impact of gravity free fall to icicle to and the effect of explosive shock wave and explosive gas etc. to icicle, high efficiency, safety, pollution-free completion icebreaking work.
2. The utility model discloses unmanned aerial vehicle has the stronger characteristics of suitability and flexibility, and the image technology cooperation that its machine carried opens ice the bullet and carries out the operation, and information such as the freezing scope of distinguishable coastal harbor mouth department and protected building arrange the scheme that opens ice of throwing, can solve that the danger coefficient that opens ice is big, topography and weather are limited and actual problems such as environmental pollution, and the high efficiency utilizes CO 2 And carrying out emergency rescue operation.
Drawings
Fig. 1 is a schematic structural view of an ice breaking bomb according to an embodiment of the invention;
FIG. 2 is a flow chart of an emergency rescue ice breaking method of an unmanned aerial vehicle carrying an ice breaking bomb according to an embodiment of the present invention;
fig. 3 is the utility model discloses an embodiment unmanned aerial vehicle carries on emergency rescue system of icebreaking bullet's structural block diagram.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more clearly understood, the present invention will be further described in detail with reference to the accompanying drawings and examples, which are not intended to limit the present invention.
In this embodiment, utilize unmanned aerial vehicle to carry on emergency rescue equipment of shell that opens ice, including unmanned aerial vehicle, shell that opens ice and ground control center, carry on in the unmanned aerial vehicle and put in device, real-time image device, positioner and control center system. The unmanned aerial vehicle can work independently, also can work cooperatively with the unmanned aerial vehicle according to the ice breaking working strength, a throwing device is carried in the unmanned aerial vehicle and used for throwing ice breaking bombs, and the ice breaking bombs can be respectively and independently thrown; the real-time imaging device can monitor the actual conditions of the site environment and the ice layer in real time so as to ensure the putting work; the positioning device accurately positions the projectile throwing position and the flight path; and the control center system controls the throwing device according to the positioning device, the real-time imaging device and relevant data of the throwing device, so that the throwing height and the detonation time of the icebreaking bomb are controlled.
As shown in fig. 1 to 3, the embodiment of the utility model discloses an including warhead 1, projectile shell 3 and fin 4 are connected, the warhead is the cone that has the radian, first two-thirds department is buffer structure 2, set up to solid increase warhead weight, thereby guarantee that the projectile falls relevant position and invades the ice sheet, remaining one-third department sets up buffer, in order to prevent the harm of action to the projectile inside under the gravity, the afterbody structure is four mutually perpendicular's fin 4, the fin is used for stabilizing projectile flight, guarantee that the projectile descends in the correct position. CO2 2 The liquid storage tank 9 is made of high-density alloy material and stores CO 2 At the same time, it is also the place where the phase changes, CO 2 Filling CO through a transfusion tube by using a filling device 2 ，CO 2 The liquid storage pipe is connected with the igniter. The detonating device comprises a charging head 5, a heating tube 8, an electronic fuse 7, a sealing gasket 12, a shearing sheet 11 and an energy release strip 10. The filling head is provided with a resistance core 6 for conducting the detonation current. The heating tube 8 is used for heating liquid CO 2 The heating tube has special chemical composition and can generate heat under extremely low current, thereby enabling CO to be generated 2 The liquid state is converted into the supercritical state. An electronic fuse 7 controls the resistive core 6 on the filling head. Shear blade 11 and gasket 12 in liquid CO 2 The sealing function is realized before the phase change, when the detonating device is electrified and detonated, the thickness of the shearing sheet 11 controls the detonation force during the detonationSize. The energy release strip 10 is made of high-density alloy material and is high-pressure CO 2 And in a gas release channel, the detonating device is controlled by a ground control center, and when the detonating device invades a corresponding position, the detonator is excited, so that current is conducted. Before ice breaking, filling liquid CO into the liquid storage pipe by filling equipment 2 Heating tube 8 for liquid CO 2 Heating is carried out, CO 2 The phase change occurs, the volume is rapidly increased, the energy is increased and then breaks the energy discharging strip, and the energy is released from the side wall at a high speed, so that the ice breaking effect is achieved.
In this embodiment, a method for using an ice breaking bomb for emergency rescue that can be carried by an unmanned aerial vehicle includes the following steps:
1) The method comprises the steps that large-scale sea ice freezing phenomenon occurs in coastal ports, an unmanned aerial vehicle real-time image system surveys the site environment before ice breaking operation is carried out, an ice breaking working scheme is designed according to the freezing degree of an ice layer, and it is determined that liquid CO is filled in ice breaking bullets 2 Weight, the bullet quantity of opening ice and the position isoparametric of opening ice if the condition of freezing is comparatively serious, the operation of opening ice is accomplished to multiplicable unmanned aerial vehicle quantity.
2) Filling liquid CO into the elastomer by using filling equipment 2 And loading the ice breaking bomb into the corresponding position of the unmanned aerial vehicle, and checking the unmanned aerial vehicle system, the ice breaking bomb and the ground control center.
3) According to the working scheme of ice breaking, the unmanned aerial vehicle can take off without obstacles, and when the unmanned aerial vehicle reaches an accurate position, the unmanned aerial vehicle can carry out the bomb-throwing operation and activate the detonating device.
4) And after the explosion is confirmed, confirming the ice breaking condition by using the unmanned aerial vehicle, finishing the ice breaking operation if the ice breaking is complete, and performing the ice breaking operation again according to the field condition if the ice breaking is incomplete.
Example 1:
in the middle 12 th month of the Yingkou port, the icing period is in, the thickness of frozen seawater is about 15cm, the ship cannot normally run, and the unmanned aerial vehicle is adopted to carry ice breaking bombs for ice breaking.
The specific process comprises the following steps:
1) Before ice breaking operation is carried out, the real-time image system of the unmanned aerial vehicle surveys the site environment, and an ice breaking working scheme is designed according to the freezing degree of an ice layer to ensureLiquid CO filled in ice breaking bomb 2 Weight, number of icebreaking bullets, icebreaking position and the like.
2) Filling liquid CO into the elastomer by using filling equipment 2 And the ice breaking bomb is loaded into the corresponding position of the unmanned aerial vehicle, and the unmanned aerial vehicle system, the ice breaking bomb and the ground control center are checked.
3) According to the working scheme of ice breaking, the unmanned aerial vehicle can take off without obstacles, and when the unmanned aerial vehicle reaches an accurate position, the unmanned aerial vehicle can carry out the bomb-throwing operation and activate the detonating device.
4) And after the explosion is confirmed, the unmanned aerial vehicle is used for confirming the ice breaking condition, if the ice is completely broken, the ice breaking operation is finished, and if the ice is not completely broken, the unmanned aerial vehicle is operated again to break the ice according to the field condition.
Example 2:
the great-lian changxing island port is difficult to drive a transport ship due to the fact that the air temperature suddenly drops and enters the icing period, and a large unmanned aerial vehicle is adopted to put liquid carbon dioxide in the port to blast and break ice.
The specific process comprises the following steps:
1) Before ice breaking operation is carried out, an unmanned aerial vehicle real-time image system surveys the field environment, an ice breaking working scheme is designed according to the freezing degree of an ice layer, and it is determined that an ice breaking bomb is filled with liquid CO 2 Weight, number of icebreaking bullets, and icebreaking position.
2) Filling liquid CO into the elastomer by using filling equipment 2 And the ice breaking bomb is loaded into the corresponding position of the unmanned aerial vehicle, and the unmanned aerial vehicle system, the ice breaking bomb and the ground control center are checked.
3) According to the working scheme of ice breaking, the unmanned aerial vehicle can take off without obstacles, and when the unmanned aerial vehicle reaches an accurate position, the unmanned aerial vehicle can carry out the bomb-throwing operation and activate the detonating device.
4) And after the explosion is confirmed, confirming the ice breaking condition by using the unmanned aerial vehicle, finishing the ice breaking operation if the ice breaking is complete, and performing the ice breaking operation again according to the field condition if the ice breaking is incomplete.
Example 3:
the port of Jinzhou is influenced by icing of the port of the Bohai sea area, freezing disasters are serious, and an unmanned aerial vehicle is adopted to carry an ice breaking bomb to break ice.
1) Before ice breaking operation is carried out, an unmanned aerial vehicle real-time image system surveys the field environment, an ice breaking working scheme is designed according to the freezing degree of an ice layer, and it is determined that liquid CO is filled in an ice breaking bomb 2 Weight, number of icebreaking bullets, icebreaking position and the like.
2) Filling liquid CO into the elastomer by using filling equipment 2 And loading the ice breaking bomb into the corresponding position of the unmanned aerial vehicle, and checking the unmanned aerial vehicle system, the ice breaking bomb and the ground control center.
3) According to the working scheme of ice breaking, the unmanned aerial vehicle can take off without obstacles, and when the unmanned aerial vehicle reaches an accurate position, the unmanned aerial vehicle can carry out the bomb-throwing operation and activate the detonating device.
4) And after the explosion is confirmed, confirming the ice breaking condition by using the unmanned aerial vehicle, finishing the ice breaking operation if the ice breaking is complete, and performing the ice breaking operation again according to the field condition if the ice breaking is incomplete.
Although embodiments of the present invention have been shown and described, it is understood that the above embodiments are exemplary and should not be construed as limiting the present invention, and that variations, modifications, substitutions and alterations can be made to the above embodiments by those of ordinary skill in the art without departing from the scope of the present invention.
In the description of the present specification, it is to be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", "axial", "radial", "circumferential", and the like, indicate orientations or positional relationships based on those shown in the drawings, and are used merely for convenience of description and for simplicity of description, but do not indicate or imply that the device or element referred to must have a particular orientation, be constructed in a particular orientation, and be operated, and thus should not be construed as limiting the present patent application.
Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include at least one such feature. In the description of this patent application, "plurality" means at least two, e.g., two, three, etc., unless explicitly specified otherwise.
In this specification, unless expressly stated or limited otherwise, the terms "mounted," "connected," and "fixed" are to be construed broadly and may, for example, be fixedly connected, detachably connected, or integral to one another; can be mechanically or electrically connected; they may be directly connected or indirectly connected through intervening media, or they may be connected internally or in any other suitable relationship, unless expressly stated otherwise. The specific meanings of the above terms in the present specification can be understood by those of ordinary skill in the art as appropriate.
In this specification, unless explicitly stated or limited otherwise, a first feature may be "on" or "under" a second feature such that the first and second features are in direct contact, or the first and second features are in indirect contact via an intermediate. Also, a first feature "on," "over," and "above" a second feature may be directly or diagonally above the second feature, or may simply indicate that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature may be directly under or obliquely under the first feature, or may simply mean that the first feature is at a lesser elevation than the second feature.
In the description of the present specification, reference to the description of "one embodiment," "some embodiments," "an example," "a specific example," or "some examples" or the like means that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the present invention. In this specification, the schematic representations of the terms used above are not necessarily intended to refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples. Moreover, various embodiments or examples and features of various embodiments or examples described in this specification can be combined and combined by one skilled in the art without being mutually inconsistent.
While embodiments of the present invention have been shown and described, it is to be understood that they have been presented by way of example only, and not limitation, and that changes, modifications, substitutions and alterations may be made thereto by those of ordinary skill in the art without departing from the scope of the present invention.
Claims (4)
1. A but ice breaking bullet that unmanned aerial vehicle carried on for emergency rescue, including warhead, projectile body shell and afterbody structure, the bottom of projectile body shell sets up the warhead, the top of projectile body shell is provided with the afterbody structure, its characterized in that, be provided with CO on the projectile body shell 2 A liquid storage tank and an igniter, the CO 2 The liquid storage pot sets up the inside of projectile body shell, ignition sets up the top of projectile body shell, and ignition includes filling head, heating tube, electron detonator, shear slice and earial drainage strip, the heating tube with the electron detonator setting is in CO 2 In the liquid storage tank, the electronic fuse is arranged at the bottom end of the heating tube, the filling head is arranged at the top end of the shell, a resistor core is arranged on the filling head, and the CO is 2 An energy release strip is arranged on the liquid storage tank, and a shear slice is arranged on the shell of the bullet body.
2. The unmanned aerial vehicle-mounted icebreaker for emergency rescue of claim 1, wherein the energy release strip comprises a first energy release strip and a second energy release strip, and the first energy release strip is disposed at the CO 2 The left side of the liquid storage tank, the second energy discharge strip is arranged on the CO 2 The right side of liquid storage pot, the shearing piece includes first shearing piece and second shearing piece, first shearing piece sets up the left side of projectile body shell, the second shearing piece sets up the right side of projectile body shellThe first shearing sheet and the first energy discharging strip are arranged correspondingly, and the second shearing sheet and the second energy discharging strip are arranged correspondingly.
3. The unmanned aerial vehicle-mounted icebreaker for emergency rescue of claim 2, further comprising a sealing gasket, wherein the sealing gasket comprises a first sealing gasket and a second sealing gasket, the first shear blade is connected with the projectile body housing through the first sealing gasket, and the second shear blade is connected with the projectile body housing through the second sealing gasket.
4. An unmanned aerial vehicle-mounted icebreaker for emergency rescue according to claim 3, wherein the tail structure is a tail for stabilizing the flight of the projectile body, the tail comprises a first tail, a second tail, a third tail and a fourth tail, and the first tail, the second tail, the third tail and the fourth tail are perpendicular to each other.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222961495.7U CN218600400U (en) | 2022-11-08 | 2022-11-08 | Ice breaking bomb used for emergency rescue and capable of being carried by unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222961495.7U CN218600400U (en) | 2022-11-08 | 2022-11-08 | Ice breaking bomb used for emergency rescue and capable of being carried by unmanned aerial vehicle |
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| Publication Number | Publication Date |
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| CN218600400U true CN218600400U (en) | 2023-03-10 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202222961495.7U Active CN218600400U (en) | 2022-11-08 | 2022-11-08 | Ice breaking bomb used for emergency rescue and capable of being carried by unmanned aerial vehicle |
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| CN (1) | CN218600400U (en) |
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2022
- 2022-11-08 CN CN202222961495.7U patent/CN218600400U/en active Active
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