CN118220424B - Combined multifunctional unmanned ship - Google Patents
Combined multifunctional unmanned ship Download PDFInfo
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- CN118220424B CN118220424B CN202410635447.XA CN202410635447A CN118220424B CN 118220424 B CN118220424 B CN 118220424B CN 202410635447 A CN202410635447 A CN 202410635447A CN 118220424 B CN118220424 B CN 118220424B
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- 238000012544 monitoring process Methods 0.000 claims abstract description 22
- 230000001105 regulatory effect Effects 0.000 claims description 11
- 239000007788 liquid Substances 0.000 claims description 6
- 238000000034 method Methods 0.000 claims description 3
- 238000010030 laminating Methods 0.000 claims description 2
- 230000005484 gravity Effects 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 230000006872 improvement Effects 0.000 description 3
- 238000012806 monitoring device Methods 0.000 description 3
- 230000008859 change Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 230000001681 protective effect Effects 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000003044 adaptive effect Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000011365 complex material Substances 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000012946 outsourcing Methods 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000002441 reversible effect Effects 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B35/00—Vessels or similar floating structures specially adapted for specific purposes and not otherwise provided for
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B17/00—Vessels parts, details, or accessories, not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B43/00—Improving safety of vessels, e.g. damage control, not otherwise provided for
- B63B43/02—Improving safety of vessels, e.g. damage control, not otherwise provided for reducing risk of capsizing or sinking
- B63B43/10—Improving safety of vessels, e.g. damage control, not otherwise provided for reducing risk of capsizing or sinking by improving buoyancy
- B63B43/14—Improving safety of vessels, e.g. damage control, not otherwise provided for reducing risk of capsizing or sinking by improving buoyancy using outboard floating members
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B17/00—Vessels parts, details, or accessories, not otherwise provided for
- B63B2017/0045—Caps, hoods, or the like devices for protective purposes, not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B35/00—Vessels or similar floating structures specially adapted for specific purposes and not otherwise provided for
- B63B2035/006—Unmanned surface vessels, e.g. remotely controlled
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B43/00—Improving safety of vessels, e.g. damage control, not otherwise provided for
- B63B43/02—Improving safety of vessels, e.g. damage control, not otherwise provided for reducing risk of capsizing or sinking
- B63B43/10—Improving safety of vessels, e.g. damage control, not otherwise provided for reducing risk of capsizing or sinking by improving buoyancy
- B63B43/14—Improving safety of vessels, e.g. damage control, not otherwise provided for reducing risk of capsizing or sinking by improving buoyancy using outboard floating members
- B63B2043/145—Improving safety of vessels, e.g. damage control, not otherwise provided for reducing risk of capsizing or sinking by improving buoyancy using outboard floating members pneumatic, e.g. inflatable on demand
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Geophysics And Detection Of Objects (AREA)
Abstract
The invention discloses a combined multifunctional unmanned ship, which comprises a body, wherein a propeller is arranged at the tail part of the body, an integrated circuit board for remote control is arranged on the body in an embedded manner, and a storage battery is arranged on the body in an embedded manner; the buoyancy cabin is characterized by further comprising a combined rod, wherein the combined rod is fixed on two sides of the machine body, the outer end of the combined rod is located in the combined groove, a fixing component is arranged between the combined rod and the combined groove and used for fixing the position of the combined rod, the bottom of the buoyancy cabin is connected with a limiting frame through a vertical plate, an air bag is fixed between the limiting frame and the bottom of the buoyancy cabin, and a bearing plate is connected in a cavity of the side wall of the lower half part of the hollow part of the middle of the machine body through a first elastic telescopic rod. This multi-functional unmanned ship of combination formula can install different monitoring facilities, adjusts buoyancy according to the weight of equipment simultaneously, adjusts the protection area according to the size of equipment.
Description
Technical Field
The invention relates to the technical field of unmanned ships, in particular to a combined multifunctional unmanned ship.
Background
With the development of remote control technology, the ocean monitoring means using unmanned ship as carrier is widely used, carries various monitoring sensors and equipment on unmanned ship to realize monitoring to the direction such as environment, quality of water of ocean, have the effect such as improvement monitoring effect, the loaded down with trivial details degree of reduction personnel follow-up monitoring and improvement monitoring security, but current unmanned ship has following problem when using:
The existing unmanned ship is mainly produced by binding various monitoring sensors and equipment with the unmanned ship when leaving the factory, the mode can improve the integral integrity, but when monitoring for different purposes is carried out on marine environments, different types of unmanned ships are generally needed, the aim of combined multifunctional monitoring is inconvenient to achieve through a single type of unmanned ship, so that a plurality of types of unmanned ships are needed to meet basic monitoring demands, resource waste is caused, meanwhile, the unmanned ship and various monitoring sensors and equipment are adaptively processed, complex material processing steps are involved, economic benefits are influenced, further, stable buoyancy and equipment impact protection are needed to be considered, the change of marine storms is easy to cause impact damage on the monitoring sensors and equipment, and service life is influenced.
Aiming at the problems, innovative design is urgently needed on the basis of the original unmanned ship.
Disclosure of Invention
The invention aims to provide a combined multifunctional unmanned ship, which aims to solve the problems that the prior art provides the existing unmanned ship, the combined multifunctional monitoring is inconvenient to realize through a single unmanned ship, and stable buoyancy and equipment impact protection are required to be considered.
In order to achieve the above purpose, the present invention provides the following technical solutions: the combined multifunctional unmanned ship comprises a body, wherein a propeller is arranged at the tail part of the body, an integrated circuit board for remote control is arranged on the body in an embedded manner, and a storage battery is arranged on the body in an embedded manner;
The buoyancy cabin is characterized by further comprising a combined rod, wherein the combined rod is fixed on two sides of the machine body, the outer end of the combined rod is positioned in the combined groove, the combined groove is formed in the top of the buoyancy cabin, a fixing component is arranged between the combined rod and the combined groove and used for fixing the position of the combined rod, the bottom of the buoyancy cabin is connected with a limiting frame through a vertical plate, an air bag is fixed between the limiting frame and the bottom of the buoyancy cabin, a bearing plate is connected in a cavity of the side wall of the lower half part of the hollow part of the middle part of the machine body through a first elastic telescopic rod, an inflation component is arranged between the bearing plate and the combined rod and the buoyancy cabin, and the inflation component is used for inflating the air bag according to the weight of loaded monitoring equipment;
The first screw rod, the lateral wall cavity of the hollow department in fuselage middle part is installed in first screw rod lateral rotation, and the thread bush is equipped with the clamping lever on the first screw rod, first screw rod is connected with the regulating spindle through the belt, and the embedded rotation of regulating spindle is installed in the fuselage to the outer end of regulating spindle is provided with the knob, the middle part of regulating spindle is connected with the second screw rod through the awl tooth group, and the second screw rod rotates and sets up in the movable inslot, and the movable groove is seted up in fuselage top front end position department, the thread bush is equipped with main guard plate on the second screw rod, and main guard plate both ends are embedded laminating slidable mounting has vice guard plate, be provided with the guard region adjustment subassembly between the top of vice guard plate and fuselage, and the guard region adjustment subassembly is used for adjusting the extension length of vice guard plate according to the position of main guard plate.
Preferably, the fixing assembly comprises a fixing head, the fixing head is arranged in a side wall cavity of the combination groove in an embedded elastic sliding mode through a first spring, the outer end of the fixing head is located in the fixing groove, and the fixing groove is formed in the side face of the combination rod.
Preferably, the top of the outer end of the fixing head is designed into an inclined plane structure, the outer end of the fixing head is in concave-convex fit with the fixing groove, and the top of the inner end of the fixing head is designed into a vertical structure to extend out of the top of the buoyancy cabin.
Preferably, through holes distributed in an array are formed in the top of the limiting frame, two limiting frames are symmetrically arranged at the bottom of the vertical plate, and the width of each limiting frame is larger than the initial width of the air bag.
Preferably, the inflation assembly comprises a first oil cavity, the first oil cavity is formed in the machine body, a first piston rod is arranged in the first oil cavity, one end of the first piston rod is connected with the bearing plate, the first oil cavity is connected with a second oil cavity through a pipeline, the second oil cavity is formed in the outer end of the combined rod, the second oil cavity is connected with a second piston rod through a second spring, the bottom of the second piston rod penetrates through the combined rod to be abutted to be provided with an engineering piece, the top of the engineering piece is located in the combined groove, the bottom of the engineering piece is located in the movable cavity, the movable cavity is formed in the buoyancy cabin, a second elastic telescopic rod is connected between the bottom of the engineering piece and the bottom of the movable cavity, a third piston rod is fixed at the bottom of the engineering piece, the bottom of the third piston rod is located in the inflator, and the inflator is fixed at the bottom of the movable cavity, and the inflator is connected with an inflation inlet of the air bag.
Preferably, the top rod piece of the first piston rod is designed to be in a 匚 -shaped structure, and the moving direction of the first piston rod is the same as that of the second piston rod.
Preferably, two clamping rods are symmetrically arranged at the hollow part of the middle part of the machine body, the clamping rods are in fit sliding in the machine body through a first screw rod, and the section of each clamping rod is designed to be of a T-shaped structure.
Preferably, the bottom of the main protection plate is designed to be in a convex structure and is in fit sliding in the movable groove through the second screw, and the overlooking section of the main protection plate is designed to be in a V-shaped structure.
Preferably, the protection area adjusting assembly comprises a toothed roller, the toothed roller is installed in the main protection plate in an embedded mode, a gear is connected to the bottom of the toothed roller, a rack is meshed with the inner side of the gear, the rack is fixed in an adjusting groove, and the adjusting groove is formed in the top of the machine body.
Preferably, the toothed roller is meshed with the outer serrated area of the auxiliary protection plate, the inclination angle of the auxiliary protection plate is consistent with that of the main protection plate, and the bottom of the auxiliary protection plate and the bottom of the main protection plate are in the same horizontal plane.
Compared with the prior art, the invention has the beneficial effects that:
1. According to the invention, different outsourcing monitoring devices can be placed in the hollow part of the middle part of the fuselage for positioning and clamping fixation, the unmanned ship can meet the monitoring requirements of different functions, special customization is not required according to various different monitoring functions, the processing cost is reduced, meanwhile, an inflation assembly is matched, the air bag is inflated by utilizing the gravity of the device, so that the deployment width of the air bag is adaptive to the gravity of the device, the unmanned ship can be ensured to have stable draft on the basis of being suitable for monitoring devices of different specifications, the stability of the unmanned ship in advancing on the water surface is improved on the one hand, the stable debugging of the monitoring device is maintained on the other hand, the change of the draft is not required to be considered in the debugging and using process, the use efficiency is further improved, and the unmanned ship has good practicability;
2. According to the invention, the two clamping rods can be driven to clamp and stabilize the equipment through rotating the adjusting shaft, meanwhile, the positions of the main protection plates can be synchronously adjusted, and the positions of the auxiliary protection plates are adjusted in real time by matching with the protection area adjusting assembly, so that the main protection plates and the auxiliary protection plates which are designed into the V-shaped structures are in line with the setting of reducing resistance in aerodynamics, on the other hand, the fixed equipment can be protected from impact through a shielding space formed by expanding the two auxiliary protection plates at the rear end, the damage caused by wind and wave impact to the equipment is avoided, on the basis, the adjusting shaft is only required to be rotated, the extension length of the auxiliary protection plates can be adjusted in the process of clamping and fixing the equipment, so that the auxiliary protection plates and the main protection plates can be adjusted adaptively when aiming at monitoring equipment with different specifications, and the resistance can be reduced as much as possible on the basis of protecting the auxiliary protection plates, and the service time of the unmanned ship is prolonged.
Drawings
FIG. 1 is a schematic top view of the present invention;
FIG. 2 is a schematic view of the front cross-section structure of the present invention;
FIG. 3 is a schematic view of the internal structure of the buoyancy module according to the present invention;
FIG. 4 is an enlarged schematic view of the structure of FIG. 3A according to the present invention;
FIG. 5 is a schematic view of a limiting frame according to the present invention;
FIG. 6 is a schematic top view of a main shield of the present invention;
Fig. 7 is a schematic diagram showing the front sectional structure of the auxiliary guard plate of the present invention.
In the figure: 1. a body; 2. a propeller; 3. a combination rod; 4. a combination groove; 5. a buoyancy chamber; 6. a fixing assembly; 61. a first spring; 62. a fixed head; 63. a fixing groove; 7. a riser; 8. a limit frame; 9. an air bag; 10. a first elastic telescopic rod; 11. a receiving plate; 12. an inflation assembly; 121. the first oil liquid cavity; 122. a first piston rod; 123. the second oil liquid cavity; 124. a second spring; 125. a second piston rod; 126. a I-shaped piece; 127. a movable cavity; 128. a second elastic telescopic rod; 129. a third piston rod; 1210. an inflator; 13. a first screw; 14. a clamping rod; 15. an adjusting shaft; 16. a second screw; 17. a movable groove; 18. a main protection plate; 19. an auxiliary protection plate; 20. a protective area adjustment assembly; 201. a tooth roller; 202. a gear; 203. a rack; 204. the groove is adjusted.
Detailed Description
The following description of the embodiments of the present invention will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present invention, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
Referring to fig. 1 to 7, the present invention provides a technical solution: the multifunctional unmanned combined ship comprises a body 1, a propeller 2, a combined rod 3, a combined groove 4, a buoyancy cabin 5, a fixed component 6, a first spring 61, a fixed head 62, a fixed groove 63, a vertical plate 7, a limiting frame 8, an air bag 9, a first elastic telescopic rod 10, a bearing plate 11, an inflation component 12, a first oil cavity 121, a first piston rod 122, a second oil cavity 123, a second spring 124, a second piston rod 125, an I-shaped piece 126, a movable cavity 127, a second elastic telescopic rod 128, a third piston rod 129, an inflator 1210, a first screw 13, a clamping rod 14, an adjusting shaft 15, a second screw 16, a movable groove 17, a main protection plate 18, an auxiliary protection plate 19, a protection area adjusting component 20, a tooth roller 201, a gear 202, a rack 203 and an adjusting groove 204.
Embodiment one: referring to fig. 1 to 5, a propeller 2 is mounted at the tail of a body 1, an integrated circuit board for remote control is mounted on the body 1 in an embedded manner, and a storage battery is mounted on the body 1 in an embedded manner; the combined rod 3 is fixed on two sides of the machine body 1, the outer end of the combined rod 3 is positioned in the combined groove 4, the combined groove 4 is formed in the top of the buoyancy cabin 5, a fixing component 6 is arranged between the combined rod 3 and the combined groove 4, the fixing component 6 is used for fixing the position of the combined rod 3, the bottom of the buoyancy cabin 5 is connected with a limiting frame 8 through a vertical plate 7, an air bag 9 is fixed between the limiting frame 8 and the bottom of the buoyancy cabin 5, a bearing plate 11 is connected in a cavity of the side wall of the lower half part of the hollow part of the middle part of the machine body 1 through a first elastic telescopic rod 10, an inflation component 12 is arranged between the bearing plate 11 and the combined rod 3 and the buoyancy cabin 5, the inflation component 12 is used for inflating the air bag 9 according to the weight of loaded monitoring equipment, when the unmanned ship is put into water, the unmanned ship is remotely operated through a carried remote control integrated circuit board, and the use effect of the air bag 9 can be improved through a hole structure arranged on the limiting frame 8;
The fixing assembly 6 comprises a fixing head 62, the fixing head 62 is embedded and elastically slidably mounted in a side wall cavity of the combination groove 4 through a first spring 61, the outer end of the fixing head 62 is positioned in a fixing groove 63, and the fixing groove 63 is formed in the side face of the combination rod 3; the top of the outer end of the fixed head 62 is designed into an inclined surface structure, the outer end of the fixed head 62 is in concave-convex fit with the fixed groove 63, and the top of the inner end of the fixed head 62 is designed into a vertical structure to extend out of the top of the buoyancy chamber 5; the top of the limiting frame 8 is provided with through holes distributed in an array, two limiting frames 8 are symmetrically arranged at the bottom of the vertical plate 7, and the width of the limiting frame 8 is larger than the initial width of the air bag 9; the inflation assembly 12 comprises a first oil cavity 121, the first oil cavity 121 is arranged in the machine body 1, a first piston rod 122 is arranged in the first oil cavity 121, one end of the first piston rod 122 is connected with the bearing plate 11, the first oil cavity 121 is connected with a second oil cavity 123 through a pipeline, the second oil cavity 123 is arranged in the outer end of the combined rod 3, the second oil cavity 123 is connected with a second piston rod 125 through a second spring 124, the bottom of the second piston rod 125 penetrates through the combined rod 3 to be abutted against an engineering piece 126, the top of the engineering piece 126 is positioned in the combined groove 4, the bottom of the engineering piece 126 is positioned in a movable cavity 127, the movable cavity 127 is arranged in the buoyancy chamber 5, a second elastic telescopic rod 128 is connected between the bottom of the engineering piece 126 and the bottom of the movable cavity 127, the bottom of the engineering piece 126 is fixedly provided with a third piston rod 129, the bottom of the third piston rod 129 is positioned in an inflator 1210, the inflator is fixedly arranged at the bottom of the movable cavity 127, and the inflator 1210 is connected with an inflation port 1210 of the airbag 9; the rod piece at the top of the first piston rod 122 is designed to be in a 匚 -shaped structure, and the moving direction of the first piston rod 122 and the moving direction of the second piston rod 125 are the same;
The monitoring equipment with the corresponding sensor is placed on the bearing plate 11, and the air bag 9 can be inflated through the inflation assembly 12, so that the air bag 9 can be adaptively adjusted according to the gravity of the equipment, and the unmanned ship is guaranteed to have stable buoyancy.
Embodiment two: on the basis of the first embodiment, referring to fig. 1 and 6-7, a first screw rod 13 is transversely and rotatably installed in a side wall cavity at a hollow part of the machine body 1, a clamping rod 14 is sleeved on the first screw rod 13 in a threaded manner, the first screw rod 13 is connected with an adjusting shaft 15 through a belt, the adjusting shaft 15 is rotatably installed in the machine body 1 in an embedded manner, a knob is arranged at the outer end of the adjusting shaft 15, the middle part of the adjusting shaft 15 is connected with a second screw rod 16 through a bevel gear group, the second screw rod 16 is rotatably arranged in a movable groove 17, the movable groove 17 is formed at the front end position of the top of the machine body 1, a main protection plate 18 is sleeved on the second screw rod 16 in a threaded manner, two ends of the main protection plate 18 are in embedded fit and sliding manner, a protection area adjusting component 20 is arranged between the auxiliary protection plate 19 and the top of the machine body 1, and the protection area adjusting component 20 is used for adjusting the extension length of the auxiliary protection plate 19 according to the position of the main protection plate 18;
two clamping rods 14 are symmetrically arranged at the hollow part of the middle part of the machine body 1, the clamping rods 14 slide in an attaching way in the machine body 1 through a first screw rod 13, and the section of each clamping rod 14 is designed to be of a T-shaped structure; the bottom of the main protection plate 18 is designed to be a convex structure which is in fit sliding in the movable groove 17 through the second screw 16, and the overlooking section of the main protection plate 18 is designed to be a V-shaped structure; the protection area adjusting assembly 20 comprises a toothed roller 201, the toothed roller 201 is installed in the main protection plate 18 in an embedded rotating mode, a gear 202 is connected to the bottom of the toothed roller 201, a rack 203 is meshed with the inner side of the gear 202, the rack 203 is fixed in an adjusting groove 204, and the adjusting groove 204 is formed in the top of the machine body 1; the toothed roller 201 is meshed with the outer serrated area of the auxiliary protection plate 19, the inclination angle of the auxiliary protection plate 19 is consistent with that of the main protection plate 18, and the bottom of the auxiliary protection plate 19 is in the same horizontal plane with that of the main protection plate 18;
The adjusting shaft 15 is rotated to drive the clamping rod 14 to move to clamp and fix equipment, and the positions and the extending lengths of the main protection plate 18 and the auxiliary protection plate 19 are adjusted to prevent impact protection for equipment with different widths.
Working principle: when the combined multifunctional unmanned ship is used, as shown in fig. 1-7, the combined rod 3 is inserted into the combined groove 4, the inclined surface at the top of the fixed head 62 is stressed and contracted, the combined rod 3 and the buoyancy cabin 5 are combined and fixed by being matched with the first spring 61 to be finally clamped into the fixed groove 63, then the corresponding monitoring equipment is placed into the hollow part in the middle of the machine body 1, the equipment extrudes the bearing plate 11, the first elastic telescopic rod 10 is matched for shrinkage supporting, the bearing plate 11 moves downwards by a corresponding distance according to the weight of the equipment, the bearing plate 11 drives the first piston rod 122 to move downwards in the first oil cavity 121, the second piston rod 125 can be driven to move downwards in the second oil cavity 123, the second piston rod 125 pushes the workpiece 126 to move downwards in the movable cavity 127, the third piston rod 129 is pushed to move downwards in the vertical cylinder 1210, the air bag 9 is inflated, the air bag 9 is transversely expanded under the action of the vertical plate 7 and the limit frame 8, and the corresponding expansion of the air bag 9 is realized according to the gravity of the equipment, and the unmanned ship can keep stable draft under water;
Then rotate the regulating spindle 15, the regulating spindle 15 drives the first screw 13 to rotate, drive two clamp levers 14 to move relatively, clamp the operation to the apparatus, the regulating spindle 15 drives the second screw 16 to rotate at the same time, can drive the main guard plate 18 to slide in the movable groove 17, the main guard plate 18 moves to the apparatus direction, the bottom gear 202 of the toothed roller 201 meshes with rack 203 at this moment, can drive the toothed roller 201 to rotate, by the external engagement of toothed roller 201 and auxiliary guard plate 19, make the main guard plate 18 move inwards while moving inwards, the auxiliary guard plate 19 moves inwards at the edge of the main guard plate 18 too, and then clamp and fasten while carrying on the timing to different specification apparatuses, the expansion length and protective range of main guard plate 18 and auxiliary guard plate 19 correspond to apparatus, reduce the resistance on the basis of protecting against shock to the apparatus, while dismantling, according to the above-mentioned step reverse operation can, then manually pull the fixed head 62, make it disengage from fixed groove 63, can finish the whole dismantlement, reduce whole volume and space occupation, easy to carry and store.
What has not been described in detail in this specification is prior art that is well known to those skilled in the art, and in the description of the present invention, unless otherwise specified, the meaning of "a plurality" is two or more; the terms "upper," "lower," "left," "right," "inner," "outer," "front," "rear," "head," "tail," and the like are used as an orientation or positional relationship based on that shown in the drawings, merely to facilitate description of the invention and to simplify the description, and do not indicate or imply that the devices or elements referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore should not be construed as limiting the invention. Furthermore, the terms "first," "second," "third," and the like are used for descriptive purposes only and are not to be construed as indicating or implying relative importance. In the description of the present invention, it should be noted that, unless explicitly specified and limited otherwise, the terms "connected," "connected," and "connected" are to be construed broadly, and may be either fixedly connected, detachably connected, or integrally connected, for example; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium. The specific meaning of the above terms in the present invention will be understood in specific cases by those of ordinary skill in the art.
Although the present invention has been described with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described, or equivalents may be substituted for elements thereof, and any modifications, equivalents, improvements and changes may be made without departing from the spirit and principles of the present invention.
Claims (9)
1. The combined multifunctional unmanned ship comprises a body (1), wherein a propeller (2) is arranged at the tail part of the body (1), an integrated circuit board for remote control is arranged on the body (1) in an embedded manner, and a storage battery is arranged on the body (1) in an embedded manner;
The method is characterized in that: the hydraulic air pump is characterized by further comprising a combined rod (3), wherein the combined rod (3) is fixed on two sides of the machine body (1), the outer end of the combined rod (3) is positioned in the combined groove (4), the combined groove (4) is formed in the top of the buoyancy cabin (5), a fixing component (6) is arranged between the combined rod (3) and the combined groove (4), the fixing component (6) is used for fixing the position of the combined rod (3), the bottom of the buoyancy cabin (5) is connected with a limiting frame (8) through a vertical plate (7), an air bag (9) is fixed between the limiting frame (8) and the bottom of the buoyancy cabin (5), a bearing plate (11) is connected in a cavity of the lower half side wall of the hollow part of the middle of the machine body (1) through a first elastic telescopic rod (10), an inflation component (12) is arranged between the bearing plate (11) and the combined rod (3) and the buoyancy cabin (5), the inflation component (12) is used for inflating the air bag (9) according to the weight of loaded monitoring equipment, the inflation component (12) comprises a first cavity (121), the first cavity (121) is connected with the first cavity (121) and the first cavity (121) is formed in the first cavity (122), the first cavity (121) is connected with the first cavity (122) and the first cavity (122) is formed in the first cavity (121) and the piston rod (122), the first oil liquid cavity (121) is connected with the second oil liquid cavity (123) through a pipeline, the second oil liquid cavity (123) is formed in the outer end of the combined rod (3), a second piston rod (125) is connected in the second oil liquid cavity (123) through a second spring (124), the bottom of the second piston rod (125) penetrates through the combined rod (3) to be abutted against a workpiece (126), the top of the workpiece (126) is positioned in the combined groove (4), the bottom of the workpiece (126) is positioned in the movable cavity (127), the movable cavity (127) is formed in the buoyancy cabin (5), a second elastic telescopic rod (128) is connected between the bottom of the workpiece (126) and the bottom of the movable cavity (127), a third piston rod (129) is fixed at the bottom of the workpiece (126), the bottom of the third piston rod (129) is positioned in the inflator (1210), and the inflator (1210) is fixed at the bottom of the movable cavity (127), and the inflator (1210) is connected with an inflation port (9);
The utility model provides a first screw rod (13), first screw rod (13) transversely rotate and install in the lateral wall cavity of fuselage (1) middle part hollow department, and the thread bush is equipped with clamping lever (14) on first screw rod (13), first screw rod (13) are connected with regulating spindle (15) through the belt, and regulating spindle (15) embedded rotation is installed in fuselage (1) to the outer end of regulating spindle (15) is provided with the knob, the middle part of regulating spindle (15) is connected with second screw rod (16) through the awl tooth group, and second screw rod (16) rotate and set up in movable groove (17) to movable groove (17) are seted up in fuselage (1) top front end position department, the thread bush is equipped with main guard plate (18) on second screw rod (16), and main guard plate (18) both ends embedded laminating slidable mounting has vice guard plate (19), be provided with between the top of vice guard plate (19) and fuselage (1) and protect regional adjustment subassembly (20), and protect regional adjustment subassembly (20) are used for stretching out according to the position adjustment pair guard plate (19) of main guard plate (18).
2. A modular multi-functional unmanned ship according to claim 1, wherein: the fixing assembly (6) comprises a fixing head (62), the fixing head (62) is embedded and elastically slidably mounted in a side wall cavity of the combination groove (4) through a first spring (61), the outer end of the fixing head (62) is located in a fixing groove (63), and the fixing groove (63) is formed in the side face of the combination rod (3).
3. A modular multi-functional unmanned ship according to claim 2, wherein: the top of the outer end of the fixing head (62) is designed into an inclined surface structure, the outer end of the fixing head (62) is in concave-convex fit with the fixing groove (63), and the top of the inner end of the fixing head (62) is designed into a vertical structure to extend out of the top of the buoyancy cabin (5).
4. A modular multi-functional unmanned ship according to claim 1, wherein: the top of spacing frame (8) has offered the through-hole of array distribution, and spacing frame (8) are provided with two in riser (7) bottom symmetry to the width of spacing frame (8) is greater than the initial width of gasbag (9).
5. A modular multi-functional unmanned ship according to claim 1, wherein: the top rod piece of the first piston rod (122) is designed to be in a 匚 -shaped structure, and the moving direction of the first piston rod (122) is the same as that of the second piston rod (125).
6. A modular multi-functional unmanned ship according to claim 1, wherein: two clamping rods (14) are symmetrically arranged at the hollow part of the middle of the machine body (1), the clamping rods (14) are in fit sliding in the machine body (1) through first screw rods (13), and the section of each clamping rod (14) is designed to be of a T-shaped structure.
7. A modular multi-functional unmanned ship according to claim 1, wherein: the bottom of the main protection plate (18) is designed to be in a convex structure and is in fit sliding in the movable groove (17) through the second screw rod (16), and the overlooking section of the main protection plate (18) is designed to be in a V-shaped structure.
8. A modular multi-functional unmanned ship according to claim 1, wherein: the protection area adjusting assembly (20) comprises a toothed roller (201), the toothed roller (201) is installed in the main protection plate (18) in an embedded rotating mode, a gear (202) is connected to the bottom of the toothed roller (201), a rack (203) is meshed with the inner side of the gear (202), the rack (203) is fixed in an adjusting groove (204), and the adjusting groove (204) is formed in the top of the machine body (1).
9. A modular multi-functional unmanned ship according to claim 8, wherein: the toothed roller (201) is meshed with the outer serrated area of the auxiliary protection plate (19), the inclination angle of the auxiliary protection plate (19) is consistent with that of the main protection plate (18), and the bottom of the auxiliary protection plate (19) is in the same horizontal plane with the bottom of the main protection plate (18).
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| CN202410635447.XA CN118220424B (en) | 2024-05-22 | 2024-05-22 | Combined multifunctional unmanned ship |
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| US6830004B2 (en) * | 2001-04-10 | 2004-12-14 | Floatlogic, Inc. | Inflating watercraft flotation device |
| US6470818B1 (en) * | 2001-04-10 | 2002-10-29 | Float Rail, Inc. | Automatic inflating watercraft flotation device |
| US7246566B2 (en) * | 2003-11-26 | 2007-07-24 | Marion Hyper-Submersible Powerboat Design Llc | Combination surface and submersible watercraft |
| AT515558B1 (en) * | 2014-07-21 | 2015-10-15 | Heiligenmann Barbara | sailing catamaran |
| CN109505737A (en) * | 2018-11-26 | 2019-03-22 | 中国华能集团清洁能源技术研究院有限公司 | A kind of floatation type sea-borne wind power generation apparatus and its working method |
| CN114212208B (en) * | 2022-01-20 | 2022-11-25 | 北京史河科技有限公司 | Control device of rust removal robot for inner cabin of ship |
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| CN115973351A (en) * | 2023-03-21 | 2023-04-18 | 鲁东大学 | Deformable twin-hull unmanned ship |
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