CN116902157A - Movable hangar submersible - Google Patents

Movable hangar submersible Download PDF

Info

Publication number
CN116902157A
CN116902157A CN202310494470.7A CN202310494470A CN116902157A CN 116902157 A CN116902157 A CN 116902157A CN 202310494470 A CN202310494470 A CN 202310494470A CN 116902157 A CN116902157 A CN 116902157A
Authority
CN
China
Prior art keywords
fixedly connected
hangar
worm
floating cabin
buoyancy module
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN202310494470.7A
Other languages
Chinese (zh)
Inventor
陈乐春
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
JIANGSU DIGITAL EAGLE TECHNOLOGY DEVELOPMENT CO LTD
Original Assignee
JIANGSU DIGITAL EAGLE TECHNOLOGY DEVELOPMENT CO LTD
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by JIANGSU DIGITAL EAGLE TECHNOLOGY DEVELOPMENT CO LTD filed Critical JIANGSU DIGITAL EAGLE TECHNOLOGY DEVELOPMENT CO LTD
Priority to CN202310494470.7A priority Critical patent/CN116902157A/en
Publication of CN116902157A publication Critical patent/CN116902157A/en
Pending legal-status Critical Current

Links

Classifications

    • 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
    • B63B35/50—Vessels or floating structures for aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63G—OFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
    • B63G8/00—Underwater vessels, e.g. submarines; Equipment specially adapted therefor
    • B63G8/14—Control of attitude or depth
    • B63G8/22—Adjustment of buoyancy by water ballasting; Emptying equipment for ballast tanks
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H25/00—Steering; Slowing-down otherwise than by use of propulsive elements; Dynamic anchoring, i.e. positioning vessels by means of main or auxiliary propulsive elements
    • B63H25/42—Steering or dynamic anchoring by propulsive elements; Steering or dynamic anchoring by propellers used therefor only; Steering or dynamic anchoring by rudders carrying propellers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H5/00—Arrangements on vessels of propulsion elements directly acting on water
    • B63H5/07—Arrangements on vessels of propulsion elements directly acting on water of propellers
    • B63H5/08—Arrangements on vessels of propulsion elements directly acting on water of propellers of more than one propeller
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00—Ground or aircraft-carrier-deck installations
    • B64F1/02—Arresting gear; Liquid barriers
    • B64F1/025—Arresting gear; Liquid barriers using decelerating or arresting beds
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/34—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering
    • H02J7/35—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering with light sensitive cells

Abstract

The invention discloses a movable hangar submersible vehicle, which is a ship striking device with low cost and high efficiency. The intelligent floating cabin comprises a machine base and a floating cabin, wherein the bottom of the machine base is fixedly connected to the top of the floating cabin, the top of the machine base is provided with a solar photovoltaic plate, two ends of the machine base are rotationally connected with door plates, the top of the floating cabin is provided with a sliding rail inside the machine base, the sliding rail is provided with an unmanned aerial vehicle, the inside of the floating cabin is fixedly connected with a partition plate, the partition plate divides the inside area of the floating cabin into an upper part and a lower part, two sides of the bottom of the floating cabin are fixedly connected with sleeves, paddles are arranged inside the sleeves, a water pump is arranged on one side of the bottom of the floating cabin, and ventilation holes are formed in the top of the floating cabin. The unmanned aerial vehicle can be deployed on the sea surface, has smaller body shape and semi-submerged state, so that the part which is simultaneously positioned on water and under water is smaller, the probability of being detected can be reduced, the cost is low, and a plurality of submersible floats are deployed, so that the fight range is wider, the hit success rate is high, and the survival rate of the body is high and can be recycled.

Description

Movable hangar submersible
Technical Field
The invention relates to the field of a floating submersible, in particular to a movable hangar floating submersible, which is a device for striking enemy warships or enemy aircraft carriers with low cost and high efficiency.
Background
The current mode of striking the target aircraft carrier has the defects of mine deployment, missile launching, submarine surface ship attack and the like. For example, deployment of a mine, which is often ineffective because it cannot move; the missile is launched, because the target is moving, very accurate coordinates are needed, the target is needed to be locked by a satellite, the data given by the satellite are not instant data, the coordinate position signal of the target is required to be continuously corrected for the missile, and the guidance precision is difficult to ensure; attack of fighter plane, submarine or surface ship has the problems of high cost, high manufacturing cost and large target of the attack weapon, and extremely high outburst prevention difficulty, easy sinking and large task failure loss along with the continuous improvement of the anti-outburst prevention capability of enemy.
Disclosure of Invention
The present invention has been made in view of the above and/or problems occurring in the prior art. The invention aims to solve the technical problem of designing a hangar submersible vehicle which can be loaded with an unmanned plane for attack, reduce the probability of being detected and is a striking device with low cost and high efficiency.
In order to solve the technical problems, the invention provides the following technical scheme:
the utility model provides a portable hangar floats and dives ware, includes hangar and buoyancy module, hangar bottom fixedly connected with is at buoyancy module top, and hangar top fixedly connected with solar photovoltaic board, the hangar both ends rotate and are connected with the door plant, the buoyancy module top is located the inside slide rail that is provided with of hangar, and is provided with unmanned aerial vehicle on the slide rail, the inside fixedly sealed connection of buoyancy module has a baffle, and the baffle divide into upper and lower two parts with buoyancy module inner region, buoyancy module bottom both sides fixedly connected with sleeve, and the inside paddle that is provided with of sleeve, the water pump is installed to buoyancy module bottom one side, the bleeder vent has been seted up at buoyancy module top.
As an improvement of the invention, the tail end of the sliding rail is rotatably connected to the top of the floating cabin, one side of the sliding rail is provided with the deceleration block, the tail end of the deceleration block is inserted with the fixed column, one end of the fixed column is fixedly connected with the first spring, the other end of the first spring is fixedly connected to the inner cavity of the deceleration block, and the outer end of the deceleration block is inclined.
As an improvement of the invention, the top of the floating cabin is provided with an arc groove at the top end of the sliding rail, the circle of the arc groove coincides with the position of the sliding rail, which is rotationally connected with the floating cabin, a second spring is movably connected in the arc groove, one end of the second spring is fixedly connected at the bottom of the sliding rail, two sliding rails are fixedly connected with pull ropes at the outer sides of one ends of the sliding rails, which are close to the arc grooves, the top of the floating cabin is rotationally connected with a roller at one side of the arc groove, the other end of the pull rope is wound at one side of the roller, and the tail end of the roller penetrates through the top of the floating cabin and extends into the floating cabin.
As an improvement of the invention, the top of the inner cavity of the floating cabin is fixedly connected with a first motor, the two ends of a first motor shaft are fixedly connected with connecting shafts, the two ends of each connecting shaft are fixedly connected with a first worm, one side of each first worm is connected with a first worm wheel in a meshed manner, and the top of each first worm wheel is fixedly connected with the tail end of a winding roller.
As an improvement of the invention, the two ends of the partition plate are fixedly connected with the fixed cylinder in a penetrating way, the top of the fixed cylinder is conical, the top of the fixed cylinder is communicated with the bottom of the fixed cylinder, the bottom of the fixed cylinder is fixedly connected with the fixed ring, the inside of the fixed ring is slidably connected with the connecting column, the top of the connecting column is fixedly connected with the piston, and the shape of the top of the piston is matched with that of the top of the fixed cylinder.
As an improvement of the invention, grooves are formed on the outer sides of the piston and the fixed ring, a sliding groove is formed on the inner side of the fixed ring, a sliding rod is fixedly connected to the side face of the connecting column, the section shape of the sliding rod is matched with that of the sliding groove, a buoyancy block is fixedly connected to the bottom of the connecting column, and the section diameter of the buoyancy block is larger than that of the connecting column.
As an improvement of the invention, the bottom of the inner cavity of the floating cabin is fixedly connected with the waterproof shell, the two ends of the floating cabin, which are positioned in the waterproof shell, are fixedly connected with the second motor, the shaft end of the second motor is fixedly connected with the second worm, one side of the second worm is connected with the second worm wheel in a meshed manner, the bottom end of the second worm wheel is fixedly connected with the transmission shaft, and the tail end of the transmission shaft penetrates through the bottom of the floating cabin and extends to the outer side.
As an improvement of the invention, the two ends of the sleeve are fixedly connected with the filter screen, the two ends of the inside of the sleeve are fixedly connected with the connecting frames, the rotating shaft is rotatably connected between the two connecting frames, the tail ends of the paddles are fixedly connected on the rotating shaft, the outer side of the middle of the rotating shaft is fixedly connected with the third worm wheel, one side of the third worm wheel is meshed with the third worm, and the top of the third worm is fixedly connected to the bottom of the transmission shaft.
The beneficial effects of the invention are as follows:
according to the invention, the unmanned plane can be deployed on the sea surface, has smaller body shape and is in a semi-submerged state, so that the part which is simultaneously positioned on water and under water is smaller, the probability of being detected can be reduced, the cost is low, and a plurality of submersible floats are deployed, so that the operational range is wider. Specifically:
the submersible vehicle disclosed by the invention has the advantages that one half of the submersible vehicle is in the potential water, the other half of the submersible vehicle floats on the water surface, the volume is small, the target is small, the detection on the water surface is difficult, and the detection of the enemy sonar under the water surface is also difficult. The part of the solar energy photovoltaic panel exposed on the water surface is provided with a solar energy photovoltaic panel, has a solar energy power generation function, can be deployed at any position according to requirements, such as a table sea, can be used for free airlines and can be used for 24-hour uninterrupted combat.
The invention has the advantages that the operation radius of the submersible vehicle is extremely large, the unmanned aerial vehicle base is arranged in the submersible vehicle, the precise coordinates are not needed, and the unmanned aerial vehicle can be released to attack the target as long as the submersible vehicle moves to the target 3 km or 5 km range, the operation range depends on the performance of the carried unmanned aerial vehicle, and the operation radius is extremely large; if hundreds of the devices of the present invention are deployed at one time, the entire combat area can be covered. The released unmanned plane can fly close to the target to launch the attack, and the attack success rate is greatly improved.
The invention relates to a submersible vehicle, which has the key characteristics of receiving only signals and not transmitting signals. In the process of the task, the submersible vehicle is put in a certain position, and under the normal condition, the submersible vehicle only receives signals, does not emit signals, does not expose itself, and is difficult to detect by enemies. When the satellite finds an enemy mixing warship or a certain warship, the satellite prepares a submersible vehicle near the target, the coordinate position of the target is sent to the submersible vehicle, the submersible vehicle is executed only by receiving a satellite signal command, the submersible vehicle is buried on the advancing route of the target after sailing, when the target approaches, other units send attack commands to the submersible vehicle through the satellite, the hangar of the submersible vehicle is opened, and an unmanned plane is sent to the coordinate position to perform an attack task.
The submersible vehicle can be recovered. After the attack task is successful, the unmanned aerial vehicle returns to the position of the submersible vehicle, and can be recovered and opened back to the parent port; if the attack task fails, only the unmanned aerial vehicle is lost, and the submersible can be opened back to the parent port.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings that are needed in the description of the embodiments will be briefly described below, it being obvious that the drawings in the following description are only some embodiments of the present invention, and that other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art. Wherein:
fig. 1 is a schematic structural diagram of a mobile hangar submersible according to an embodiment of the present invention;
fig. 2 is a schematic diagram of an internal structure of a hangar in a mobile hangar buoy according to an embodiment of the present invention;
FIG. 3 is a schematic view of a sliding rail portion of a mobile hangar submersible vehicle according to an embodiment of the present invention;
FIG. 4 is a schematic view of a portion of a roller in a mobile hangar submersible according to an embodiment of the present invention;
FIG. 5 is a schematic view of an internal structure of a buoyancy module in a mobile hangar submersible according to an embodiment of the present invention;
FIG. 6 is a schematic diagram of a piston and a fixed cylinder in a mobile hangar submersible according to an embodiment of the present invention;
fig. 7 is a schematic view of an internal structure of a sleeve in a mobile hangar submersible according to an embodiment of the present invention.
In the figure: 1. a hangar; 2. a solar photovoltaic panel; 3. a door panel; 4. a buoyancy chamber; 5. a filter screen; 6. unmanned plane; 7. a slide rail; 8. a deceleration block; 9. a first spring; 10. fixing the column; 11. an arc-shaped groove; 12. a second spring; 13. a pull rope; 14. a roller; 15. a first worm wheel; 16. a first worm; 17. a connecting shaft; 18. a first motor; 19. a fixed cylinder; 20. a piston; 21. a connecting column; 22. a buoyancy block; 23. a groove; 24. a fixing ring; 25. a slide bar; 26. a chute; 27. a partition plate; 28. a water pump; 29. ventilation holes; 30. a waterproof case; 31. a second motor; 32. a second worm; 33. a second worm wheel; 34. a third worm; 35. a third worm wheel; 36. a rotating shaft; 37. a paddle; 38. a connecting frame; 39. a sleeve; 40. and a transmission shaft.
Description of the embodiments
In order that the above-recited objects, features and advantages of the present invention will become more readily apparent, a more particular description of the invention will be rendered by reference to specific embodiments thereof which are illustrated in the appended drawings.
Examples
The embodiment provides a portable hangar submersible vehicle, including hangar 1 and buoyancy module 4, hangar 1 bottom fixedly connected with is at buoyancy module 4 top, and hangar 1 top fixedly connected with solar photovoltaic board 2, hangar 1 both ends rotate and are connected with door plant 3, buoyancy module 4 top is located inside slide rail 7 that is provided with of hangar 1, and be provided with unmanned aerial vehicle 6 on the slide rail 7, the inside fixed seal of buoyancy module 4 is connected with a baffle 27, and baffle 27 divide into upper and lower two parts with buoyancy module 4 inside region, buoyancy module 4 bottom both sides fixedly connected with sleeve 39, and sleeve 39 inside is provided with paddle 37, water pump 28 is installed to buoyancy module 4 bottom one side, bleeder vent 29 has been seted up at buoyancy module 4 top.
Referring to 2, 3, 4, the end of the sliding rail 7 is rotationally connected to the top of the floating cabin 4, one side of the sliding rail 7 is provided with a speed reducing block 8, the end of the speed reducing block 8 is inserted with a fixed column 10, one end of the fixed column 10 is fixedly connected with a first spring 9, the other end of the first spring 9 is fixedly connected to the inner cavity of the speed reducing block 8, the outer end of the speed reducing block 8 is in an inclined plane shape, the top of the floating cabin 4 is provided with an arc groove 11 at the top of the sliding rail 7, the circle of the arc groove 11 coincides with the position of the sliding rail 7, which is rotationally connected with the floating cabin 4, a second spring 12 is movably connected inside the arc groove 11, one end of the second spring 12 is fixedly connected to the bottom of the sliding rail 7, the outer sides of one ends of the two sliding rails 7 close to the arc grooves 11 are fixedly connected with a pull rope 13, the top of the floating cabin 4 is rotationally connected to a roller 14 at one side of the arc groove 11, and the other end of the pull rope 13 is wound on one side of the roller 14, the tail end of the roller 14 penetrates through the top of the floating cabin 4 and extends to the inside, a first motor 18 is fixedly connected to the top of the inner cavity of the floating cabin 4, the two ends of the shaft of the first motor 18 are fixedly connected with a connecting shaft 17, the two ends of the connecting shaft 17 are fixedly connected with a first worm 16, one side of the first worm 16 is connected with a first worm wheel 15 in a meshed mode, the top of the first worm wheel 15 is fixedly connected to the tail end of the roller 14, when the unmanned aerial vehicle 6 starts to execute tasks, the door plate 3 is opened, the first motor 18 is started, the first motor 18 drives the first worm 16 to rotate through the connecting shaft 17, the first worm 16 drives the first worm wheel 15 to rotate through meshing, so that the roller 14 is driven to rotate, the roller 14 winds the pull rope 13 and enables the sliding rail 7 to rotate outwards, the second spring 12 is compressed at the moment, the speed reducing block 8 is not contacted with the bottom of the unmanned aerial vehicle 6 at the moment, after the unmanned aerial vehicle 6 executes tasks, the door plate 3 returns to the hangar 1, at this time, the first motor 18 rotates reversely to drive the winding roller 14 to rotate reversely, so that the pull rope 13 is in a loose state, the elastic force of the second spring 12 enables the sliding rail 7 to reset, when the unmanned aerial vehicle 6 enters the garage, the speed is high, the bottom is contacted with the speed reducing block 8, the speed reducing block 8 compresses the first spring 9 backwards after being pressed by the unmanned aerial vehicle 6, and the speed of the unmanned aerial vehicle 6 is reduced through the plurality of speed reducing blocks 8 until the unmanned aerial vehicle stops.
Examples
The embodiment is based on the previous embodiment, and is different from the previous embodiment in that:
referring to fig. 5 and 6, both ends of a partition 27 are fixedly connected with a fixed cylinder 19 in a penetrating manner, the top of the fixed cylinder 19 is conical, the top and the bottom of the fixed cylinder 19 are communicated, the bottom of the fixed cylinder 19 is fixedly connected with a fixed ring 24, the inside of the fixed ring 24 is slidably connected with a connecting column 21, the top of the connecting column 21 is fixedly connected with a piston 20, the shape of the top of the piston 20 is matched with that of the top of the fixed cylinder 19, grooves 23 are formed on the outer sides of the piston 20 and the fixed ring 24, a sliding groove 26 is formed on the inner side of the fixed ring 24, a sliding rod 25 is fixedly connected with the side surface of the connecting column 21, the section shape of the sliding rod 25 is matched with that of the sliding groove 26, the bottom of the connecting column 21 is fixedly connected with a buoyancy block 22, and the section diameter of the buoyancy block 22 is larger than that of the connecting column 21, when the water pump 28 is started, seawater enters the buoyancy module 4 and is located in the area below the partition plate 27 when the water pump 28 pumps water, at the moment, the piston 20 is not attached to the top of the fixed cylinder 19 under the action of gravity, air is discharged from the groove 23, when the water surface passes over the buoyancy block 22, the buoyancy block 22 floats upwards and enables the piston 20 to be attached to the top of the fixed cylinder 19, at the moment, the upper and lower areas of the partition plate 27 are separated, water cannot enter the upper portion of the partition plate 27, when the submersible vehicle floats upwards at a certain height, the water pump 28 is started, the water pump 28 pumps the seawater, and meanwhile, the water surface descends to enable the buoyancy block 22 to fall under the action of gravity, at the moment, the top of the piston 20 is separated from the top of the fixed cylinder 19 again, and the upper and lower portions of the partition plate 27 are communicated, so that air pressure is balanced.
Examples
The embodiment is based on the previous embodiment, and is different from the previous embodiment in that:
referring to fig. 7, the bottom of the inner cavity of the buoyancy chamber 4 is fixedly connected with the waterproof shell 30, the buoyancy chamber 4 is located at two ends inside the waterproof shell 30 and is fixedly connected with the second motor 31, the shaft end of the second motor 31 is fixedly connected with the second worm 32, one side of the second worm 32 is in meshed connection with the second worm wheel 33, the bottom end of the second worm wheel 33 is fixedly connected with the transmission shaft 40, the tail end of the transmission shaft 40 penetrates through the bottom of the buoyancy chamber 4 and extends to the outside, the two ends of the sleeve 39 are fixedly connected with the filter screen 5, the two ends of the sleeve 39 are fixedly connected with the connecting frames 38, a rotating shaft 36 is rotatably connected between the two connecting frames 38, the tail ends of the paddles 37 are fixedly connected to the rotating shaft 36, the outer side of the middle of the rotating shaft 36 is fixedly connected with the third worm wheel 35, one side of the third worm wheel 35 is in meshed connection with the third worm 34, the top of the third worm 34 is fixedly connected to the bottom of the transmission shaft 40, the second motor 31 is started, the second motor 31 is rotated to drive the second worm wheel 32, and drives the second worm 33 to rotate through the meshing, the second worm 40 drives the third worm 34 to rotate, the third worm 35 is driven to rotate through the transmission shaft 40, the third worm 34 is meshed to drive the third worm wheel 35 to rotate, the paddles 36 to rotate, and the paddles 37 are driven to rotate, so that the paddles 37 are driven to rotate, and the paddles 37 rotate to provide power to the two linear or the two pulleys 31 through the rotation and the two linear or the rotation to move through the rotation of the rotating shafts 31.
In this embodiment, when the vehicle is sailing, the second motor 31 is started, the second motor 31 rotates to drive the second worm 32 to rotate, and the second worm wheel 33 is driven to rotate through engagement, the second worm wheel 33 drives the third worm 34 to rotate through the transmission shaft 40, the third worm 34 drives the third worm wheel 35 to rotate through engagement, so that the rotation shaft 36 drives the blade 37 to rotate, power is provided for the submersible vehicle, and linear movement or turning of the submersible vehicle is realized by controlling the rotation speeds and directions of the two second motors 31;
when the unmanned aerial vehicle 6 starts to execute a task, the door plate 3 is opened, the first motor 18 is started, the first motor 18 drives the first worm 16 to rotate through the connecting shaft 17, the first worm 16 drives the first worm wheel 15 to rotate through meshing, so that the roller 14 is driven to rotate, the roller 14 winds the pull rope 13 and enables the sliding rail 7 to rotate outwards, the second spring 12 is compressed at the moment, meanwhile, the speed reducing block 8 is not contacted with the bottom of the unmanned aerial vehicle 6, the unmanned aerial vehicle can take off at the moment, after the unmanned aerial vehicle 6 executes the task, the unmanned aerial vehicle returns to the hangar 1 through the door plate 3, at the moment, the first motor 18 reversely rotates to drive the roller 14 to rotate, so that the pull rope 13 is in a loose state, the sliding rail 7 is reset by the elastic force of the second spring 12, the speed is high when the unmanned aerial vehicle 6 enters the garage, the bottom is contacted with the speed reducing block 8, the speed of the unmanned aerial vehicle 6 is reduced by the plurality of speed reducing blocks 8 until the unmanned aerial vehicle 6 stops;
when the submersible vehicle is submerged at a certain height, the water pump 28 is started, seawater enters the area below the baffle plate 27 in the buoyancy chamber 4 when the water pump 28 pumps water, the piston 20 is not attached to the top of the fixed cylinder 19 under the action of gravity, air is discharged from the groove 23, when the water surface passes over the buoyancy block 22, the buoyancy block 22 floats upwards and enables the piston 20 to be attached to the top of the fixed cylinder 19, the upper and lower areas of the baffle plate 27 are separated, water flow cannot enter the upper part of the baffle plate 27, when the submersible vehicle is submerged at a certain height, the water pump 28 is started, the water pump 28 pumps the seawater, the water surface descends to enable the buoyancy block 22 to fall under the action of gravity, the top of the piston 20 is detached from the top of the fixed cylinder 19 again, and the upper and lower parts of the baffle plate 27 are communicated, so that the air pressure is balanced.
It should be noted that the above embodiments are only for illustrating the technical solution of the present invention and not for limiting the same, and although the present invention has been described in detail with reference to the preferred embodiments, it should be understood by those skilled in the art that the technical solution of the present invention may be modified or substituted without departing from the spirit and scope of the technical solution of the present invention, which is intended to be covered in the scope of the claims of the present invention.

Claims (8)

1. The utility model provides a portable hangar floats and dives ware which characterized in that: including hangar (1) and buoyancy module (4), hangar (1) bottom fixedly connected with is at buoyancy module (4) top, and hangar (1) top fixedly connected with solar photovoltaic board (2), hangar (1) both ends rotate and are connected with door plant (3), buoyancy module (4) top is located inside slide rail (7) that are provided with of hangar (1), and is provided with unmanned aerial vehicle (6) on slide rail (7), inside fixedly connected with baffle (27) of buoyancy module (4), and baffle (27) divide into upper and lower two parts with buoyancy module (4) inner area, buoyancy module (4) bottom both sides fixedly connected with sleeve (39), and sleeve (39) inside be provided with paddle (37), water pump (28) are installed to buoyancy module (4) bottom one side, bleeder vent (29) have been seted up at buoyancy module (4) top.
2. The mobile hangar submersible of claim 1, wherein: the end of the sliding rail (7) is rotationally connected to the top of the floating cabin (4), a speed reducing block (8) is arranged on one side of the sliding rail (7), a fixing column (10) is inserted into the end of the speed reducing block (8), one end of the fixing column (10) is fixedly connected with a first spring (9), the other end of the first spring (9) is fixedly connected to the inner cavity of the speed reducing block (8), and the outer end of the speed reducing block (8) is inclined.
3. The mobile hangar submersible of claim 1, wherein: the utility model discloses a buoyancy module, including buoyancy module, arc wall (11) have been seted up on the top of buoyancy module (4) top in slide rail (7), and the circular of arc wall (11) is rotated with slide rail (7) and is connected the position department of buoyancy module (4) and coincide mutually, the inside swing joint of arc wall (11) has second spring (12), and the one end fixedly connected with of second spring (12) is in slide rail (7) bottom, two outside fixedly connected with stay cord (13) that slide rail (7) are close to arc wall (11) one end, buoyancy module (4) top is located arc wall (11) one side and rotates and be connected with roller (14), and the other end winding of stay cord (13) is in roller (14) one side, roller (14) end runs through buoyancy module (4) top and extends to inside.
4. A mobile hangar submersible according to claim 3, wherein: the floating cabin is characterized in that a first motor (18) is fixedly connected to the top of an inner cavity of the floating cabin (4), connecting shafts (17) are fixedly connected to two ends of a shaft of the first motor (18), first worms (16) are fixedly connected to two ends of the connecting shafts (17), first worm wheels (15) are connected to one side of each first worm (16) in a meshed mode, and the tops of the first worm wheels (15) are fixedly connected to the tail ends of the winding rollers (14).
5. The mobile hangar submersible of claim 1, wherein: the utility model discloses a fixed cylinder, including baffle (27), fixed cylinder (19), piston (20), fixed cylinder (19) top and bottom intercommunication, fixed cylinder (19) bottom fixedly connected with solid fixed ring (24), and solid fixed ring (24) inside sliding connection has spliced pole (21), the top fixedly connected with piston (20) of spliced pole (21), and piston (20) top shape and fixed cylinder (19) top looks adaptation.
6. The mobile hangar submersible as recited in claim 5 wherein: the piston (20) and the fixed ring (24) are both provided with grooves (23), the inner side of the fixed ring (24) is provided with sliding grooves (26), the side face of the connecting column (21) is fixedly connected with sliding rods (25), the section shape of the sliding rods (25) is matched with the section shape of the sliding grooves (26), the bottom of the connecting column (21) is fixedly connected with a buoyancy block (22), and the section diameter of the buoyancy block (22) is larger than that of the connecting column (21).
7. The mobile hangar submersible of claim 1, wherein: the inner cavity bottom of the floating cabin (4) is fixedly connected with a waterproof shell (30), the floating cabin (4) is located at two ends inside the waterproof shell (30) and is fixedly connected with a second motor (31), the shaft end of the second motor (31) is fixedly connected with a second worm (32), one side of the second worm (32) is connected with a second worm wheel (33) in a meshed mode, the bottom end of the second worm wheel (33) is fixedly connected with a transmission shaft (40), and the tail end of the transmission shaft (40) penetrates through the bottom of the floating cabin (4) and extends to the outer side.
8. The mobile hangar submersible as recited in claim 7 wherein: the utility model discloses a motor vehicle, including sleeve (39), transmission shaft (40), sleeve (39), connecting frame (38), paddle (37), worm wheel (35), worm (34) and transmission shaft (40) bottom, sleeve (39) both ends fixedly connected with filter screen (5), sleeve (39) inside both ends fixedly connected with link (38), and rotate between two link (38) and be connected with pivot (36), paddle (37) end fixedly connected with is in pivot (36), outside fixedly connected with third worm wheel (35) in the middle of pivot (36), and third worm wheel (35) one side meshing is connected with third worm (34), third worm (34) top fixedly connected with transmission shaft (40) bottom.
CN202310494470.7A 2023-05-05 2023-05-05 Movable hangar submersible Pending CN116902157A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202310494470.7A CN116902157A (en) 2023-05-05 2023-05-05 Movable hangar submersible

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202310494470.7A CN116902157A (en) 2023-05-05 2023-05-05 Movable hangar submersible

Publications (1)

Publication Number Publication Date
CN116902157A true CN116902157A (en) 2023-10-20

Family

ID=88355269

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202310494470.7A Pending CN116902157A (en) 2023-05-05 2023-05-05 Movable hangar submersible

Country Status (1)

Country Link
CN (1) CN116902157A (en)

Similar Documents

Publication Publication Date Title
CN107380423B (en) Water-air amphibious unmanned aerial vehicle
CN204568035U (en) A kind of multi-function operation type under-water robot
JP4880795B1 (en) Departing and landing aircraft, takeoff equipment and hull reduction equipment
CN108216532A (en) Fixed-wing air-sea is dwelt aircraft and control method more
CN108622342B (en) Multi-stage separable unmanned underwater vehicle
CN110641663B (en) Large underwater vehicle with self-disposable wings
CN110641662B (en) Underwater glider capable of presetting large load underwater
CN113085462B (en) Cross-medium unmanned aerial vehicle device and control method thereof
JP2018525264A (en) Submarine with retractable wing assembly and keel assembly
CN214928770U (en) Amphibious unmanned underwater vehicle
CN113320676B (en) Cross-medium aircraft device and control method thereof
CN102849192B (en) Solar unmanned boat
KR101304775B1 (en) Flying ship with submarine functions
CN115042922A (en) Ocean monitor based on self-adsorption principle
CN116902157A (en) Movable hangar submersible
CN115675805B (en) Cross-medium carrying unmanned aerial vehicle submarine
CN112298504B (en) Winged electric forward and reverse bidirectional extrusion propulsion type intelligent underwater unmanned vehicle
JP2012240667A (en) V/stol aircraft of turboshaft engine
CN214165267U (en) Novel unmanned navigation ware can dive
CN116353861A (en) Integrated inspection, beating and supplementing type split, recycling and supplementing cross-medium unmanned platform and system
CN111422332B (en) Launching type flexible fishing robot for marine suspended matters
CN113501093A (en) Unmanned aerial bomb ice breaking submersible vehicle
CN112339954B (en) Wingless electric forward and reverse bidirectional extrusion spiral propulsion type intelligent underwater unmanned aircraft
CN202896862U (en) Solar energy unmanned boat
RU164143U1 (en) TWO MEDIUM UNMANNED AIRCRAFT

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination