CN116946328B

CN116946328B - Rescue unmanned ship

Info

Publication number: CN116946328B
Application number: CN202311212776.5A
Authority: CN
Inventors: 周忠明; 周前
Original assignee: Jiangsu Jincheng Shipbuilding Co ltd
Current assignee: Jiangsu Jincheng Shipbuilding Co ltd
Priority date: 2023-09-20
Filing date: 2023-09-20
Publication date: 2023-12-29
Anticipated expiration: 2043-09-20
Also published as: CN116946328A

Abstract

The invention discloses a rescue unmanned ship, which relates to the technical field of water rescue and comprises an unmanned ship body, wherein a signal antenna is fixedly arranged at the top of a front cavity of the unmanned ship body, an omnibearing angle adjusting component is fixedly arranged on the surface of the top wall of the unmanned ship body, a photovoltaic panel is arranged on the surface of a top cabin of the unmanned ship body, two groups of double extending components are arranged on the surface of the inner bottom end of the unmanned ship body, and signals received and transmitted by the signal antenna can be reflected by the cooperation of the omnibearing angle adjusting component, the signal transmitter, a filter, a signal receiver, a signal amplifier and an automatic antenna coordinator, so that the wireless transmission environment is intelligently reconfigured, the performance of a wireless communication network is further remarkably improved, the rescue operation efficiency of the unmanned ship body and the unmanned ship is ensured, and the problem that rescue signals of rescue workers are delayed possibly caused is avoided.

Description

Rescue unmanned ship

Technical Field

The invention relates to the technical field of water rescue, in particular to a rescue unmanned ship.

Background

The offshore rescue is a search, rescue and other work made by a pointer on an offshore accident and the like, and compared with land rescue, the offshore rescue has more unpredictability, so the difficulty is also higher, the traditional offshore rescue adopts modes of manually driving a ship or helicopter to search for a rescue target, and the like, consumes a great amount of manpower and material resources and has lower efficiency, and in some scenes, an unmanned rescue vessel is adopted to carry out the offshore rescue.

But among the prior art, when using unmanned aerial vehicle to rescue, easily make and receive regional magnetic field signal influence at sea, cause unmanned aerial vehicle's rescue signal to produce the delay to probably lead to rescue personnel's rescue time delay, simultaneously, traditional unmanned rescue vessel is when large-scale waters rescue process, whole search and rescue inefficiency, and unmanned ship is easily received sea condition influence, causes unmanned ship to receive the damage, can't in time rescue operation, consequently just need propose a new rescue unmanned ship.

Disclosure of Invention

The invention aims to provide a rescue unmanned ship, which solves the problems that when the unmanned ship is used for rescue operation, the unmanned ship is easily influenced by regional magnetic field signals at sea, and the rescue signals of the unmanned ship are delayed, so that the rescue time of rescue personnel is possibly delayed, and the whole rescue efficiency is low when the traditional unmanned rescue ship is used for rescue in a large water area, and the unmanned ship is easily influenced by sea conditions, so that the unmanned ship is damaged, and the rescue operation cannot be timely performed.

In order to achieve the above purpose, the present invention provides the following technical solutions: the utility model provides a rescue unmanned ship, including unmanned ship body, unmanned ship body's front cavity top fastening installs signal antenna, unmanned ship body's roof surface fastening installs all-round angle adjustment subassembly, and unmanned ship body's top cabin surface mounting is provided with the photovoltaic board, unmanned ship body's inside bottom surface mounting is provided with two sets of double extension subassemblies, unmanned ship body's top is placed and is installed unmanned aerial vehicle subassembly, and unmanned ship body's inside welding has the thermal-insulated mounting panel, thermal-insulated mounting panel's diapire surface fastening installs autoloading subassembly, and thermal-insulated mounting panel's top surface mounting is provided with central singlechip, central singlechip's avris is connected with signal transmitter through the circuit, and central singlechip's on the surface is connected with GPRS chipset through the circuit, signal receiver's avris is connected with signal amplifier through the circuit on the avris surface, and central singlechip's back side is connected with automatic antenna coordinator through the circuit; the all-round angle adjusting part includes flexible electric putter, flexible electric putter's side fastening connection has the terminal box, the connection pivot is installed to the bottom of terminal box, the both ends outside is provided with the damping pivot about the connection pivot, and the both ends are installed about the connection pivot and turn to the supporting seat, the limit side frame that turns to the supporting seat is established and is installed angle accommodate motor, and the internally mounted of terminal box is provided with brushless motor, brushless motor's inside output shaft external connection has first gear, the tooth angle end meshing of first gear is connected with the second gear, the top connection of second gear is provided with a line section of thick bamboo, the top intercommunication of line section of thick bamboo has the erection column, two sets of fastening hoops of fastening connection are established to the cover of both ends about the outside week side of erection column, movable mounting is installed to the limit side fastening of two sets of fastening hoops, movable mounting's internally mounted is provided with IRS reflection panel.

Preferably, two groups of electric cylindrical guide rails are arranged at two ends of the side of the unmanned ship body, and electric lifting doors are arranged at the outer periphery sides of the two groups of electric cylindrical guide rails.

Preferably, the fin plates are arranged on the left side wing edge and the right side wing edge of the front cabin of the unmanned ship body, the guide posts are arranged on the back side surface of the fin plates, the screw driving structures are arranged at the two ends of the back side of the unmanned ship body, the driving power supply is arranged at the rear end of the unmanned ship body, and the driving stirring sheet group is arranged at the front end of the unmanned ship body.

Preferably, the dual extension assembly comprises a first-stage guide rail seat, two guide posts are mounted at the left end and the right end of the first-stage guide rail seat, a first adjusting bolt is mounted at the central end of the first-stage guide rail seat, a sliding connecting block is arranged between the first adjusting bolt and the outer mounting of the two guide posts, the top of the sliding connecting block is fixedly connected with a connecting base plate, and a first driving progressive motor is mounted at the side end of the first adjusting bolt.

Preferably, the top fastening connection of connecting substrate has the second grade guide rail seat, two connection slide posts are installed at the left and right sides both ends of second grade guide rail seat, install the forked tail slider on the avris surface of second grade guide rail seat, and the center end installation of second grade guide rail seat is provided with second adjusting bolt, the externally mounted of second adjusting bolt and two connection slide posts is provided with the sliding block, the top fastening connection of sliding block has the seat of placing, the left and right sides symmetry of placing the seat is provided with the hydraulic stem, and the center end surface mounting of placing the seat is provided with position sensor, and the side end connection of second adjusting bolt installs the second drive motor of progress.

Preferably, the surface mounting of inner chamber avris of unmanned ship body is provided with two sets of secondary output power supplies, and the avris of two sets of secondary output power supplies is connected with the stabiliser through circuit electric connection, and the avris of two sets of secondary output power supplies is provided with wireless charging end.

Preferably, the unmanned aerial vehicle assembly comprises an unmanned aerial vehicle base, an unmanned aerial vehicle chamber is arranged at the top of the unmanned aerial vehicle base, carbon fiber wings are arranged at the left end and the right end of the unmanned aerial vehicle chamber, a charging end is arranged at the back side of the unmanned aerial vehicle chamber, an entering end is arranged at the top of the unmanned aerial vehicle chamber, an obstacle avoidance sensor is arranged on the surface of the unmanned aerial vehicle chamber, and a discharge port is arranged at the bottom of the unmanned aerial vehicle base.

Preferably, the automatic feeding component comprises a connecting vertical frame, the bottom of the connecting vertical frame is fixedly connected with a mounting frame, the inner mounting of the mounting frame is provided with a time sequence controller, and the side frame of the mounting frame is provided with a rotating motor.

Preferably, the internally mounted of mounting bracket is provided with three groups of drive shafts, and the inside output shaft erection joint of a set of drive shaft and rotating electrical machines, and the outside left and right sides cover of three groups of drive shafts is established and is installed drive chain gear, and drive chain gear's outside tooth angle end meshing is connected with drive chain, and drive chain's outside fastening is connected with the linking frame, and the side fastening of linking frame has rescue material to place the case, and the side installation of rescue material to place the case is provided with automatic switch door.

Preferably, the inner part of the cavity of the unmanned ship body is fixedly provided with a separation frame, the outer wall surface of the separation frame and the inner wall surface of the unmanned ship body are symmetrically provided with dovetail grooves, and the dovetail grooves are in sliding connection with dovetail sliding blocks.

Compared with the prior art, the invention has the beneficial effects that:

1. according to the invention, through the cooperation of the all-dimensional angle adjusting assembly, the signal transmitter, the filter, the signal receiver, the signal amplifier and the automatic antenna coordinator, the rescue operation signals of the unmanned aerial vehicle are conveniently conveyed by the signal amplifier, the signal receiver and the automatic antenna coordinator, when the rescue signals are conveyed in an unstable condition, a remote worker conveys the control signals to the central singlechip, the central singlechip respectively sends the control signals to the angle adjusting motor and the brushless motor, the brushless motor drives the first gear and the second gear to operate, the mounting column, the wire barrel, the two groups of fastening hoops, the movable mounting rack and the IRS reflecting panel are driven to perform circumferential track operation, the IRS reflecting panel can reflect signals received and transmitted by the signal antenna through integrating a large number of low-cost passive reflecting elements on a plane, thereby intelligently reconfiguring a wireless propagation environment, further remarkably improving the performance of a wireless communication network, guaranteeing the rescue operation efficiency of the unmanned ship body and the unmanned aerial vehicle, simultaneously, after the angle adjusting motor receives the control signals, the angle adjusting motor drives the rotating shaft to rotate under the cooperation of the steering support seat, the rotating shaft is connected with the rotating shaft and the rotating shaft is further convenient to rotate, the IRS reflecting panel can rotate synchronously, and the rotating shaft is further can be rotated, and the rotating shaft is convenient to rotate, and the IRS reflecting panel can rotate synchronously, and the rotating shaft can rotate and the rotating shaft is further can rotate.

2. According to the invention, under the cooperation of the double extension assembly and the unmanned aerial vehicle, when the unmanned aerial vehicle is required to take off and land, a control signal is conveniently sent to the first driving progress motor, so that the first driving progress motor drives the first adjusting bolt to carry out displacement operation, meanwhile, under the cooperation of the two guide posts, the stability of the displacement operation is conveniently improved, then under the cooperation of the sliding connecting block and the connecting base plate, the secondary guide rail seat is driven to carry out displacement extension operation, after the displacement extension operation of the secondary guide rail seat reaches a preset position, the control signal is sent to the second driving progress motor, so that the second driving progress motor is started, the second adjusting bolt is driven to carry out extension under the cooperation of the two connecting slide posts, and the sliding block and the placing seat are driven to enable the unmanned aerial vehicle to be placed above the placing seat conveniently, so that the unmanned aerial vehicle extends out of a ship body of the unmanned aerial vehicle, and the lifting of the unmanned aerial vehicle cannot be influenced.

3. In the invention, the automatic feeding component and the unmanned aerial vehicle component can send control signals to the rotating motor, so that the rotating motor drives the three groups of driving shafts to rotate under the cooperation of the time sequence controller, thereby driving the chain gears to synchronously rotate under the rotatability cooperation of the three groups of driving shafts, and further driving the chain to drive the connecting frame and the rescue material placing box to rotate, when the rescue material placing box is matched with the position sensor to reach the position above the entering end arranged at the top of the unmanned aerial vehicle cavity, the rescue material placing box is convenient to fall into the unmanned aerial vehicle cavity under the cooperation of the automatic switch door, after the unmanned aerial vehicle takes off, rescue operation is carried out, and in the rescue process, the unmanned aerial vehicle is matched with the obstacle avoidance sensor, when being convenient for unmanned aerial vehicle searches rescue operation in regional scope, can detect the back to the place ahead barrier for unmanned aerial vehicle can avoid the barrier automatically, avoid causing the damage to unmanned aerial vehicle, then search back the navigation when unmanned aerial vehicle in regional scope and fall behind placing the seat, under the cooperation of position sensor simultaneously, be convenient for improve unmanned aerial vehicle and place seat elevating position's accuracy, after unmanned aerial vehicle descends and places, operate with above-mentioned step again, make unmanned aerial vehicle place to the inside of unmanned ship body in second grade guide rail seat and one-level guide rail seat cooperation lower refund, later under the cooperation of hydraulic stem, carry out the centre gripping to unmanned aerial vehicle fixedly, and after fixed, make charging end and wireless charging end charge the operation under electromagnetic induction mode, be convenient for improve unmanned aerial vehicle rescue's continuation of voyage operation.

Drawings

FIG. 1 is a schematic view of the internal section of a rescue unmanned ship according to the present invention;

FIG. 2 is a schematic view of a rescue unmanned ship in a front view;

FIG. 3 is a schematic side view of the rescue unmanned ship;

FIG. 4 is a schematic view showing an installation position of an inner structure of a rescue unmanned ship body according to the present invention;

FIG. 5 is a schematic structural view of an omni-directional angle adjustment assembly for a rescue unmanned ship according to the present invention;

FIG. 6 is a schematic view of a rescue unmanned ship with an angle adjusting assembly separated;

FIG. 7 is a schematic structural view of a dual extension assembly, an unmanned aerial vehicle assembly and an automatic feeding assembly of the rescue unmanned aerial vehicle of the present invention;

FIG. 8 is a schematic structural view of a double extension assembly of the rescue unmanned ship of the present invention;

fig. 9 is a schematic structural view of a rescue unmanned ship unmanned plane assembly according to the present invention;

fig. 10 is a schematic structural view of an automatic feeding assembly of a rescue unmanned ship.

In the figure: 1. unmanned ship hulls; 2. a fin; 3. a flow guiding column; 4. a driving power supply; 5. a photovoltaic panel; 6. an electric lifting door; 7. a propeller drive structure; 8. a signal antenna; 9. an omni-directional angle adjustment assembly; 91. a telescopic electric push rod; 92. a steering support seat; 93. a junction box; 94. the connecting rotating shaft; 95. an angle adjusting motor; 96. damping the rotating shaft; 97. a mounting column; 98. a fastening hoop; 99. a flexible mounting rack; 990. an IRS reflective panel; 991. a brushless motor; 992. a first gear; 993. a second gear; 994. a wire barrel; 10. driving the stirring sheet group; 11. an electric cylinder guide rail; 12. a dual extension assembly; 120. a first-stage guide rail seat; 121. a guide post; 122. a sliding connection block; 123. a first adjusting bolt; 124. a first drive progressive motor; 125. a connection substrate; 126. a second-stage guide rail seat; 127. a second adjusting bolt; 128. a sliding block; 129. a placement seat; 1290. a hydraulic rod; 1291. a secondary output power supply; 1292. a wireless charging end; 1293. a voltage stabilizer; 13. an unmanned aerial vehicle assembly; 131. an unmanned aerial vehicle base; 132. a carbon fiber airfoil; 133. a charging end; 134. an entry end; 135. an obstacle avoidance sensor; 14. a separation frame; 15. a thermally insulating mounting plate; 16. an automatic feeding component; 161. connecting the vertical frame; 162. a mounting frame; 163. a timing controller; 164. a rotating electric machine; 165. a drive shaft; 166. a drive chain gear; 167. a drive chain; 168. a connecting frame; 169. a rescue material placement box; 1690. automatically opening and closing a door; 17. a central single chip microcomputer; 18. a signal transmitter; 19. a GPRS chipset; 20. a filter; 21. a signal receiver; 22. a signal amplifier; 23. an automatic antenna coordinator.

Detailed Description

The following description of the embodiments of the present invention will be made clearly and fully with reference to the accompanying drawings, in which it is evident that the embodiments described are only some, but not all embodiments of the invention. 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. 1-10: the rescue unmanned ship comprises an unmanned ship body 1, wherein a signal antenna 8 is fixedly arranged at the top of a front cavity of the unmanned ship body 1, an omnibearing angle adjusting component 9 is fixedly arranged on the surface of the top wall of the unmanned ship body 1, a photovoltaic panel 5 is arranged on the surface of a top cabin of the unmanned ship body 1, two groups of double extension components 12 are arranged on the surface of the bottom end inside the unmanned ship body 1, an unmanned plane component 13 is arranged at the top of the two groups of double extension components 12, a heat insulation mounting plate 15 is welded inside the unmanned ship body 1, an automatic feeding component 16 is fixedly arranged on the surface of the bottom wall of the heat insulation mounting plate 15, a central singlechip 17 is arranged on the surface of the top of the heat insulation mounting plate 15, a signal emitter 18 is connected to the side of the central singlechip 17 through a line, a GPRS chip set 19 is connected to the surface of the central singlechip 17 through a line, a filter 20 is connected to the side of the signal emitter 18 through a line, a signal receiver 21 is connected to the side surface of the side of the central singlechip 17 through a line, and a signal amplifier 22 is connected to the side surface of the signal receiver 21 through a line, and a signal coordinator 23 is connected to the back side of the central singlechip 17 through a line coordinator 23; the omnidirectional angle adjusting assembly 9 comprises a telescopic electric push rod 91, a junction box 93 is fixedly connected to the side end of the telescopic electric push rod 91, a connecting rotating shaft 94 is installed at the bottom end of the junction box 93, damping rotating shafts 96 are arranged outside the left end and the right end of the connecting rotating shaft 94, steering supporting seats 92 are installed at the left end and the right end of the connecting rotating shaft 94, an angle adjusting motor 95 is installed on side frames of the steering supporting seats 92, a brushless motor 991 is arranged in the inner installation of the junction box 93, a first gear 992 is externally connected to an internal output shaft of the brushless motor 991, a second gear 993 is connected to the tooth angle end of the first gear 992 in a meshed mode, a wire barrel 994 is connected to the top of the second gear 993, two groups of fastening hoops 98 are fixedly connected to the upper end and the lower end of the outer circumference of the mounting post 97 in a sleeved mode, a movable mounting frame 99 is installed on the side of the two groups of fastening hoops 98, and an IRS reflecting panel 990 is arranged in the inner installation of the movable mounting frame 99.

According to the illustration in fig. 1-4, two groups of electric cylindrical guide rails 11 are installed at two ends of the side of the unmanned ship body 1, and electric lifting doors 6 are installed at the outer periphery sides of the two groups of electric cylindrical guide rails 11, so that when the unmanned ship is used for operating and lifting, the electric lifting doors 6 can be matched with the two groups of electric cylindrical guide rails 11 to lift, and the unmanned ship is convenient to rescue.

According to the illustration shown in fig. 1-4, fin plates 2 are installed on the left side and the right side of the front cabin of the unmanned ship body 1, guide posts 3 are installed on the back side surface of the fin plates 2, propeller driving structures 7 are installed at the two ends of the back side of the unmanned ship body 1, driving power sources 4 are installed at the rear end of the unmanned ship body 1, driving stirring sheet sets 10 are installed at the front end of the unmanned ship body 1, the automatic driving speed of the unmanned ship body 1 is conveniently improved under the cooperation of the fin plates 2 and the guide posts 3, the influence of water flow on the unmanned ship body 1 is reduced, and under the action of photovoltaic plates 5, the driving power sources 4 convert light energy into electric energy and store the electric energy in the driving power sources 4, and follow-up power supply and cruising for the unmanned ship are conveniently carried out.

According to the embodiments shown in fig. 1, fig. 4, fig. 7 and fig. 8, the dual extension assembly 12 includes a primary guide rail seat 120, two guide posts 121 are installed at the left and right ends of the primary guide rail seat 120, a first adjusting bolt 123 is installed at the center end of the primary guide rail seat 120, a sliding connection block 122 is installed at the outer ends of the first adjusting bolt 123 and the two guide posts 121, a connection substrate 125 is fastened to the top of the sliding connection block 122, a first driving progressive motor 124 is installed at the side end of the first adjusting bolt 123, the primary guide rail seat 120 is fastened and installed on the inner bottom wall surface of the unmanned ship body 1 through a fastening bolt, and then when the unmanned plane needs to take off and land, a control signal is sent to the first driving progressive motor 124, so that the first driving progressive motor 124 drives the first adjusting bolt 123 to perform displacement operation, and simultaneously under the cooperation of the two guide posts 121, the stability of the displacement operation is facilitated to be improved, and then under the cooperation of the sliding connection block 122 and the connection substrate 125, the second guide rail seat 126 is driven to perform displacement extension operation.

According to the fig. 1, fig. 4, fig. 7 and fig. 8 show, connect the top fastening connection of base plate 125 and have second guide rail seat 126, two connection slide posts are installed at the both ends about second guide rail seat 126, install the forked tail slider on the avris surface of second guide rail seat 126, and the center end installation of second guide rail seat 126 is provided with second adjusting bolt 127, the externally mounted of second adjusting bolt 127 and two connection slide posts is provided with sliding block 128, the top fastening connection of sliding block 128 has place seat 129, place seat 129's left and right sides symmetry and be provided with hydraulic stem 1290, and place seat 129's center end surface mounting is provided with position sensor, and second adjusting bolt 127's side end connection has second drive progress motor, after second guide rail seat 126 carries out displacement extension operation and reaches the preset position, send control signal to the second drive progress motor, thereby drive second adjusting bolt 127 under the cooperation of two connection slide posts, and then drive sliding block 128 and place seat 129 and make and place seat 129 and place the precision of the cooperation of unmanned aerial vehicle under the position sensor 129, make the unmanned aerial vehicle carry out the cooperation under the position of unmanned aerial vehicle under the position of carrying out, the unmanned aerial vehicle carries out the improvement of the position sensor under the position of unmanned aerial vehicle 129, and the unmanned aerial vehicle is placed in advance, the unmanned aerial vehicle is placed in the position of the unmanned aerial vehicle 120, the unmanned aerial vehicle is convenient for the step down, and the unmanned aerial vehicle is placed under the position of the position 120.

According to the arrangement shown in fig. 1, fig. 4, fig. 7 and fig. 8, two sets of secondary output power sources 1291 are installed on the surface of the side of the inner cavity of the unmanned ship body 1, the voltage stabilizer 1293 is electrically connected to the side of the two sets of secondary output power sources 1291 through a circuit, the wireless charging end 1292 is arranged on the side of the two sets of secondary output power sources 1291, and under the cooperation of the voltage stabilizer 1293 and the two sets of secondary output power sources 1291, the wireless charging end 1292 can perform charging and cruising operation on the unmanned plane after the unmanned plane is placed in the unmanned ship body 1.

According to the fig. 1, fig. 4, fig. 7 and fig. 9 show, unmanned aerial vehicle 13 includes unmanned aerial vehicle base 131, unmanned aerial vehicle base 131's top installation is provided with unmanned aerial vehicle cavity, unmanned aerial vehicle cavity's left and right sides both ends set up and install carbon fiber wing 132, and unmanned aerial vehicle cavity's dorsal part installation is provided with the end 133 that charges, unmanned aerial vehicle cavity's top has been seted up and has been put into end 134, unmanned aerial vehicle cavity's on-surface installation is provided with keeps away barrier sensor 135, wherein, the discharge port has been seted up to unmanned aerial vehicle base 131's bottom, after unmanned aerial vehicle carries out rescue operation, rescue goods transport is done, return to place holder 129 top for charging end 133 and wireless charging end 1292 charge operation under electromagnetic induction mode, then under entering end 134 and discharge port cooperation, make rescue materials advance to pour into and discharge to waiting for the rescue personnel department, then under keeping away barrier sensor 135 cooperation, when unmanned aerial vehicle is convenient for carrying out search rescue operation in regional scope, can avoid unmanned aerial vehicle to avoid the obstacle to avoid causing the damage to unmanned aerial vehicle automatically.

According to the embodiments shown in fig. 1, 4, 7 and 10, the automatic feeding unit 16 includes a connection frame 161, a bottom fastening connection mounting frame 162 of the connection frame 161, a timing controller 163 installed in the mounting frame 162, a rotating motor 164 installed on a side frame of the mounting frame 162, the connection frame 161 fastened to the bottom wall surface of the heat insulation mounting plate 15, and then a control signal is sent to the rotating motor 164, so that the rotating motor 164 performs uniform operation under the cooperation of the timing controller 163.

According to the illustration of fig. 1, fig. 4, fig. 7 and fig. 10, the internally mounted of mounting bracket 162 is provided with three sets of drive shafts 165, and the inside output shaft installation connection of a set of drive shafts 165 and rotating electrical machines 164, drive chain gear 166 is established to the outside left and right sides cover of three sets of drive shafts 165, drive chain gear 166's outside tooth angle end meshing is connected with drive chain 167, drive chain 167's outside fastening is connected with link up frame 168, link up frame 168's side fastening is connected with rescue material and place case 169, the avris installation of rescue material place case 169 is provided with automatic switch door 1690, when rotating electrical machines 164 carries out the operation, drive three sets of drive shafts 165 and rotate, thereby under the rotatableness cooperation of three sets of drive shafts 165, make drive chain gear 166 drive link up frame 168 and rescue material place case 169 rotate, under the cooperation of position sensor, reach unmanned aerial vehicle cavity top open entrance end 134 top when rescue material place case 169, the cooperation of being convenient for rescue material place case 169 falls into unmanned aerial vehicle cavity, the rescue material is convenient for wait to transport to the personnel to rescue place.

According to the illustration in fig. 1 and 4, the separation frame 14 is fixedly installed inside the cavity of the unmanned ship body 1, the dovetail sliding grooves are symmetrically formed in the outer wall surface of the separation frame 14 and the inner wall surface of the unmanned ship body 1, the dovetail sliding grooves are in sliding connection with the dovetail sliding blocks, and the separation frame 14 is utilized to facilitate the operation of two groups of rescue unmanned ship bodies 1 to be placed.

The wiring diagrams of the angle adjusting motor 95, the IRS reflecting panel 990, the obstacle avoidance sensor 135, the time schedule controller 163, the automatic switch door 1690, the central single chip microcomputer 17, the signal transmitter 18, the GPRS chipset 19, the filter 20, the signal receiver 21, the signal amplifier 22, the automatic antenna coordinator 23 and the position sensor in the present invention belong to the common knowledge in the art, and the working principle thereof is a known technology, and the model thereof is selected to be suitable according to the actual use, so that the control mode and the wiring arrangement will not be explained in detail for the angle adjusting motor 95, the IRS reflecting panel 990, the obstacle avoidance sensor 135, the time schedule controller 163, the automatic switch door 1690, the central single chip microcomputer 17, the signal transmitter 18, the GPRS chipset 19, the filter 20, the signal receiver 21, the signal amplifier 22, the automatic antenna coordinator 23 and the position sensor.

The application method and the working principle of the device are as follows: firstly, when the unmanned ship body 1 performs rescue operation, under the cooperation of the signal antenna 8 and the signal transmitter 18, the transmitted signal is transmitted, so that after the remote rescue center receives the signal, the operation of workers in the rescue center is facilitated, then under the cooperation of the filter 20, the transmitted and received signal wave is stabilized in the wavelength frequency, so that the transmitted and received signal is more stable, then, the signal amplifier 22, the signal receiver 21 and the automatic antenna coordinator 23 are utilized, the transmission of the rescue operation signal of the unmanned ship is facilitated, and when the unstable condition occurs in the transmission of the rescue signal, the remote workers transmit the control signal to the central singlechip 17, so that the central singlechip 17 respectively transmits the control signal to the angle adjusting motor 95 and the brushless motor 991, the brushless motor 991 drives the first gear 992 and the second gear 993 to operate, thereby driving the mounting post 97, the wire barrel 994, the two groups of fastening hoops 98, the movable mounting frame 99 and the IRS reflecting panel 990 to operate in a circumferential track, the IRS reflecting panel 990 can reflect the signals received and transmitted by the signal antenna 8 by integrating a large number of low-cost passive reflecting elements on a plane, thereby intelligently reconfiguring the wireless transmission environment, further remarkably improving the performance of a wireless communication network, ensuring the rescue operation efficiency of the unmanned ship 1 and the unmanned aerial vehicle, simultaneously, when the angle adjusting motor 95 receives the control signals, the angle adjusting motor 95 drives the connecting rotating shaft 94 and the damping rotating shaft 96 to rotate under the cooperation of the steering supporting seat 92, and when the connecting rotating shaft 94 and the damping rotating shaft 96 rotate, the telescopic electric push rod 91 is synchronously started, so that the IRS reflecting panel 990 can perform elevation angle rotation adjustment, the IRS reflecting panel 990 can reflect signals in different directions, then the electric lifting door 6 is matched with the two groups of electric cylindrical guide rails 11 to perform lifting operation, thus the two groups of unmanned aerial vehicles in the unmanned aerial vehicle body 1 perform pre-take-off rescue operation, then when the unmanned aerial vehicle needs to take off and land, a control signal is sent to the first driving progressive motor 124, the first driving progressive motor 124 drives the first adjusting bolt 123 to perform displacement operation, the stability of the displacement operation is conveniently improved under the cooperation of the two guide posts 121, then under the cooperation of the sliding connecting block 122 and the connecting substrate 125, the secondary guide rail seat 126 is driven to carry out displacement extension operation, after the secondary guide rail seat 126 carries out displacement extension operation to reach a preset position, a control signal is sent to the second driving progressive motor, so that the second driving progressive motor is started, the second adjusting bolt 127 is driven to carry out extension under the cooperation of two connecting sliding posts, the sliding block 128 and the placing seat 129 are driven to carry out extension, the unmanned aerial vehicle is convenient to place above the placing seat 129, then a control signal is sent to the rotating motor 164, the rotating motor 164 is driven to drive the three groups of driving shafts 165 to rotate under the cooperation of the time sequence controller 163, the driving chain gear 166 is driven to synchronously rotate under the cooperation of the rotatability of the three groups of driving shafts 165, thereby make drive chain 167 drive link up frame 168 and rescue material place case 169 and rotate, under the cooperation of position sensor when rescue material place case 169, get into the entering end 134 top that unmanned aerial vehicle cavity top was seted up, be convenient for rescue material place case 169 under the cooperation of automatic switch door 1690, fall into the unmanned aerial vehicle cavity, afterwards, after the unmanned aerial vehicle takes off, rescue operation is carried out, and in rescue process, make the unmanned aerial vehicle keep away under the cooperation of barrier sensor 135, when the unmanned aerial vehicle is convenient for search rescue operation in regional scope, can detect the place ahead barrier after, make unmanned aerial vehicle can avoid the barrier voluntarily, avoid causing the damage to unmanned aerial vehicle, then when unmanned aerial vehicle search returning and place after seat 129 in regional scope, simultaneously under the cooperation of position sensor, be convenient for improve unmanned aerial vehicle and place seat 129 elevating position's accuracy, after unmanned aerial vehicle drops, operate with above-mentioned step again, make unmanned aerial vehicle carry out the operation under second grade guide seat 126 and one-level guide seat 120 cooperation down to unmanned aerial vehicle hull 1's inside, after cooperation carries out the rescue operation, can avoid the barrier to the unmanned aerial vehicle, avoid causing damage to unmanned aerial vehicle, then, charge 1292 carries out the fixed operation under the cooperation, and charge 1292, and charge the end is convenient for charging operation, the unmanned aerial vehicle is carried out, the charging operation is carried out, and the end is carried out under the electromagnetic induction, after 1292.

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

1. The utility model provides a rescue unmanned ship which characterized in that: including unmanned hull (1), signal antenna (8) is installed in the front cavity top fastening of unmanned hull (1), all-round angle adjustment subassembly (9) is installed in the fastening on the roof surface of unmanned hull (1), just install on the top cabin surface of unmanned hull (1) and be provided with photovoltaic board (5), the inside bottom surface mounting of unmanned hull (1) is provided with two sets of double extension subassembly (12), two sets of unmanned aerial vehicle subassembly (13) are placed at the top of double extension subassembly (12), just the inside welding of unmanned hull (1) has thermal-insulated mounting panel (15), automatic feeding subassembly (16) are installed in the bottom wall surface fastening of thermal-insulated mounting panel (15), and the top surface mounting of thermal-insulated mounting panel (15) is provided with central singlechip (17), the limit side of central singlechip (17) is connected with signal transmitter (18) through the circuit, and on the surface of central singlechip (17) is connected with GPRS chipset (19) through the circuit, the limit side of signal transmitter (18) is connected with signal amplifier (21) through circuit, the limit side of signal transmitter (21) is connected with signal amplifier (21) through the surface of signal amplifier (21), the back side of the central singlechip (17) is connected with an automatic antenna coordinator (23) through a circuit;

all-round angle adjusting part (9) are including flexible electric putter (91), and the side fastening connection of flexible electric putter (91) has terminal box (93), connection pivot (94) are installed to the bottom of terminal box (93), both ends outside is provided with damping pivot (96) about connection pivot (94), just both ends are installed about connection pivot (94) turn to supporting seat (92), install angle adjusting motor (95) in the limit side frame of turning to supporting seat (92), just the internally mounted of terminal box (93) is provided with brushless motor (991), the inside output shaft external connection of brushless motor (991) has first gear (992), the tooth angle end meshing of first gear (992) is connected with second gear (993), the top connection of second gear (993) is provided with a section of thick bamboo (994), the top intercommunication of a section of thick bamboo (994) has erection column (97), both ends cover is established fastening connection both ends and is connected with both sides hoop 98) about the outside week side of erection column (97), the inside mounting bracket (990) is provided with two sets of hoop 98), hoop (99) are installed on the inside mounting bracket (99).

2. Rescue unmanned ship according to claim 1, wherein: two groups of electric cylindrical guide rails (11) are arranged at two ends of the side of the unmanned ship body (1), and electric lifting doors (6) are arranged on the outer periphery sides of the two groups of electric cylindrical guide rails (11).

3. Rescue unmanned ship according to claim 1, wherein: the unmanned ship is characterized in that fin plates (2) are arranged on the left side wing edge and the right side wing edge of the front cabin of the unmanned ship body (1), guide posts (3) are arranged on the back side surface of the fin plates (2), propeller driving structures (7) are arranged at the two ends of the back side of the unmanned ship body (1), a driving power supply (4) is arranged at the rear end of the unmanned ship body (1), and a driving stirring sheet group (10) is arranged at the front end of the unmanned ship body (1).

4. Rescue unmanned ship according to claim 1, wherein: the double extension assembly (12) comprises a first-stage guide rail seat (120), two guide posts (121) are arranged at the left end and the right end of the first-stage guide rail seat (120), a first adjusting bolt (123) is arranged at the central end of the first-stage guide rail seat (120), a sliding connecting block (122) is arranged at the outer parts of the first adjusting bolt (123) and the two guide posts (121), a connecting base plate (125) is fixedly connected to the top of the sliding connecting block (122), and a first driving progressive motor (124) is arranged at the side end of the first adjusting bolt (123) in a connecting mode.

5. Rescue unmanned ship according to claim 4, wherein: the utility model discloses a motor, including connecting base plate (125), connecting base plate (126) are connected in top fastening, two connection slide posts are installed at both ends about second guide base plate (126), install the forked tail slider on the avris surface of second guide base plate (126), just the center end installation of second guide base plate (126) is provided with second adjusting bolt (127), second adjusting bolt (127) and two the externally mounted of connection slide post is provided with slider (128), the top fastening of slider (128) has place seat (129), the left and right sides symmetry of placing seat (129) is provided with hydraulic stem (1290), just the center end surface mounting of placing seat (129) is provided with position sensor, just the side end connection of second adjusting bolt (127) is installed second drive motor.

6. Rescue unmanned ship according to claim 1, wherein: two groups of secondary output power sources (1291) are arranged on the surface of the side of the inner cavity of the unmanned ship body (1), the sides of the two groups of secondary output power sources (1291) are electrically connected with voltage regulators (1293) through circuits, and wireless charging ends (1292) are arranged on the sides of the two groups of secondary output power sources (1291).

7. Rescue unmanned ship according to claim 1, wherein: unmanned aerial vehicle unit (13) include unmanned aerial vehicle base (131), the top installation of unmanned aerial vehicle base (131) is provided with the unmanned aerial vehicle cavity, both ends set up about the unmanned aerial vehicle cavity and install carbon fiber wing (132), just the dorsal part installation of unmanned aerial vehicle cavity is provided with charging end (133), entering end (134) have been seted up at the top of unmanned aerial vehicle cavity, the surface mounting of unmanned aerial vehicle cavity is provided with keeps away barrier sensor (135), wherein, the discharge gate has been seted up to the bottom of unmanned aerial vehicle base (131).

8. Rescue unmanned ship according to claim 1, wherein: the automatic feeding assembly (16) comprises a connecting vertical frame (161), a mounting frame (162) is fixedly connected to the bottom of the connecting vertical frame (161), a time sequence controller (163) is arranged in the mounting frame (162), and a rotating motor (164) is arranged on the side frame of the mounting frame (162).

9. Rescue unmanned ship according to claim 8, wherein: the inside mounting of mounting bracket (162) is provided with three drive shaft (165), and a set of drive shaft (165) with inside output shaft erection joint of rotating electrical machines (164), three sets of outside left and right sides cover of drive shaft (165) is established and is installed drive chain gear (166), the outside tooth angle end meshing of drive chain gear (166) is connected with drive chain (167), the outside fastening of drive chain (167) has link up frame (168), the side fastening of link up frame (168) has rescue material to place case (169), the avris of rescue material place case (169) is installed and is provided with automatic switch door (1690).

10. Rescue unmanned ship according to claim 1, wherein: the inside fastening of cavity of unmanned hull (1) is installed and is separated frame (14), the outer wall surface of separating frame (14) and the inner wall surface symmetry of unmanned hull (1) have been seted up the forked tail spout, forked tail spout and forked tail slider sliding connection.