CN109334978B - Unmanned reconnaissance aircraft damage separation information transmission device in maritime intelligent cruise - Google Patents
Unmanned reconnaissance aircraft damage separation information transmission device in maritime intelligent cruise Download PDFInfo
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- 238000010521 absorption reaction Methods 0.000 claims abstract description 27
- 238000002955 isolation Methods 0.000 claims abstract description 12
- 238000001514 detection method Methods 0.000 claims description 16
- 238000006243 chemical reaction Methods 0.000 claims description 15
- 238000007667 floating Methods 0.000 claims description 13
- 238000007789 sealing Methods 0.000 claims description 10
- 238000004090 dissolution Methods 0.000 claims description 9
- 238000003466 welding Methods 0.000 claims description 9
- 238000011835 investigation Methods 0.000 claims description 8
- 238000000034 method Methods 0.000 abstract description 4
- 239000013535 sea water Substances 0.000 description 10
- 150000003839 salts Chemical class 0.000 description 4
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D2045/0065—Black boxes, devices automatically broadcasting distress signals
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Abstract
The invention provides a damage separation information transmission device of an unmanned reconnaissance aircraft in maritime intelligent cruise, which comprises a reconnaissance aircraft body, a power wing, a concealed independent transmission device of the reconnaissance aircraft, a tail frame and a propulsion propeller, wherein the propulsion propeller is arranged at the tail part of the reconnaissance aircraft body, an elastic plate deforms after the water absorption plate absorbs water and swells, the water absorption plate is matched with the traction line to control the cut-off valve rod to be separated from the isolation area of the storage battery and the driver, the driver can generate kinetic energy in a short time after the hidden independent transmission device of the scout is separated, and the transportation information can quickly escape, so that when the scout unmanned aerial vehicle enters the space of unknown creatures, even if a large-range signal interference device is arranged facing unknown organisms or the unknown organisms are knocked down in the process of detecting the unmanned aerial vehicle, the surveyor can still recover effective information outside a local control area through the hidden escape capability of the information collection device.
Description
Technical Field
The invention belongs to the field of unmanned aerial vehicles, and particularly relates to an unmanned reconnaissance aircraft damage separation information transmission device in maritime intelligent cruise.
Background
Since the land area of the ocean is as large as seventy percent, even though the developed technology still exists in a vast ocean today, mysterious sea areas to be explored, countless explorationists and geological researchers feel right, and since many events which cannot be covered by the knowledge field up to now occur in the mysterious sea areas, the events cannot be explained and even the real objects cannot be seen, many explorationists try to control and explore the sea areas in a distant place through unmanned scout machines.
Based on the above description, the inventor finds that the existing unmanned reconnaissance plane damage separation information transmission device in maritime intelligent cruise mainly has the following defects, such as:
when the investigation unmanned aerial vehicle enters a mystery sea area, if a special signal isolation magnetic field appears in the sea area, a surveying party loses control over the investigation unmanned aerial vehicle, the reconnaissance aircraft is difficult to complete information collection, if no signal interference device exists, an unknown organism falls off the investigation unmanned aerial vehicle in the process of reconnaissance, and the surveying party is also difficult to receive effective information.
Disclosure of Invention
In order to solve the technical problems, the invention provides a damage separation information transmission device for an unmanned reconnaissance aircraft in maritime intelligent cruising, which aims to solve the problems that when the existing reconnaissance unmanned aerial vehicle enters a mystery sea area, if a special signal isolation magnetic field appears in the sea area, a reconnaissance unmanned aerial vehicle is out of control by a reconnaissance party, the information collection by the reconnaissance aircraft is difficult to complete, if no signal interference device exists, unknown organisms knock down the reconnaissance unmanned aerial vehicle in the reconnaissance process, and the reconnaissance aircraft is also difficult to receive effective information by the reconnaissance party.
Aiming at the defects of the prior art, the purpose and the effect of the unmanned reconnaissance plane damage separation information transmission device in the maritime intelligent cruise are achieved by the following specific technical means: the unmanned reconnaissance aircraft damage separation information transmission device in the marine intelligent cruise comprises a reconnaissance aircraft body, power wings, a reconnaissance aircraft hidden independent transmission device, a tail frame and a propulsion propeller, wherein the propulsion propeller is installed at the tail of the reconnaissance aircraft body, one end, close to the tail, of the outer ring surface of the reconnaissance aircraft body is fixedly connected with the top end of the tail frame in a welding mode, the power wings are two in number and are fixedly installed on the left side and the right side of the middle of the outer ring surface of the reconnaissance aircraft body in an embedded mode respectively, the two reconnaissance aircraft hidden independent transmission devices are two in number, and the top ends of the two in number correspond to the lower surfaces of the power wings and are fixedly connected with.
The scout hidden independent transmission device comprises a movable floating mechanism, a dissolution and separation mechanism, a sealing connecting pipe, a waterproof camera, a double control mechanism, a water absorption extension mechanism, a supporting through pipe, a propelling mechanism and a scout barrel, the top end of the movable floating mechanism is fixedly connected with the bottom end of the power wing through the dissolution and separation mechanism, the bottom end of the movable floating mechanism is movably connected with the top end of the outer ring surface of the investigation cylinder, the upper surface and the lower surface in the investigation cylinder are fixedly provided with two supporting through pipes, the middle of the supporting through pipe is fixedly connected to the outer ring surface of the double-control mechanism in an electric welding mode, the propelling mechanism is fixedly arranged at the tail part of the detection cylinder, the propelling mechanism and the double-control mechanism are fixedly connected together at one end far away from the sealing connecting pipe, and the waterproof camera is fixedly installed at the head end of the investigation cylinder through the sealing connecting pipe.
Preferably, the movable floating mechanism comprises a buoyancy color changing plate, a high-transparency waterproof cover, a solar energy conversion plate, a limiting ejector rod and a torque shaft rod, the buoyancy color changing plate, the high-transparency waterproof cover and the solar energy conversion plate are respectively provided with two parts and are arranged at the left end and the right end of the torque shaft rod, the limiting ejector rod is provided with twenty parts and ten groups which are fixedly arranged at the left end and the right end of the torque shaft rod respectively, the high-transparency waterproof cover is arranged inside the buoyancy color changing plate in an embedded mode, and the solar energy conversion plate is arranged inside the buoyancy color changing plate in an embedded mode, so that the buoyancy of the hidden independent transfer device of the scout can be increased after the scout is unfolded.
Preferably, the dissolving and separating mechanism comprises a connecting plate, through holes and water-soluble connecting rods, the through holes are nine and integrated with the connecting plate, the water-soluble connecting rods are nine and penetrate through the middle of the through holes, and therefore when the underwater reconnaissance aircraft can keep a hard state without absorbing salt water, the concealed independent transfer device of the reconnaissance aircraft can be fixed below the unmanned aerial vehicle.
Preferably, the double control mechanism comprises a transmission line, a storage box, a closed shell, a storage battery, a built-in power line, a cut-off valve rod, a driver and a torsional spring wire wheel, wherein the storage box is fixedly connected with the waterproof camera through the transmission line, the driver is fixedly installed at the right end inside the closed shell, the storage battery is fixedly installed in the middle of the inside of the closed shell, the storage box is fixedly installed at the left end inside the closed shell, the cut-off valve rod is used for isolating the storage battery from the driver, the storage battery is connected with the bottom end of the solar energy conversion plate through the built-in power line, one end of the torsional spring wire wheel is movably connected with one end of the water absorption extension mechanism, and therefore information collected by the scout before falling can be effectively stored.
Preferably, the water absorption extension mechanism comprises a traction wire, a water absorption plate, an elastic plate and two fixing blocks, the elastic plate is embedded in the outer annular surface of the water absorption plate, the fixing blocks are installed on the inner surface of the water absorption plate in an embedded mode, and the bottom end of the traction wire is fixedly connected with the fixing blocks.
Preferably, the propulsion mechanism comprises ring grooves, power blades and a brake paddle rod, the ring grooves are provided with four ring grooves and integrated with the detection cylinder, the power blades are correspondingly embedded into the ring grooves, and the middle ends of the power blades are fixed on the outer ring surface of the brake paddle rod in a welding mode.
Preferably, the buoyancy color-changing plate is a water ripple color-changing plate, and the two expanded buoyancy color-changing plates form a conical water breaking structure.
Preferably, the connecting plate is fixedly connected with the bottom end of the power wing through a water-soluble connecting rod.
Compared with the prior art, the invention has the following advantagesAdvantageous effects：
According to the invention, the water-soluble connecting rod is matched with the connecting plate, so that the hidden independent transfer device of the reconnaissance aircraft can be fixed below the unmanned aerial vehicle when the water-soluble connecting rod can keep a hard state when saline water is not absorbed, and the hidden independent transfer device of the reconnaissance aircraft can be quickly separated from the main body of the unmanned aerial vehicle after the water-soluble connecting rod reacts with seawater and melts when the water-soluble connecting rod is absorbed and soaked in seawater.
The storage box is in an isolated state with seawater in the closed shell, and is not in direct contact with the seawater, so that complete storage of data can be guaranteed.
The buoyancy color-changing plate is matched with the solar energy conversion plate, so that buoyancy support is respectively provided for the hidden independent transmission device of the scout after the scout is unfolded, the scout is prevented from sinking into the sea to cause information loss due to the self weight, and meanwhile, power is continuously supplied to the interior of the scout, and the continuous work of the driver is kept.
The elastic plate deforms after the water absorption plate absorbs water and swells, the elastic plate is matched with the water absorption plate to pull and match the traction line to control the cutoff valve rod to be separated from the isolation area of the storage battery and the driver, and the conductive ends on the two sides are contacted, so that the driver can generate kinetic energy in a short time after the hidden independent transmission device of the reconnaissance machine is separated, and transportation information can quickly escape, and therefore when the reconnaissance unmanned aerial vehicle enters the space of unknown organisms, even if a large-range signal interference device is arranged facing the unknown organisms, or the unknown organisms knock down the unknown organisms in the reconnaissance process of the reconnaissance unmanned aerial vehicle, a surveyor can still recover effective information outside a local control area through the hidden escape capability of the information collection device.
Drawings
FIG. 1 is a schematic structural diagram of an unmanned reconnaissance aircraft damage separation information transmission device in marine intelligent cruise.
Fig. 2 is a schematic view of the internal structure of the concealed independent transmission device of the scout.
Fig. 3 is a schematic top view of the concealed independent transmission device of the scout aircraft after being unfolded.
Fig. 4 is an enlarged schematic structural view of the dual-control mechanism in fig. 3.
Fig. 5 is a front view structural diagram of the concealed independent delivery device of the scout aircraft after being unfolded.
Fig. 6 is an enlarged schematic view of the dissolution and detachment mechanism of fig. 3.
Fig. 7 is an enlarged schematic view of the propulsion mechanism of fig. 3.
In the figure: a reconnaissance machine body-1, a power wing-2, a reconnaissance machine concealed independent transmission device-3, a tail frame-4, a propulsion paddle-5, a movable floating mechanism-31, a dissolution and separation mechanism-32, a sealing connecting pipe-33, a waterproof camera-34, a double control mechanism-35, a water absorption extension mechanism-36, a supporting through pipe-37, a propulsion mechanism-38, a reconnaissance cylinder-39, a buoyancy color changing plate-311, a high transparent waterproof cover-312, a solar energy conversion plate-313, a limiting ejector rod-314, a torque shaft rod-315, a connecting plate-321, a through hole-322, a water-soluble connecting rod-323, a transmission line-351, a storage box-352, a sealed shell-353, a storage battery-354, a built-in power line-355, a water-, A cutoff valve rod-356, a driver-357, a torsion spring wire wheel-358, a traction wire-361, a water absorption plate-362, an elastic plate-363, a fixed block-364, a ring groove-381, a power paddle-382 and a brake paddle rod-383.
Detailed Description
The embodiments of the present invention will be described in further detail with reference to the drawings and examples. The following examples are intended to illustrate the invention but are not intended to limit the scope of the invention.
In the description of the present invention, "a plurality" means two or more unless otherwise specified; the terms "upper", "lower", "left", "right", "inner", "outer", "front", "rear", "head", "tail", and the like, indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, are only for convenience in describing and simplifying the description, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed in a particular orientation, and be operated, and thus, should not be construed as limiting the 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 is to be noted that, unless otherwise explicitly specified or limited, the terms "connected" and "connected" are to be interpreted broadly, e.g., as being fixed or detachable or integrally connected; can be mechanically or electrically connected; may be directly connected or indirectly connected through an intermediate. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
Examples
As shown in figures 1 to 7:
the invention provides a damage separation information transmission device of an unmanned reconnaissance aircraft in intelligent maritime cruising, which comprises a reconnaissance aircraft body 1, power wings 2, a reconnaissance aircraft hidden independent transmission device 3, a tail frame 4 and propulsion propellers 5, wherein the propulsion propellers 5 are installed at the tail part of the reconnaissance aircraft body 1, one end, close to the tail part, of the outer annular surface of the reconnaissance aircraft body 1 is fixedly connected with the top end of the tail frame 4 in a welding mode, the power wings 2 are totally provided with two parts and are fixedly installed at the left side and the right side of the middle of the outer annular surface of the reconnaissance aircraft body 1 respectively in an embedding mode, the top ends of the two parts of the reconnaissance aircraft hidden independent transmission devices 3 are fixedly connected with the lower surface of the position, corresponding to the power wings.
The concealed independent transmission device 3 of the scout comprises a movable floating mechanism 31, a dissolution and separation mechanism 32, a sealing connecting pipe 33, a waterproof camera 34, a double control mechanism 35, a water absorption and extension mechanism 36, support through pipes 37, a propulsion mechanism 38 and a scout barrel 39, wherein the top end of the movable floating mechanism 31 is fixedly connected with the bottom end of the power wing 2 through the dissolution and separation mechanism 32, the bottom end of the movable floating mechanism 31 is movably connected with the top end of the outer annular surface of the scout barrel 39, the upper and lower surfaces in the scout barrel 39 are fixedly provided with the two support through pipes 37, the middle parts of the support through pipes 37 are fixedly connected with the outer annular surface of the double control mechanism 35 in an electric welding manner, the propulsion mechanism 38 is fixedly arranged at the tail part of the scout barrel 39, and the propulsion mechanism 38 and one end of the double control mechanism 35 far away from the sealing connecting pipe, the waterproof camera 34 is fixedly installed at the head end of the investigation cylinder 39 through the sealing connection pipe 33.
The movable floating mechanism 31 comprises a buoyancy color changing plate 311, a high-transparency waterproof cover 312, a solar energy conversion plate 313, a limiting ejector rod 314 and a torque shaft rod 315, wherein the buoyancy color changing plate 311, the high-transparency waterproof cover 312 and the solar energy conversion plate 313 are respectively provided with two and are installed at the left end and the right end of the torque shaft rod 315, the limiting ejector rod 314 is provided with twenty and ten groups in total and is respectively and fixedly installed at the left end and the right end of the torque shaft rod 315, the high-transparency waterproof cover 312 is installed inside the buoyancy color changing plate 311 in an embedded mode, and the solar energy conversion plate 313 is installed inside the buoyancy color changing plate 311 in an embedded mode, so that the buoyancy of the scout hidden independent transmission device 3 after being unfolded can be increased.
The dissolving and separating mechanism 32 comprises a connecting plate 321, through holes 322 and water-soluble connecting rods 323, the through holes 322 are totally nine and integrated with the connecting plate 321, the water-soluble connecting rods 323 are totally nine and penetrate through the middle of the through holes 322, and therefore when the underwater reconnaissance aircraft can keep a hard state without absorbing salt water, the concealed independent transfer device of the reconnaissance aircraft can be fixed below the unmanned aerial vehicle.
Wherein, the double control mechanism 35 comprises a transmission line 351, a storage box 352, a closed shell 353, a storage battery 354, a built-in power line 355, a cut-off valve rod 356, a driver 357 and a torsion spring reel 358, the storage box 352 is fixedly connected to the waterproof camera 34 by the transmission line 351, the driver 357 is fixedly arranged at the right end inside the sealed shell 353, the storage battery 354 is fixedly arranged in the middle inside the sealed shell 353, the storage box 352 is fixedly installed at the left end in the interior of the hermetic case 353, the cutoff valve rod 356 isolates the connection of the storage battery 354 and the driver 357, the battery 354 is connected to the bottom end of the solar energy conversion plate 313 through the built-in power line 355, one end of the torsion spring wire wheel 358 is movably connected with one end of the water absorption extension mechanism 36, so that the information collected by the scout before falling can be effectively stored.
The water absorption extension mechanism 36 comprises a traction line 361, a water absorption plate 362, an elastic plate 363 and a fixed block 364, wherein the traction line 361, the water absorption plate 362, the elastic plate 363 and the fixed block 364 are respectively provided with two, the elastic plate 363 is embedded on the outer ring surface of the water absorption plate 362, the fixed block 364 is installed on the inner surface of the water absorption plate 362 in an embedded mode, the bottom end of the traction line 361 is fixedly connected with the fixed block 364, so that the deformation can be rapidly generated by absorbing seawater, and a power supply is connected through a deformation control driver.
The propulsion mechanism 38 comprises annular grooves 381, power paddles 382 and a brake paddle rod 383, wherein the annular grooves 381 are provided with four grooves and are integrated with the detection cylinder 39, the power paddles 382 are provided with four grooves which are correspondingly embedded in the annular grooves 381, and the middle ends of the four grooves are fixed on the outer annular surface of the brake paddle rod 383 in a welding mode, so that the paddles with the four-page structure can generate strong thrust instantly after being started, and a hidden independent transmission device of the detection machine separated from a host machine is enabled to be rapidly away from a drop point.
The buoyancy color-changing plate 311 is a water wave gradient plate, and the two expanded buoyancy color-changing plates 311 are combined into a conical water breaking structure, so that the color similar to the sea surface can be displayed on the sea surface, and the hiding effect is achieved.
The connecting plate 321 is fixedly connected with the bottom end of the power wing 2 through a water-soluble connecting rod 323, so that the water-soluble connecting rod 323 can absorb seawater to melt after the aircraft crashes, and the hidden independent transfer device of the reconnaissance aircraft can be quickly separated from the main body of the unmanned aerial vehicle.
The specific use mode and function of the embodiment are as follows:
the hidden independent transfer device 3 of the reconnaissance aircraft can be fixed below the unmanned aerial vehicle when a water-soluble connecting rod 323 can keep a hard state when not absorbing salt water after the unmanned reconnaissance aircraft is interfered by external signals or impacted by external force, the hidden independent transfer device 3 of the reconnaissance aircraft can be fixed under the unmanned aerial vehicle when the water-soluble connecting rod 323 can keep a hard state when not absorbing salt water, the hidden independent transfer device of the reconnaissance aircraft can be quickly separated from the main body of the unmanned aerial vehicle after the water-soluble connecting rod 323 is soaked in the sea water and is melted after the water-soluble connecting rod 323 reacts with the sea water, after the main body is separated, the buoyancy color-changing plate 311 is firstly unfolded, is exposed after being unfolded due to the fact that the solar energy conversion plate is arranged on the inner surface, and provides buoyancy support for the hidden independent transfer device 3 of the reconnaissance aircraft after being unfolded so as to avoid sinking the, the driver 357 is kept working continuously, the elastic plate 363 deforms after the water absorption plate 362 absorbs water and swells, the elastic plate is matched with the water absorption plate 362 to pull and match the traction line 361 to control the cutoff valve rod 356 to be separated from the isolation area of the storage battery 354 and the driver 357, the conductive ends on the two sides are in contact, the driver 357 can generate kinetic energy in a short time after the hidden independent transmission device 3 of the reconnaissance machine is separated, the transportation information escapes quickly, the storage box 352 is in an isolation state with seawater in the sealed shell 353 and does not directly contact with the seawater, complete storage of data can be guaranteed, and when the hidden independent transmission device 3 of the reconnaissance machine avoids attack of unknown organisms and escapes from a local signal interference area through the buoyancy color changing plate, the recovery work of the information can be completed conveniently through a positioner in the storage box 352.
The embodiments of the present invention have been presented for purposes of illustration and description, and are not intended to be exhaustive or limited to the invention in the form disclosed. Many modifications and variations will be apparent to those of ordinary skill in the art. The embodiment was chosen and described in order to best explain the principles of the invention and the practical application, and to enable others of ordinary skill in the art to understand the invention for various embodiments with various modifications as are suited to the particular use contemplated.
Claims (8)
1. Unmanned reconnaissance aircraft damage separation information transmission device in marine intelligent cruise, its structure includes reconnaissance organism (1), power wing (2), reconnaissance aircraft concealed independent transmission device (3), tailstock (4), propulsion oar (5), its characterized in that: the detection machine is characterized in that the propelling propeller (5) is installed at the tail of the detection machine body (1), one end, close to the tail, of the outer annular surface of the detection machine body (1) is fixedly connected with the top end of the tail frame (4) in a welding mode, the two power wings (2) are arranged in total and are fixedly installed on the left side and the right side of the middle of the outer annular surface of the detection machine body (1) in an embedding mode respectively, the two hidden independent transmission devices (3) of the detection machine are arranged in total, the top ends of the two hidden independent transmission devices respectively correspond to the power wings (2), the lower surfaces of the three integral parts of one end of the detection machine body (1) are fixedly connected, and each hidden independent transmission device (3) of the detection machine comprises a movable floating mechanism (31), a dissolution and separation mechanism (32), a sealing connecting pipe (33), a waterproof camera (34), a double control mechanism (35), a water, A propelling mechanism (38) and a detection cylinder (39), wherein the top end of the movable floating mechanism (31) is fixedly connected with the bottom end of the power wing (2) through the dissolution and separation mechanism (32), the bottom end of the movable floating mechanism (31) is movably connected with the top end of the outer ring surface of the detection cylinder (39), the upper surface and the lower surface inside the detection cylinder (39) are fixedly provided with two support through pipes (37), the middle of the supporting through pipe (37) is fixedly connected with the outer ring surface of the double-control mechanism (35) in an electric welding way, the propelling mechanism (38) is fixedly arranged at the tail part of the investigation cylinder (39), the propelling mechanism (38) and one end of the double-control mechanism (35) far away from the sealing connecting pipe (33) are fixedly connected together, the waterproof camera (34) is fixedly installed at the head end of the detection cylinder (39) through the sealing connecting pipe (33).
2. The marine intelligent cruise flight unmanned reconnaissance aircraft damage isolation information transfer device of claim 1, wherein: the movable floating mechanism (31) comprises a buoyancy color changing plate (311), a high-transparency waterproof cover (312), a solar conversion plate (313), a limiting ejector rod (314) and a torque shaft rod (315), wherein the buoyancy color changing plate (311), the high-transparency waterproof cover (312) and the solar conversion plate (313) are respectively provided with two parts and installed at the left end and the right end of the torque shaft rod (315), the limiting ejector rod (314) is provided with twenty parts and ten groups of parts which are fixedly installed at the left end and the right end of the torque shaft rod (315), the high-transparency waterproof cover (312) is installed inside the buoyancy color changing plate (311) in an embedded mode, and the solar conversion plate (313) is installed inside the buoyancy color changing plate (311) in an embedded mode.
3. The marine intelligent cruise flight unmanned reconnaissance aircraft damage isolation information transfer device of claim 1, wherein: the dissolution and separation mechanism (32) comprises a connecting plate (321), through holes (322) and water-soluble connecting rods (323), wherein the through holes (322) are totally nine and integrated with the connecting plate (321), and the water-soluble connecting rods (323) are totally nine and penetrate through the middle of the through holes (322).
4. The marine intelligent cruise flight unmanned reconnaissance aircraft damage isolation information transfer device of claim 1, wherein: the double-control mechanism (35) comprises a transmission line (351), a storage box (352), a closed shell (353), a storage battery (354), a built-in power line (355), a cut-off valve rod (356), a driver (357) and a torsion spring reel (358), wherein the storage box (352) is fixedly connected with the waterproof camera (34) through the transmission line (351), the driver (357) is fixedly installed at the right end inside the closed shell (353), the storage battery (354) is fixedly installed in the middle inside the closed shell (353), the storage box (352) is fixedly installed at the left end inside the closed shell (353), the cut-off valve rod (356) isolates the connection between the storage battery (354) and the driver (357), and the storage battery (354) is connected with the bottom end of the solar energy conversion plate (313) through the built-in power line (355), one end of the torsion spring wire wheel (358) is movably connected with one end of the water absorption extending mechanism (36).
5. The marine intelligent cruise unmanned reconnaissance aircraft damage isolation information transfer device according to claim 1 or 4, characterized in that: the water absorption extension mechanism (36) comprises a traction line (361), a water absorption plate (362), an elastic plate (363) and a fixing block (364), wherein the traction line (361), the water absorption plate (362), the elastic plate (363) and the fixing block (364) are respectively provided with two, the elastic plate (363) is embedded in the inner ring surface of the water absorption plate (362), the fixing block (364) is installed on the outer surface of the water absorption plate (362) in an embedded mode, and the bottom end of the traction line (361) is fixedly connected with the fixing block (364).
6. The marine intelligent cruise flight unmanned reconnaissance aircraft damage isolation information transfer device of claim 1, wherein: the propulsion mechanism (38) comprises annular grooves (381), power paddles (382) and a brake paddle rod (383), wherein the annular grooves (381) are provided with four parts and integrated with the detection cylinder (39), the power paddles (382) are provided with four parts which are correspondingly embedded into the annular grooves (381), and the middle ends of the four parts are fixed on the outer annular surface of the brake paddle rod (383) in a welding mode.
7. The marine intelligent cruise flight unmanned reconnaissance aircraft damage isolation information transfer device of claim 2, wherein: the buoyancy color-changing plate (311) is a water wave color-changing plate, and the two expanded buoyancy color-changing plates (311) are combined into a conical water breaking structure.
8. The isolated information transfer device for unmanned reconnaissance aircraft damage in maritime intelligent cruise according to claim 3, characterized in that: the connecting plate (321) is fixedly connected with the bottom end of the power wing (2) through a water-soluble connecting rod (323).
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| US9676477B1 (en) * | 2014-08-25 | 2017-06-13 | Amazon Techonlogies, Inc. | Adjustable unmanned aerial vehicles |
| CN107672751B (en) * | 2017-09-13 | 2024-02-20 | 余拓 | Multifunctional submerged device with unmanned aerial vehicle take-off and landing platform |
| CN108128453A (en) * | 2018-01-08 | 2018-06-08 | 浙江大学 | A kind of air-sea dual-purpose solar unmanned plane and its control method |
| CN108482669B (en) * | 2018-02-23 | 2020-12-29 | 哈尔滨工业大学（威海） | Sea-air amphibious aircraft |
| CN108341059A (en) * | 2018-03-21 | 2018-07-31 | 安徽云翼航空技术有限公司 | A kind of battlefield is scouted and defence unmanned plane |
| CN108563176A (en) * | 2018-07-04 | 2018-09-21 | 哈尔滨工业大学 | A kind of buoy micro-system for marine exploration |
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2018
- 2018-09-30 CN CN201811161365.7A patent/CN109334978B/en active Active
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