CN109334978A - Scounting aeroplane damage separation information transfer device in maritime affairs intelligence cruise - Google Patents
Scounting aeroplane damage separation information transfer device in maritime affairs intelligence cruise Download PDFInfo
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- CN109334978A CN109334978A CN201811161365.7A CN201811161365A CN109334978A CN 109334978 A CN109334978 A CN 109334978A CN 201811161365 A CN201811161365 A CN 201811161365A CN 109334978 A CN109334978 A CN 109334978A
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- 238000012546 transfer Methods 0.000 title claims abstract description 43
- 238000000926 separation method Methods 0.000 title claims abstract description 18
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 46
- 238000011835 investigation Methods 0.000 claims abstract description 35
- 238000002845 discoloration Methods 0.000 claims description 21
- 238000007789 sealing Methods 0.000 claims description 18
- 230000000694 effects Effects 0.000 claims description 16
- 230000009977 dual effect Effects 0.000 claims description 14
- 238000003780 insertion Methods 0.000 claims description 12
- 230000037431 insertion Effects 0.000 claims description 12
- 230000001141 propulsive effect Effects 0.000 claims description 12
- 238000004090 dissolution Methods 0.000 claims description 10
- 238000003466 welding Methods 0.000 claims description 8
- 230000005540 biological transmission Effects 0.000 claims description 7
- 210000000481 breast Anatomy 0.000 claims description 3
- 238000009434 installation Methods 0.000 claims description 3
- 230000007704 transition Effects 0.000 claims description 3
- 229930091051 Arenine Natural products 0.000 claims 1
- 238000006243 chemical reaction Methods 0.000 claims 1
- 238000009738 saturating Methods 0.000 claims 1
- 239000013535 sea water Substances 0.000 description 11
- 238000010586 diagram Methods 0.000 description 6
- 238000002955 isolation Methods 0.000 description 4
- 150000003839 salts Chemical class 0.000 description 4
- 230000007812 deficiency Effects 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 241000272517 Anseriformes Species 0.000 description 1
- 230000005526 G1 to G0 transition Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 244000144992 flock Species 0.000 description 1
- 238000007654 immersion Methods 0.000 description 1
- 230000002045 lasting effect Effects 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 238000011160 research Methods 0.000 description 1
Classifications
-
- 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
-
- 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
-
- 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
-
- 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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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Studio Devices (AREA)
- Photovoltaic Devices (AREA)
Abstract
The present invention provides scounting aeroplane damage separation information transfer device in maritime affairs intelligence cruise, including investigating body, power wing, reconnaissance plane hidden independence transfer device, tailstock, promote paddle, investigation body tail portion is equipped with propulsion paddle, the present invention generates deformation after water sucting plate water suction swells because of elastic plate, the isolated area for pulling cooperation traction line traffic control block valve bar to be detached from battery and driver is matched with water sucting plate, driver can be made to generate kinetic energy in the short time after the disengaging of reconnaissance plane hidden independence transfer device, transportation intelligence is quickly fled from, to make Drones for surveillance when entering unknown territorial sky, even if being equipped with large-scale signal interference device in face of unknown, or it is shot down during Drones for surveillance investigates by unknown, it exploration side still can be by the hidden escape ability of information acquisition device on ground Effective information is recycled outside square control area.
Description
Technical field
The invention belongs to unmanned plane fields, and more specifically, in particular to scounting aeroplane damages in maritime affairs intelligence cruise
Ruin separation information transfer device.
Background technique
Since ocean land occupation sphere area is up to 71 percent, though science and technology flourishing today in vast ocean still
The mysterious sea areas for so needing to be explored in the presence of many, this allows countless explorer and geological scientific research personnel to go after like a flock of ducks, due to
The event that many kens so far can not still cover occurred in mysterious sea area, to can not explain it or even nothing
Method sees its true appearance clearly, and by scounting aeroplane, sea area carries out manipulation exploration to it in the distance for many scouts' trials.
Based on foregoing description, the inventors discovered that, scounting aeroplane damage separates information in existing maritime affairs intelligence cruise
Transfer device is primarily present following deficiency, such as:
Drones for surveillance is when entering mysterious sea area, if occurring special signal isolation magnetic field in sea area, exploration side is to detecing
Looking into unmanned plane will be out of hand, and reconnaissance plane is difficult to complete to collect information, if when no signal countermeasure set, unknown is being detectd
It is shot down during looking into unmanned plane investigation, exploration side equally will also be difficult to receive effective information.
Summary of the invention
In order to solve the above technical problem, the present invention provides scounting aeroplane damage separation information in maritime affairs intelligence cruise
Transfer device, to solve existing Drones for surveillance when entering mysterious sea area, if occurring special signal isolation magnetic field in sea area,
Exploration side will be out of hand to Drones for surveillance, and reconnaissance plane is difficult to complete to collect information, if when no signal countermeasure set, not
Know that biology is shot down during Drones for surveillance's investigation, exploration side equally will also be difficult to receive asking for effective information
Topic.
In view of the deficiencies of the prior art, scounting aeroplane damage separation information transmitting dress in maritime affairs intelligence cruise of the present invention
The purpose and effect set, are reached by technological means in detail below: scounting aeroplane damage separation feelings in maritime affairs intelligence cruise
Transfer device, including investigation body, power wing, reconnaissance plane hidden independence transfer device, tailstock, propulsion paddle are reported, it is described to detect
Look into body tail portion and the propulsion paddle be installed, the external anchor ring of scout by caudad one end by welding with it is described
Tailstock top is connected to a fixed, and the power wing sets there are two altogether and is fixedly mounted on described detect by way of insertion respectively
Look into the left and right sides among body outer ring surface, the reconnaissance plane hidden independence transfer device set altogether there are two and its top it is right respectively
The power wing is answered to be fixedly connected lower surface at the entire length one third of described investigation body one end.
The reconnaissance plane hidden independence transfer device include activity float mechanism, dissolution releasing mechanism, sealed joint pipe,
Water-proof CCD camera, dual control mechanism, water suction spreader mechanism, support siphunculus, propulsive mechanism, investigation cylinder, activity float mechanism top
End be fixed together by the dissolution releasing mechanism and power wing bottom end, activity float mechanism bottom end and
Investigation cylinder outer ring surface top is movably connected, and there are two the branch for upper and lower surface fixed installation inside the investigation cylinder
Siphunculus is supportted, is fixedly connected on dual control mechanism outer ring surface, the pusher by the way of electric welding among the support siphunculus
Structure is fixedly mounted on the tail portion of the investigation cylinder, and the propulsive mechanism and the dual control mechanism are far from described sealed joint pipe one end
It is fixed together, the water-proof CCD camera is fixedly mounted on investigation cylinder head end by the sealed joint pipe.
Preferably, the activity float mechanism includes buoyancy discoloration plate, high transparency waterproof cover, solar energy reformer plate, limit
Position mandril, torque shaft, the buoyancy discoloration plate, high transparency waterproof cover, solar energy reformer plate are respectively provided with two and are mounted on institute
State torque shaft left and right ends, the spacing mandril be equipped with altogether be equipped with altogether 20 and ten one group be respectively and fixedly installed to it is described
Torque shaft left and right ends, the high transparency waterproof cover is mounted on the buoyancy discoloration intralamellar part by way of insertion, described
Solar energy reformer plate is mounted on buoyancy discoloration intralamellar part by way of insertion, therefore can increase reconnaissance plane hidden and independently transmit dress
Set buoyancy after deployment.
Preferably, the dissolution releasing mechanism includes connecting plate, through-hole, water-soluble connecting rod, the through-hole is equipped with altogether
It nine and is integrated with the connecting plate, the water solubility connecting rod is equipped with nine and altogether through in the through-hole
Between, therefore when being able to maintain hardened condition when not absorbing salt water, it can change and enough reconnaissance plane hidden independence transfer device is fixed on nothing
Man-machine lower section.
Preferably, the dual control mechanism includes transmission line, the storage box, sealing shell, battery, built-in power line, cuts
Disconnected valve rod, driver, torsional spring line wheel, the storage box are fixedly connected on one by the transmission line and the water-proof CCD camera
It rises, right end is fixedly installed with the driver inside the sealing shell, and the sealing shell bosom is fixedly mounted
Battery is stated, left end is fixedly installed with the storage box in the sealing shell inside, and the electric power storage is isolated in the truncation valve rod
The connection in pond and the driver, the battery are connected by the built-in power line with solar energy reformer plate bottom end
It connects, torsional spring line wheel one end is flexibly connected with described water suction spreader mechanism one end, therefore can effectively save reconnaissance plane in air crash
Preceding collected information.
Preferably, the water suction spreader mechanism includes draught line, water sucting plate, elastic plate, fixed block, the draught line,
Wash water plate, elastic plate, fixed block are respectively provided with two, and the elastic plate is embedded in the water sucting plate outer ring surface, and the fixed block is logical
The mode for crossing insertion is mounted on water sucting plate inner surface, and the draught line bottom end is fixed together with fixed block.
Preferably, the propulsive mechanism include annular groove, power blade, braking loom, the annular groove set altogether there are four and
It is integrated with the investigation cylinder, the power blade sets that there are four be correspondingly embedded in the annular groove and intermediate ends are logical altogether
The mode for crossing welding is fixed on braking loom outer ring surface.
Preferably, the buoyancy discoloration plate is the buoyancy discoloration board group conjunction after water ripples transition slab and two expansion
Tapered one's water breaks structure.
Preferably, the connecting plate is fixedly connected by water-soluble connecting rod with power wing bottom end.
Compared with prior art, the present invention has as followsBeneficial effect:
The present invention is because water-soluble connecting rod with connecting plate by matching, by water-soluble connecting rod in when not absorbing salt water
When being able to maintain hardened condition, it can change and enough reconnaissance plane hidden independence transfer device is fixed below unmanned plane, connect in water solubility
When extension bar absorbs immersion in the seawater, water-soluble connecting rod enables reconnaissance plane hidden independently transmit dress after melting after reacting with seawater
It sets and is quickly separated with unmanned plane main body.
The present invention is in isolation with seawater because the storage box is in sealing shell, does not contact directly with seawater, energy
Enough ensure the full storage of data.
The present invention is because buoyancy discoloration plate is matched with solar energy reformer plate, after deployment respectively to reconnaissance plane hidden independence
Transfer device provides buoyancy support, sinks to marine in order to avoid should be own wt, causes the loss of information, while lasting supplying to internal
To power supply, continuing working for driver is kept.
The present invention matches pulling cooperation draught line with water sucting plate because elastic plate generates deformation after water sucting plate water suction swells
Control truncation valve rod is detached from the isolated area of battery and driver, enables the conducting end on both sides be in contact, driver can be made to detect
It examines and generates kinetic energy in the short time after machine hidden independence transfer device is detached from, transportation intelligence is quickly fled from, to make to investigate nobody
Machine is when entering unknown territorial sky, even if being equipped with large-scale signal interference device in face of unknown, or by unknown
It is shot down during Drones for surveillance's investigation, exploration side can still pass through the hidden escape ability of information acquisition device
Effective information is recycled outside local control area.
Detailed description of the invention
Fig. 1 is the structural representation of scounting aeroplane damage separation information transfer device in maritime affairs intelligence of the present invention cruise
Figure.
Fig. 2 is the schematic diagram of internal structure of reconnaissance plane hidden independence transfer device.
Fig. 3 is the overlooking structure diagram after the expansion of reconnaissance plane hidden independence transfer device.
Fig. 4 is the enlarged structure schematic diagram of Tu3Zhong dual control mechanism.
Fig. 5 is the positive structure diagram after the expansion of reconnaissance plane hidden independence transfer device.
Fig. 6 is the enlarged structure schematic diagram that releasing mechanism is dissolved in Fig. 3.
Fig. 7 is the enlarged structure schematic diagram of propulsive mechanism in Fig. 3.
In figure: investigation body -1, reconnaissance plane hidden independence transfer device -3, tailstock -4, promotes paddle-at power wing -2
5, activity float mechanism -31, dissolution releasing mechanism -32, sealed joint pipe -33, water-proof CCD camera -34, dual control mechanism -35, suction
Water spreader mechanism -36, support siphunculus -37, propulsive mechanism -38, investigation cylinder -39, buoyancy discoloration plate -311, high transparency waterproof cover -
312, solar energy reformer plate -313, spacing mandril -314, torque shaft -315, connecting plate -321, through-hole -322, water-soluble connection
Bar -323, transmission line -351, the storage box -352, sealing shell -353, battery -354, built-in power line -355, truncation valve rod -
356, driver -357, torsional spring line wheel -358, draught line -361, water sucting plate -362, elastic plate -363, fixed block -364, annular groove -
381, power blade -382, braking loom -383.
Specific embodiment
Embodiments of the present invention are described in further detail with reference to the accompanying drawings and examples.Following embodiment is used for
Illustrate the present invention, but cannot be used to limit the scope of the invention.
In the description of the present invention, unless otherwise indicated, the meaning of " plurality " is two or more；Term " on ",
The orientation or positional relationship of the instructions such as "lower", "left", "right", "inner", "outside", " front end ", " rear end ", " head ", " tail portion " is
It is based on the orientation or positional relationship shown in the drawings, is merely for convenience of description of the present invention and simplification of the description, rather than instruction or dark
Show that signified device or element must have a particular orientation, be constructed and operated in a specific orientation, therefore should not be understood as pair
Limitation of the invention.In addition, term " first ", " second ", " third " etc. are used for description purposes only, and should not be understood as instruction or
Imply relative importance.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " connected " " connects
Connect " it shall be understood in a broad sense, for example, it may be being fixedly connected, it may be a detachable connection, or be integrally connected；It can be machine
Tool connection, is also possible to be electrically connected；It can be directly connected, it can also be indirectly connected through an intermediary.For this field
For those of ordinary skill, the concrete meaning of above-mentioned term in the present invention can be understood with concrete condition.
Embodiment
As shown in attached drawing 1 to attached drawing 7:
The present invention provides scounting aeroplane damage separation information transfer device in maritime affairs intelligence cruise, including investigation body
1, power wing 2, reconnaissance plane hidden independence transfer device 3, tailstock 4, propulsion paddle 5,1 tail portion of the investigation body installation is
State promote paddle 5,1 outer ring surface of investigation body lean on caudad one end by welding with the 4 top stationary phase of tailstock
Connection, the power wing 2 set there are two altogether and are fixedly mounted on 1 outer ring surface of investigation body by way of insertion respectively
The intermediate left and right sides, the reconnaissance plane hidden independence transfer device 3 set altogether there are two and its top respectively correspond the power
Wing 2 is fixedly connected lower surface at 1 one end entire length one third of investigation body.
The reconnaissance plane hidden independence transfer device 3 includes activity float mechanism 31, dissolution releasing mechanism 32, sealing company
Adapter tube 33, water-proof CCD camera 34, dual control mechanism 35, water suction spreader mechanism 36, support siphunculus 37, propulsive mechanism 38, investigation cylinder 39,
31 top of activity float mechanism is fixedly connected on one with 2 bottom end of power wing by the dissolution releasing mechanism 32
It rises, 31 bottom end of activity float mechanism is movably connected with the 39 outer ring surface top of investigation cylinder, the investigation cylinder 39
Internal upper and lower surface is fixedly mounted there are two the support siphunculus 37, is fixed by the way of being welded among the support siphunculus 37
It is connected to 35 outer ring surface of dual control mechanism, the propulsive mechanism 38 is fixedly mounted on the tail portion of the investigation cylinder 39, described to push away
It is fixed together into mechanism 38 with the dual control mechanism 35 far from described 33 one end of sealed joint pipe, the water-proof CCD camera
34 are fixedly mounted on investigation 39 head end of cylinder by the sealed joint pipe 33.
Wherein, the activity float mechanism 31 includes buoyancy discoloration plate 311, high transparency waterproof cover 312, solar energy reformer plate
313, spacing mandril 314, torque shaft 315, buoyancy the discoloration plate 311, high transparency waterproof cover 312, solar energy reformer plate 313
Be respectively provided with two and be mounted on 315 left and right ends of torque shaft, the spacing mandril 314 altogether be equipped with altogether be equipped with 20 and
Ten one group is respectively and fixedly installed to 315 left and right ends of torque shaft, the side that the high transparency waterproof cover 312 passes through insertion
Formula is mounted on inside the buoyancy discoloration plate 311, and the solar energy reformer plate 313 is mounted on buoyancy discoloration by way of insertion
Inside plate 311, therefore the buoyancy of reconnaissance plane hidden independence transfer device 3 after deployment can be increased.
Wherein, the dissolution releasing mechanism 32 includes connecting plate 321, through-hole 322, water-soluble connecting rod 323, the through-hole
322 are equipped with nine altogether and are integrated with the connecting plate 321, and the water solubility connecting rod 323 is equipped with nine altogether and passes through
When being through among the through-hole 322, therefore being able to maintain hardened condition when not absorbing salt water, it can change enough that reconnaissance plane hidden is independent
Transfer device is fixed below unmanned plane.
Wherein, the dual control mechanism 35 include transmission line 351, it is the storage box 352, sealing shell 353, battery 354, built-in
Power supply line 355, truncation valve rod 356, driver 357, torsional spring line wheel 358, the storage box 352 by the transmission line 351 with
The water-proof CCD camera 34 is fixed together, and the 353 inside right end of sealing shell is fixedly installed with the driver
357,353 bosom of sealing shell is fixedly installed with the battery 354, left end in 353 inside of sealing shell
It is fixedly installed with the storage box 352, the company of the battery 354 and the driver 357 is isolated in the truncation valve rod 356
It connects, the battery 354 is connected by the built-in power line 355 with 313 bottom end of solar energy reformer plate, the torsional spring
358 one end of line wheel is flexibly connected with described 36 one end of water suction spreader mechanism, therefore can effectively be saved reconnaissance plane and be received before air crash
The information collected.
Wherein, the water suction spreader mechanism 36 includes draught line 361, water sucting plate 362, elastic plate 363, fixed block 364, institute
It states draught line 361, wash water plate 362, elastic plate 363, fixed block 364 and is respectively provided with two, the elastic plate 363 is embedded in the suction
362 outer ring surface of water plate, the fixed block 364 are mounted on 362 inner surface of water sucting plate, the draught line 361 by way of insertion
Bottom end is fixed together with fixed block 364, therefore can be by absorbing seawater to quickly generate deformation, and passes through shape control
Driver powers on.
Wherein, the propulsive mechanism 38 includes annular groove 381, power blade 382, braking loom 383, and the annular groove 381 is total
If there are four and be integrated with the investigation cylinder 39, the power blade 382 set altogether there are four be correspondingly embedded in described
In annular groove 381 and intermediate ends are fixed on braking 383 outer ring surface of loom by welding, therefore the blade of four page structures can open
Moment generates powerful thrust after moving, and makes the reconnaissance plane hidden independence transfer device after being detached from host is separate rapidly to fall a little.
Wherein, the buoyancy discoloration plate 311 is that the buoyancy after water ripples transition slab and two expansion changes colour 311 groups of plate
Taper one's water breaks structure is synthesized, therefore at sea, it can show for color similar with sea, to have the function that hidden.
Wherein, the connecting plate 321 is fixedly connected by water-soluble connecting rod 323 with 2 bottom end of power wing, therefore energy
After enough air crashes water-soluble connecting rod 323 absorb enabled after seawater melts reconnaissance plane hidden independence transfer device quickly with unmanned owner
Body separation.
The specifically used mode and effect of the present embodiment:
After scounting aeroplane loses kinetic energy generation air crash under by outer signals interference or external impacts in the present invention, by
Reconnaissance plane hidden can independently be transmitted dress when 323 are able to maintain hardened condition when not absorbing salt water by water-soluble connecting rod
It sets 3 to be fixed below unmanned plane, absorbs seawater in the seawater due to impregnating in water-soluble connecting rod 323 after air crash, it is water-soluble
Connecting rod 323 enables reconnaissance plane hidden independence transfer device quick 3 separate with unmanned plane main body after melting after reacting with seawater,
After main body disengaging, buoyancy discoloration plate 311 is unfolded to be provided with solar energy reformer plate due to playing inner surface first, after deployment by it
Exposure, buoyancy change colour plate 311 after deployment respectively to the offer buoyancy support of reconnaissance plane hidden independence transfer device 3, Yi Mianying
It is sunk to for own wt marine, causes the loss of information, while to internal sustainable supply power supply, keeping continuing for driver 357
Work, elastic plate 363 generate deformation after the water suction of water sucting plate 362 swells, and pulling cooperation draught line is matched with water sucting plate 362
361 control truncation valve rods 356 are detached from the isolated area of batteries 354 and driver 357, and the conducting end on both sides is enabled to be in contact, can be with
Driver 357 is set to generate kinetic energy in the short time after the disengaging of reconnaissance plane hidden independence transfer device 3, transportation intelligence is quickly escaped
From being in isolation with seawater because the storage box 352 is in sealing shell 353, do not contact directly, can ensure with seawater
The full storage of data, when reconnaissance plane hidden independence transfer device 3 passes through the attack for hiding unknown of buoyancy discoloration plate
And when escaping from local signal interference area, the recovery operation of information is completed convenient for exploration side by the locator in the storage box 352.
The embodiment of the present invention is given for the purpose of illustration and description, and is not exhaustively or by this to send out
It is bright to be limited to disclosed form.Many modifications and variations are obvious for the ordinary skill in the art.Choosing
Selecting and describe embodiment is and to make those skilled in the art to more preferably illustrate the principle of the present invention and practical application
It will be appreciated that the present invention is to design various embodiments suitable for specific applications with various modifications.
Claims (8)
1. scounting aeroplane damage separation information transfer device in maritime affairs intelligence cruise, structure includes investigation body (1), dynamic
Power wing (2), tailstock (4), promotes paddle (5) at reconnaissance plane hidden independence transfer device (3), it is characterised in that:
Investigation body (1) tail portion is equipped with the propulsion paddle (5), and investigation body (1) outer ring surface leans on caudad one end
It is connected to a fixed by welding with the tailstock (4) top, the power wing (2) sets there are two altogether and passes through respectively
The mode of insertion is fixedly mounted on the left and right sides, the reconnaissance plane hidden among investigation body (1) outer ring surface and independently passes
There are two delivery device (3) is set altogether and its top respectively corresponds the power wing (2) and integrally grows in described investigation body (1) one end
Lower surface is fixedly connected at degree one third.
The reconnaissance plane hidden independence transfer device (3) includes activity float mechanism (31), dissolution releasing mechanism (32), sealing
Connecting tube (33), water-proof CCD camera (34), dual control mechanism (35), water suction spreader mechanism (36), support siphunculus (37), propulsive mechanism
(38), cylinder (39) are investigated, activity float mechanism (31) top passes through the dissolution releasing mechanism (32) and the engine
The wing (2) bottom end is fixed together, and activity float mechanism (31) bottom end and investigation cylinder (39) the outer ring surface top are living
Dynamic to link together, there are two the support siphunculus (37), the branch for the internal upper and lower surface fixed installation of the investigation cylinder (39)
Support siphunculus (37) is intermediate to be fixedly connected on dual control mechanism (35) outer ring surface, the propulsive mechanism (38) by the way of electric welding
It is fixedly mounted on the tail portion of investigation cylinder (39), the propulsive mechanism (38) and the dual control mechanism (35) are far from the sealing
Connecting tube (33) one end is fixed together, and the water-proof CCD camera (34) is fixedly mounted by the sealed joint pipe (33)
In investigation cylinder (39) head end.
2. scounting aeroplane damage separation information transfer device in maritime affairs intelligence cruise as defined in claim 1,
Be characterized in that: the activity float mechanism (31) includes buoyancy discoloration plate (311), high transparency waterproof cover (312), solar energy conversion
Plate (313), spacing mandril (314), torque shaft (315), buoyancy discoloration plate (311), high transparency waterproof cover (312), too
Positive energy reformer plate (313) is respectively provided with two and is mounted on torque shaft (315) left and right ends, the spacing mandril (314)
It is equipped with altogether and is respectively and fixedly installed to torque shaft (315) left and right ends equipped with 20 and ten one group altogether, it is described high saturating
Bright waterproof cover (312) is mounted on buoyancy discoloration plate (311) inside, the solar energy reformer plate by way of insertion
(313) it is internal that buoyancy discoloration plate (311) is mounted on by way of insertion.
3. scounting aeroplane damage separation information transfer device in maritime affairs intelligence cruise as defined in claim 1,
Be characterized in that: the dissolution releasing mechanism (32) includes connecting plate (321), through-hole (322), water-soluble connecting rod (323), described
Through-hole (322) is equipped with nine altogether and is integrated with the connecting plate (321), and the water solubility connecting rod (323) sets altogether
There are nine and intermediate through the through-hole (322).
4. scounting aeroplane damage separation information transfer device in maritime affairs intelligence cruise as defined in claim 1,
Be characterized in that: the dual control mechanism (35) includes transmission line (351), the storage box (352), sealing shell (353), battery
(354), built-in power line (355), truncation valve rod (356), driver (357), torsional spring line wheel (358), the storage box (352)
It is fixed together by the transmission line (351) and the water-proof CCD camera (34), the sealing shell (353) is internal right
End is fixedly installed with the driver (357), and sealing shell (353) bosom is fixedly installed with the battery
(354), left end is fixedly installed with the storage box (352) in sealing shell (353) inside, the truncation valve rod (356)
The connection of the battery (354) Yu the driver (357) is isolated, the battery (354) passes through the built-in power line
(355) it is connected with solar energy reformer plate (313) bottom end, described torsional spring line wheel (358) one end and the water suction spreadboard
Structure (36) one end is flexibly connected.
5. such as scounting aeroplane damage separation information transfer device in maritime affairs intelligence according to claim 1 or 4 cruise,
It is characterized by: the water suction spreader mechanism (36) includes draught line (361), water sucting plate (362), elastic plate (363), fixed block
(364), the draught line (361), wash water plate (362), elastic plate (363), fixed block (364) are respectively provided with two, the elastic force
Plate (363) is embedded in the water sucting plate (362) outer ring surface, and the fixed block (364) is mounted on water sucting plate by way of insertion
(362) inner surface, draught line (361) bottom end are fixed together with fixed block (364).
6. scounting aeroplane damage separation information transfer device in maritime affairs intelligence cruise as defined in claim 1,
Be characterized in that: the propulsive mechanism (38) includes annular groove (381), power blade (382), braking loom (383), the annular groove
(381) it sets there are four and is integrated with the investigation cylinder (39) altogether, the power blade (382) sets that there are four correspondences altogether
It is embedded in the annular groove (381) and intermediate ends is fixed on braking loom (383) outer ring surface by welding.
7. such as scounting aeroplane damage separation information transfer device in maritime affairs intelligence according to claim 2 cruise,
Be characterized in that: buoyancy discoloration plate (311) is buoyancy discoloration plate (311) group after water ripples transition slab and two expansion
Synthesize taper one's water breaks structure.
8. such as scounting aeroplane damage separation information transfer device in maritime affairs intelligence according to claim 3 cruise,
Be characterized in that: the connecting plate (321) is fixedly connected by water-soluble connecting rod (323) with power wing (2) bottom end.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811161365.7A CN109334978B (en) | 2018-09-30 | 2018-09-30 | Unmanned reconnaissance aircraft damage separation information transmission device in maritime intelligent cruise |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811161365.7A CN109334978B (en) | 2018-09-30 | 2018-09-30 | Unmanned reconnaissance aircraft damage separation information transmission device in maritime intelligent cruise |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109334978A true CN109334978A (en) | 2019-02-15 |
| CN109334978B CN109334978B (en) | 2020-10-16 |
Family
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