CN108482669A - The amphibious aircraft of air-sea - Google Patents
The amphibious aircraft of air-sea Download PDFInfo
- Publication number
- CN108482669A CN108482669A CN201810183460.0A CN201810183460A CN108482669A CN 108482669 A CN108482669 A CN 108482669A CN 201810183460 A CN201810183460 A CN 201810183460A CN 108482669 A CN108482669 A CN 108482669A
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- CN
- China
- Prior art keywords
- glider
- nacelle
- umbilical cables
- unmanned plane
- hook
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- 238000007789 sealing Methods 0.000 claims description 25
- 230000005484 gravity Effects 0.000 claims description 6
- 239000000463 material Substances 0.000 claims description 3
- 239000007787 solid Substances 0.000 claims description 2
- 230000000694 effects Effects 0.000 abstract description 10
- 230000007774 longterm Effects 0.000 abstract description 9
- 238000005265 energy consumption Methods 0.000 abstract description 5
- 238000012544 monitoring process Methods 0.000 abstract description 5
- 238000004891 communication Methods 0.000 abstract description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 16
- 230000009471 action Effects 0.000 description 9
- 238000007667 floating Methods 0.000 description 6
- 238000010586 diagram Methods 0.000 description 5
- 238000000034 method Methods 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- 230000007423 decrease Effects 0.000 description 3
- 230000005611 electricity Effects 0.000 description 3
- 230000009467 reduction Effects 0.000 description 2
- 230000008859 change Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 239000013535 sea water Substances 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 210000003954 umbilical cord Anatomy 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63G—OFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
- B63G8/00—Underwater vessels, e.g. submarines; Equipment specially adapted therefor
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C35/00—Flying-boats; Seaplanes
- B64C35/008—Amphibious sea planes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63G—OFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
- B63G8/00—Underwater vessels, e.g. submarines; Equipment specially adapted therefor
- B63G8/001—Underwater vessels adapted for special purposes, e.g. unmanned underwater vessels; Equipment specially adapted therefor, e.g. docking stations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63G—OFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
- B63G8/00—Underwater vessels, e.g. submarines; Equipment specially adapted therefor
- B63G8/14—Control of attitude or depth
- B63G8/20—Steering equipment
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H19/00—Marine propulsion not otherwise provided for
- B63H19/02—Marine propulsion not otherwise provided for by using energy derived from movement of ambient water, e.g. from rolling or pitching of vessels
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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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/27—Adaptation for use in or on movable bodies
- H01Q1/34—Adaptation for use in or on ships, submarines, buoys or torpedoes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63G—OFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
- B63G8/00—Underwater vessels, e.g. submarines; Equipment specially adapted therefor
- B63G8/001—Underwater vessels adapted for special purposes, e.g. unmanned underwater vessels; Equipment specially adapted therefor, e.g. docking stations
- B63G2008/002—Underwater vessels adapted for special purposes, e.g. unmanned underwater vessels; Equipment specially adapted therefor, e.g. docking stations unmanned
- B63G2008/005—Underwater vessels adapted for special purposes, e.g. unmanned underwater vessels; Equipment specially adapted therefor, e.g. docking stations unmanned remotely controlled
- B63G2008/007—Underwater vessels adapted for special purposes, e.g. unmanned underwater vessels; Equipment specially adapted therefor, e.g. docking stations unmanned remotely controlled by means of a physical link to a base, e.g. wire, cable or umbilical
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T70/00—Maritime or waterways transport
- Y02T70/50—Measures to reduce greenhouse gas emissions related to the propulsion system
- Y02T70/5218—Less carbon-intensive fuels, e.g. natural gas, biofuels
- Y02T70/5236—Renewable or hybrid-electric solutions
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Ocean & Marine Engineering (AREA)
- Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
- Details Of Aerials (AREA)
- Emergency Lowering Means (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of amphibious aircraft of air-sea, it includes unmanned plane and glider, it is characterized in that the unmanned plane lower end is connected through caring for device and draft gear with glider, unmanned plane nacelle both sides are respectively symmetrically equipped with solar panel, the solar panel is connected with the controller in the body of unmanned engine room, to reach automatic power, electric energy is provided to controller, for the control of underwater glider, the electronic equipments such as the communication of unmanned plane provide electric energy, make its long-term continue working, the present invention is due to using the above structure, it can rapid reconnaissance, it again can be with long term monitoring, and there is structure novel, it is stable, cruising ability is strong, low energy consumption, it is energy saving, it can automatic power, activity duration is long, the advantages that movement speed is fast.
Description
Technical field
The present invention relates to the unmanned automation equipments of air-sea, specifically a kind of to provide power using wave energy, are dedicated to
The long-range amphibious aircraft of air-sea scouted with long term monitoring.
Background technology
In recent years, the application of unmanned machine is more and more universal, is related to that field is more extensive, and function is also more and more various
Change.But the cruising ability of common unmanned plane is very limited, and energy consumption is big, cannot can be supplied with solar energy as some low power consuming equipment
Electricity, therefore long-term continuous duty can not be executed.Such as naval reconnaissance, the prior art are to use underwater glider, can be made for a long time
Industry, but equipment movement is slow.
Invention content
It is an object of the invention to solve the deficiencies in the prior art, a kind of structure novel, stable, cruising ability are provided
By force, low energy consumption, it is energy saving, can automatic power, the activity duration is long, movement speed is fast, can rapid reconnaissance and can be long-term
The amphibious aircraft of air-sea of monitoring.
The technical solution adopted by the present invention to solve the technical problems is：
A kind of amphibious aircraft of air-sea, including unmanned plane and glider, it is characterised in that the unmanned plane lower end is through caring for device
It is connected with draft gear with glider, unmanned plane nacelle both sides are respectively symmetrically equipped with solar panel, the sun
Energy solar panel is connected with the controller in the body of unmanned engine room, and to reach automatic power, electric energy is provided to controller, is underwater sliding
The electronic equipments such as the control of row device, the communication of unmanned plane provide electric energy, make its long-term continue working, the device of caring for includes a left side
Motor, left spring, left push rod, the soft set of left sealing, upper left hook, lower-left hook, right motor, right spring, right push rod, right sealing are soft
Set, upper right hook and bottom right hook,
The lower-left hook and bottom right hook are respectively separated and are fixed on glider nacelle upper end, and along glider nacelle central axis
It is alternatively arranged, the left soft set of sealing and the soft set of right sealing are separately mounted to unmanned plane nacelle lower wall, and the left push rod seal is worn
It crosses in the soft set of left sealing, the upper end and unmanned engine room body and is hinged, lower end is fixedly connected with upper left hook, the left push rod top
The left side and the left spring in the body of unmanned engine room are inconsistent, and the left motor output shaft being equipped in the right side and unmanned engine room body is inconsistent,
The left spring left end is fixedly connected with the left socle for being fixed on unmanned plane nacelle lower end, and the lower-left hook links up with phase with upper left
Mounting；The right push rod seal passes through to be hinged in the soft set of right sealing, the upper end and unmanned engine room body, and lower end and upper right hook are solid
Fixed connection, the right push rod upper left and the right spring in the body of unmanned engine room are inconsistent, are equipped in the right side and unmanned engine room body
Right motor output shaft it is inconsistent, the right spring left end is fixedly connected with the right support for being fixed on unmanned plane nacelle lower end, institute
Bottom right hook is stated mutually to mount with upper right hook；
The draft gear is located in the body of unmanned engine room comprising umbilical cables driving motor, umbilical cables spool, umbilical cables, spool
Bearing and bearing block, the umbilical cables driving motor and bearing block are separately fixed in the body of unmanned engine room, the umbilical cables spool
Both ends are fixedly connected with the bearing seat through bearing respectively, and the umbilical cables spool drives through umbilical cables driving motor, the umbilical cables
Umbilical cables are wound on spool, described umbilical cables one end is fixed on umbilical cables spool, and the other end slides through unmanned plane lower end
The water-stop threading hole that position of centre of gravity is equipped with is fixedly connected with glider upper end position of centre of gravity, is worn to be connected in the umbilical cables and be led
Line, described conducting wire one end are connected with the controller in the body of unmanned engine room, and the other end is connected with the controller in glider nacelle
Connect, the umbilical cables driving motor, left motor, right motor respectively in the body of unmanned engine room controller be connected, to reach
When glider to be discharged, controller controls left motor, right motor action, and upper left hook and upper right hook is made to be hung respectively with lower-left
Hook and bottom right hook separation, meanwhile, the action of umbilical cables driving motor, umbilical cables decentralization, glider is dived beneath the water, and passes through umbilical cord
Cable traction slide device slides or controls under water the underwater depth of glider, has reached that cruising ability is strong, work of rapid reconnaissance
With.
The present invention can glider nacelle both sides respectively symmetrically and be equipped with along glider nacelle axle center linear array
Wing plate, the wing plate are hinged through shaft and glider nacelle, and the shaft drives through the sliding motor in glider, the cunning
Row motor is controlled through the controller in glider, and to reach the up and down motion for utilizing wave, the unmanned plane by being used as floating body is led
Glider moves up and down under diversion, power is provided to the glider of wave driving, before the unmanned plane to realize wave driving
Into with little need for other energy, the size of forward thrust is proportional to the amplitude difference on sea and lower layer's glider, in wave
Unrestrained propradation, wing plate inclination angle is corresponding with the inclination angle that wave rises, and runs the power for providing advance under water for glider；
Wave declines state, and wing plate rotates under wave action, keeps the inclination angle that wing plate inclination angle declines with wave corresponding, is glider
Operation provides the power to advance under water；State among lifting, that is, when horizontally advancing, wing plate rotates under wave action
To level, advance resistance is reduced when glider being made to run under water, to reach the underwater wing plate by unmanned plane as floating body, profit
With the up and down motion of wave, power is provided to the glider of wave driving, to realize that the unmanned plane of wave driving advances, because
Energy is greatly saved with little need for other energy in this.
The cross section of glider nacelle of the present invention is in back taper, fast to reach reduction glider resistance, movement speed
Effect.
The present invention can be equipped with tail vane, central shaft tail in glider on the central shaft of glider nacelle tail portion
Portion's motor driving, the tail portion motor drive through the controller in glider, to reach in lifting process, to the left by tail vane
Or swing to the right, the underwater direction of glider is adjusted, and then have adjusted the direction of motion.
The present invention can use shaft conducting slip ring at umbilical cables spool center, and the shaft conducting slip ring is through unmanned plane
Interior controller control, so that umbilical cables spool in rotation process, is not limited arbitrary rotation by conducting wire.
The soft set of left sealing and the soft set of right sealing of the present invention are respectively adopted rubber material and are made, with reach flexibility it is good,
The effect of good water-proof effect.
The present invention is due to using the above structure, you can with rapid reconnaissance and can with long term monitoring, and with structure novel,
Stable, cruising ability is strong, low energy consumption, it is energy saving, can automatic power, the advantages that activity duration is long, movement speed is fast.
Description of the drawings
Fig. 1 is original state structural schematic diagram of the present invention.
Fig. 2 is the structural schematic diagram of working condition of the present invention.
Fig. 3 is the structural schematic diagram of unmanned plane in the present invention.
Fig. 4 is the vertical view of glider in Fig. 1.
Fig. 5 is the left view of glider in Fig. 1.
Fig. 6 is the movement schematic diagram of glider tail vane in Fig. 4.
Movement schematic diagram when Fig. 7 is present invention work.
Reference numeral：Unmanned plane 1, glider 2, solar panel 3, left motor 4, left spring 5, left push rod 6, left sealing
It is soft set 7, upper left hook 8, lower-left hook 9, right motor 10, right spring 11, right push rod 12, it is right sealing it is soft set 13, upper right hook 14,
Bottom right hook 15, left socle 16, right support 17, umbilical cables driving motor 18, umbilical cables spool 19, umbilical cables 20, bearing block 21,
Wing plate 22, shaft 23, tail vane 24.
Specific implementation mode
The present invention will be described with reference to the accompanying drawings and examples.
As shown in the picture, the amphibious aircraft of a kind of air-sea, including unmanned plane 1 and glider 2, the structure and cunning of unmanned plane 1
The structure of row device 2 is same as the prior art, this is not repeated, it is characterised in that 1 lower end of the unmanned plane is through caring for device and traction
Device is connected with glider 2, and 1 nacelle both sides of the unmanned plane are respectively symmetrically equipped with solar panel 3, the solar-electricity
Pond plate 3 is connected with the controller in 1 nacelle of unmanned plane, to reach automatic power, electric energy is provided to controller, to slide under water
The electronic equipments such as the control of device, the communication of unmanned plane provide electric energy, make its long-term continue working, the device of caring for includes left electricity
Machine 4, left spring 5, left push rod 6, the soft set 7 of left sealing, upper left hook 8, lower-left hook 9, right motor 10, right spring 11, right push rod
12, the soft set 13 of right sealing, upper right hook 14 and bottom right hook 15,
The lower-left hook 9 and bottom right hook 15 are respectively separated and are fixed on 2 nacelle upper end of glider, and along 2 nacelle of glider
Mandrel line is alternatively arranged, and the left soft set 7 of sealing and the right soft set 13 that seals are separately mounted to 1 nacelle lower wall of unmanned plane, the left side
Left articulated shaft in the soft set 7 of the left sealing of 6 hermetically passing of push rod, 1 nacelle of the upper end and unmanned plane is hinged, and lower end is linked up with upper left
8 are fixedly connected, and 6 upper left of left push rod and the left spring 5 in 1 nacelle of unmanned plane are inconsistent, the right side and 1 nacelle of unmanned plane
4 output shaft of left motor being inside equipped with is inconsistent, 5 left end of the left spring and the left socle 16 for being fixed on 1 nacelle lower end of unmanned plane
It is fixedly connected, the lower-left hook 9 links up with the mounting of 8 phases with upper left；The soft set 13 of the right sealing of 12 hermetically passing of right push rod, thereon
End is hinged with the right articulated shaft in 1 nacelle of unmanned plane, and lower end is fixedly connected with upper right hook 14, and 12 top of right push rod is left
Face and the right spring 11 in 1 nacelle of unmanned plane are inconsistent, and 10 output shaft of right motor being equipped in the right side and 1 nacelle of unmanned plane offsets
Touch, 11 left end of right spring is fixedly connected with the right support 17 for being fixed on 1 nacelle lower end of unmanned plane, bottom right hook 15 and
Upper right links up with the mounting of 14 phases；
The draft gear is located in 1 nacelle of unmanned plane comprising umbilical cables driving motor 18, umbilical cables spool 19, umbilical cables
20, spool bearing and bearing block 21, the umbilical cables driving motor 18 and bearing block 21 are separately fixed in 1 nacelle of unmanned plane,
19 both ends of umbilical cables spool are fixedly connected through bearing with bearing block 21 respectively, and the umbilical cables spool 19 drives through umbilical cables
Motor 18 drives, and is wound with umbilical cables 20 on the umbilical cables spool 19,20 one end of the umbilical cables is fixed on umbilical cables spool
On 19, the other end slides through the water-stop threading hole and glider upper end position of centre of gravity that unmanned plane lower end position of centre of gravity is equipped with
It is fixedly connected, is worn in the umbilical cables and be connected to conducting wire, described conducting wire one end is connected with the controller in the body of unmanned engine room, another
End be connected with the controller in glider nacelle, the umbilical cables driving motor 18, left motor 4, right motor 10 respectively with nothing
Controller in man-machine 1 nacelle is connected, and to reach when glider to be discharged, controller controls left motor 4, right motor 10
Action makes upper left hook 8 and upper right hook 14 be detached respectively with lower-left hook 9 and bottom right hook 15, meanwhile, umbilical cables driving electricity
Machine 18 acts, and umbilical cables 20 are transferred, and glider 2 dives beneath the water, and slided under water by 20 traction slide device 2 of umbilical cables or
2 underwater depth of glider is controlled, has haved the function that cruising ability is strong, rapid reconnaissance.
The present invention can 2 nacelle both sides of the glider respectively symmetrically and set along glider nacelle axle center linear array
There are wing plate 22, the wing plate 22 to be hinged through shaft and 1 nacelle of glider, the shaft is driven through the sliding motor in glider
Dynamic, the sliding motor is controlled through the controller in glider, to reach the up and down motion for utilizing wave, by being used as floating body
Unmanned plane 1 draws underwater glider 2 and moves up and down, and power is provided to the glider of wave driving, to realize that wave drives
Unmanned plane advance, with little need for other energy, size and sea and the amplitude difference of underwater glider of forward thrust
Proportional, in wave propradation, 22 inclination angle of wing plate is corresponding with the inclination angle that wave rises, such as Fig. 7（It is right）It is shown, it is glider
2 power that operation offer is advanced under water；Decline state in wave, wing plate 22 rotates under wave action, and wing plate 22 is made to incline
Angle is corresponding with the inclination angle that wave declines, such as Fig. 7（In）It is shown, run the power that advance is provided under water for glider 2；It is rising
Intermediate state drops, that is, when horizontally advancing, wing plate 22 is rotated under wave action to level, inclination angle such as Fig. 7（It is left）It is shown, make
Glider 2 reduces advance resistance when running under water, to reach the underwater wing plate by unmanned plane as floating body, utilizes wave
It moves up and down, power is provided to the glider of wave driving, to realize that the unmanned plane of wave driving advances, therefore, hardly
Other energy are needed, energy is greatly saved.
The cross section of 2 nacelle of glider of the present invention is in back taper, fast to reach reduction glider resistance, movement speed
Effect.
The present invention can be equipped with tail vane 24 on the central shaft of 2 nacelle tail portion of the glider, and the central shaft is through glider
Interior tail portion motor driving, the tail portion motor drive through the controller in glider, to reach in lifting process, pass through tail vane
24 leftward or rightward swings adjust the underwater direction of glider, and then have adjusted the direction of motion.
The present invention can use shaft conducting slip ring at 19 center of umbilical cables spool, and the shaft conducting slip ring is through nobody
Controller control in machine, so that umbilical cables spool in rotation process, is not limited arbitrary rotation by conducting wire.
The soft set 7 of left sealing of the present invention and the soft set of right sealing 13 are respectively adopted rubber material and are made, to reach flexibility
Good, good water-proof effect effect.
At work, unmanned plane carries glider and carries out investigations to specified marine site the present invention, and unmanned plane carries glider
It is moved down to marine, after glider touches seawater, the controller in unmanned plane controls left motor 4, right motor 10 acts, upper left
Hook 8 and upper right hook 14 are detached with lower-left hook 9 and bottom right hook 15 respectively, meanwhile, umbilical cables driving motor 18 acts, navel
Band cable 20 is transferred, and glider 2 is dived beneath the water, and slides or control under water glider 2 by 20 traction slide device 2 of umbilical cables
Underwater depth, at this point, unmanned plane as float across the sea, the unmanned plane 1 by being used as floating body draws underwater cunning
Row device 2 moves up and down, and provides power to the glider of wave driving, several to realize that the unmanned plane of wave driving advances
Other energy are not needed, the size and the amplitude difference of sea and underwater glider of forward thrust are in direct ratio, in wave
Propradation, 22 inclination angle of wing plate is corresponding with the inclination angle that wave rises, such as Fig. 7（It is right）It is shown, it runs and carries under water for glider 2
For the power of advance；Decline state in wave, wing plate 22 rotates under wave action, and 22 inclination angle of wing plate is made to decline with wave
Inclination angle is corresponding, such as Fig. 7（In）It is shown, run the power that advance is provided under water for glider 2；State among lifting,
When horizontally advancing, wing plate 22 is rotated under wave action to level, inclination angle such as Fig. 7（It is left）It is shown, make glider 2 under water
Advance resistance is reduced when operation, to reach the underwater wing plate by unmanned plane as floating body, using the up and down motion of wave, gives wave
The glider of wave driving provides power, to realize that the unmanned plane of wave driving advances, therefore, with little need for other energy
Amount, is greatly saved energy；During lifting, by the movement of tail vane, the underwater direction of glider is adjusted.
The present invention is due to using the above structure, you can with rapid reconnaissance and can with long term monitoring, and with structure novel,
Stable, cruising ability is strong, low energy consumption, it is energy saving, can automatic power, the advantages that activity duration is long, movement speed is fast.
Claims (6)
1. a kind of amphibious aircraft of air-sea, including unmanned plane and glider, it is characterised in that the unmanned plane lower end is through caring for dress
Set and be connected with draft gear with glider, unmanned plane nacelle both sides respectively symmetrically be equipped with solar panel, it is described too
It is positive can solar panel be connected with the controller in the body of unmanned engine room, it is described care for device include left motor, left spring, left push rod,
Left soft set, upper left hook, lower-left hook, right motor, right spring, right push rod, the soft set of right sealing, upper right hook and the bottom right of sealing is hung
Hook,
The lower-left hook and bottom right hook are respectively separated and are fixed on glider nacelle upper end, and along glider nacelle central axis
It is alternatively arranged, the left soft set of sealing and the soft set of right sealing are separately mounted to unmanned plane nacelle lower wall, and the left push rod seal is worn
It crosses in the soft set of left sealing, the upper end and unmanned engine room body and is hinged, lower end is fixedly connected with upper left hook, the left push rod top
The left side and the left spring in the body of unmanned engine room are inconsistent, and the left motor output shaft being equipped in the right side and unmanned engine room body is inconsistent,
The left spring left end is fixedly connected with the left socle for being fixed on unmanned plane nacelle lower end, and the lower-left hook links up with phase with upper left
Mounting；The right push rod seal passes through to be hinged in the soft set of right sealing, the upper end and unmanned engine room body, and lower end and upper right hook are solid
Fixed connection, the right push rod upper left and the right spring in the body of unmanned engine room are inconsistent, are equipped in the right side and unmanned engine room body
Right motor output shaft it is inconsistent, the right spring left end is fixedly connected with the right support for being fixed on unmanned plane nacelle lower end, institute
Bottom right hook is stated mutually to mount with upper right hook；
The draft gear is located in the body of unmanned engine room comprising umbilical cables driving motor, umbilical cables spool, umbilical cables, spool
Bearing and bearing block, the umbilical cables driving motor and bearing block are separately fixed in the body of unmanned engine room, the umbilical cables spool
Both ends are fixedly connected with the bearing seat through bearing respectively, and the umbilical cables spool drives through umbilical cables driving motor, the umbilical cables
Umbilical cables are wound on spool, the umbilical cables are fixed and are wrapped on umbilical cables spool, described umbilical cables one end and unmanned plane
Controller in nacelle is connected, and the other end slides through the water-stop threading hole and cunning that unmanned plane lower end position of centre of gravity is equipped with
Row device upper end position of centre of gravity is fixedly connected, and is worn in the umbilical cables and is connected to conducting wire, in described conducting wire one end and unmanned engine room body
Controller is connected, and the other end is connected with the controller in glider nacelle, the umbilical cables driving motor, left motor, the right side
Motor respectively in the body of unmanned engine room controller be connected.
2. the amphibious aircraft of a kind of air-sea according to claim 1, it is characterised in that distinguish glider nacelle both sides
It symmetrically and along glider nacelle axle center linear array is equipped with wing plate, the wing plate is hinged through shaft and glider nacelle, institute
It states shaft to drive through the sliding motor in glider, the sliding motor is controlled through the controller in glider.
3. the amphibious aircraft of a kind of air-sea according to claim 1 or 2, it is characterised in that the glider nacelle it is transversal
Face is in back taper.
4. the amphibious aircraft of a kind of air-sea according to claim 3, it is characterised in that in glider nacelle tail portion
Mandrel is equipped with tail vane, and central shaft tail portion motor in glider drives, and the tail portion motor is through the control in glider
Device drives.
5. the amphibious aircraft of a kind of air-sea according to claim 1, it is characterised in that umbilical cables spool center uses
Shaft conducting slip ring, the shaft conducting slip ring are controlled through the controller in unmanned plane.
6. the amphibious aircraft of a kind of air-sea according to claim 1, it is characterised in that the left soft set of sealing and right sealing
Soft set is respectively adopted rubber material and is made.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810155002 | 2018-02-23 | ||
| CN2018101550026 | 2018-02-23 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108482669A true CN108482669A (en) | 2018-09-04 |
| CN108482669B CN108482669B (en) | 2020-12-29 |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109334978A (en) * | 2018-09-30 | 2019-02-15 | 李元芳 | Scounting aeroplane damage separation information transfer device in maritime affairs intelligence cruise |
| CN109436321A (en) * | 2018-10-25 | 2019-03-08 | 南京理工大学 | A kind of water sky of bionical electric ray is dual-purpose to detect dozen type unmanned plane |
| CN114684341A (en) * | 2022-04-28 | 2022-07-01 | 中国船舶科学研究中心 | Underwater observation device and operation method |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109229362A (en) * | 2018-11-26 | 2019-01-18 | 吉林大学 | A kind of combined type unmanned plane applied to hydrospace detection |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH09287896A (en) * | 1996-04-23 | 1997-11-04 | Nec Corp | Towing device |
| JP2002250766A (en) * | 2001-02-22 | 2002-09-06 | Nec Corp | Method and system for underwater towed body position measurement |
| US20110162573A1 (en) * | 2009-06-12 | 2011-07-07 | Race Roger E | Towed antenna system and method |
| CN206307246U (en) * | 2016-10-28 | 2017-07-07 | 杭州电子科技大学 | A kind of unmanned boat adds the combined system of unmanned submersible |
| US20180050797A1 (en) * | 2016-08-22 | 2018-02-22 | Harris Corporation | Tethered unmanned aerial vehicle |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP3860430B2 (en) * | 2001-04-13 | 2006-12-20 | 三菱電機株式会社 | Rescue signal transmitter |
| GB0803834D0 (en) * | 2008-02-29 | 2008-04-09 | Strachan & Henshaw Ltd | Buoy |
| CN201914465U (en) * | 2010-12-31 | 2011-08-03 | 航宇救生装备有限公司 | Safeguard station swim bladder |
| CN203553328U (en) * | 2013-09-12 | 2014-04-16 | 西南交通大学 | Underwater telescopic antenna |
| CN104149966A (en) * | 2014-07-30 | 2014-11-19 | 中国电子科技集团公司第三十八研究所 | Air bag of integrated tile type antenna array front |
| CN205982618U (en) * | 2016-07-18 | 2017-02-22 | 合肥佳瑞林电子技术有限公司 | Radar detection device under water |
-
2018
- 2018-03-06 CN CN201810183632.4A patent/CN108482621B/en active Active
- 2018-03-06 CN CN201810183460.0A patent/CN108482669B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH09287896A (en) * | 1996-04-23 | 1997-11-04 | Nec Corp | Towing device |
| JP2002250766A (en) * | 2001-02-22 | 2002-09-06 | Nec Corp | Method and system for underwater towed body position measurement |
| US20110162573A1 (en) * | 2009-06-12 | 2011-07-07 | Race Roger E | Towed antenna system and method |
| US20180050797A1 (en) * | 2016-08-22 | 2018-02-22 | Harris Corporation | Tethered unmanned aerial vehicle |
| CN206307246U (en) * | 2016-10-28 | 2017-07-07 | 杭州电子科技大学 | A kind of unmanned boat adds the combined system of unmanned submersible |
Non-Patent Citations (1)
| Title |
|---|
| 张丽娟: "潜射无人机：空海两栖作战"秃鹰"", 《科技日报》 * |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109334978A (en) * | 2018-09-30 | 2019-02-15 | 李元芳 | Scounting aeroplane damage separation information transfer device in maritime affairs intelligence cruise |
| CN109436321A (en) * | 2018-10-25 | 2019-03-08 | 南京理工大学 | A kind of water sky of bionical electric ray is dual-purpose to detect dozen type unmanned plane |
| CN114684341A (en) * | 2022-04-28 | 2022-07-01 | 中国船舶科学研究中心 | Underwater observation device and operation method |
| CN114684341B (en) * | 2022-04-28 | 2023-02-28 | 中国船舶科学研究中心 | Underwater observation device and operation method |
Also Published As
| Publication number | Publication date |
|---|---|
| CN108482621A (en) | 2018-09-04 |
| CN108482669B (en) | 2020-12-29 |
| CN108482621B (en) | 2020-02-14 |
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