CN109250114A - A kind of structure improved sensorcraft waterborne - Google Patents
A kind of structure improved sensorcraft waterborne Download PDFInfo
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- CN109250114A CN109250114A CN201811277943.3A CN201811277943A CN109250114A CN 109250114 A CN109250114 A CN 109250114A CN 201811277943 A CN201811277943 A CN 201811277943A CN 109250114 A CN109250114 A CN 109250114A
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- fixing axle
- piston
- drone body
- inlet pipe
- battery
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- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 142
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims abstract description 16
- 238000010248 power generation Methods 0.000 claims abstract description 14
- 238000007667 floating Methods 0.000 claims description 46
- 238000007599 discharging Methods 0.000 claims description 22
- 238000009434 installation Methods 0.000 claims description 15
- 238000000034 method Methods 0.000 abstract description 4
- 238000001514 detection method Methods 0.000 description 11
- 230000005611 electricity Effects 0.000 description 10
- 230000015572 biosynthetic process Effects 0.000 description 6
- 230000001681 protective effect Effects 0.000 description 5
- 230000005674 electromagnetic induction Effects 0.000 description 3
- 230000006698 induction Effects 0.000 description 3
- 239000007787 solid Substances 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 230000008901 benefit Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000002146 bilateral effect Effects 0.000 description 1
- 230000003139 buffering effect Effects 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 230000005389 magnetism Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
- 238000004804 winding 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
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/54—Floats
- B64C25/56—Floats inflatable
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/24—Aircraft characterised by the type or position of power plant using steam, electricity, or spring force
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03B—MACHINES OR ENGINES FOR LIQUIDS
- F03B13/00—Adaptations of machines or engines for special use; Combinations of machines or engines with driving or driven apparatus; Power stations or aggregates
- F03B13/12—Adaptations of machines or engines for special use; Combinations of machines or engines with driving or driven apparatus; Power stations or aggregates characterised by using wave or tide energy
- F03B13/14—Adaptations of machines or engines for special use; Combinations of machines or engines with driving or driven apparatus; Power stations or aggregates characterised by using wave or tide energy using wave energy
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
-
- 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
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/30—Energy from the sea, e.g. using wave energy or salinity gradient
-
- 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
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Abstract
The present invention provides a kind of structure improved sensorcrafts waterborne, belong to air vehicle technique field.The present invention includes drone body, the surrounding of the drone body is equipped with rotor, pedestal is equipped with below four rotors, there is in the pedestal equipped with lower end the storage chamber of opening, extension airbag is equipped in the storage chamber, the pedestal is equipped with compressed gas cylinder, the compressed gas cylinder is connected by pipe with extension airbag, the gas outlet of the compressed gas cylinder is equipped with solenoid valve one, cavity is equipped in the drone body, controller and battery are equipped in the cavity, the solenoid valve one is electrically connected by controller with battery, two sides below the drone body are respectively equipped with can be such that drone body swims on the water surface when unmanned plane drop to the water surface, the power generator of power generation can also be can be carried out using wave, the power generator is electrically connected with battery.The configuration of the present invention is simple can prevent unmanned plane damage in accidental falling.
Description
Technical field
The invention belongs to air vehicle technique fields, are related to a kind of structure improved sensorcraft waterborne.
Background technique
Unmanned plane is to utilize the not manned aircraft of radio robot and the presetting apparatus provided for oneself manipulation, unmanned plane
Structure is simple, use cost is low, has obtained in the fields such as field construction, exploration, communications and transportation, tourism, live game coverage extensively
Using.
Unmanned plane is also used for detection operations waterborne at present, using the mobility of unmanned plane, shortens detection time, saves
The cost of artificial detection, but there is also some factors of instability for unmanned plane detection waterborne, when water surface stormy waves is larger, nothing
Man-machine be possibly blown falls in water, due to not having to buffer and provide the device of buoyancy on unmanned plane, directly contacts the water surface and is easy to make
At damage；Further, since unmanned plane limited battery capacity, needs to return to charging when there is not enough power supply, leads to detection mission
It can not be carried out continuously.
Summary of the invention
The purpose of the present invention is there is the above problem in view of the prior art, a kind of structure improved detection waterborne is proposed
Unmanned plane can prevent unmanned plane from surprisingly falling and be damaged, additionally it is possible to give the unmanned plane for falling to the water surface to fill using wave energy
Electricity improves cruising ability.
Object of the invention can be realized by the following technical scheme: a kind of structure improved sensorcraft waterborne, packet
Drone body is included, the surrounding of the drone body is equipped with rotor, is equipped with pedestal below four rotors, described
There is in pedestal equipped with lower end the storage chamber of opening, extension airbag is equipped in the storage chamber, the pedestal is equipped with compressed gas
Bottle, the compressed gas cylinder are connected by pipe with extension airbag, and the gas outlet of the compressed gas cylinder is equipped with solenoid valve one, institute
State and be equipped with cavity in drone body, be equipped with controller and battery in the cavity, the solenoid valve one by controller with
Battery is electrically connected, and the two sides below the drone body, which are respectively equipped with, can make unmanned plane when unmanned plane drop to the water surface
Ontology is swum on the water surface, moreover it is possible to can be carried out the power generator of power generation, two power generator bilateral symmetries using wave
Setting, the power generator are electrically connected with battery.
When unmanned plane is when executing detection mission waterborne, there is biggish stormy waves, when making unmanned plane that accidental falling occur, this
When the solenoid valve one on compressed gas cylinder opened by controller, discharge the compressed air in compressed gas cylinder, compressed air passes through pipe
Son enters in extension airbag, and extension airbag expands downwards rapidly, and four in drone body extension airbags is made first to contact water
Buffer function is played in face, and four extension airbags can also be such that drone body steadily swims on the water surface, and stormy waves is waited to continue to hold later
Row detection mission；In addition, making it drop to the water surface automatically by controller when the case where not enough power supply occurs in unmanned plane, send out
Electric installation can be such that drone body swims on the water surface, can be carried out power generation using wave, and electric energy is stored in battery
It is interior, improve the cruising ability of unmanned plane.
In the above-mentioned structure improved sensorcraft waterborne of one kind, the cavity is equipped with gyroscope, the gyro
Instrument is electrically connected by controller with battery.
When shaking by a relatively large margin occurs in drone body, the signal of change in location can be sent to by the gyroscope
Controller, controller open the solenoid valve one of compressed gas cylinder in advance, inflate to extension airbag, prevent drone body from hurtling down
Directly hit the water surface.
In the above-mentioned structure improved sensorcraft waterborne of one kind, the lower end of the extension airbag is vertically arranged with row
Tracheae, the exhaust pipe are equipped with solenoid valve two, and the solenoid valve two is electrically connected by controller with battery.
After stormy waves, controller opens the solenoid valve two on exhaust pipe, the compressed air in four extension airbags from
The discharge of respective exhaust pipe, gives drone body to provide a upward thrust, takes off power-assisted to unmanned plane, make its it is quick on
It rises, reduces the consumption of electric energy when taking off.
In the above-mentioned structure improved sensorcraft waterborne of one kind, the power generator include fixing axle, two it is solid
Fixed board one and two connecting rod one, two fixed plates one are vertically arranged on the downside of drone body, and two described solid
Fixed board one and two connecting rod one corresponds, and one end of the connecting rod one is hinged by articulated shaft and corresponding fixed plate one,
The other end of two connecting rods one is respectively fixedly connected in fixing axle, and the fixing axle is horizontally disposed, the both ends of the fixing axle
Be respectively equipped with can limit fixing axle rotated on the position-limit mechanism of articulated shaft slewing area, the fixing axle be provided with it is cylindric
Floating body, the length direction of the outer lateral edge floating body of the floating body is circumferentially uniformly provided with several rotating vanes, and the floating body is located at two
Being equipped between connecting rod one, in the floating body can drive floating body to rotate the power generation mechanism to generate electricity using wave.
When unmanned plane drops to the water surface, four extension airbags and two floating bodies contact the water surface simultaneously, play buffer function,
Buoyancy can also be provided to drone body simultaneously, float on it on water surface, the rotating vane on floating body is driven by wave stroke
Floating body is rotated around fixing axle, and power generation mechanism is generated electricity using the rotation of floating body, environmentally protective；The position-limit mechanism can limit
Determine slewing area of the fixing axle around articulated shaft, fixing axle is avoided to cross ambassador's drone body contact water around the rotational angle of articulated shaft
Face is turned on one's side, and the stability of unmanned plane charging waterborne is improved；In addition, when unmanned plane drops to ground, it can basis
Different landform adjusts the height of two floating bodies, so that drone body is kept horizontality, avoids turning on one's side.
In the above-mentioned structure improved sensorcraft waterborne of one kind, the power generation mechanism includes permanent magnet one, permanent magnetism
Iron two and coil, the floating body is interior to be equipped with installation cavity, and the magnet one and magnet two are oppositely arranged on the side wall of installation cavity, and
And magnetic pole in the fixing axle on the contrary, be arranged in parallel there are two through-hole one, two through-holes one are located at the two of installation cavity
End, the axis of two through-holes one are vertical with the axis of fixing axle and in the same plane, and the coil is logical by two
Hole one is wrapped in the outside of fixing axle, and the coil is electrically connected with battery.
Since two floating bodies are rotated by wave stroke around fixing axle, make permanent magnet one, the permanent magnet two in installation cavity
It relatively rotates with the coil wound in fixing axle, according to electromagnetic induction principle, coil cuts permanent magnet one and permanent magnet two
Magnetic induction line, generate induced current, electric energy is stored in battery, it is environmentally protective.
In the above-mentioned structure improved sensorcraft waterborne of one kind, the position-limit mechanism includes fixed plate two, connecting rod
Two, piston rod and piston cylinder, the piston cylinder are vertically arranged on the side wall of drone body by bracket, the piston rod
One end is located in piston cylinder and end is installed with piston, and the other end of the piston rod stretches out piston cylinder and end is fixed with connection
Column, the piston are slidably arranged in piston cylinder, and the piston will be divided into epicoele and cavity of resorption inside piston cylinder, the epicoele is under
Intracavitary to fill water, the top of the epicoele is equipped with upper water inlet pipe and upper water-out pipe, and the bottom of the cavity of resorption is equipped with lower water inlet pipe
And lower discharging tube, the upper side of the drone body are equipped with water tank, the upper water inlet pipe, upper water-out pipe, lower water inlet pipe
It is connected with water tank with lower discharging tube, is equipped with list on the upper water inlet pipe, upper water-out pipe, lower water inlet pipe and lower discharging tube
To valve, the upper cover of piston rod be equipped with reset spring, the reset spring between piston and piston cylinder, the connecting column
Outside is equipped with fixed plate three, and the fixed plate three and one end of connecting rod two are hinged, the other end and fixed plate two of the connecting rod two
One end it is hinged, the end of the other end of the fixed plate two and fixing axle is connected.
When wave stroke floating body rotates fixing axle around the outside of hinged axial drone body, driven by connecting rod two
Piston rod and piston slide downward, the reset spring on piston rod are compressed, and the reset spring can limit fixing axle around hinge
The range that spindle is turned out, is always positioned at drone body on the water surface, when piston slide downward, under intracavitary water by
It is flowed into water tank to squeezing from lower discharging tube, while upper intracavitary formation negative pressure, upper water inlet pipe draw water from water tank to epicoele
It is interior；When wave stroke floating body rotates fixing axle around the inside of hinged axial drone body, by connecting rod two with piston
Bar and piston upward sliding, the reset spring on piston rod are stretched, and the reset spring can limit fixing axle around articulated shaft
The range inwardly rotated prevents from closely drone body being made to turn on one's side very much due to two floating body distances, when piston upward sliding,
Upper intracavitary water, which is squeezed from upper water-out pipe, to be flowed into water tank, at the same under intracavitary formation negative pressure, lower water inlet pipe is from water storage
Case draws water under intracavitary；Further, since the setting of check valve be so that upper water inlet pipe and lower water inlet pipe can only intake, upper water-out pipe and
Lower discharging tube can only be discharged, it is ensured that piston cylinder works normally, and works as a buffer to unmanned plane landing.
In the above-mentioned structure improved sensorcraft waterborne of one kind, the upper water inlet pipe, upper water-out pipe, lower water inlet pipe
It is provided with generator with branch is passed through in the through-hole of lower discharging tube, the input shaft end of the generator is equipped with impeller, the hair
Motor is electrically connected with battery.
When piston rod band piston slide downward, under intracavitary water be squeezed from lower discharging tube and be flowed into water tank
It is interior, while upper intracavitary formation negative pressure, upper water inlet pipe draw water from water tank to upper intracavitary, in upper water inlet pipe and lower discharging tube water flow
The dynamic wheel rotation driven in respective through-hole, makes electrical power generators；When piston rod band piston upward sliding, upper intracavitary water
Be squeezed from upper water-out pipe and be flowed into water tank, at the same under intracavitary formation negative pressure, lower water inlet pipe draws water from water tank under
Intracavitary, the water flowing in upper water-out pipe and lower water inlet pipe drives the wheel rotation in respective through-hole, makes electrical power generators again, will
Wave energy is converted into electric energy, improves the utilization rate of wave energy.
Compared with prior art, the invention has the following advantages that
1, when unmanned plane is when executing detection mission waterborne, there is biggish stormy waves, make unmanned plane that biggish shaking occur
When, position variation signal is sent to controller by gyroscope, and controller opens the solenoid valve one on compressed gas cylinder, release pressure in advance
Compressed air in contracting gas cylinder, compressed air are entered in extension airbag by pipe, and extension airbag expands downwards rapidly, work as nothing
Man-machine when being blown off by stormy waves to the water surface, four extension airbags and two floating bodies first contact the water surface, play buffer function, and four flexible
Air bag can also be such that drone body steadily swims on the water surface, after waiting stormy waves, open the electromagnetism on exhaust pipe by controller
The compressed air in four extension airbags is discharged from respective exhaust pipe in valve two, provides a upward thrust to unmanned plane,
It takes off power-assisted to unmanned plane, makes its rapid increase, reduce the consumption of electric energy when taking off；
2, when the case where not enough power supply occurs in unmanned plane, the water surface is dropped to by controller automatically, utilizes wave stroke
Blade on floating body drives floating body to rotate around fixing axle, makes on the permanent magnet one and permanent magnet two and fixing axle in installation cavity
The coil of winding relatively rotates, and according to electromagnetic induction principle, coil cuts the magnetic induction line of permanent magnet one and permanent magnet two, produces
Raw induced current, electric energy is stored in battery, environmentally protective；
3, it when wave stroke floating body rotates fixing axle around the outside of hinged axial unmanned plane, is driven and is lived by connecting rod two
Stopper rod and piston slide downward, the reset spring on piston rod are compressed, and the reset spring can limit fixing axle around hinged
The range that axis is turned out, is always positioned at unmanned plane on the water surface, when wave stroke floating body makes fixing axle around hinged axial nothing
When man-machine inside rotates, piston rod and piston upward sliding are driven by connecting rod two, the reset spring on piston rod is stretched,
The reset spring can limit the range that fixing axle is inwardly rotated around articulated shaft, prevent from closely making very much nothing due to two floating body distances
It is man-machine to turn on one's side；
4, when piston rod band piston slide downward, under intracavitary water be squeezed from lower discharging tube and be flowed into water tank
It is interior, while upper intracavitary formation negative pressure, upper water inlet pipe draw water from water tank to upper intracavitary, in upper water inlet pipe and lower discharging tube water flow
The dynamic wheel rotation driven in respective through-hole, makes electrical power generators；When piston rod band piston upward sliding, upper intracavitary water
Be squeezed from upper water-out pipe and be flowed into water tank, at the same under intracavitary formation negative pressure, lower water inlet pipe draws water from water tank under
Intracavitary, the water flowing in upper water-out pipe and lower water inlet pipe drives the wheel rotation in respective through-hole, makes electrical power generators again, will
Wave energy is converted into electric energy, improves the utilization rate of wave energy.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of this structure improved sensorcraft waterborne；
Fig. 2 is the cross-sectional view in Fig. 1 at A-A；
Fig. 3 is the cross-sectional view in Fig. 1 at B-B；
Fig. 4 is the cross-sectional view in Fig. 1 at C-C；
Fig. 5 is the partial enlarged view in Fig. 1 at D；
Structural schematic diagram when Fig. 6 is extension airbag inflation；
Fig. 7 is the partial sectional view of upper water inlet pipe, upper water-out pipe, lower water inlet pipe, lower discharging tube.
In figure: 1, drone body；1a, rotor；1b, cavity；1c, controller；1d, battery；1e, fixed plate one；1f,
Articulated shaft；2, floating body；2a, installation cavity；2b, permanent magnet one；2c, permanent magnet two；2d, rotating vane；3, fixing axle；3a, through-hole one；
3b, connecting rod one, 3c, connecting rod two；3d, fixed plate two；4, coil；5, connecting column；5a, fixed plate three；6, piston rod；6a, piston
Cylinder；6b, piston；6c, reset spring；7, epicoele；7a, upper water inlet pipe；7b, upper water-out pipe；8, cavity of resorption；8a, lower water inlet pipe；8b,
Lower discharging tube；9, camera；10, pedestal；10a, storage chamber；10b, compressed gas cylinder；11, extension airbag；12, gyroscope；13, it stores up
Water tank；14, generator；14a, impeller.
Specific embodiment
Following is a specific embodiment of the present invention in conjunction with the accompanying drawings, technical scheme of the present invention will be further described,
However, the present invention is not limited to these examples.
As shown in Fig. 1 to 7, a kind of structure improved sensorcraft waterborne, including drone body 1, the unmanned plane
The surrounding of ontology 1 is equipped with rotor 1a, and pedestal 10 is equipped with below four rotor 1a, is equipped with lower end in the pedestal 10
Extension airbag 11 is equipped in storage chamber 10a, the storage chamber 10a with opening, the pedestal 10 is equipped with compressed gas cylinder
10b, the compressed gas cylinder 10b are connected by pipe with extension airbag 11, and the gas outlet of the compressed gas cylinder 10b is equipped with electricity
Magnet valve one, the drone body 1 is interior to be equipped with cavity 1b, is equipped with controller 1c and battery 1d, the electricity in the cavity 1b
Magnet valve one is electrically connected by controller 1c with battery 1d, and the two sides of 1 lower section of drone body, which are respectively equipped with, works as unmanned plane
Drone body 1 can be made to swim on the water surface when droping to the water surface, moreover it is possible to it can be carried out the power generator of power generation using wave,
Two power generator are symmetrical set, and the power generator is electrically connected with battery 1d.
Unmanned plane carries out detection waterborne using camera 9, when stormy waves waterborne is larger, makes unmanned plane that accidental falling occur
When, the solenoid valve one on compressed gas cylinder 10b is opened by controller 1c at this time, discharges the compressed air in compressed gas cylinder 10b, pressure
Contracting air is entered in extension airbag 11 by pipe, and the expansion downwards rapidly of extension airbag 11 makes four in drone body 1
Extension airbag 11 first contacts the water surface, plays buffer function, and four extension airbags 11 can also make drone body 1 steadily swim in water
On face, stormy waves is waited to continue to execute detection mission later；In addition, passing through controller when the case where not enough power supply occurs in unmanned plane
1c makes it drop to the water surface automatically, and power generator can be such that drone body 1 swims on the water surface, can be carried out hair using wave
Electricity, and electric energy is stored in battery 1d, improve the cruising ability of unmanned plane.
Specifically, the cavity 1b is equipped with gyroscope 12, and the gyroscope 12 passes through controller 1c and battery 1d
Electrical connection.
When shaking by a relatively large margin occurs in drone body 1, the gyroscope 12 can be sent out the signal of change in location
Controller 1c is given, controller 1c opens the solenoid valve one of compressed gas cylinder 10b in advance, inflates to extension airbag 11, prevents nobody
Machine ontology 1, which hurtles down, directly hits the water surface.
Specifically, the lower end of the extension airbag 11 is vertically arranged with exhaust pipe 11a, and the exhaust pipe 11a is equipped with
Solenoid valve two, the solenoid valve two are electrically connected by controller 1c with battery 1d.
After stormy waves, controller 1c opens the solenoid valve two on exhaust pipe 11a, the compression in four extension airbags 11
Air is discharged from respective exhaust pipe 11a, and drone body 1 is given to provide a upward thrust, takes off power-assisted, makes to unmanned plane
Its rapid increase reduces the consumption of electric energy when taking off.
Specifically, the power generator includes one 3b of connecting rod of fixed plate one 1e and two of fixing axle 3, two, two institutes
It states one 1e of fixed plate to be vertically arranged on the downside of drone body 1, two fixed plates, one 1e and two one 3b of connecting rod
It corresponds, one end of one 3b of connecting rod is hinged by articulated shaft 1f and corresponding one 1e of fixed plate, two connecting rods
The other end of one 3b is respectively fixedly connected in fixing axle 3, and the fixing axle 3 is horizontally disposed, and the both ends of the fixing axle 3 are respectively equipped with
Can limit fixing axle 3 rotated on the position-limit mechanism of articulated shaft 1f slewing area, the fixing axle 3 be provided with it is columned floating
Body 2, the length direction of the outer lateral edge floating body 2 of the floating body 2 are circumferentially uniformly provided with several rotating vanes 2d, and the floating body 2 is located at two
Between a one 3b of connecting rod, being equipped in the floating body 2 can drive floating body 2 to rotate the power generation mechanism to generate electricity using wave.
When unmanned plane drops to the water surface, four extension airbags 11 and two floating bodies 2 contact the water surface simultaneously, play buffering and make
With, while buoyancy can also be provided to drone body 1, float on it on water surface, the rotating vane 2d on floating body 2 is rushed by wave
It hits and floating body 2 is driven to rotate around fixing axle 3, power generation mechanism is generated electricity using the rotation of floating body 2, environmentally protective；The limit
Mechanism can limit fixing axle 3 around the slewing area of articulated shaft 1f, and fixing axle 3 is avoided to cross ambassador around the rotational angle of articulated shaft 1f
Drone body 1 contacts the water surface or turns on one's side, and improves the stability of unmanned plane charging waterborne；In addition, when unmanned plane lands
When to ground, the height of two floating bodies 2 can be adjusted according to different landform, so that drone body 1 is kept horizontality, kept away
Exempt to turn on one's side.
Specifically, the power generation mechanism includes one 2b of permanent magnet, two 2c of permanent magnet and coil 4, is equipped in the floating body 2
Installation cavity 2a, one 2b of magnet and two 2c of magnet are oppositely arranged on the side wall of installation cavity 2a, and magnetic pole is on the contrary, described solid
One 3a of through-hole there are two being arranged in parallel on dead axle 3, two one 3a of through-hole are located at the both ends of installation cavity 2a, described in two
The axis of one 3a of through-hole is vertical with the axis of fixing axle 3 and in the same plane, and the coil 4 is twined by two one 3a of through-hole
It is wound on the outside of fixing axle 3, the coil 4 is electrically connected with battery 1d.
Since two floating bodies 2 are rotated by wave stroke around fixing axle 3, make one 2b of permanent magnet in installation cavity 2a, forever
The coil 4 wound in two 2c of magnet and fixing axle 3 relatively rotates, and according to electromagnetic induction principle, coil 4 cuts permanent magnet one
The magnetic induction line of two 2c of 2b and permanent magnet generates induced current, electric energy is stored in battery 1d, environmentally protective.
Specifically, the position-limit mechanism includes two 3d of fixed plate, two 3c of connecting rod, piston rod 6 and piston cylinder 6a, the work
Plug cylinder 6a is vertically arranged on the side wall of drone body 1 by bracket, one end of the piston rod 6 be located in piston cylinder 6a and
End is installed with piston 6b, and the other end of the piston rod 6 stretches out piston cylinder 6a and end is fixed with connecting column 5, the piston
6b is slidably arranged in piston cylinder 6a, and the piston 6b will be divided into epicoele 7 and cavity of resorption 8 inside piston cylinder 6a, the epicoele 7 is under
Water is filled in chamber 8, the top of the epicoele 7 is equipped with upper water inlet pipe 7a and upper water-out pipe 7b, the bottom of the cavity of resorption 8 are equipped with down
Water inlet pipe 8a and lower discharging tube 8b, the upper side of the drone body 1 are equipped with water tank 13, the upper water inlet pipe 7a, on
Outlet pipe 7b, lower water inlet pipe 8a and lower discharging tube 8b are connected with water tank 13, the upper water inlet pipe 7a, upper water-out pipe 7b,
It is equipped with check valve on lower water inlet pipe 8a and lower discharging tube 8b, reset spring 6c, the reset bullet are arranged on the piston rod 6
For spring 6c between piston 6b and piston cylinder 6a, the outside of the connecting column 5 is equipped with three 5a of fixed plate, three 5a of fixed plate with
One end of two 3c of connecting rod is hinged, and one end of the other end and two 3d of fixed plate of two 3c of connecting rod is hinged, two 3d of fixed plate
The other end and fixing axle 3 end be connected.
When wave stroke floating body 2 rotates fixing axle 3 to the outside of drone body 1 around articulated shaft 1f, pass through connecting rod
Two 3c drive piston rod 6 and piston 6b slide downward, and the reset spring 6c on piston rod 6 is compressed, and the reset spring 6c can
To limit the range that fixing axle 3 is turned out around articulated shaft 1f, it is always positioned at drone body 1 on the water surface, as piston 6b
When slide downward, the water in cavity of resorption 8 is squeezed from lower discharging tube 8b and is flowed into water tank 13, while being formed in epicoele 7 negative
Pressure, upper water inlet pipe 7a draw water from water tank 13 into epicoele 7；When wave stroke floating body 2 make fixing axle 3 around articulated shaft 1f to nobody
When the inside rotation of machine ontology 1, piston rod 6 and piston 6b upward sliding are driven by two 3c of connecting rod, the reset bullet on piston rod 6
Spring 6c is stretched, and the reset spring 6c can limit the range that fixing axle 3 is inwardly rotated around articulated shaft 1f, prevents due to two
Floating body 2 is apart from closely making drone body 1 turn on one's side very much, and when piston 6b upward sliding, the water in epicoele 7 is squeezed from upper
Outlet pipe 7b is flowed into water tank 13, while negative pressure is formed in cavity of resorption 8, and lower water inlet pipe 8a draws water from water tank 13 to cavity of resorption 8
It is interior；Further, since the setting of check valve be so that upper water inlet pipe 7a and lower water inlet pipe 8a can only intake, upper water-out pipe 7b and lower water outlet
Pipe 8b can only be discharged, it is ensured that piston cylinder 6a is worked normally, and is worked as a buffer to unmanned plane landing.
Specifically, logical in the through-hole of the upper water inlet pipe 7a, upper water-out pipe 7b, lower water inlet pipe 8a and lower discharging tube 8b
It crosses branch and is provided with generator 14, the input shaft end of the generator 14 is equipped with impeller 14a, the generator 14 and battery 1d
Electrical connection.
When piston rod 6 is with piston 6b slide downward, the water in cavity of resorption 8, which is squeezed from lower discharging tube 8b, is flowed into storage
In water tank 13, while negative pressure is formed in epicoele 7, upper water inlet pipe 7a draws water from water tank 13 into epicoele 7, and upper water inlet pipe 7a is under
Water flowing in outlet pipe 8b drives the impeller 14a in respective through-hole to rotate, and generator 14 is made to generate electricity；It lives when piston rod 6 drives
When filling in 6b upward sliding, the water in epicoele 7, which is squeezed from upper water-out pipe 7b, to be flowed into water tank 13, while shape in cavity of resorption 8
At negative pressure, lower water inlet pipe 8a draws water from water tank 13 into cavity of resorption 8, and the water flowing in upper water-out pipe 7b and lower water inlet pipe 8a drives
Impeller 14a rotation in respective through-hole, makes generator 14 generate electricity again, converts electric energy for wave energy, improve the benefit of wave energy
With rate.
Those skilled in the art can various modifications may be made to described specific embodiment, supplement or
It is substituted using similar method, however, it does not deviate from the spirit of the invention or beyond the scope of the appended claims.
Claims (7)
1. a kind of structure improved sensorcraft waterborne, including drone body (1), the surrounding of the drone body (1)
It is equipped with rotor (1a), which is characterized in that be equipped with pedestal (10) below four rotors (1a), in the pedestal (10)
There is the storage chamber (10a) of opening equipped with lower end, be equipped with extension airbag (11) in the storage chamber (10a), the pedestal (10)
It is equipped with compressed gas cylinder (10b), the compressed gas cylinder (10b) is connected by pipe with extension airbag (11), the compressed gas
The gas outlet of bottle (10b) is equipped with solenoid valve one, cavity (1b) is equipped in the drone body (1), in the cavity (1b)
Equipped with controller (1c) and battery (1d), the solenoid valve one is electrically connected by controller (1c) with battery (1d), described
Two sides below drone body (1), which are respectively equipped with when unmanned plane drop to the water surface, can be such that drone body (1) swims in
On the water surface, moreover it is possible to can be carried out the power generator of power generation using wave, two power generator are symmetrical set, the hair
Electric installation is electrically connected with battery (1d).
2. the structure improved sensorcraft waterborne of one kind according to claim 1, which is characterized in that the cavity (1b)
It is equipped with gyroscope (12), the gyroscope (12) is electrically connected by controller (1c) with battery (1d).
3. the structure improved sensorcraft waterborne of one kind according to claim 2, which is characterized in that the extension airbag
(11) lower end is vertically arranged with exhaust pipe (11a), and the exhaust pipe (11a) is equipped with solenoid valve two, the solenoid valve two-way
Controller (1c) is crossed to be electrically connected with battery (1d).
4. the structure improved sensorcraft waterborne of one kind according to claim 3, which is characterized in that the power generator
Including fixing axle (3), two fixed plates one (1e) and two connecting rods one (3b), two fixed plates one (1e) are vertically arranged in
On the downside of drone body (1), two fixed plates one (1e) and two connecting rods one (3b) are corresponded, the connecting rod
One end of one (3b) by articulated shaft (1f) and corresponding fixed plate one (1e) hingedly, two connecting rods one (3b) it is another
End is respectively fixedly connected on fixing axle (3), and the fixing axle (3) is horizontally disposed, and the both ends of the fixing axle (3) are respectively equipped with can
Fixing axle (3) are limited around the position-limit mechanism of articulated shaft (1f) slewing area, rotation is provided with columned on the fixing axle (3)
Floating body (2), the length direction of the outer lateral edge floating body (2) of the floating body (2) is circumferentially uniformly provided with several rotating vanes (2d), described floating
Body (2) is located between two connecting rods one (3b), and being equipped in the floating body (2) can drive floating body (2) rotation to carry out using wave
The power generation mechanism of power generation.
5. the structure improved sensorcraft waterborne of one kind according to claim 4, which is characterized in that the power generation mechanism
Including permanent magnet one (2b), permanent magnet two (2c) and coil (4), it is equipped with installation cavity (2a) in the floating body (2), the magnet one
(2b) and magnet two (2c) are oppositely arranged on the side wall of installation cavity (2a), and magnetic pole is on the contrary, parallel in the fixing axle (3)
There are two through-hole one (3a), two through-holes one (3a) to be located at the both ends of installation cavity (2a), two through-holes for setting
The axis of one (3a) is vertical with the axis of fixing axle (3) and in the same plane, and the coil (4) passes through two through-holes one
(3a) is wrapped in the outside of fixing axle (3), and the coil (4) is electrically connected with battery (1d).
6. the structure improved sensorcraft waterborne of one kind according to claim 5, which is characterized in that the position-limit mechanism
Including fixed plate two (3d), connecting rod two (3c), piston rod (6) and piston cylinder (6a), the piston cylinder (6a) is vertical by bracket
It is arranged on the side wall of drone body (1), one end of the piston rod (6) is located in piston cylinder (6a) and end is installed with work
It fills in (6b), the other end of the piston rod (6) stretches out piston cylinder (6a) and end is fixed with connecting column (5), the piston (6b)
It is slidably arranged in piston cylinder (6a), the piston (6b) will be divided into epicoele (7) and cavity of resorption (8) inside piston cylinder (6a), described
Water is filled in epicoele (7) and cavity of resorption (8), the top of the epicoele (7) is equipped with upper water inlet pipe (7a) and upper water-out pipe (7b), institute
The bottom for stating cavity of resorption (8) is equipped with lower water inlet pipe (8a) and lower discharging tube (8b), and the upper side of the drone body (1) is equipped with
Water tank (13), the upper water inlet pipe (7a), upper water-out pipe (7b), lower water inlet pipe (8a) and lower discharging tube (8b) are and water tank
(13) it is connected, is equipped with list on the upper water inlet pipe (7a), upper water-out pipe (7b), lower water inlet pipe (8a) and lower discharging tube (8b)
It to valve, is arranged with reset spring (6c) on the piston rod (6), the reset spring (6c) is located at piston (6b) and piston cylinder
Between (6a), the outside of the connecting column (5) is equipped with fixed plate three (5a), and the one of the fixed plate three (5a) and connecting rod two (3c)
End is hinged, and the other end of the connecting rod two (3c) and one end of fixed plate two (3d) are hinged, the fixed plate two (3d) it is another
The end at end and fixing axle (3) is connected.
7. the structure improved sensorcraft waterborne of one kind according to claim 6, which is characterized in that the upper water inlet pipe
Generator (14) are provided with by branch in the through-hole of (7a), upper water-out pipe (7b), lower water inlet pipe (8a) and lower discharging tube (8b),
The input shaft end of the generator (14) is equipped with impeller (14a), and the generator (14) is electrically connected with battery (1d).
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| Application Number | Priority Date | Filing Date | Title |
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| CN201811277943.3A CN109250114B (en) | 2018-10-30 | 2018-10-30 | Structure-improved water detection unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201811277943.3A CN109250114B (en) | 2018-10-30 | 2018-10-30 | Structure-improved water detection unmanned aerial vehicle |
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| CN109250114B CN109250114B (en) | 2023-12-19 |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109941433A (en) * | 2019-03-12 | 2019-06-28 | 深圳市律远汇智科技有限公司 | A kind of unmanned flight's device with forced landing function for patrol on the sea |
| CN111661335A (en) * | 2020-06-24 | 2020-09-15 | 王振清 | Self-stabilizing agricultural unmanned aerial vehicle |
| CN113064221A (en) * | 2021-03-17 | 2021-07-02 | 陕西省大气探测技术保障中心 | Unmanned aerial vehicle meteorological observation system |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105857532A (en) * | 2015-07-06 | 2016-08-17 | 周剑辉 | General offshore platform as well as buoyancy adjustment method and stable power generation method thereof |
| CN106368905A (en) * | 2016-10-19 | 2017-02-01 | 浙江海洋大学 | Offshore wind power generation device |
| CN106382183A (en) * | 2016-10-19 | 2017-02-08 | 浙江海洋大学 | Wave energy power generation device |
| CN106762372A (en) * | 2016-12-29 | 2017-05-31 | 浙江海洋大学 | A kind of structure improved electric generator using sea wave energy |
| CN206615390U (en) * | 2017-04-07 | 2017-11-07 | 南京信息工程大学 | A kind of unmanned plane falls over into water sink preventing apparatus |
| CN107719666A (en) * | 2016-08-11 | 2018-02-23 | 肖凤伟 | Amphibious unmanned plane |
-
2018
- 2018-10-30 CN CN201811277943.3A patent/CN109250114B/en active Active
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105857532A (en) * | 2015-07-06 | 2016-08-17 | 周剑辉 | General offshore platform as well as buoyancy adjustment method and stable power generation method thereof |
| US20180141622A1 (en) * | 2015-07-06 | 2018-05-24 | Jianhui Zhou | Universal offshore platform, and buoyancy regulation method and stable power generation method thereof |
| CN107719666A (en) * | 2016-08-11 | 2018-02-23 | 肖凤伟 | Amphibious unmanned plane |
| CN106368905A (en) * | 2016-10-19 | 2017-02-01 | 浙江海洋大学 | Offshore wind power generation device |
| CN106382183A (en) * | 2016-10-19 | 2017-02-08 | 浙江海洋大学 | Wave energy power generation device |
| CN106762372A (en) * | 2016-12-29 | 2017-05-31 | 浙江海洋大学 | A kind of structure improved electric generator using sea wave energy |
| CN206615390U (en) * | 2017-04-07 | 2017-11-07 | 南京信息工程大学 | A kind of unmanned plane falls over into water sink preventing apparatus |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109941433A (en) * | 2019-03-12 | 2019-06-28 | 深圳市律远汇智科技有限公司 | A kind of unmanned flight's device with forced landing function for patrol on the sea |
| CN111661335A (en) * | 2020-06-24 | 2020-09-15 | 王振清 | Self-stabilizing agricultural unmanned aerial vehicle |
| CN113064221A (en) * | 2021-03-17 | 2021-07-02 | 陕西省大气探测技术保障中心 | Unmanned aerial vehicle meteorological observation system |
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|---|---|
| CN109250114B (en) | 2023-12-19 |
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