CN207636341U - A kind of water intaking aircraft - Google Patents

A kind of water intaking aircraft Download PDF

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Publication number
CN207636341U
CN207636341U CN201721799008.4U CN201721799008U CN207636341U CN 207636341 U CN207636341 U CN 207636341U CN 201721799008 U CN201721799008 U CN 201721799008U CN 207636341 U CN207636341 U CN 207636341U
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CN
China
Prior art keywords
control
seal casinghousing
water
flight
signal
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Expired - Fee Related
Application number
CN201721799008.4U
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Chinese (zh)
Inventor
范文兵
马爽
马浩宇
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Zhengzhou University
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Zhengzhou University
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Priority to CN201721799008.4U priority Critical patent/CN207636341U/en
Application granted granted Critical
Publication of CN207636341U publication Critical patent/CN207636341U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model is related to a kind of water intaking aircraft, the gondola being connected to including unmanned plane and by cable below unmanned plane, it is provided with pressure sensor on the seal casinghousing of gondola, water fetching device is equipped in seal casinghousing, rotation is provided with the shaft wound for cable and shaft driving motor on the fuselage of unmanned plane, flight-control computer and signal receiver are additionally provided on fuselage, flight-control computer is connected with the control of shaft driving motor, control circuit board is equipped in seal casinghousing, control circuit board is connect with pressure sensor signal, control circuit board is connected with water fetching device control, control circuit board is connect with flight-control computer signal the signal of pressure sensor is reached flight-control computer and control signal is reached control circuit board to control the keying of water fetching device by flight-control computer.The signal of pressure sensor detection is converted into the depth of water body by control circuit board, flight-control computer and signal receiver, to take the water sample of designated depth.

Description

A kind of water intaking aircraft
Technical field
The utility model is related to aircraft fields, and in particular to a kind of water intaking aircraft.
Background technology
Water quality is related to the life and health of people, and the monitoring and improvement to water quality are a big weights of the Party and the people's government work Content is wanted, in the monitoring of environmental pollution and the investigation of water pollution, truly to reflect water pollution situation, it is necessary to acquisition tool Representational water sample.Traditional water quality sampling mode generally directly takes water sample on bank, needs staff to take at this time With some tools, such as sampler, sampled on bank.If necessary to be sampled in the occasion such as river center far from bank When, then it needs sample collector to take vessel and is sampled, waste man power and money, taken in the water body of the encirclements such as marshland, mire, ice cube When sample, it may threaten to the life of people.
Currently, unmanned plane have been applied in take photo by plane, express delivery, post-disaster search and rescue, data acquisition etc. fields, show the hair of unmanned plane Exhibition has a high potential.In recent years, unmanned plane starts to show up prominently in commercial market, wherein agricultural plant protection and electric power energy inspection this two A field is showing more urgent demand trend at present, and has more considerable market scale foreground.
Authorization Notice No. is that the Chinese utility model patent of 205879594 U of CN discloses a kind of sampling of water quality unmanned plane, Including unmanned plane, pump, hose and sampling bottle, sampling bottle is mounted on pump, and one end of hose is connected on pump, and pump is mounted on nobody The lower section of machine body is extracted into sampling bottle under hose to below the water surface and by pump processing water when sampling, and realizing remote control should Unmanned plane carries out the sampling of water quality, and sampling is convenient.But some occasions need to be sampled inspection to the water sample at different depth It surveys, and above-mentioned unmanned plane then can not be to there is the water of specific requirement depth to be sampled monitoring.
Invention content
The purpose of this utility model is to provide a kind of can realize to there is the water sample of specific depth requirements to be sampled detection Water intaking aircraft.
To achieve the above object, a kind of water intaking aircraft of the utility model adopts the following technical scheme that:A kind of water intaking is winged Row device, including unmanned plane and the gondola below unmanned plane is connected to by cable, the gondola includes seal casinghousing, seal casinghousing On be provided with pressure sensor for detecting the depth that gondola is located in water body, be provided with water fetching device in seal casinghousing, nobody Machine includes fuselage, and the shaft driving motor for being provided with the shaft and drive shaft rotation that are wound for cable, fuselage are rotated on fuselage On be additionally provided with flight-control computer and connect with flight-control computer signal for being connect with external equipment to show Or the signal receiver of storage data information, flight-control computer are connected with the control of shaft driving motor, are set in seal casinghousing It is equipped with control circuit board, control circuit board is connect with pressure sensor signal, and control circuit board is connected with water fetching device control, control Circuit board processed is connect with flight-control computer signal the signal of pressure sensor is reached flight-control computer and is incited somebody to action Control signal reaches control circuit board to control the keying of water fetching device by flight-control computer.
The first mounting hole is provided on the seal casinghousing, pressure sensor is seal-installed in the first mounting hole.
The inside of the seal casinghousing is additionally provided with the video camera being connect with control circuit partitioned signal, is arranged on seal casinghousing There is the second mounting hole of the camera sealing installation for video camera.
The seal casinghousing includes the upper shell and lower housing of releasable connection together, is arranged between upper shell and lower housing There is sealing ring.
The water fetching device is syringe, and syringe includes cylinder, piston and piston rod, and the end of cylinder is equipped with nipple, It is provided with the mounting hole installed for nipple circumferential seal in seal casinghousing, is additionally provided in seal casinghousing for driving syringe Piston rod is moved back and forth to draw water sample or discharge water sample to clean the driving mechanism of syringe.
The quantity of the syringe is two, and is spaced setting, and driving mechanism is the rudder being set between two syringes The output end of machine, steering engine is connected with screw rod, is connected by connecting plate between the piston rod of two syringes, screw rod and connecting rod spiral shell Line connects.
Strainer is provided at mounting hole on the seal casinghousing.
The beneficial effects of the utility model:Unmanned plane during flying is controlled to specified region, by turning by flight-control computer Axis driving motor drives pivot decentralization or rolls gondola, the signal detected by pressure sensor by control circuit board, Flight-control computer and signal receiver are converted into the depth of water body, are fetched water by control circuit board drive after reaching designated depth Device is fetched water, and the water sample of designated depth can be thus taken.
Description of the drawings
Fig. 1 is a kind of structural schematic diagram of one embodiment of water intaking aircraft of the utility model;
Fig. 2 is the structural schematic diagram of gondola in Fig. 1;
Fig. 3 is the structural schematic diagram of gondola bottom in Fig. 2;
Fig. 4 is that the structural schematic diagram after shell is removed in Fig. 1;
Fig. 5 is the structural schematic diagram of driving mechanism;
Fig. 6 is the structural schematic diagram of shaft.
Specific implementation mode
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole Embodiment.Based on the embodiments of the present invention, the every other embodiment that those of ordinary skill in the art are obtained all belongs to In the range of the utility model protection.
A kind of water intaking aircraft of the utility model as shown in figs 1 to 6, including unmanned plane 1 and is hung on by cable 3 The gondola 2 of 1 lower section of unmanned plane, unmanned plane 1 include fuselage and four rotors 4 being set on fuselage, and four rotors 4 are symmetrical At four angles all around of fuselage and it is in sustained height, and the radius of four rotors 4 is all identical, each rotor 4 has phase The rotor motor 5 answered drives.The signal for being provided with flight-control computer on fuselage and being connect with flight-control computer signal Receiver, flight-control computer are connected with the control of 4 motor of each rotor, and signal receiver is realized remote for receiving external signal Driving of the journey straighforward operation to unmanned plane.Fuselage use carbon fiber, because its compared with generic engineering plastics intensity higher, quality is more Gently, it therefore can utmostly mitigate fuselage weight, increase cruise duration, while the use of carbon fiber ensure that fuselage intensity, carry The high safety of flight.
Gondola 2 includes seal casinghousing 8, and video camera 20, syringe 16, steering engine 18, pressure sensing are provided in seal casinghousing 8 Device 21, control circuit board 13 and gondola battery 12, gondola battery 12 pass through control circuit board 13 and video camera 20, pressure sensor 21, steering engine 18 is electrically connected, and video camera 20 and pressure sensor 21 are connect with 13 equal signal sampling of control circuit board, control circuit Plate 13 is with the control connection of steering engine 18 to control unlatching, rotation direction and the closing of steering engine.Control circuit board 13 passes through above-mentioned cable 3 Connect with the flight-control computer signal on the fuselage of unmanned plane, and connect with external equipment signal by signal receiver with The information of reflection video camera shooting and the parameter of pressure sensor in real time.It is provided on seal casinghousing 8 for above-mentioned cable seal The cable hole 9 passed through, cable connect with 13 signal of control circuit board in seal casinghousing across cable hole 9, are provided on fuselage The shaft driving motor 7 that the shaft 6 and drive shaft 6 wound for cable 3 rotates, be provided with fixed cable in shaft 6 so that It is provided with the electric connection for being electrically connected with cable 3 in shaft 6 convenient for the cable mounting hole 61 of winding in cable mounting hole 61 62, plug 63 is electrically connected on electric connection 62, and the socket inserted for plug 63 is provided on fuselage and is powered with realizing, this module The design of change is easily installed and dismantles.The quantity of cable is two, and the quantity of shaft 6 is also two, shaft driving motor 7 Quantity is one, and two shafts are located at the both sides of shaft driving motor and synchronize driving by shaft driving motor to transfer or roll Gondola.Unmanned machine battery is set on fuselage, unmanned machine battery uses lithium battery, unmanned machine battery to pass through flight-control computer It powers to rotor motor and shaft driving motor, rotor motor and shaft driving motor connect with the control of flight-control computer signal It connects.
The quantity of syringe 16 in seal casinghousing be two and spacing parallel arranging setting, syringe include cylinder, piston and The end of piston rod 15, cylinder is equipped with nipple, is provided with the mounting hole installed for nipple circumferential seal in seal casinghousing 8, seals Strainer is provided on shell at mounting hole.Cylinder is fixed on the inside of seal casinghousing by fixed frame 17, and steering engine 18 is located at two Between a syringe 16 and be fixedly connected on fixed frame 17, fixed frame 17 include along syringe axis direction it is spaced Two fixed plates.The piston rod 15 of two syringes 16 is connected with connecting plate 19, and connecting plate 19, which is tightened up a screw, is connected with screw rod 22, spiral shell The other end of bar 22 is sequentially connected with the output end of steering engine 18, and steering engine 18 drives the rotation of screw rod 22 and then passes through 19 band of connecting plate Dynamic two piston rods 15 move, and steering engine 18 is formed for driving the piston rod of syringe to move back and forth to draw water sample or discharge water Sample is to clean the driving mechanism of syringe.Voltage changing module 14 is electrically connected between control circuit board and steering engine, so that gondola battery Pressure regulation uses voltage to steering engine.
It is set to the first mounting hole 11 for being installed for the sealing of pressure sensor 21 on the bottom wall of seal casinghousing 8 and is used for For the second mounting hole 11 of the camera sealing installation of video camera 20, the setting of pressure sensor 21 is used to judge gondola depth, Convenient for underwater control.The material of seal casinghousing 8 is clear hard plastics, and the thickness of reasonable design is to mitigate weight.For maximum journey Degree ensures that the stability of gondola in water, 8 shape of seal casinghousing are class cylinder, can comply with the flow direction of water.In seal casinghousing What face was placed also has illuminator, when gondola executes task in water, can be taken pictures, be recorded a video and be passed to flight control meter In calculation machine, real time monitoring sub-marine situations simultaneously will be on parameter feedback to external equipment.Temperature sensor is also equipped on seal casinghousing, Water temperature can be measured in real time during dive.Seal casinghousing be two-piece unit formula structure, seal casinghousing include upper shell and Lower housing, upper shell and lower housing are linked together by circumferentially disposed multiple screws, are provided between upper shell and lower housing Sealing ring.
In the other embodiment of the utility model, the nipple of each syringe can also be located at the inside of seal casinghousing, this When each nipple on be sealedly connected with water pipe, the water pipe perforation that the water supply seal of tube installs is provided on seal casinghousing, by water pipe into Row is drawn or discharge water sample;The quantity of syringe can be one, or three or more;Driving mechanism can also include Two and it is respectively used to driving the first syringe and the second syringe;Gondola battery can not also be set in seal casinghousing, it can be with Pass through the power supplies such as circuit board and steering engine and video camera in order to control of unmanned machine battery and cable.

Claims (7)

1. a kind of water intaking aircraft, it is characterised in that:It is connected to the gondola below unmanned plane, institute including unmanned plane and by cable It includes seal casinghousing to state gondola, and pressure sensor is provided on seal casinghousing and is used to detect the depth that gondola is located in water body, close Water fetching device is provided in capsule body, unmanned plane includes fuselage, is rotated on fuselage and is provided with the shaft wound for cable and driving The shaft driving motor of shaft rotation, is additionally provided with flight-control computer on fuselage and is connect with flight-control computer signal For connect with external equipment to show or store the signal receiver of data information, flight-control computer and shaft driving Motor control connects, and control circuit board is provided in seal casinghousing, and control circuit board is connect with pressure sensor signal, control electricity The control of road plate and water fetching device connects, and control circuit board is connect with flight-control computer signal with by the signal of pressure sensor It reaches flight-control computer and control signal is reached into control circuit board to control water fetching device by flight-control computer Keying.
2. water intaking aircraft according to claim 1, it is characterised in that:The first installation is provided on the seal casinghousing Hole, pressure sensor are seal-installed in the first mounting hole.
3. water intaking aircraft according to claim 1, it is characterised in that:The inside of the seal casinghousing is additionally provided with and controls The video camera of circuit board signal processed connection is provided with the second installation of the camera sealing installation for video camera on seal casinghousing Hole.
4. water intaking aircraft according to claim 1, it is characterised in that:The seal casinghousing include releasable connection together Upper shell and lower housing, sealing ring is provided between upper shell and lower housing.
5. the water intaking aircraft according to any one of claim 1-4, it is characterised in that:The water fetching device is injection Device, syringe include cylinder, piston and piston rod, and the end of cylinder is equipped with nipple, is provided in seal casinghousing for nipple circumferential direction The mounting hole for sealing installation, be additionally provided in seal casinghousing for drive the piston rod of syringe to move back and forth with draw water sample or Discharge water sample is to clean the driving mechanism of syringe.
6. water intaking aircraft according to claim 5, it is characterised in that:The quantity of the syringe is two, and is spaced Setting, driving mechanism are the steering engine being set between two syringes, and the output end of steering engine is connected with screw rod, two syringes It is connected by connecting plate between piston rod, screw rod is threadedly coupled with connecting rod.
7. water intaking aircraft according to claim 5, it is characterised in that:It is provided at mounting hole on the seal casinghousing Strainer.
CN201721799008.4U 2017-12-21 2017-12-21 A kind of water intaking aircraft Expired - Fee Related CN207636341U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201721799008.4U CN207636341U (en) 2017-12-21 2017-12-21 A kind of water intaking aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201721799008.4U CN207636341U (en) 2017-12-21 2017-12-21 A kind of water intaking aircraft

Publications (1)

Publication Number Publication Date
CN207636341U true CN207636341U (en) 2018-07-20

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201721799008.4U Expired - Fee Related CN207636341U (en) 2017-12-21 2017-12-21 A kind of water intaking aircraft

Country Status (1)

Country Link
CN (1) CN207636341U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112326354A (en) * 2020-11-07 2021-02-05 信阳师范学院 Water taking device for lake and marsh research

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112326354A (en) * 2020-11-07 2021-02-05 信阳师范学院 Water taking device for lake and marsh research

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CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20180720

Termination date: 20181221

CF01 Termination of patent right due to non-payment of annual fee