CN107031843A - A kind of three jet pipes water spray aircraft - Google Patents
A kind of three jet pipes water spray aircraft Download PDFInfo
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- CN107031843A CN107031843A CN201710162226.5A CN201710162226A CN107031843A CN 107031843 A CN107031843 A CN 107031843A CN 201710162226 A CN201710162226 A CN 201710162226A CN 107031843 A CN107031843 A CN 107031843A
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- water spraying
- aircraft
- spraying mechanism
- steering wheel
- water
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- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 title claims abstract description 229
- 239000007921 spray Substances 0.000 title claims abstract description 38
- 230000007246 mechanism Effects 0.000 claims abstract description 278
- 238000005507 spraying Methods 0.000 claims abstract description 147
- 239000008400 supply water Substances 0.000 claims description 3
- RKTYLMNFRDHKIL-UHFFFAOYSA-N copper;5,10,15,20-tetraphenylporphyrin-22,24-diide Chemical compound [Cu+2].C1=CC(C(=C2C=CC([N-]2)=C(C=2C=CC=CC=2)C=2C=CC(N=2)=C(C=2C=CC=CC=2)C2=CC=C3[N-]2)C=2C=CC=CC=2)=NC1=C3C1=CC=CC=C1 RKTYLMNFRDHKIL-UHFFFAOYSA-N 0.000 claims description 2
- 230000000875 corresponding effect Effects 0.000 claims description 2
- 230000008450 motivation Effects 0.000 claims 1
- 238000005096 rolling process Methods 0.000 abstract description 7
- 230000005484 gravity Effects 0.000 abstract description 5
- 238000005516 engineering process Methods 0.000 abstract description 4
- 230000001737 promoting effect Effects 0.000 abstract description 4
- 230000000694 effects Effects 0.000 description 5
- 229910000831 Steel Inorganic materials 0.000 description 4
- 230000008901 benefit Effects 0.000 description 4
- 239000010959 steel Substances 0.000 description 4
- 239000000243 solution Substances 0.000 description 3
- 238000009434 installation Methods 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 230000002153 concerted effect Effects 0.000 description 1
- 230000001276 controlling effect Effects 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
-
- 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
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/16—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting
- B64D1/18—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting by spraying, e.g. insecticides
-
- 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
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/20—Remote controls
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Pest Control & Pesticides (AREA)
- Special Spraying Apparatus (AREA)
Abstract
The present invention relates to vehicle technology field, more particularly to a kind of three jet pipes water spray aircraft, including aircraft body, first water spraying mechanism, the second water spraying mechanism, the first drive mechanism, the second drive mechanism and water supply mechanism, first water spraying mechanism is located at the bottom of aircraft body, and the first drive mechanism is connected with the first water spraying mechanism；The quantity of second water spraying mechanism is two, and two the second water spraying mechanisms are symmetrically located at the both sides of aircraft body, and the second drive mechanism is connected with the second water spraying mechanism；Water supply mechanism is connected with the first water spraying mechanism and the second water spraying mechanism.Three jet pipe water spray aircraft only need to be by the deflection angle of the first drive mechanism, the water spraying mechanism of motor adjustment first of the second drive mechanism and the second water spraying mechanism, it can control aircraft and realize rolling, driftage and pitch attitude in three dimensions, posture without adjusting aircraft by the pose adjustment center of gravity of people again, it can thus realize unmanned, it is simple to operate, more promotional value.
Description
Technical field
The present invention relates to vehicle technology field, more particularly to three jet pipes water spray aircraft.
Background technology
The of the prior art of water spray aircraft for entertainment project does not use automatic Pilot technology, it is necessary to have
People stands or sat and it is driven on board the aircraft, it is impossible to which remotely-piloted vehicle carries out unmanned independent flight.
The JETOVATOR of the Jetavation companies exploitation in such as U.S. is a kind of water spray for the pilot steering for being used to entertain
Aircraft, mainly adjusts the position of center of gravity and the direction of manipulation two lateral jet pipes water spray to control aircraft by the posture of people
Posture realizes flight.This manned water spray aircraft is very high to the fitness and manipulation skill set requirements of human pilot,
It can not be manipulated without the personnel of specialized training, therefore only be adapted to the stunt of professional athlete
The content of the invention
(1) technical problem to be solved
The technical problem to be solved in the present invention is that solution needs are manned, and needs to be adjusted according to the change of the posture of people
The state of flight of whole aircraft, the requirement to driver is higher, the problem of being not easy to operation.
(2) technical scheme
In order to solve the above-mentioned technical problem, the invention provides a kind of three jet pipe water spray aircraft, including aircraft body,
First water spraying mechanism, the second water spraying mechanism, the first drive mechanism, the second drive mechanism and water supply mechanism, first sprinkler
Structure is located at the bottom of the aircraft body, and first drive mechanism is connected with first water spraying mechanism, for driving
State the rotation of the first water spraying mechanism；The quantity of second water spraying mechanism is two, and two second water spraying mechanisms are symmetrically set
In the both sides of the aircraft body, second drive mechanism is connected with second water spraying mechanism, for driving described
The rotation of two water spraying mechanisms；The water supply mechanism is connected with first water spraying mechanism and the second water spraying mechanism.
Wherein, the quantity of first drive mechanism is two, the front end of the aircraft body provided with two it is vertical and
First installing plate of orthogonal setting, first drive mechanism is installed on first installing plate correspondingly,
Two first drive mechanisms apply the power of two vertical direction to first water spraying mechanism, so that first sprinkler
Structure is deflected to any direction.
Wherein, first drive mechanism includes the first steering wheel, head rod and the first connecting bracket, first rudder
Machine is on first installing plate, and first installing plate installed perpendicular to it of swing arm of first steering wheel；It is described
First connecting bracket is shaped as L-shaped, and swing arm and institute of the base parallel to first steering wheel of first connecting bracket
State the connection of the first water spraying mechanism；The head rod is vertically arranged, and one end of the head rod and first rudder
The swing arm of machine is hinged, and the other end and the vertical edge of first connecting bracket are hinged.
Wherein, second drive mechanism includes the second steering wheel, the second connecting rod and the second connecting bracket, second rudder
Machine is installed on the second installing plate of the rear end of the aircraft body, and second installing plate is vertically arranged, and described second
The swing arm of steering wheel connects parallel to second installing plate, the center of the swing arm of the second steering wheel and the drive shaft of second steering wheel
Connect；The quantity of second connecting bracket is two, and second connecting bracket is shaped as L-shaped, and two described second connect
Fore-and-aft direction of the base of support along the aircraft body is connect to set and be connected with two second water spraying mechanisms respectively；Institute
The quantity for stating the second connecting rod is two, and second connecting rod is vertically arranged, and two second connecting rods are connected respectively
In the two ends of the swing arm of second steering wheel, and one end of second connecting rod is connected with the swing arm of second steering wheel, separately
One end is connected with the vertical edge of second connecting bracket.
Wherein, the bottom of the aircraft body is provided with the first spacing groove, and the first spacing groove is along the flight
The width of device body is set, and first water spraying mechanism is movably arranged in the described first spacing groove.
Wherein, the quantity of first drive mechanism is one, and first drive mechanism includes the 3rd steering wheel, the 3rd company
Extension bar and the 3rd connecting bracket, the aircraft body are the tetragonal body structure being vertically arranged, and the 3rd steering wheel is located at described
The inside of aircraft body, and on the front end face or rear end face of the aircraft body, the swing arm of the 3rd steering wheel is put down
Row is set in the front end face and rear end face of the aircraft body；3rd connecting bracket is shaped as L-shaped, and the described 3rd connect
The base of support is connect parallel to the swing arm of the 3rd steering wheel and is connected with first water spraying mechanism；3rd connecting rod is erected
Directly set, and one end of the 3rd connecting rod and the swing arm of the 3rd steering wheel are hinged, the other end is connected branch with the described 3rd
The vertical edge of frame is hinged.
Wherein, the quantity of second drive mechanism is two, and two second drive mechanisms are correspondingly with two
The individual second water spraying mechanism connection, second drive mechanism includes the 4th steering wheel, the 4th connecting rod and the 4th connecting bracket,
On the side that two the 4th steering wheels be respectively arranged in the aircraft body two be arranged in parallel, and the 4th steering wheel
Swing arm perpendicular to the side of the aircraft body；4th connecting bracket is shaped as L-shaped, the 4th connecting bracket
Base parallel to the 4th steering wheel swing arm and be connected with second water spraying mechanism；4th connecting rod is set vertically
Put, and one end of the 4th connecting rod and the swing arm of the 4th steering wheel are hinged, the other end and the 4th connecting bracket
Vertical edge is hinged.
Wherein, the second spacing groove, the second spacing groove are respectively equipped with two sides of the aircraft body
Set along the fore-and-aft direction of the aircraft body, second water spraying mechanism is movably arranged in the described second spacing groove
It is interior.
Wherein, first water spraying mechanism and the second water spraying mechanism include shower nozzle and and flexible hose, the flexibility is soft
Pipe is connected by connecting tube with the water supply mechanism, and first drive mechanism and the second drive mechanism are connected to described the
On the shower nozzle of one water spraying mechanism and the second water spraying mechanism.
Wherein, Fei Kong mechanisms are provided with the aircraft casing, the Fei Kong mechanisms include battery, circuit board, sensor
With wireless instructions receiver, the battery provides electric energy for the flight of the aircraft, and the sensor is used to detect described fly
The attitude information of row device, the wireless instructions receiver is used to receive telecommand, and the circuit board is examined according to the sensor
The telecommand that the attitude information and the wireless instructions receiver measured is received obtains first water spraying mechanism and second
The expectation deflection angle of water spraying mechanism, and control first drive mechanism, the second drive mechanism and the water supply mechanism to make phase
The action answered.
(3) beneficial effect
The above-mentioned technical proposal of the present invention has the following advantages that：A kind of three jet pipe water spray aircraft that the present invention is provided, bag
Include aircraft body, the first water spraying mechanism, the second water spraying mechanism, the first drive mechanism, the second drive mechanism and water supply mechanism, institute
The bottom that the first water spraying mechanism is located at the aircraft body is stated, first drive mechanism connects with first water spraying mechanism
Connect, for driving first water spraying mechanism to rotate；The quantity of second water spraying mechanism is two, two second water sprays
Mechanism is symmetrically located at the both sides of the aircraft body, and second drive mechanism is connected with second water spraying mechanism, is used
In the rotation for driving second water spraying mechanism；The water supply mechanism connects with first water spraying mechanism and the second water spraying mechanism
Connect.In use, first driving mechanisms control the first water spraying mechanism rotational angle is to realize the rolling of aircraft, the second drive mechanism
Control the second water spraying mechanism rotational angle to realize the pitching and driftage of aircraft, water supply mechanism is to the first water spraying mechanism and second
Supply water in water spraying mechanism, the water sprayed from the first water spraying mechanism and the second water spraying mechanism to aircraft body provide one it is reverse
Thrust, the number of output can adjust the size of thrust, pass through the first drive mechanism, the second drive mechanism and water supply mechanism
Effect, can be achieved the control to aircraft flight posture, and three jet pipe water spray aircraft need to only pass through the first drive mechanism, second
The water spraying mechanism of motor adjustment first of drive mechanism and the deflection angle of the second water spraying mechanism, you can control aircraft is in three-dimensional space
Between realize rolling, driftage and pitch attitude, the posture without adjusting aircraft by the pose adjustment center of gravity of people again, thus can
Realize unmanned, simple to operate, more promotional value.
Except it is described above present invention solves the technical problem that, constitute technical scheme technical characteristic and have this
Outside the advantage that the technical characteristic of a little technical schemes is brought, what other technical characteristics of the invention and these technical characteristics were brought
Advantage, will be further illustrated with reference to accompanying drawing.
Brief description of the drawings
Fig. 1 is a kind of structural representation for three jet pipe water spray aircraft that the embodiment of the present invention one is provided；
Fig. 2 is a kind of upward view for three jet pipe water spray aircraft that the embodiment of the present invention one is provided；
Fig. 3 is a kind of right view for three jet pipe water spray aircraft that the embodiment of the present invention one is provided；
Fig. 4 is a kind of front view for three jet pipe water spray aircraft that the embodiment of the present invention one is provided；
Fig. 5 is a kind of top view for three jet pipe water spray aircraft that the embodiment of the present invention one is provided；
Fig. 6 is a kind of front view for three jet pipe water spray aircraft that the embodiment of the present invention two is provided；
Fig. 7 is a kind of right view for three jet pipe water spray aircraft that the embodiment of the present invention two is provided；
Fig. 8 is a kind of left view for three jet pipe water spray aircraft that the embodiment of the present invention two is provided；
Fig. 9 is a kind of upward view for three jet pipe water spray aircraft that the embodiment of the present invention two is provided.
In figure：1：Aircraft casing；2：First drive mechanism；3：Second drive mechanism；4：First water spraying mechanism；5：Second
Water spraying mechanism；6：Water supply mechanism；7：Connecting tube；8：Fei Kong mechanisms；9：Second spacing groove；101：First installing plate；41：Spray
Head；42：Flexible steel in flat section tubing；51：Shower nozzle；52：Flexible steel in flat section tubing；102：Second installing plate；103：Side plate；201：First steering wheel；
202：Head rod；203：First connecting bracket；301：Second steering wheel；302：Second connecting rod；303：Second connecting bracket；
304：The swing arm of second steering wheel；701：Three-way pipe；204：3rd steering wheel；205：3rd connecting rod；206：3rd connecting bracket；
305：4th steering wheel；306：The swing arm of 4th steering wheel；307：4th connecting rod；308：4th connecting bracket；10：First is spacing logical
Groove.
Embodiment
To make the purpose, technical scheme and advantage of the embodiment of the present invention clearer, below in conjunction with the embodiment of the present invention
In accompanying drawing, the technical scheme in the embodiment of the present invention is clearly and completely described, it is clear that described embodiment is
A part of embodiment of the present invention, rather than whole embodiments.Based on the embodiment in the present invention, ordinary skill people
The every other embodiment that member is obtained on the premise of creative work is not made, belongs to the scope of protection of the invention.
In the description of the invention, it is necessary to illustrate, unless otherwise clearly defined and limited, term " installation ", " phase
Even ", " connection " should be interpreted broadly, for example, it may be being fixedly connected or being detachably connected, or be integrally connected；Can
To be mechanical connection or electrical connection；Can be joined directly together, can also be indirectly connected to by intermediary, Ke Yishi
The connection of two element internals.For the ordinary skill in the art, with concrete condition above-mentioned term can be understood at this
Concrete meaning in invention.
In addition, in the description of the invention, unless otherwise indicated, " multiple ", " many ", " multigroup " be meant that two or
Two or more, " several ", " some ", " some groups " are meant that one or more.
Embodiment one
As shown in Figures 1 to 5, three jet pipe provided in an embodiment of the present invention water spray aircraft, including aircraft body 1, the
One water spraying mechanism 4, the second water spraying mechanism 5, the first drive mechanism 2, the second drive mechanism 3 and water supply mechanism 6, the first water spraying mechanism
2 are located at the bottom of aircraft body 1, and the first drive mechanism 2 is connected with the first water spraying mechanism 4, for driving the first water spraying mechanism 4
Rotate；The quantity of second water spraying mechanism 5 is two, and two the second water spraying mechanisms 5 are symmetrically located at the both sides of aircraft body 1,
Second drive mechanism 3 is connected with the second water spraying mechanism 5, the rotation for driving the second water spraying mechanism 5；Water supply mechanism 6 and first
The water spraying mechanism 5 of water spraying mechanism 4 and second is connected.In use, the first drive mechanism 2 control the rotational angle of the first water spraying mechanism 4 with
Realize the rolling of aircraft, the second drive mechanism 3 controls the rotational angle of the second water spraying mechanism 5 to realize the pitching and partially of aircraft
Boat, water supply mechanism 6 supplies water into the first water spraying mechanism 4 and the second water spraying mechanism 5, from the first water spraying mechanism 4 and the second sprinkler
Structure 5 spray water give aircraft body 1 provide a reverse thrust, output number can adjust the size of thrust, lead to
The effect of the first drive mechanism 2, the second drive mechanism 3 and water supply mechanism 6 is crossed, the control to aircraft flight posture can be achieved,
Three jet pipe water spray aircraft need to only pass through the first drive mechanism, the water spraying mechanism of motor adjustment first of the second drive mechanism and the
The deflection angle of two water spraying mechanisms, you can control aircraft realizes rolling, driftage and pitch attitude in three dimensions, without leading to again
Remarkable pose adjustment center of gravity adjusts the posture of aircraft, thus can realize unmanned, simple to operate, more promotional value
Further, the quantity of the first drive mechanism 2 is two, and the front end of aircraft body 1 is provided with two vertical and phases
First installing plate 101 of mutual vertical setting, the first drive mechanism 2 is installed on the first installing plate 101 correspondingly, two
First drive mechanism 2 applies the power of two vertical direction to the first water spraying mechanism 4, so that the first water spraying mechanism 4 is to any direction
Deflection.Two side plates 103 of aircraft body 1 be arranged in parallel, and the quantity of the first installing plate 101 is two, two first installations
Front end of the plate 101 respectively with two side plates 103 is connected, and the angle between the first installing plate 101 and side plate 103 is 135 degree, two
Individual first installing plate 101 is arranged in a mutually vertical manner, and the second water spraying mechanism 5 is on two side plates 103 of aircraft body 1, and second
Installing plate 102 is connected between the rear end of two side plates 103, is vertically arranged with two side plates 103.
Further, the structure of two the first drive mechanisms 2 is identical, is carried out by taking one of them first drive mechanism 2 as an example
Illustrate, the first drive mechanism 2 includes the first steering wheel 201, the connecting bracket 203 of head rod 202 and first, the first steering wheel 201
On the first installing plate 101, and the first installing plate 101 for being installed perpendicular to it of swing arm of the first steering wheel 201；First connection branch
Frame 202 is shaped as L-shaped, and swing arm and first water spraying mechanism of the base parallel to the first steering wheel 201 of the first connecting bracket 202
4 connections；Head rod 202 is vertically arranged, and one end of head rod 202 and the swing arm of the first steering wheel 101 are hinged, another
The vertical edge with the first connecting bracket 203 is held to be hinged.In the present embodiment, head rod 202 is bulb connecting rod, the first steering wheel
201 swing arm and the first connecting bracket 203 are divided into the both sides of head rod 202, and two with head rod 202 respectively
End is hinged.In the swing arm level of the first steering wheel 201, the base vertical of the first connecting bracket 203 in first connecting bracket
The head rod 202 of 203 connections.When in use, control the swing arm of two the first steering wheels 201 to rotate respectively, connect by first
The connecting bracket 203 of extension bar 202 and first provides the active force of two vertical direction to the first water spraying mechanism 4, by adjusting two
The size and Orientation of active force, is combined into making a concerted effort for any direction and size, and then realize the first water spraying mechanism 4 to any direction
Deflection.
Further, the second drive mechanism 3 includes the second steering wheel 301, the second connecting rod 302 and the second connecting bracket 303,
Second steering wheel 301 is installed on the second installing plate 102 of the rear end of aircraft body, and the second installing plate 102 is vertically arranged, and the
The swing arm of two steering wheels 301 is parallel to the second installing plate 102, the center of the swing arm 304 of the second steering wheel and the driving of the second steering wheel 301
Axle is connected；The quantity of second connecting bracket 303 is two, and the second connecting bracket 303 is shaped as L-shaped, two second connections
Fore-and-aft direction of the base of support 303 along aircraft body 1 sets and is connected respectively with two the second water spraying mechanisms 5；Second connects
The quantity of extension bar 302 is two, and the second connecting rod 302 is vertically arranged, and two the second connecting rods 302 are connected to the second rudder
The two ends of the swing arm 304 of machine, and one end of the second connecting rod 302 is connected with the swing arm 304 of the second steering wheel, the other end and second connects
Connect the vertical edge connection of support 302.During the drive shaft turns of the second steering wheel 301, the clockwise or inverse time is done in the swing arm 304 of the second steering wheel
Pin is rotated, now, and upwards, the other end is downward, so as to drive the second connecting rod 302 1 for one end of the swing arm 304 of the second steering wheel
Motion upwards, one moves downward, and then realizes the Differential Control of two the second water spraying mechanisms 5, that is, realizes one second water spray
Mechanism 5 is deflected forward, and another second water spraying mechanism 5 is to post deflection, by the control of the angle of two the second water spraying mechanisms 5,
The torque of pitching and the driftage of aircraft can be combined into.
Further, the second spacing groove 9, the second spacing groove are respectively equipped with two side plates 103 of aircraft body 1
9 are set along the fore-and-aft direction of aircraft body 1, and the second water spraying mechanism 5 is movably arranged in the second spacing groove 9.Second limit
The setting of position groove 9, preferably limits the second water spraying mechanism 5 and is only capable of deflecting in the longitudinal direction, more accurately defines the
The deflection angle of two water spraying mechanisms 5, reduces offset error.
Further, be provided with Fei Kong mechanisms 8 in aircraft casing 1, Fei Kong mechanisms 8 include battery, circuit board, sensor and
Wireless instructions receiver, battery provides electric energy for the flight of aircraft, and sensor is used for the attitude information of sense aircraft, wirelessly
Command receiver is used to receive telecommand, and the attitude information and wireless instructions receiver that circuit board is detected according to sensor connect
The telecommand received obtains the expectation deflection angle of each jet pipe, and controls the first drive mechanism 2, the second drive mechanism 3 and supply
Water dispenser structure 6 makes corresponding action.
Further, the first water spraying mechanism 4 include shower nozzle 41 and with flexible hose 42, the second water spraying mechanism 5 include shower nozzle
51 and flexible steel in flat section tubing 52.By taking the first water spraying mechanism 4 as an example, flexible hose 42 is connected by connecting tube 7 with water supply mechanism 6, the
One drive mechanism 2 and the second drive mechanism 3 are connected to the spray of the water spraying mechanism 5 of shower nozzle 41 and second of the first water spraying mechanism 4
On first 51.The purpose for setting flexible hose 42 and flexible hose 52 is that can occur when being easy to shower nozzle 41 and shower nozzle 51 in stress
Deflection.Water supply mechanism 6 is water pump, and the water inlet pipe of water pump is connected with water tank, and the outlet pipe of water pump is connected with connecting tube, Fei Kong mechanisms
6 adjust the injection flow rate of each shower nozzle by controlling the power of water pump, and then realize the effect of adjustment thrust size.Connecting tube 7
The first connecting tube being connected including the outlet pipe with water pump, the housing water inlet pipe on aircraft casing, located at aircraft shell
The three-way pipe 701 in internal portion and the housing outlet pipe being connected on aircraft casing with jet pipe, the first connecting tube, housing enter
Water pipe, three-way pipe 701 and housing outlet pipe are sequentially connected, and three-way pipe 701 has a water inlet and three delivery ports, and one is entered
The mouth of a river is connected with housing water inlet pipe, and three delivery ports are connected with three housing outlet pipes respectively, three housing outlet pipes respectively with
Three flexible steel in flat section tubing connections.Water produces huge pressure when being entered after water pump and three-way pipe 701 in shower nozzle, so that
Reverse thrust is provided to aircraft body 1, wherein the first connecting tube is flexible pipe, its length is according to the flight of place and aircraft
Scope is determined
Embodiment two
As shown in Figures 6 to 9, the present embodiment is similar to embodiment one, is by the first drive mechanism 2 and the second driving
Mechanism 3 changes the deflection angle of the first water spraying mechanism 4 and the second water spraying mechanism 5, to realize the adjustment of aircraft flight posture, two
The similarity of person is repeated no more, and its difference is：The four directions for being shaped as being vertically arranged of aircraft body in the present embodiment
Body structure, the quantity of the first drive mechanism 2 is one, and the first drive mechanism 2 includes the 3rd steering wheel 204, the and of the 3rd connecting rod 205
3rd connecting bracket 206, the 3rd steering wheel 204 be located at aircraft body 1 inside, and located at aircraft body 1 front end face or
On rear end face, the swing arm of the 3rd steering wheel 204 is set parallel to the front end face and rear end face of aircraft body 1；3rd connecting bracket
206 are shaped as L-shaped, and the base of the 3rd connecting bracket 206 is connected with the first water spraying mechanism 4, the swing arm of the 3rd steering wheel 204 is in
During horizontal level, the base of the 3rd connecting bracket 206 is parallel with the swing arm of the 3rd steering wheel 204；3rd connecting rod 205 is set vertically
Put, and one end of the 3rd connecting rod 205 and the swing arm of the 3rd steering wheel 204 are hinged, the vertical edge of the other end and the 3rd connecting bracket 206
It is hinged.
Further, the quantity of the second drive mechanism 3 be two, two the second drive mechanisms 3 correspondingly with two
Second water spraying mechanism 5 is connected, and the second drive mechanism 3 includes the 4th steering wheel 305, the 4th connecting rod 307 and the 4th connecting bracket
308, on the side that two the 4th steering wheels 305 be respectively arranged in aircraft body 1 two be arranged in parallel, and the pendulum of the 4th steering wheel
Arm 306 is perpendicular to two sides of aircraft body 1；4th connecting bracket 308 is shaped as L-shaped, the 4th connecting bracket 308 with
Second water spraying mechanism 5 is connected, and during 306 level of swing arm of the 4th steering wheel, base and the 4th steering wheel of the 4th connecting bracket 308
Swing arm 306 is parallel；4th connecting rod 307 is vertically arranged, and one end of the 4th connecting rod 307 and the swing arm 306 of the 4th steering wheel are cut with scissors
Connect, the other end and the vertical edge of the 4th connecting bracket 308 are hinged.Because two the second water spraying mechanisms 5 connect two different second
Drive mechanism 3, two the second drive mechanisms 3 can be controlled individually, thus can realize the synchronization of two the second water spraying mechanisms 5
Rotate, the differential of two the second water spraying mechanisms 5 can be realized again, and rotational angle can be any angle in given range,
The control of spin like this can be realized, pitch control can be realized again.
Further, the bottom plate of aircraft body 1 is provided with the first spacing groove 10, and the first spacing groove 10 is along aircraft
The width of body 1 sets and (set along the direction perpendicular to aircraft body side), and the first water spraying mechanism 4 is moveable
In the first spacing groove 10.The setting of first spacing groove 10 preferably defines the yawing moment of the first water spraying mechanism 4,
Ensure that the first water spraying mechanism 2 can only be deflected along the direction of two sides perpendicular to aircraft, it is ensured that deflection precision, reduce
Offset error.
It should be noted that the three jet pipes water spray aircraft that embodiment one and embodiment two are provided can realize pitching,
Driftage and roll attitude, the two can achieve the effect that identical, but embodiment two reduces one for embodiment one
First drive mechanism, its weight is lighter, and flight efficiency is also higher.
In use, the first drive mechanism drives the deflection of the first water spraying mechanism, the second drive mechanism drives the second water spraying mechanism
Deflection, by the combination of the first water spraying mechanism and the deflection angle of the second water spraying mechanism, realizes a variety of flight attitudes of aircraft
Control.
In summary, a kind of three jet pipe water spray aircraft that the present invention is provided, including aircraft body, the first sprinkler
Structure, the second water spraying mechanism, the first drive mechanism, the second drive mechanism and water supply mechanism, first water spraying mechanism is located at described
The bottom of aircraft body, first drive mechanism is connected with first water spraying mechanism, for driving first water spray
Mechanism is rotated；The quantity of second water spraying mechanism is two, and two second water spraying mechanisms are symmetrically located at the flight
The both sides of device body, second drive mechanism is connected with second water spraying mechanism, for driving second water spraying mechanism
Rotation；The water supply mechanism is connected with first water spraying mechanism and the second water spraying mechanism.In use, the first drive mechanism control
The first water spraying mechanism rotational angle is made to realize the rolling of aircraft, second driving mechanisms control the second water spraying mechanism rotational angle
To realize the pitching and driftage of aircraft, water supply mechanism supplies water into the first water spraying mechanism and the second water spraying mechanism, from the first spray
The water that water dispenser structure and the second water spraying mechanism spray gives aircraft body to provide a reverse thrust, output number can adjust
The size of thrust is saved, by the effect of the first drive mechanism, the second drive mechanism and water supply mechanism, be can be achieved to aircraft flight
The control of posture, three jet pipe water spray aircraft only need to be by the motor adjustment first of the first drive mechanism, the second drive mechanism
The deflection angle of water spraying mechanism and the second water spraying mechanism, you can control aircraft realizes rolling, driftage and pitching in three dimensions
Posture, without adjusting the posture of aircraft by the pose adjustment center of gravity of people again, thus can realize unmanned, operation letter
List, more promotional value.
Finally it should be noted that：The above embodiments are merely illustrative of the technical solutions of the present invention, rather than its limitations；Although
The present invention is described in detail with reference to the foregoing embodiments, it will be understood by those within the art that：It still may be used
To be modified to the technical scheme described in foregoing embodiments, or equivalent substitution is carried out to which part technical characteristic；
And these modification or replace, do not make appropriate technical solution essence depart from various embodiments of the present invention technical scheme spirit and
Scope.
Claims (10)
- The aircraft 1. a kind of three jet pipe is sprayed water, it is characterised in that：Including aircraft body, the first water spraying mechanism, the second sprinkler Structure, the first drive mechanism, the second drive mechanism and water supply mechanism, first water spraying mechanism are located at the bottom of the aircraft body Portion, first drive mechanism is connected with first water spraying mechanism, for driving first water spraying mechanism to rotate；Described The quantity of two water spraying mechanisms is two, and two second water spraying mechanisms are symmetrically located at the both sides of the aircraft body, institute State the second drive mechanism to be connected with second water spraying mechanism, the rotation for driving second water spraying mechanism；It is described to supply water Mechanism is connected with first water spraying mechanism and the second water spraying mechanism.
- The aircraft 2. three jet pipe according to claim 1 is sprayed water, it is characterised in that：The quantity of first drive mechanism is Two, first installing plate of the front end provided with two vertical and orthogonal settings of the aircraft body, described first drives Motivation structure is installed on first installing plate correspondingly, and two first drive mechanisms give first water spraying mechanism Apply the power of two vertical direction, so that first water spraying mechanism is deflected to any direction.
- The aircraft 3. three jet pipe according to claim 2 is sprayed water, it is characterised in that：First drive mechanism includes first Steering wheel, head rod and the first connecting bracket, first steering wheel is on first installing plate, and first steering wheel First installing plate installed perpendicular to it of swing arm；First connecting bracket is shaped as L-shaped, and first connection The base of support is connected parallel to the swing arm of first steering wheel with first water spraying mechanism；The head rod is set vertically Put, and one end of the head rod and the swing arm of first steering wheel are hinged, the other end and first connecting bracket Vertical edge is hinged.
- The aircraft 4. three jet pipe according to claim 3 is sprayed water, it is characterised in that：Second drive mechanism includes second Steering wheel, the second connecting rod and the second connecting bracket, second steering wheel are installed on the second peace of the rear end of the aircraft body Fill plate on, second installing plate is vertically arranged, and second steering wheel swing arm parallel to second installing plate, the second rudder The center of the swing arm of machine is connected with the drive shaft of second steering wheel；The quantity of second connecting bracket is two, and described Second connecting bracket is shaped as L-shaped, the fore-and-aft direction of the bases of two second connecting brackets along the aircraft body Set and be connected respectively with two second water spraying mechanisms；The quantity of second connecting rod is two, and described second connects Extension bar is vertically arranged, and two second connecting rods are connected to the two ends of the swing arm of second steering wheel, and described second One end of connecting rod is connected with the swing arm of second steering wheel, and the other end is connected with the vertical edge of second connecting bracket.
- The aircraft 5. three jet pipe according to claim 1 is sprayed water, it is characterised in that：The bottom of the aircraft body is provided with First spacing groove, width of the first spacing groove along the aircraft body is set, first water spraying mechanism It is movably arranged in the described first spacing groove.
- The aircraft 6. three jet pipe according to claim 5 is sprayed water, it is characterised in that：The quantity of first drive mechanism is One, first drive mechanism includes the 3rd steering wheel, the 3rd connecting rod and the 3rd connecting bracket, and the aircraft body is perpendicular The tetragonal body structure directly set, the 3rd steering wheel is located at the inside of the aircraft body, and located at the aircraft body Front end face or rear end face on, the swing arm of the 3rd steering wheel is set parallel to the front end face and rear end face of the aircraft body Put；3rd connecting bracket is shaped as L-shaped, the swing arm of the base of the 3rd connecting bracket parallel to the 3rd steering wheel And be connected with first water spraying mechanism；3rd connecting rod is vertically arranged, and one end of the 3rd connecting rod with it is described The swing arm of 3rd steering wheel is hinged, and the other end and the vertical edge of the 3rd connecting bracket are hinged.
- The aircraft 7. three jet pipe according to claim 6 is sprayed water, it is characterised in that：The quantity of second drive mechanism is Two, two second drive mechanisms are connected with two second water spraying mechanisms correspondingly, second driving machine Structure includes the 4th steering wheel, the 4th connecting rod and the 4th connecting bracket, and two the 4th steering wheels are respectively arranged in the aircraft On the side that two of body be arranged in parallel, and the 4th steering wheel swing arm perpendicular to the side of the aircraft body；Institute State the L-shaped that is shaped as of the 4th connecting bracket, the base of the 4th connecting bracket parallel to the 4th steering wheel swing arm and with The second water spraying mechanism connection；4th connecting rod is vertically arranged, and one end and the described 4th of the 4th connecting rod The swing arm of steering wheel is hinged, and the other end and the vertical edge of the 4th connecting bracket are hinged.
- 8. the three jet pipes water spray aircraft according to claim any one of 1-7, it is characterised in that：The aircraft body The second spacing groove is respectively equipped with two sides, fore-and-aft direction of the second spacing groove along the aircraft body is set Put, second water spraying mechanism is movably arranged in the described second spacing groove.
- 9. the three jet pipes water spray aircraft according to claim any one of 1-7, it is characterised in that：First water spraying mechanism Include with the second water spraying mechanism shower nozzle and and flexible hose, the flexible hose passes through connecting tube and the water supply mechanism and connects Connect, first drive mechanism and the second drive mechanism are connected to the spray of first water spraying mechanism and the second water spraying mechanism On head.
- 10. the three jet pipes water spray aircraft according to claim any one of 1-7, it is characterised in that：The aircraft casing Interior to be provided with Fei Kong mechanisms, the Fei Kong mechanisms include battery, circuit board, sensor and wireless instructions receiver, and the battery is The flight of the aircraft provides electric energy, and the sensor is used for the attitude information for detecting the aircraft, the wireless instructions Receiver is used to receive telecommand, attitude information and the wireless instructions that the circuit board is detected according to the sensor The telecommand that receiver is received obtains the expectation deflection angle of first water spraying mechanism and the second water spraying mechanism, and controls institute State the first drive mechanism, the second drive mechanism and the water supply mechanism and make corresponding action.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710162226.5A CN107031843B (en) | 2017-03-17 | 2017-03-17 | A kind of three jet pipes water spray aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710162226.5A CN107031843B (en) | 2017-03-17 | 2017-03-17 | A kind of three jet pipes water spray aircraft |
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| Publication Number | Publication Date |
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| CN107031843A true CN107031843A (en) | 2017-08-11 |
| CN107031843B CN107031843B (en) | 2019-06-14 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201710162226.5A Active CN107031843B (en) | 2017-03-17 | 2017-03-17 | A kind of three jet pipes water spray aircraft |
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| CN108910046A (en) * | 2018-07-13 | 2018-11-30 | 北京航空航天大学 | A kind of water spray aircraft adjusting gesture stability mode based on flow |
| CN111907710A (en) * | 2020-08-17 | 2020-11-10 | 来宾市农业科学院 | Sugarcane medicament spraying system |
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Also Published As
| Publication number | Publication date |
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| CN107031843B (en) | 2019-06-14 |
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