CN108995812A - It is adjusted based on flow and jet pipe swings the water spray aircraft for mixing gesture stability mode - Google Patents
It is adjusted based on flow and jet pipe swings the water spray aircraft for mixing gesture stability mode Download PDFInfo
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- CN108995812A CN108995812A CN201810770765.1A CN201810770765A CN108995812A CN 108995812 A CN108995812 A CN 108995812A CN 201810770765 A CN201810770765 A CN 201810770765A CN 108995812 A CN108995812 A CN 108995812A
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- water spraying
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- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 title claims abstract description 271
- 239000007921 spray Substances 0.000 title claims abstract description 47
- 230000007246 mechanism Effects 0.000 claims abstract description 116
- 238000005507 spraying Methods 0.000 claims abstract description 92
- 230000008520 organization Effects 0.000 claims abstract description 36
- 230000005611 electricity Effects 0.000 claims description 3
- 239000007787 solid Substances 0.000 claims 1
- 238000005516 engineering process Methods 0.000 abstract description 3
- 230000001276 controlling effect Effects 0.000 description 8
- 238000010586 diagram Methods 0.000 description 5
- 230000008901 benefit Effects 0.000 description 4
- 230000005484 gravity Effects 0.000 description 4
- 238000009434 installation Methods 0.000 description 4
- 230000001105 regulatory effect Effects 0.000 description 4
- 230000001737 promoting effect Effects 0.000 description 3
- 230000008859 change Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- TVEXGJYMHHTVKP-UHFFFAOYSA-N 6-oxabicyclo[3.2.1]oct-3-en-7-one Chemical compound C1C2C(=O)OC1C=CC2 TVEXGJYMHHTVKP-UHFFFAOYSA-N 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000033228 biological regulation Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- JEGUKCSWCFPDGT-UHFFFAOYSA-N h2o hydrate Chemical compound O.O JEGUKCSWCFPDGT-UHFFFAOYSA-N 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 230000007704 transition Effects 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
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- Life Sciences & Earth Sciences (AREA)
- Pest Control & Pesticides (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Nozzles (AREA)
- Special Spraying Apparatus (AREA)
Abstract
The present invention relates to vehicle technology fields, more particularly to the water spray aircraft that mixing gesture stability mode is swung with jet pipe is adjusted based on flow, including flow control valve, water inlet pipe, water spraying mechanism, direction adjustment organization and driving mechanism, water spraying mechanism has water inlet and multiple water jets, water inlet is connect with water inlet pipe, flow control valve is rotatably set between water inlet and multiple water jets, for controlling the water flow for flowing to each water jet, driving mechanism is connect with flow control valve, and direction adjustment organization is used to adjust the water spraying direction of at least one water jet.The water sprayed from water spraying mechanism provides a reversed thrust to aircraft body, by adjusting the amount of water sprayed of each water jet and the water spraying direction of water jet, the control to aircraft flight posture can be achieved, the size of the amount of water sprayed of each water jet need to be only adjusted by flow control valve, and water spraying direction is adjusted by direction adjustment organization, aircraft can be realized in the stabilized flight of three-dimensional space.
Description
Technical field
The present invention relates to vehicle technology fields, more particularly to a kind of adjusted based on flow to swing mixing posture control with jet pipe
The water spray aircraft of mode processed.
Background technique
The in the prior art of water spray aircraft for entertainment project does not use automatic Pilot technology, it is necessary to have
People stands or sits and drives on board the aircraft to it, is unable to remotely-piloted vehicle and carries out unmanned independent flight.
Such as the JETOVATOR of the Jetavation company exploitation in the U.S. is a kind of water spray of pilot steering for amusement
Aircraft is mainly adjusted the position of center of gravity by the posture of people and manipulates the direction of two lateral jet pipes water spray to control aircraft
Posture realizes flight.This manned water spray aircraft is very high to the physical fitness and manipulation skill requirement of driver,
It can not be manipulated without the personnel of specialized training, therefore only be adapted to the stunt of professional athlete.
Summary of the invention
(1) technical problems to be solved
The technical problem to be solved by the present invention is to solve existing water spray aircraft mainly by the attitude regulation of people, it is not easy
The problem of operation.
(2) technical solution
It is adjusted in order to solve the above-mentioned technical problems, the present invention provides one kind based on flow and jet pipe swings mixing posture control
The water spray aircraft of mode processed, including flow control valve, water inlet pipe, water spraying mechanism, direction adjustment organization and driving mechanism, it is described
Water spraying mechanism has water inlet and multiple water jets, and the water inlet is connect with the water inlet pipe, and the flow control valve can turn
Dynamic is set between the water inlet and multiple water jets, for controlling the water flow for flowing to each water jet, institute
It states driving mechanism to connect with the flow control valve, for driving the flow control valve to rotate, the direction adjustment organization is used
In the water spraying direction for adjusting at least one water jet.
Wherein, the water spraying mechanism includes upper hose, connecting cylinder and sparge pipe, and one end of the upper hose is the water inlet
Mouthful, the other end is connect with the side wall of the connecting cylinder；One end of the sparge pipe is the water jet, the other end and the connection
The side wall connection of cylinder；The open end of the flow control valve from the connecting cylinder is mounted in the connecting cylinder, and is located at water flow
On path, for controlling the water flow entered in the sparge pipe from the upper hose.
Wherein, the quantity of each sparge pipe is two, and two sparge pipes are symmetrically set in the two of the connecting cylinder
Side, the sparge pipe include flowing water section and spray-type air washer section, and the flowing water section is connect with the side wall of the connecting cylinder, the spray-type air washer section edge
The end of the flowing water section is bent to form L-shaped structure.
Wherein, the direction adjustment organization includes connection hose, the first gimbaled nozzle, link assembly and the first driving electricity
One end of machine, the connection hose is connect with the water jet of the sparge pipe, and the other end is connect with first gimbaled nozzle, institute
It states the first driving motor to connect by the connection component with first gimbaled nozzle, for driving first gimbaled nozzle
It swings.
Wherein, first driving motor is fixedly mounted on the sparge pipe, the output shaft of first driving motor
It is arranged perpendicular to the spray-type air washer section, the link assembly includes the first connector, the second connector and third connector, and described the
A connection piece is mounted on the output shaft of first driving motor, and the third connector is fixed on described first and swings spray
Guan Shang, one end of second connector and first connector are hinged, and the other end and the third connector are hinged.
Wherein, the direction adjustment organization includes the second driving motor and the second gimbaled nozzle, the end of the spray-type air washer section
Outer surface be arc surface, the inner wall of second gimbaled nozzle is the arc surface matched with the end of the spray-type air washer section, and
Second gimbaled nozzle is rotatably set in the end of the spray-type air washer section, and the outer wall of the spray-type air washer section is equipped with mounting rack,
Second driving motor is mounted on the mounting rack, and the output shaft of second driving motor is set perpendicular to the spray-type air washer section
It sets and is connect with second gimbaled nozzle, for driving second gimbaled nozzle to swing.
Wherein, the side wall of the spray-type air washer section is equipped with the shaft part vertical with the spray-type air washer section, the shaft part and described second
Driving motor is set to the opposite two sides of second gimbaled nozzle, and the outer wall of second gimbaled nozzle is equipped with sleeve, institute
It states sleeve to be rotatably set on the shaft part, the output shaft of second driving motor and the axis of the gimbaled nozzle hang down
It is straight and non-intersecting.
Wherein, the flow control valve includes interconnecting piece and adjustment portion, and the interconnecting piece is used to connect with the driving mechanism
It connects, the shape of the cross section of the adjustment portion is round smaller part, semicircle or large semi-circular, and the driving mechanism is driving institute
During stating flow control valve rotation, the adjustment portion is entered in two sparge pipes for adjusting from the upper hose
Water flow；The outer wall of the sparge pipe is equipped with support frame, and the driving mechanism includes third driving motor, and the third
Driving motor is installed on support frame as described above, and the output shaft of the third driving motor passes through support frame as described above and the interconnecting piece
Connection.
Wherein, the quantity of the water spraying mechanism is multiple, the driving mechanism, the flow control valve and the sprinkler
The quantity of structure is identical, and is arranged in a one-to-one correspondence with the water spraying mechanism；The sparge pipe of at least one water spraying mechanism is equipped with
The direction adjustment organization.
Wherein, the quantity of the water spraying mechanism is two, is followed successively by the first water spraying mechanism and the second water spraying mechanism, described the
One water spraying mechanism and second water spraying mechanism are fixed in cross-lap joint, and first water spraying mechanism and second water spray
The water jet of each sparge pipe of mechanism is towards identical, wherein first water spraying mechanism and/or second sprinkler
The sparge pipe of structure is equipped with direction adjustment organization.
(3) beneficial effect
Above-mentioned technical proposal of the invention has the advantages that a kind of adjusted based on flow provided by the invention is put with jet pipe
The water spray aircraft of dynamic mixing gesture stability mode, including flow control valve, water inlet pipe, water spraying mechanism, direction adjustment organization and
There is water inlet and multiple water jets, water inlet to connect with water inlet pipe for driving mechanism, water spraying mechanism, and flow control valve is rotatable
Between water inlet and multiple water jets, for controlling the water flow for flowing to each water jet, driving mechanism and flow are adjusted
Valve connection, for driving flow control valve to rotate, direction adjustment organization is used to adjust the water spraying direction of at least one water jet.From
Water spraying mechanism spray water give aircraft body provide a reversed thrust, amount of water sprayed number can adjust the big of thrust
It is small, by adjusting the amount of water sprayed of each water jet and the water spraying direction of water jet, it can be achieved that control to aircraft flight posture,
The water spray aircraft need to only adjust the size of the amount of water sprayed of each water jet by flow control valve, and pass through direction adjustment organization
Adjust water spraying direction, aircraft can be realized in the stabilized flight of three-dimensional space, no longer need to by the pose adjustment center of gravity of people come
The posture of aircraft is adjusted, thus can realize unmanned, easy to operate, more promotional value.
In addition to it is described above present invention solves the technical problem that, constitute technical solution technical characteristic and have this
Except advantage brought by the technical characteristic of a little technical solutions, other technical characteristics of the invention and these technical characteristic brings
Advantage will be further illustrated in conjunction with attached drawing.
Detailed description of the invention
The disassembly figure of aircraft that Fig. 1 is water spraying mechanism provided in an embodiment of the present invention when being one (does not include direction tune
Save mechanism)；
The assembling figure of aircraft that Fig. 2 is water spraying mechanism provided in an embodiment of the present invention when being one (does not include direction tune
Save mechanism)；
Fig. 3 is that the state diagram under one state of flow control valve provided in an embodiment of the present invention (does not include that direction adjusts machine
Structure)；
Fig. 4 is the sectional view along A-A (not including direction adjustment organization) in Fig. 3；
Fig. 5 is that the state diagram under one state of flow control valve provided in an embodiment of the present invention (does not include that direction adjusts machine
Structure)；
Fig. 6 is the sectional view along A-A (not including direction adjustment organization) in Fig. 5；
Fig. 7 is that the state diagram under one state of flow control valve provided in an embodiment of the present invention (does not include that direction adjusts machine
Structure)；
Fig. 8 is the sectional view along A-A (not including direction adjustment organization) in Fig. 7；
Fig. 9 is structural schematic diagram (including the direction one for the aircraft that the embodiment of the present invention is provided when water spraying mechanism is one
Kind regulating mechanism)；
Figure 10 is another direction view of Fig. 9；
Structural schematic diagram (including the another kind of Figure 11 is water spraying mechanism provided in an embodiment of the present invention when being two aircraft
Direction adjustment organization)；
Figure 12 is the view in another direction of Figure 11.
In figure: 1: third driving motor；2: the output shaft of third driving motor；3: fixture block；4: interconnecting piece；5: adjustment portion；
6: connecting cylinder；7: upper hose；8: sparge pipe；9: support frame；401: card slot；402: buckle；801: flowing water section；802: spray-type air washer section；
10: link assembly；11: connection hose；12: the first gimbaled nozzles；13: the first driving motors；14: position-limited rack；Connect at 101: the first
Fitting；102: the second connectors；103: third connector；15: the first water spraying mechanisms；16: the second driving motors；Drive at 17: the second
The output shaft of dynamic motor；18: rocker arm；19: the second gimbaled nozzles；20: sleeve；21: mounting rack；22: the second water spraying mechanisms；23:
Water inlet pipe；24: article carrying platform；25: shaft part.
Specific embodiment
In order to make the object, technical scheme and advantages of the embodiment of the invention clearer, below in conjunction with the embodiment of the present invention
In attached drawing, technical scheme in the embodiment of the invention is clearly and completely described, it is clear that described embodiment is
A part of the embodiments of the present invention, instead of all the embodiments.Based on the embodiments of the present invention, ordinary skill people
Member's every other embodiment obtained without making creative work, shall fall within the protection scope of the present invention.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " installation ", " phase
Even ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or be integrally connected；It can
To be mechanical connection, it is also possible to be electrically connected；It can be directly connected, can also can be indirectly connected through an intermediary
Connection inside two elements.For the ordinary skill in the art, above-mentioned term can be understood at this with concrete condition
Concrete meaning in invention.
In addition, in the description of the present invention, unless otherwise indicated, " multiple ", " more ", " multiple groups " be meant that two or
Two or more, " several ", " several ", " several groups " are meant that one or more.
As shown in Figures 1 to 12, mixing appearance is swung with jet pipe for a kind of adjust based on flow provided in an embodiment of the present invention
The water spray aircraft of state control mode, including flow control valve, water inlet pipe 23, water spraying mechanism, direction adjustment organization and driving machine
Structure, water spraying mechanism have water inlet and multiple water jets, and water inlet is connect with water inlet pipe 23, and water inlet pipe is connected with water pump, water
Water pressurization is entered water inlet pipe 23 by pump, is then sprayed by water spraying mechanism, so that reaction force is generated, the flying height of aircraft
It is related with the pressure of water pump.Flow control valve is rotatably set between water inlet and multiple water jets, each for controlling flow direction
The water flow of a water jet, driving mechanism are connect with flow control valve, for driving flow control valve to rotate, direction adjustment organization
For adjusting the water spraying direction of at least one water jet.The water sprayed from water spraying mechanism to aircraft body provide one it is reversed
Thrust, amount of water sprayed number can adjust the size of thrust, pass through the water spray of the amount of water sprayed and water jet that adjust each water jet
Direction is, it can be achieved that control to aircraft flight posture, the water spray aircraft need to only adjust each water spray by flow control valve
Mouthful amount of water sprayed size and by direction adjustment organization adjusting water spraying direction, aircraft can be realized in the stabilization of three-dimensional space
Flight, no longer needs to the posture that aircraft is adjusted by the pose adjustment center of gravity of people, thus can realize unmanned, operation letter
List, more promotional value.
Further, water spraying mechanism includes upper hose 7, connecting cylinder 6 and sparge pipe 8, in one embodiment of invention, even
The open at one end of connect cylinder 6, other end closing；Upper hose 7 is connected between water inlet pipe 23 and connecting cylinder 6, specifically, upper hose 7
One end be the filling pipe end being connect with water inlet pipe 23, the other end is connect with the side wall of connecting cylinder 6；One end of sparge pipe 8 is water spray
Mouthful, the other end is connect with the side wall of connecting cylinder 6；The open end of flow control valve from connecting cylinder 6 is mounted in connecting cylinder 6, and position
In on flow path, for controlling the water flow entered in sparge pipe 8 from upper hose 7.Process of the flow control valve in rotation
In the adjustable water flow entered from upper hose 7 in sparge pipe 8, that is, adjust water jet amount of water sprayed size, into
And realize the adjustment to the flight attitude of aircraft.
Further, the quantity of sparge pipe 8 is two in each water spraying mechanism, and the shape of sparge pipe 8 is L shape, and two
Sparge pipe 8 is symmetrically set in the two sides of connecting cylinder 6.Specifically, sparge pipe 8 includes flowing water section 801 and spray-type air washer section 802, flowing water section 801
It is connect along the direction perpendicular to connecting cylinder 6 with the side wall of connecting cylinder 6, spray-type air washer section 802 is bent along the end of flowing water section 801, with stream
Angle between water section 801 is close to 90 degree, and arc transition between spray-type air washer section 802 and flowing water section 801, in the present embodiment, two
The flowing water section of a sparge pipe 8 is arranged along straight line, and the spray-type air washer section of two sparge pipes 8 is bent in the same direction, therefore two sprays
The water spraying direction of water pipe 8 is identical.
Further, as shown in Figure 9 and Figure 10, in one embodiment of the present of invention, direction adjustment organization includes that connection is soft
Pipe 11, the first gimbaled nozzle 12, link assembly 10 and the first driving motor 13 connect one end of hose 11 and the spray of sparge pipe 8
Mouth of a river connection, that is, connect with the end of spray-type air washer section 802, the other end of connection hose 11 is connect with the first gimbaled nozzle 12,
First driving motor 13 is connect by connection component 10 with the first gimbaled nozzle 12, for driving the first gimbaled nozzle 12 to swing.
Specifically, the first driving motor 13 is fixedly mounted on sparge pipe 8, and in the present embodiment, the first driving motor 13
It being mounted on by fixed frame on the outer wall of spray-type air washer section 802, the output shaft of the first driving motor 13 is arranged perpendicular to spray-type air washer section 802,
Link assembly 10 includes the first connector 101, the second connector 102 and third connector 103, the installation of the first connector 101
On the output shaft of the first driving motor 13, third connector 103 is fixed on the first gimbaled nozzle 12, the second connector 102
One end and the first connector 101 it is hinged, the other end and third connector hinged 103.Specifically, the one of the first connector 101
End is fixed on the output shaft of the first driving motor 13, and the shape of third connector 103 is L shape, and the one of third connector 103
End is fixed on the outer wall of the first gimbaled nozzle 12, the other end of third connector 103 and the second connector hinged 102, and second
The both ends of connector 102 are respectively arranged on the shaft vertical with the second connector 102, and two shafts are rotatably inserted in first respectively
Hole on connector 101 and in the hole of third connector 103, realizes the second connector 102 and the first connector 101 and third company
Fitting 103 it is hinged.
As shown in FIG. 11 and 12, in another embodiment of the present invention, direction adjustment organization includes the second driving motor
16 and second gimbaled nozzle 19, the outer surface of the end of spray-type air washer section is arc surface, and the inner wall of the second gimbaled nozzle 19 is and water spray
The arc surface that matches of end of section, and the second gimbaled nozzle 19 is rotatably set in the end of spray-type air washer section, spray-type air washer section it is outer
Wall is equipped with mounting rack 21, and the second driving motor 16 is mounted on mounting rack 21, and the output shaft 17 of the second driving motor 16 is vertical
It is arranged in spray-type air washer section and is connect with the second gimbaled nozzle 19, for drives the second gimbaled nozzle 19 to swing.
Specifically, the side wall of spray-type air washer section is equipped with the shaft part 25 vertical with spray-type air washer section, shaft part 25 and the second driving motor 16
Set on the opposite two sides of the second gimbaled nozzle 19, the outer wall of the second gimbaled nozzle 19 is equipped with sleeve 20, and sleeve 20 can be rotated
Be set on shaft part 25 and play the role of fixing the second gimbaled nozzle 19, the output shaft 17 of the second driving motor 16 and the second pendulum
The axis of dynamic jet pipe 19 is vertical and non-intersecting, and the outer wall of the second gimbaled nozzle 19 is equipped with rocker arm 18, realizes the second driving motor
16 output shaft 17 drives the second gimbaled nozzle 19 to swing when rotating, guarantee the swing effect of the second gimbaled nozzle 19, the second pendulum
Dynamic jet pipe 19 changes the direction of water spray during swing.
Further, flow control valve includes interconnecting piece 4 and adjustment portion 5, and interconnecting piece 4 is adjusted for connecting with driving mechanism
The shape of the cross section in section portion 5 is round smaller part, semicircle or large semi-circular, and driving mechanism is driving flow control valve rotation
During, adjustment portion 5 is for adjusting the water flow entered in two sparge pipes 8 from upper hose 7.In the present embodiment, it adjusts
Section portion 5 is semicircle column structure, is extend into connecting cylinder 6 from the open end of connecting cylinder 6, sparge pipe 8 is connect with connecting cylinder 6
One end is first entrance, and the diameter of first entrance is less than the diameter of connecting cylinder 6, and the size of adjustment portion 5 is rationally arranged, to be protected
Demonstrate,prove adjustment portion 5 in the course of rotation, can the openings of sizes to first entrance effectively adjusted.When adjustment portion 5 turns to
When position as shown in Figure 3 and Figure 4, the openings of sizes of two first entrances of the left and right sides is identical, flows into two sparge pipes 8
Water is identical, thus the torque generated is in equilibrium state；It is left when adjustment portion 5 turns to position as shown in Figure 5 and Figure 6
The first entrance of side opening be greater than right side first entrance opening, therefore enter right side sparge pipe 8 water flow be less than into
Enter the water flow to left side sparge pipe 8, clockwise torque will be generated；When adjustment portion 5 turns to as shown in Figure 7 and Figure 8
Position when, the first entrance on right side opening be greater than left side first entrance opening, enter right side sparge pipe 8 water flow
Amount is greater than the water flow for entering left side sparge pipe 8, will generate anticlockwise torque.Therefore pass through rotation flow regulating valve
The amount of water sprayed of adjustable difference sparge pipe 8, and then realize the adjustment to flight attitude.
Further, interconnecting piece 4 is rotatably fastened on the open end of connecting cylinder 6, and interconnecting piece is equipped with card slot 401,
Driving mechanism includes the fixture block 3 cooperated with card slot 401.In the present embodiment, the open end of connecting cylinder 6 has the flange to turn up,
There is buckle 402, buckle 402 is fastened on flange, and interconnecting piece 4 can be rotated around the axis of connecting cylinder 6 on interconnecting piece 4.Buckle
402 avoid flow control valve in the impact by hydraulic pressure with the disengagement of connecting cylinder 6 with the design of flange, ensure that overall structure
Stability.The shape of fixture block 3 is cross, and the shape of card slot 401 is also cross, and fixture block 3 is embedded in card slot 401, and logical
It crosses screw and connect fixture block 3 with interconnecting piece 4.
In addition connecting cylinder can be the tubular structure of both ends open, and circular slab and connecting cylinder is arranged in the end of adjustment portion
One open end cooperation, avoids water from flowing out.
Further, the outer wall of sparge pipe 8 is equipped with support frame 9, and driving mechanism includes third driving motor 1, and third
Driving motor 1 is installed on support frame 9, and the output shaft 2 of third driving motor 1 passes through support frame 9, and fixture block 3 is mounted on third drive
On the output shaft 2 of dynamic motor 1.During rotation, band rotation connection 4 rotates together the output shaft 2 of third driving motor 1, into
And adjustment portion 5 is driven to rotate in connecting cylinder 6.
Further, the quantity of water spraying mechanism can be also possible to multiple for one, when the quantity of water spraying mechanism is one
When, structure is as Figure 1-10 shows.
When water spraying mechanism quantity be it is multiple, driving mechanism, flow control valve are identical as the quantity of water spraying mechanism, and with spray
Water dispenser structure is arranged in a one-to-one correspondence, and the sparge pipe of wherein at least one water spraying mechanism is equipped with direction adjustment organization.
Specifically, as shown in FIG. 11 and 12, listing the feelings that water spraying mechanism is two in one embodiment of the invention
Condition.
By taking the quantity of water spraying mechanism is two as an example, two water spraying mechanisms are followed successively by the first water spraying mechanism 15 and the second water spray
Mechanism 22, the first water spraying mechanism 15 and the second sprinkler 22 composition are fixed in cross-lap joint, that is, the first water spraying mechanism 15
Flowing water section is vertical with the flowing water section of the second water spraying mechanism 22, and each water spray of the first water spraying mechanism 15 and the second water spraying mechanism 22
The water jet of pipe is towards identical, as shown in figure 11, the water jet of the sparge pipe of the first water spraying mechanism 15 and the second water spraying mechanism 22
Downward, it in water spray, sprays water facing one direction, wherein the water spray of the first water spraying mechanism 15 and/or the second water spraying mechanism 22
Pipe is equipped with direction adjustment organization, specifically, in an embodiment of the present invention, the sparge pipe of the first water spraying mechanism 15 is equipped with side
To regulating mechanism, not set direction adjustment organization on the sparge pipe of the second water spraying mechanism 22, it will be appreciated by those skilled in the art that
, according to actual needs, direction tune can be respectively provided on the sparge pipe of the first water spraying mechanism 15 and the second water spraying mechanism 22
Mechanism is saved, or is not provided with direction adjustment organization in the first water spraying mechanism 15, setting direction adjusts machine on the second water spraying mechanism 22
Structure.And the form of direction adjustment organization can be at least one of above two direction adjustment organization.
It should be noted that the quantity of water spraying mechanism is not limited to two, it can also be three and three or more, work as sprinkler
When the quantity of structure is three or three or more, the set-up mode for being two referring to water spraying mechanism, reasonable setting three or three
The arrangement of above water spraying mechanism.
It further, further include control mechanism and power supply, control mechanism and each driving mechanism and all directions adjust machine
Structure connection, for controlling revolving speed and steering and the movement of all directions regulating mechanism of each driving mechanism, power supply is used for as spray
Water aircraft provides electric energy.Specifically, control mechanism is mainly used for controlling third driving motor 1, the second driving motor and third
The revolving speed of driving motor and steering, and then the rotation of flow control valve is controlled, it realizes and the flow of different water jets is adjusted.Pacifying
When filling control mechanism and power supply, for installation site of reasonably arranging, installation space is saved, sparge pipe 8 can be control mechanism
It is stepped down with power supply and generates bending appropriate, but to guarantee the direction for not changing water jet.
In addition, the aircraft of the embodiment of the present invention further includes article carrying platform 24, article carrying platform 24 passes through connection frame and water spray
Pipe 8 connects, and article carrying platform 24 and water jet are set on the opposite two sides of sparge pipe 8.
One provided in an embodiment of the present invention adjusts the water spray for swinging mixing gesture stability mode with jet pipe based on flow and flies
Row device, including flow control valve, water inlet pipe, water spraying mechanism, direction adjustment organization and driving mechanism, water spraying mechanism have water inlet
With multiple water jets, water inlet is connect with water inlet pipe, and flow control valve is rotatably set between water inlet and multiple water jets,
For controlling the water flow for flowing to each water jet, driving mechanism is connect with flow control valve, for driving flow control valve to turn
Dynamic, direction adjustment organization is used to adjust the water spraying direction of water jet.The water sprayed from water spraying mechanism provides one to aircraft body
A reversed thrust, the number of amount of water sprayed can adjust the size of thrust, and the change of water spraying direction can change the direction of thrust,
By the amount of water sprayed and water spraying direction that adjust each water jet, it can be achieved that control to aircraft flight posture, water spray flight
Device need to only be adjusted the size of the amount of water sprayed of each water jet by flow control valve and adjust each spray by direction adjustment organization
The water spraying direction at the mouth of a river can be realized aircraft in the stabilized flight of three-dimensional space, realize the rolling, pitching and yaw of aircraft
Control, no longer need to the posture that aircraft is adjusted by the pose adjustment center of gravity of people, thus can realize it is 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
Present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art should understand that: it still may be used
To modify the technical solutions described in the foregoing embodiments or equivalent replacement of some of the technical features；
And these are modified or replaceed, technical solution of various embodiments of the present invention that it does not separate the essence of the corresponding technical solution spirit and
Range.
Claims (10)
1. a kind of adjust the water spray aircraft for swinging mixing gesture stability mode with jet pipe based on flow, it is characterised in that: including
Flow control valve, water inlet pipe, water spraying mechanism, direction adjustment organization and driving mechanism, the water spraying mechanism have water inlet and more
A water jet, the water inlet are connect with the water inlet pipe, and the flow control valve is rotatably set to the water inlet and more
Between a water jet, for controlling the water flow for flowing to each water jet, the driving mechanism and the flow tune
Valve connection is saved, for driving the flow control valve to rotate, the direction adjustment organization is for adjusting at least one described water spray
The water spraying direction of mouth.
2. water spray aircraft according to claim 1, it is characterised in that: the water spraying mechanism includes upper hose, connecting cylinder
And sparge pipe, one end of the upper hose are the filling pipe end connecting with the water inlet pipe, the side wall of the other end and the connecting cylinder
Connection；One end of the sparge pipe is the water jet, and the other end is connect with the side wall of the connecting cylinder；The flow control valve
It is mounted in the connecting cylinder, and is located on flow path, entered in the sparge pipe for controlling from the upper hose
Water flow.
3. water spray aircraft according to claim 2, it is characterised in that: the quantity of each sparge pipe be two, two
A sparge pipe is symmetrically set in the two sides of the connecting cylinder, and the sparge pipe includes flowing water section and spray-type air washer section, the flowing water section
It is connect with the side wall of the connecting cylinder, the spray-type air washer section is bent to form L-shaped structure along the end of the flowing water section.
4. water spray aircraft according to claim 3, it is characterised in that: the direction adjustment organization include connection hose,
First gimbaled nozzle, link assembly and the first driving motor, one end of the connection hose and the water jet of the sparge pipe connect
It connects, the other end is connect with first gimbaled nozzle, and first driving motor passes through the connection component and first pendulum
Dynamic jet pipe connection, for driving first gimbaled nozzle to swing.
5. water spray aircraft according to claim 4, it is characterised in that: first driving motor is fixedly mounted on described
On sparge pipe, the output shaft of first driving motor is arranged perpendicular to the spray-type air washer section, and the link assembly includes the first company
Fitting, the second connector and third connector, first connector are mounted on the output shaft of first driving motor,
The third connector is fixed on first gimbaled nozzle, and one end of second connector and first connector are cut with scissors
It connects, the other end and the third connector are hinged.
6. water spray aircraft according to claim 3, it is characterised in that: the direction adjustment organization includes the second driving electricity
Machine and the second gimbaled nozzle, the outer surface of the end of the spray-type air washer section are arc surface, the inner wall of second gimbaled nozzle be with
The arc surface that the end of the spray-type air washer section matches, and second gimbaled nozzle is rotatably set in the end of the spray-type air washer section
The outer wall at end, the spray-type air washer section is equipped with mounting rack, and second driving motor is mounted on the mounting rack, and described second drives
The output shaft of dynamic motor is arranged perpendicular to the spray-type air washer section and connect with second gimbaled nozzle, for driving second pendulum
Dynamic jet pipe is swung.
7. water spray aircraft according to claim 6, it is characterised in that: the side wall of the spray-type air washer section is equipped with and the spray
The vertical shaft part of water section, the shaft part and second driving motor are set to the opposite two sides of second gimbaled nozzle, institute
The outer wall for stating the second gimbaled nozzle is equipped with sleeve, and the sleeve is rotatably set on the shaft part, second driving
The output shaft of motor is vertical and non-intersecting with the axis of the gimbaled nozzle.
8. water spray aircraft according to claim 2, it is characterised in that: the flow control valve includes interconnecting piece and adjusting
Portion, for the interconnecting piece for connecting with the driving mechanism, the shape of the cross section of the adjustment portion is that smaller part is round, semicircle
Or large semi-circular, and the driving mechanism, during driving flow control valve rotation, the adjustment portion is for adjusting
The water flow in two sparge pipes is entered from the upper hose；The outer wall of the sparge pipe is equipped with support frame, described
Driving mechanism includes third driving motor, and the third driving motor is installed on support frame as described above, the third driving electricity
The output shaft of machine passes through support frame as described above and connect with the interconnecting piece.
9. water spray aircraft according to claim 1-8, it is characterised in that: the quantity of the water spraying mechanism is more
A, the driving mechanism, the flow control valve are identical as the quantity of the water spraying mechanism, and a pair of with the water spraying mechanism one
It should be arranged；Wherein, the sparge pipe of at least one water spraying mechanism is equipped with the direction adjustment organization.
10. water spray aircraft according to claim 9, it is characterised in that: the quantity of the water spraying mechanism is two, successively
For the first water spraying mechanism and the second water spraying mechanism, first water spraying mechanism and second water spraying mechanism are at solid in cross-lap joint
It is fixed, and the water jet of each sparge pipe of first water spraying mechanism and second water spraying mechanism is towards identical, wherein
The sparge pipe of first water spraying mechanism and/or second water spraying mechanism is equipped with direction adjustment organization.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810770765.1A CN108995812B (en) | 2018-07-13 | 2018-07-13 | Water spraying aircraft based on flow regulation and spray pipe swing mixed attitude control mode |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810770765.1A CN108995812B (en) | 2018-07-13 | 2018-07-13 | Water spraying aircraft based on flow regulation and spray pipe swing mixed attitude control mode |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108995812A true CN108995812A (en) | 2018-12-14 |
| CN108995812B CN108995812B (en) | 2020-10-09 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810770765.1A Active CN108995812B (en) | 2018-07-13 | 2018-07-13 | Water spraying aircraft based on flow regulation and spray pipe swing mixed attitude control mode |
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| Country | Link |
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| CN (1) | CN108995812B (en) |
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| CN110466772A (en) * | 2019-07-12 | 2019-11-19 | 仲恺农业工程学院 | Hydraulic unmanned plane and plant protection system |
| CN110901910A (en) * | 2019-12-10 | 2020-03-24 | 武汉合厚丰玩具有限公司 | Automatic jet propeller for waterborne aircraft |
| CN112371052A (en) * | 2020-11-03 | 2021-02-19 | 殷震花 | Stirring and cleaning dual-purpose starting injection device for water-based paint production |
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Also Published As
| Publication number | Publication date |
|---|---|
| CN108995812B (en) | 2020-10-09 |
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