CN206437216U - A kind of amphibious unmanned plane - Google Patents
A kind of amphibious unmanned plane Download PDFInfo
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- CN206437216U CN206437216U CN201720120040.9U CN201720120040U CN206437216U CN 206437216 U CN206437216 U CN 206437216U CN 201720120040 U CN201720120040 U CN 201720120040U CN 206437216 U CN206437216 U CN 206437216U
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- fuselage
- pump
- flank
- rotor
- unmanned plane
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Abstract
The utility model provides a kind of amphibious unmanned plane, including fuselage, rudder plate, rotor, hydraulic balancer, flank, bottom pump, control end box, front end rotor and top pump, there is top pump above the fuselage head, there is bottom pump below the fuselage head, the bottom pump is corresponding with top pump position, there is front end rotor on front side of the fuselage head, there is control end box below the fuselage head, the tail end of the fuselage is provided with rudder plate, respectively there is a flank fuselage both sides, there is circular trough in the flank, there is hydraulic balancer in the circular trough of the flank, the motor of the hydraulic balancer is arranged on by support in the circular trough of flank, rotor is installed in the rotating shaft of the motor.
Description
Technical field
The utility model is related to unmanned plane field, more particularly to a kind of amphibious unmanned plane.
Background technology
With the continuous progress of science and technology, the operation strategies of unmanned plane are more and more wider, and traditional unmanned plane can only realize that sky flies
OK, and in practice, this unmanned plane limitation is very strong, such as in video capture, usually has from the air and enters water
In or enter from water the first aerial visual angle picture；It is in military surveillance, then spacing often very serious by landform, because
This needs to be redesigned for the unmanned plane on ordinary meaning for used above so that unmanned plane can realize water, sky
Flight.
Utility model content
In order to solve above-mentioned problem, the utility model provides a kind of amphibious unmanned plane, overall to use streamlined knot
Structure, and aircraft is combined with submarine, forms the method that exclusive dive is floated, and adds the principle of jet plane,
Substantially reduce resistance of the unmanned plane in water and provide powerful power to unmanned plane, thus can realize unmanned plane water,
Sky flight, for up to this purpose, the utility model provides a kind of amphibious unmanned plane, including fuselage, rudder plate, rotor, hydraulic balancer,
Flank, bottom pump, control end box, front end rotor and top pump, the fuselage are hollow, there is top pump above the fuselage head,
There is bottom pump below the fuselage head, the bottom pump is corresponding with top pump position, have front end on front side of the fuselage head
There is control end box below rotor, the fuselage head, the tail end of the fuselage is provided with rudder plate, and the fuselage both sides respectively have one
Having in flank, the flank has hydraulic balancer in circular trough, the circular trough of the flank, the motor of the hydraulic balancer leads to
Support is crossed in the circular trough of flank, rotor is installed in the rotating shaft of the motor.
Further improvement of the utility model, the hydraulic balancer includes balance base, plunger pump and motor, the motor
Be fixed in balance base, the plunger pump has three, the plunger pump angularly around motor rotating shaft center line one week, it is described
Plunger pump is connected with the mounting bracket of balance base and motor, and servomotor is fixed on balance base, balance base and three micro-columns
Pump connection is filled in, Small Plunger Pump is controlled by control end, changes balance base angle of inclination, so that change the angle of inclination of rotor,
Realize helicopter flight, steering, the principle of hovering.
Further improvement of the utility model, the fuselage main body is streamlined, and pigeon and whale are combined, given full play to
Bionics principle.Aircraft is combined with submarine.
Further improvement of the utility model, the fuselage bottom has a pair of undercarriages, set undercarriage for the ease of
Landed land.
A kind of amphibious unmanned plane of the utility model, using streamlined structure, pigeon and whale is combined, given full play to bionical
Learn principle.Aircraft is combined with submarine, the mode that the submarine dive on ordinary meaning is floated is changed, has created two
The method that this exclusive dive of unmanned plane of dwelling is floated, and the principle of jet plane is added, substantially reduce unmanned plane and exist
Resistance in water and provide powerful power to unmanned plane.
Brief description of the drawings
Fig. 1 is a kind of schematic diagram of the utility model.
Fig. 2 is another schematic diagram of the utility model.
Fig. 3 is the utility model spanwise portion structure chart.
Illustrate：
1st, fuselage；2nd, rudder plate；3rd, rotor；4th, hydraulic balancer；4-1, balance base；4-2, plunger pump；4-3, motor；5、
Flank；6th, undercarriage；7th, bottom pump；8th, control end box；9th, front end rotor；10th, top pump.
Embodiment
The utility model is described in further detail with embodiment below in conjunction with the accompanying drawings：
The utility model provides a kind of amphibious unmanned plane, integrally uses streamlined structure, and aircraft is mutually tied with submarine
Close, form the method that exclusive dive is floated, and add the principle of jet plane, substantially reduce unmanned plane in water
Resistance and powerful power is provided to unmanned plane, so that unmanned plane water, empty flight can be realized.
As a kind of embodiment of the utility model, the utility model provides a kind of amphibious unmanned plane, including fuselage 1, rudder plate
2nd, in rotor 3, hydraulic balancer 4, flank 5, bottom pump 7, control end box 8, front end rotor 9 and top pump 10, the fuselage 1
Sky, the above-head of fuselage 1 has top pump 10, and the lower head of fuselage 1 has bottom pump 7, the bottom pump 7 and top pump
10 positions are corresponding, and the rostral anterior of fuselage 1 has front end rotor 9, and the lower head of fuselage 1 has control end box 8, the machine
The tail end of body 1 is provided with rudder plate 2, and the both sides of fuselage 1, which respectively have, circular trough, the flank 5 in a flank 5, the flank 5
Circular trough in have a hydraulic balancer 4, the motor 4-3 of the hydraulic balancer 4 is arranged on the circular trough of flank 5 by support
It is interior, rotor 3 is installed in the rotating shaft of the motor 4-3.
As a kind of specific embodiment of the utility model, the utility model provide as shown in Figure 1-2 it is a kind of it is amphibious nobody
Machine, including fuselage 1, rudder plate 2, rotor 3, hydraulic balancer 4, flank 5, bottom pump 7, control end box 8, front end rotor 9 and top
Pump 10, the main body of fuselage 1 is streamlined, and pigeon and whale are combined, bionics principle is given full play to.By aircraft and submarine
It is combined, the fuselage 1 is hollow, a pair of undercarriages 6 are arranged at the bottom of fuselage 1, sets undercarriage on land to enter
Row landing, the above-head of fuselage 1 has top pump 10, and the lower head of fuselage 1 has bottom pump 7, the bottom pump 7 and top
The position of portion's pump 10 is corresponding, and the rostral anterior of fuselage 1 has front end rotor 9, and the lower head of fuselage 1 has control end box 8, institute
The tail end for stating fuselage 1 is provided with rudder plate 2, and the both sides of fuselage 1, which respectively have in a flank 5, the flank 5, circular trough, described
There is hydraulic balancer 4 in the circular trough of flank 5, the hydraulic balancer 4 includes balance base 4-1, plunger pump 4-2 as shown in Figure 3
It is fixed on motor 4-3, the motor 4-3 in balance base 4-1, the plunger pump 4-2 has three, the plunger pump 4-2 isogonisms
Spend the mounting bracket phase of the center line one week of the rotating shaft around motor 4-3, the plunger pump 4-2 and balance base 4-1 and motor 4-3
Even, servomotor is fixed on balance base, and balance base couples with three Small Plunger Pumps, and Miniature plunger is controlled by control end
Pump, changes balance base angle of inclination, so as to change the angle of inclination of rotor, realizes helicopter flight, steering, the principle of hovering,
The motor 4-3 of the hydraulic balancer 4 is arranged on by support in the circular trough of flank 5, is installed in the rotating shaft of the motor 4-3
There is rotor 3.
During the utility model airflight, left and right rotor is only allowed to work, and left and right rotor rotating speed is identical.Aircraft is used
Row DCB Specimen, flight theory is identical with helicopter, controls the angle of inclination of rotor to realize by hydro-cushion controller aerial
Flight, steering, hovering.
After the utility model dive, small rotor is realized and advanced as the power of unmanned plane；The servo electricity that rudder plate passes through afterbody
Machine controls its left/right to stir certain angle, so as to realize to the left/right-hand bend；Left and right rotor slowly runs, so as to realize fuselage
Upwardly or downwardly motion.
The utility model it is aerial on the water surface when, water is sucked fuselage by fuselage bottom pump, realizes dive；To sky from water
In, unmanned plane traffic direction is towards the water surface, after back pump surfaces, pump operation, and draws air into fuselage, same to opportunity
Body bottom pump starts draining, aircraft is floated, after aircraft or so rotor surfaces, and left and right rotor starts to rotate, and flies into sky
In.
It is described above, only it is preferred embodiment of the present utility model, is not that any other is made to the utility model
The limitation of form, and any modification made according to technical spirit of the present utility model or equivalent variations, still fall within this practicality new
Type scope claimed.
Claims (4)
1. a kind of amphibious unmanned plane, including fuselage（1）, rudder plate（2）, rotor（3）, hydraulic balancer（4）, flank（5）, bottom pump
（7）, control end box（8）, front end rotor（9）With top pump（10）, it is characterised in that：The fuselage（1）It is hollow, the fuselage
（1）Above-head has top pump（10）, the fuselage（1）Lower head has bottom pump（7）, the bottom pump（7）With top pump
（10）Position is corresponding, the fuselage（1）Rostral anterior has front end rotor（9）, the fuselage（1）Lower head has control end box
（8）, the fuselage（1）Tail end rudder plate is installed（2）, the fuselage（1）Respectively there is a flank both sides（5）, the flank（5）
Inside there are circular trough, the flank（5）Circular trough in have hydraulic balancer（4）, the hydraulic balancer（4）Motor（4-3）
Flank is arranged on by support（5）Circular trough in, the motor（4-3）Rotating shaft on rotor is installed（3）.
2. a kind of amphibious unmanned plane according to claim 1, it is characterised in that：The hydraulic balancer（4）Including balance
Seat（4-1）, plunger pump（4-2）And motor（4-3）, the motor（4-3）It is fixed on balance base（4-1）It is interior, the plunger pump（4-
2）There are three, the plunger pump（4-2）Angularly around motor（4-3）Rotating shaft center line one week, the plunger pump（4-2）With
Balance base（4-1）And motor（4-3）Mounting bracket be connected.
3. a kind of amphibious unmanned plane according to claim 1, it is characterised in that：The fuselage（1）Main body is streamlined.
4. a kind of amphibious unmanned plane according to claim 1, it is characterised in that：The fuselage（1）Bottom, which has a pair, rises and falls
Frame（6）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720120040.9U CN206437216U (en) | 2017-02-09 | 2017-02-09 | A kind of amphibious unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720120040.9U CN206437216U (en) | 2017-02-09 | 2017-02-09 | A kind of amphibious unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206437216U true CN206437216U (en) | 2017-08-25 |
Family
ID=59634196
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720120040.9U Active CN206437216U (en) | 2017-02-09 | 2017-02-09 | A kind of amphibious unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206437216U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106741933A (en) * | 2017-02-09 | 2017-05-31 | 金陵科技学院 | A kind of amphibious unmanned plane |
| CN114132499A (en) * | 2022-01-04 | 2022-03-04 | 中国海洋大学 | Sea, land and air underwater four-purpose aircraft |
-
2017
- 2017-02-09 CN CN201720120040.9U patent/CN206437216U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106741933A (en) * | 2017-02-09 | 2017-05-31 | 金陵科技学院 | A kind of amphibious unmanned plane |
| CN114132499A (en) * | 2022-01-04 | 2022-03-04 | 中国海洋大学 | Sea, land and air underwater four-purpose aircraft |
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