CN206277907U - A kind of three dwell unmanned plane - Google Patents
A kind of three dwell unmanned plane Download PDFInfo
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- CN206277907U CN206277907U CN201621153360.6U CN201621153360U CN206277907U CN 206277907 U CN206277907 U CN 206277907U CN 201621153360 U CN201621153360 U CN 201621153360U CN 206277907 U CN206277907 U CN 206277907U
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- unmanned plane
- wheel
- fuselage
- wing
- water
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Abstract
The utility model discloses a kind of three and dwells unmanned plane, and by setting in fuselage interior, the first screw mandrel stepper motor is pulled the utility model or passage sliding block is to adjust wing setting degree；The first steering wheel, the first brushless electric machine and first propeller of vertical lift are provided in two wing one end, the second steering wheel, the second brushless electric machine and the second propeller that unmanned plane is pushed ahead are provided in afterbody；Wheel is one in front and one in back set in fuselage bottom to rise and fall frame aperture, frame aperture is risen and fallen so that unmanned plane can reliably carry out steady land through wheel by the 3rd servo driving wheel undercarriage；Wheel is driven by motor so that unmanned function is walked on land.Unmanned plane is sucked in water receiver water by the water pump being arranged in fuselage, increases unmanned plane weight, to adapt to different water level depths.The utility model can realize the function of being moved under water in reliable airflight, land walking, water, so as to expand unmanned plane range of application relative to the unmanned plane of prior art.
Description
Technical field
The utility model is related to unmanned air vehicle technique field, and more particularly to a kind of three dwell unmanned plane.
Background technology
Unmanned plane because manufacturing cost is relatively low, mobility is good, survival ability is strong, no one was injured risk the advantages of, because
This occupies extremely important status in modern military war, boundless application is particularly possessed in civil area preceding
Scape, the field such as can be widely applied to military surveillance, takes photo by plane, follows the trail of, searching and rescuing.
But, the unmanned plane overwhelming majority of the prior art only realizes the function of flight, while realization is circled in the air and land in the air
Two unmanned plane quantity of function of upper walking are less, thus unmanned plane can realize circling in the air in the air simultaneously, land walking and water
In move under water three functions turn into be badly in need of solve technical problem.
Utility model content
Main purpose of the present utility model is to propose that a kind of three dwell unmanned plane, it is intended to unmanned plane is provided simultaneously with flight, land
Three kinds of functions of upper walking and diving, so as to expand the range of application of unmanned plane.
To achieve the above object, the utility model proposes a kind of three dwell unmanned plane, including fairshaped fuselage, the machine
Body upper rear is provided with vertical tail and tailplane, the vertical tail near the afterbody be also associated with for
The rudder of adjustment direction；The fuselage interior is provided with the first screw mandrel stepper motor and passes through linkage by sliding block along the fuselage
Passage before and after cephalocaudal direction, the body upper both sides are respectively provided with wing, and one end of the wing is hinged phase with one end of connecting rod
Even, the other end of the connecting rod is connected with the sliding block upper articulation, the other end of the wing be sequentially installed with the first steering wheel,
First brushless electric machine and the first propeller, the afterbody are then provided with the second steering wheel, the second brushless electric machine and second
Propeller；The fuselage bottom is one in front and one in back respectively provided with wheel and rises and falls frame aperture, and wheel frame aperture top of rising and falling is additionally provided with wheel
Undercarriage, the wheel undercarriage is risen and fallen frame aperture by the 3rd servo driving through the wheel, and the wheel undercarriage bottom sets
There is wheel electrical machine with driving moment, the wheel covered plate of frame aperture that rises and falls is closed or opened；The fuselage interior is additionally provided with water storage
Device leads to the water pump pipeline for being arranged at the fuselage outer wall.
Preferably, the fore-body both sides are respectively provided with and are moved under water under water the holding fuselage for described three unmanned planes of dwelling
The front wing of horizontal stable traveling.
Preferably, the motor for being installed on the wheel undercarriage bottom includes the first motor and the second motor, described first
The rotating speed of motor and second motor can be inconsistent.
Preferably, wheel frame aperture inside edge of rising and falling is provided with sealing rubber strip, and the cover plate is by the second screw mandrel stepping electricity
Machine is promoted and moved forward and backward along the groove of the sealing rubber strip, by the wheel undercarriage bore closure or opening.
Preferably, the head of the fuselage is fabricated by for transparent material.
Preferably, the moveable battery of the fuselage interior is arranged to be promoted before and after the 3rd screw mandrel stepper motor to change
Described three dwell unmanned plane center of gravity.
Preferably, it is additionally provided with the 4th steering wheel between the wing other end and first steering wheel.
Technical solutions of the utility model install vertical tail, tailplane and rudder by afterbody, and
Sliding block is pulled or elapsed to adjust the sweepback angle of wing, by setting the first screw mandrel stepper motor in fuselage interior so that nothing
It is man-machine can be applicable circle in the air in the air, land walking, the different operating modes moved under water under water.And wing one end is provided for unmanned plane and hangs down
The first steering wheel, the first brushless electric machine and first propeller of drop are gone straight up to, and unmanned plane is provided in afterbody and pushed away forward
The second steering wheel, the second brushless electric machine and the second propeller for entering.In addition, one in front and one in back set wheel in the bottom of fuselage rising and falling
Frame aperture, by the 3rd servo driving wheel undercarriage through wheel rise and fall frame aperture so that unmanned plane can reliable smoothly land,
And wheel is driven by motor so that unmanned plane can be walked on land.Unmanned plane is also by being arranged at machine
The water pump on body surface sucks in water receiver water, and the weight of unmanned plane is increased, and unmanned plane is moved under water in the water body of different depth
It is interior.
The utility model relative to the unmanned plane of prior art, in can realizing reliable airflight, land walking, water
The function of moving under water, so as to expand the range of application of unmanned plane.
Brief description of the drawings
In order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art, below will be to embodiment
Or the accompanying drawing to be used needed for description of the prior art is briefly described, it should be apparent that, drawings in the following description are only
It is some embodiments of the present utility model, for those of ordinary skill in the art, is not paying the premise of creative work
Under, other accompanying drawings can also be obtained according to the structure shown in these accompanying drawings.
Fig. 1 be the utility model three dwell unmanned plane VTOL when structural representation；
Fig. 2 is that the utility model three is dwelt structural representation of unmanned plane when circling in the air in the air；
Fig. 3 be the utility model three dwell unmanned plane land walking when structural representation；
Fig. 4 is the structural representation that the utility model three is dwelt when moving under water in unmanned plane water；
Fig. 5 is dwelt unmanned plane internal structure schematic diagram for the utility model three；
Fig. 6 be the utility model three dwell unmanned plane wing setting conversion structural representation；
Fig. 7 is that the utility model three is dwelt the structural representation of unmanned locomotive wheel undercarriage；
Fig. 8 is dwelt unmanned drive end unit dynamic structure schematic diagram for the utility model three；
Fig. 9 is the partial enlarged drawing at A in Fig. 8；
Figure 10 is that the dwell wheel of unmanned plane of the utility model three rises and falls the structural representation of frame aperture sealing station.
Drawing reference numeral explanation：
| Label | Title | Label | Title |
| 1 | Fuselage | 15 | Battery |
| 2 | Front wing | 16 | Water receiver |
| 3 | Wing | 17 | Water pump |
| 4 | First steering wheel | 18 | Cover plate |
| 5 | First brushless electric machine | 19 | Wheel |
| 6 | First propeller | 20 | First screw mandrel stepper motor |
| 7 | Tailplane | 21 | Connecting rod |
| 8 | Vertical tail | 22 | Sliding block |
| 9 | Rudder | 23 | First motor |
| 10 | Second steering wheel | 24 | Second motor |
| 11 | Second brushless electric machine | 25 | Wheel undercarriage |
| 12 | Second propeller | 26 | Second screw mandrel stepper motor |
| 13 | Head | 27 | Wheel rises and falls frame aperture |
| 14 | 3rd steering wheel | 28 | Sealing rubber strip |
The realization of the utility model purpose, functional characteristics and advantage will be described further referring to the drawings in conjunction with the embodiments.
Specific embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is only a part of embodiment of the present utility model, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not making creative work premise
Lower obtained every other embodiment, belongs to the scope of the utility model protection.
If it is to be appreciated that related in the utility model embodiment directionality indicate (such as upper and lower, left and right, it is preceding,
Afterwards ...), then directionality indicates to be only used for explaining relative between each part under a certain particular pose (as shown in drawings)
Position relationship, motion conditions etc., if the particular pose changes, directionality indicates also correspondingly to change therewith.
If in addition, relate to the description of " first ", " second " etc. in the utility model embodiment, should " first ", " the
Two " description etc. is only used for describing purpose, and it is not intended that indicating or implying its relative importance or implicit indicate meaning
The quantity of the technical characteristic for showing.Thus, " first " is defined, the feature of " second " can express or implicitly include at least one
Individual this feature.In addition, the technical scheme between each embodiment can be combined with each other, but must be with ordinary skill
Personnel can be implemented as basis, when the combination appearance of technical scheme is conflicting or cannot realize it will be understood that this technical side
The combination of case does not exist, not within the protection domain of the utility model requirement yet.
Referring to Fig. 1 to Fig. 5, a kind of the three of the utility model deduction dwells unmanned plane, including streamlined fuselage 1, fuselage 1
Upper rear is provided with the vertical tail 8 for controlling unmanned plane left and right directions to turn to, and for controlling unmanned plane upper and lower
To the tailplane 7 for turning to, vertical tail 8 is also associated with the direction for adjusting unmanned plane during flying direction by unmanned tail one end
Rudder 9.Preferably, the front part sides of fuselage 1 be respectively provided with for three dwell unmanned plane move under water under water when, keep the horizontal stable row of fuselage 1
The front wing 2 sailed.
Referring to Fig. 1 to Fig. 5, the first screw mandrel stepper motor 20 is provided with inside fuselage of the present utility model 1 by linkage
It is connected with sliding block 22, so as to promote the sliding block 22 to carry out front and rear passage along the cephalocaudal direction of fuselage 1.Meanwhile, the top both sides of fuselage 1
Wing 3 is respectively installed, one end and one end of connecting rod 21 of wing 3 are hinged and connected, and the other end of connecting rod 21 then with sliding block 22
Upper articulation is connected, when sliding block 22 is elapsed sliding block 22 by the first screw mandrel stepper motor 20 along unmanned plane cephalocaudal direction, sliding block
The 22 rotation adjutant connecting rods 21 being hinged with connecting rod 21 by its top are affected so that wing 3 swings along the rotary shaft of its one end
Angle.The other end of wing 3 is sequentially installed with the first steering wheel 4, the first brushless electric machine 5 and the first propeller 6, and fuselage 1
Afterbody is then sequentially installed with the second steering wheel 10, the second brushless electric machine 11 and the second propeller 12, it is preferable that the utility model machine
The 4th steering wheel is also equipped between the other end of the wing 3 and the first steering wheel 4.
Referring to Fig. 1 to Figure 10, the bottom of fuselage of the present utility model 1 is one in front and one in back respectively provided with wheel undercarriage 27, and wheel rises
The top of the frame aperture that falls 27 is additionally provided with wheel undercarriage 25, and wherein wheel undercarriage 25 is driven by the 3rd steering wheel 14 and passes through wheel to rise and fall
Frame aperture 27, the bottom of wheel undercarriage 25 of the present utility model is provided with the motor of wheel 19 with driving moment 19.Preferably, it is installed on car
The motor for taking turns undercarriage 25 includes the first motor 23 and the second motor 24, and the motor 24 of the first motor 23 and second is at nobody
When machine is turned to, the rotating speed of the first motor 23 and the second motor 24 is not consistent so that unmanned plane can in actual moving process
Conveniently turned to.
Referring to Figure 10, in the utility model, being arranged at the bottom wheel of fuselage 1 frame aperture 27 of rising and falling can be closed or be beaten by cover plate 18
Open.Preferably, the wheel endoporus edge of frame aperture 27 that rises and falls is provided with sealing rubber strip 28, the one end of cover plate 18 and the second screw mandrel stepper motor
26 are connected.When the frame aperture 27 that needs to rise and fall wheel is carried out or closed, the second screw mandrel stepper motor 26 promotes cover plate 18 along close
The envelope interior grooves of rubber strip 28 move forward and backward and are then capable of achieving.Meanwhile, wheel rise and fall frame aperture 27 internal control edge install set
Reeded sealing rubber strip 28, can effectively improve cover plate 18 and wheel be risen and fallen the sealing effectiveness of frame aperture 27.
Referring to Fig. 1 to Figure 10, the head 13 of the front portion of the utility model fuselage 1 is fabricated by for transparent material, facilitates nobody
Machine is taken photo by plane in the air during actual travel, road surface capture or water in shoot etc. activity.In fuselage of the present utility model 1
Portion is additionally provided with water receiver 16 and leads to the pipeline of water pump 17 for being arranged at the outer wall of fuselage 1, when unmanned plane need to be travelled in water body, passes through
By in the water receiver 16 inside water inspiration fuselage 1, the overall weight of unmanned plane then can quickly increase water pump 17, so that nobody
Machine is gradually fallen in water body.Meanwhile, by sucking the number of water to adjust different depth of the unmanned plane in water.In addition,
Be additionally provided with inside unmanned plane of the present utility model moveable battery 15 by the 3rd screw mandrel stepper motor along unmanned plane from beginning to end
Direction moves, so as to change three centers of gravity for dwelling unmanned plane.
Refer to Fig. 1 to Figure 10, of the present utility model three dwell unmanned plane can realize circling in the air in the air, land walking and water
In move under water three kinds of operating modes, its operation principle is：
When three dwell unmanned plane need to circle in the air in the air when, unmanned plane is firstly the need of vertical lift-off, first inside fuselage 1
Bar stepper motor 20 is moved linearly by the dilatory sliding block 22 of linkage to the caudal directions of fuselage 1, and phase is hinged with the one end of wing 3
Connecting rod 21 even swings also with the movement of sliding block 22, so as to drive wing 3 to be gradually rocked to and fuselage from parallel to fuselage 1
1 head and the tail axis is vertical so that the angle of sweep of wing 3 is 0 °, and at this moment the extending transversely amplitude of wing 3 is maximum.It is another positioned at wing 3
First steering wheel 4 at end makes the electrical axis of the first brushless electric machine 5 perpendicular to the ground and the first propeller 6 by angle adjustment
Upward, the first propeller 6 is rotated in the driving of the first brushless electric machine 5, and the bottom wheel of fuselage 1 rises and falls frame aperture 27 then by cover plate
18 are closed.First brushless electric machine 5 drives the first propeller 6, unmanned plane is obtained the active force of vertical ascent, by above-mentioned step
Suddenly, unmanned plane can be taken off in complicated landform, and without using runway help-fly.After unmanned plane rises to preset height,
The second steering wheel 10 positioned at the afterbody of fuselage 1 passes through angle adjustment so that the second brushless electric machine 11 is axially put down with the axial direction of fuselage 1
OK, the second steering wheel 10 drives the second propeller 12 to be rotated so that unmanned plane obtains the power of flight forward, at this moment first
Steering wheel 4 is by changing angle, so that the central shaft of the first brushless electric machine 5 and the diameter parallel of fuselage 1 so that the first propeller
6 pairs of unmanned planes produce the active force of flight forward, under the collective effect of the first propeller 6 and the second propeller 12, unmanned plane
Flotant function can be realized.
In flight course, the first screw mandrel stepper motor 20 is by linkage by sliding block 22 to the head of fuselage 1 for unmanned plane
Dilatory, the angle of sweep of wing 3 gradually increases from 0 °.Wherein, the angle of sweep optimized angle of wing 3 is 45 °, and the first steering wheel 4 leads to
The angle adjustment at the angle of sweep of wing 3 is crossed so that coefficient of air resistance reduction during unmanned plane during flying, in the flight of such unmanned plane
Cheng Zeke accordingly increases, and improves the operating efficiency of unmanned plane.
When unmanned plane need to carry out land walking, unmanned plane need to first carry out safe land.Second brushless electric machine 11 passes through
Gradually reduce rotating speed, the second propeller 12 tapers off rotation, and making the speed of unmanned plane airflight gradually reduces, at this moment
First steering wheel 4 passes through angle adjustment so that perpendicular to ground, the first brushless electric machine 5 passes through the electrical axis of the first brushless electric machine 5
Rotating speed is gradually reduced so that the upward lifting active force of unmanned plane is gradually decreased, so that work of the unmanned plane in self gravitation
Slow landed on ground with lower.During unmanned plane slowly lands, the second screw mandrel stepper motor 26 inside fuselage 1
Dilatory cover plate 18 so that the frame aperture 27 of rising and falling of the wheel positioned at the bottom of fuselage 1 is opened, and such 3rd steering wheel 14 passes through corresponding connecting rod
Mechanism gradually pushes out wheel undercarriage 25 to wheel frame aperture 27 of rising and falling so that unmanned plane passes through wheel undercarriage 25 and car
Wheel 19 is supported on ground., by the power wheel 19 of the bottom of wheel undercarriage 25, such unmanned plane then can be for unmanned plane
Walked land.Preferably, in the process of walking, the first screw mandrel stepper motor 20 is first to fuselage 1 by sliding block 22 for unmanned plane
Portion is elapsed so that the wing 3 of unmanned plane is folded to the afterbody of fuselage 1, and the angle of sweep of such wing 3 then becomes in 90 °.Cause
For the wing 3 of unmanned plane folds back, the transverse width of unmanned plane accordingly diminishes so that unmanned plane is during land walking
Windage diminishes, and unmanned plane makes distance travelled farther because that need not overcome unnecessary windage.When unmanned plane is travelled, by being installed on
First motor 23 of wheel undercarriage 25 and the rotating speed of the second motor 24 be not consistent so that unmanned plane is in actual moving process
Can conveniently be turned to.
When unmanned plane needs to be moved under water in water, the first screw mandrel stepper motor 20 of unmanned aerial vehicle body 1 will be by that will slide
Block 22 is elapsed to the stem of fuselage 1 so that wing 3 shrinks to the afterbody of fuselage 1, and at this moment the angle of sweep of wing 3 is then 90 °.It is arranged at machine
The bottom wheel undercarriage 25 of body 1 is carried out angle adjustment and be folded back into fuselage 1 by the 3rd steering wheel 14 by corresponding linkage
Portion, the second screw mandrel stepper motor 26 at this moment promotes cover plate 18 that wheel frame aperture 27 of rising and falling is covered into sealing.Preferably, wheel rises and falls
The endoporus edge of frame aperture 27 is provided with sealing rubber strip 28, and groove, the second screw mandrel stepper motor are provided with inside the sealing rubber strip 28
26 promote cover plate 18 to advance along the groove of sealing rubber strip 28, so that the better tightness of cover plate 18.When unmanned plane drift
After floating on water surface, by being arranged at the water pump 17 on the surface of fuselage 1 by the water receiver 16 in water inspiration to fuselage 1, and with
Water in water receiver 16 gradually increases, and the overall weight of such unmanned plane gradually increases, and unmanned plane is gradually slipped into water body,
Unmanned plane by sucking the number of water, the depth different in water to adjust unmanned plane, to adapt to operating mode in different water.So
Afterwards by being arranged at the second steering wheel 10, the second brushless electric machine 11 and second propeller 12 of the afterbody of fuselage 1, unmanned plane is produced
Motive force forward, such unmanned plane can move under water in water body.Preferably, the front part sides in fuselage 1 are respectively provided with for tieing up
The oseplane 2 of stabilization fuselage 1 when being moved under water in water holding, more stablizes and reliable when such unmanned plane moves under water in water.
The head 13 of the front portion of fuselage 1 of the utility model unmanned plane is formed using transparent material manufacture, such unmanned plane
When circling in the air in the air, moving under water in land walking and water, can all be easy to set capture apparatus and complete correlation inside unmanned plane
Admission video, shoot the work such as photo.
The 4th steering wheel can be also provided between the other end of wing 3 of the utility model unmanned plane and the first steering wheel 4, by first
The mutual cooperation of the steering wheel of steering wheel 4 and the 4th is adjusting the operating angle of the first brushless electric machine 5 so that unmanned plane is in vertical ascent mistake
Angle adjustment can be quickly carried out in journey, such unmanned plane is more steady reliable in vertical ascent.
Battery 15 inside the utility model unmanned plane is set to mobile form, and by the 3rd screw mandrel stepper motor
Battery 15 is accordingly moved in the cephalocaudal direction of fuselage 1, such unmanned plane circles in the air in the air, move under water in land walking and water
The center of gravity of process is accordingly adjusted, to adapt to different operating modes.
Preferred embodiment of the present utility model is the foregoing is only, the scope of the claims of the present utility model is not thereby limited,
It is every under design of the present utility model, the equivalent structure transformation made using the utility model specification and accompanying drawing content, or
Directly/be used in other related technical fields indirectly and be included in scope of patent protection of the present utility model.
Claims (7)
1. one kind three is dwelt unmanned plane, it is characterised in that including fairshaped fuselage, and the afterbody top is provided with vertical end
The wing and tailplane, the vertical tail are also associated with the rudder for adjustment direction near the afterbody；It is described
Fuselage interior is provided with the first screw mandrel stepper motor sliding block is elapsed along before and after the fuselage cephalocaudal direction by linkage, described
Body upper both sides are respectively provided with wing, and one end of the wing is hinged and connected with one end of connecting rod, the other end of the connecting rod with
The sliding block upper articulation is connected, and the other end of the wing is sequentially installed with the first steering wheel, the first brushless electric machine and first
Propeller, the afterbody is then provided with the second steering wheel, the second brushless electric machine and the second propeller；The fuselage bottom one
It is respectively provided with wheel after previous to rise and fall frame aperture, wheel frame aperture top of rising and falling is additionally provided with wheel undercarriage, the wheel undercarriage
Risen and fallen frame aperture through the wheel by the 3rd servo driving, the wheel undercarriage bottom is provided with wheel electrical machine with driving moment,
The wheel covered plate of frame aperture that rises and falls is closed or opened；The fuselage interior is additionally provided with water receiver and is arranged at the fuselage outer wall
Water pump pipeline lead to.
2. as claimed in claim 1 three dwell unmanned plane, it is characterised in that the fore-body both sides are respectively provided with for described
Three unmanned planes of dwelling move under water keep the front wing of standard of fuselage stabilization traveling under water.
3. as claimed in claim 1 three dwell unmanned plane, it is characterised in that be installed on the motor bag of the wheel undercarriage bottom
Include the first motor and the second motor, the rotating speed of first motor and second motor can be inconsistent.
4. as claimed in claim 1 three dwell unmanned plane, it is characterised in that wheel frame aperture inside edge of rising and falling is provided with sealing rubber
Adhesive tape, the cover plate is promoted by the second screw mandrel stepper motor and moved forward and backward along the groove of the sealing rubber strip, will be described
Wheel undercarriage bore closure or opening.
5. as claimed in claim 1 three dwell unmanned plane, it is characterised in that the head of the fuselage is for transparent material is manufactured
Into.
6. as claimed in claim 1 three dwell unmanned plane, it is characterised in that be arranged at the moveable battery quilt of the fuselage interior
Promote before and after 3rd screw mandrel stepper motor and dwelt unmanned plane center of gravity with changing described three.
7. as claimed in claim 1 three dwell unmanned plane, it is characterised in that between the wing other end and first steering wheel
It is additionally provided with the 4th steering wheel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621153360.6U CN206277907U (en) | 2016-10-31 | 2016-10-31 | A kind of three dwell unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621153360.6U CN206277907U (en) | 2016-10-31 | 2016-10-31 | A kind of three dwell unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206277907U true CN206277907U (en) | 2017-06-27 |
Family
ID=59084649
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621153360.6U Expired - Fee Related CN206277907U (en) | 2016-10-31 | 2016-10-31 | A kind of three dwell unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206277907U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106564349A (en) * | 2016-10-31 | 2017-04-19 | 广东工业大学 | Triphibian unmanned aerial vehicle |
| CN109849604A (en) * | 2019-03-29 | 2019-06-07 | 熊子见 | Folding rotor triphibian |
| CN110217064A (en) * | 2019-05-07 | 2019-09-10 | 上海海事大学 | A kind of water sky land three is dwelt submariner device |
| CN112498035A (en) * | 2020-12-15 | 2021-03-16 | 江苏集萃智能制造技术研究所有限公司 | Portable triphibian mobile robot of land, water and air |
-
2016
- 2016-10-31 CN CN201621153360.6U patent/CN206277907U/en not_active Expired - Fee Related
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106564349A (en) * | 2016-10-31 | 2017-04-19 | 广东工业大学 | Triphibian unmanned aerial vehicle |
| CN109849604A (en) * | 2019-03-29 | 2019-06-07 | 熊子见 | Folding rotor triphibian |
| CN109849604B (en) * | 2019-03-29 | 2023-10-13 | 熊子见 | Folding rotor triphibian aircraft |
| CN110217064A (en) * | 2019-05-07 | 2019-09-10 | 上海海事大学 | A kind of water sky land three is dwelt submariner device |
| CN110217064B (en) * | 2019-05-07 | 2022-08-30 | 上海海事大学 | Amphibious submersible vehicle |
| CN112498035A (en) * | 2020-12-15 | 2021-03-16 | 江苏集萃智能制造技术研究所有限公司 | Portable triphibian mobile robot of land, water and air |
| CN112498035B (en) * | 2020-12-15 | 2022-02-01 | 江苏集萃智能制造技术研究所有限公司 | Portable triphibian mobile robot of land, water and air |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170627 Termination date: 20181031 |
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| CF01 | Termination of patent right due to non-payment of annual fee |