CN111268123A - Can be used to amphibious descending unmanned aerial vehicle - Google Patents
Can be used to amphibious descending unmanned aerial vehicle Download PDFInfo
- Publication number
- CN111268123A CN111268123A CN202010182927.7A CN202010182927A CN111268123A CN 111268123 A CN111268123 A CN 111268123A CN 202010182927 A CN202010182927 A CN 202010182927A CN 111268123 A CN111268123 A CN 111268123A
- Authority
- CN
- China
- Prior art keywords
- groove
- moving
- main body
- plate
- unmanned aerial
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C35/00—Flying-boats; Seaplanes
- B64C35/001—Flying-boats; Seaplanes with means for increasing stability on the water
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C35/00—Flying-boats; Seaplanes
- B64C35/008—Amphibious sea planes
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The invention provides an amphibious landing unmanned aerial vehicle, which comprises a main body, a movable groove, a bottom groove, mounting holes, a movable plate and movable blocks, wherein the movable groove is arranged on the main body; the main body comprises an auxiliary part, an inner groove and a guide plate; the outer side of the main body is of a wedge-shaped structure, and auxiliary pieces of arc structures are arranged on two sides of the main body; an inner groove with a rectangular structure is arranged inside the main body, and a guide plate with a rectangular structure is arranged at the top end of the outer side of the inner groove; the main body is of a rectangular plate-shaped structure and is connected with the bottom of the unmanned aerial vehicle in a corresponding mounting mode; the kerve is used for establishing in the bottom of main part for unmanned aerial vehicle can assist through the kerve when taking off again, avoids the bottom and the surface of water absorption of this device together, thereby leads to the unable quick taking off of unmanned aerial vehicle, and the inside of kerve is slope column structure, is in order to make this device get bottom and surface of water separation that can be better, thereby makes breaking away from the surface of water that this device can be convenient.
Description
Technical Field
The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to an amphibious landing unmanned aerial vehicle.
Background
The unmanned plane is called as an unmanned plane for short, mainly utilizes a ground controller to control flight through a wireless sensing technology, is flexible in movement, quick in response, low in operation requirement and the like, is widely applied, and mainly has the functions of field investigation, photography, sampling, transportation and the like.
For example, application No.: CN201911160939.3 relates to an amphibious landing unmanned aerial vehicle, which comprises a body, wherein the outside of the body is fixedly connected with a horn, the top of the horn is movably connected with a motor, the top of the motor is movably connected with a rotating shaft, one end of the rotating shaft far away from the motor is fixedly connected with a wing, the bottom of the body is fixedly connected with a support frame, one end of the support frame far away from the body is movably connected with a landing gear, one end of the landing gear far away from the support frame is fixedly connected with a landing head, the outside of the landing gear is movably connected with a support rod, the outside of the support rod is movably connected with an air bag, through the matching use of the landing gear and the support frame, when the unmanned aerial vehicle lands on land, the landing gear is unfolded, the landing area of the landing gear is increased, the gravity center of the unmanned aerial, the air bag is inflated, and the effect of unmanned aerial vehicle water surface landing can be achieved.
Based on prior art discovery, current amphibious descending unmanned aerial vehicle is when using, when descending and carrying out the operation on the surface of water, fall into the aquatic easily, and great rocking appears on the surface of water easily, area of contact and the kicking block with the surface of water are less, if set up great kicking block and influence unmanned aerial vehicle's flight easily, and current amphibious descending unmanned aerial vehicle is when using, it makes the adsorption affinity great to break away from the surface of water to take off, be difficult to take off fast, and unmanned aerial vehicle falls when the aquatic at the trouble appears, can't keep unmanned aerial vehicle balanced, can't make the one side that has the kicking block stable with the surface of water contact, thereby can't avoid unmanned aerial vehicle to fall into the aquatic.
Disclosure of Invention
In order to solve the technical problems, the invention provides an amphibious landing unmanned aerial vehicle, which aims to solve the problems that when the existing amphibious landing unmanned aerial vehicle is used, when the existing amphibious landing unmanned aerial vehicle lands on the water surface to operate, the existing amphibious landing unmanned aerial vehicle is easy to fall into the water, is easy to greatly shake on the water surface, has small contact area with the water surface and small floating block, is easy to influence the flight of the unmanned aerial vehicle if the existing amphibious landing unmanned aerial vehicle is provided with the large floating block, is separated from the water surface to take off to enable the adsorption force to be large when the existing amphibious landing unmanned aerial vehicle is used, and is difficult to rapidly take off, and when the existing amphibious landing unmanned aerial vehicle breaks down and falls into the water, the unmanned aerial vehicle cannot keep balance, cannot enable one surface with the floating block to stably contact.
The invention relates to a purpose and an effect for amphibious landing unmanned aerial vehicle, which are achieved by the following specific technical means:
an amphibious landing unmanned aerial vehicle comprises a main body, a movable groove, a bottom groove, mounting holes, a movable plate and movable blocks; the main body comprises an auxiliary part, an inner groove and a guide plate; the outer side of the main body is of a wedge-shaped structure, and auxiliary pieces of arc structures are arranged on two sides of the main body; an inner groove with a rectangular structure is arranged inside the main body, and a guide plate with a rectangular structure is arranged at the top end of the outer side of the inner groove; the main body is of a rectangular plate-shaped structure and is connected with the bottom of the unmanned aerial vehicle in a corresponding mounting mode; the movable groove is arranged in the middle of the inner part of the inner groove, and the bottom end of the movable groove is positioned at the bottom of the main body; the bottom grooves are arranged at the bottom of the main body in a uniform arrangement mode; the mounting holes are formed in the outer sides of the two ends of the main body; the spring at the rear end of the moving plate is embedded in the inner hole, and a guide plate is inserted into the guide groove of the moving plate; the moving block is arranged in the moving groove, and the limiting plate on the outer side of the moving block is embedded in the limiting groove on the outer side of the moving groove.
Further, the moving groove comprises an inner hole; the movable groove is of a rectangular structure, and a limiting groove is arranged in the middle of the outer side of the movable groove; the inner hole is of a circular structure and is arranged inside the inner groove; the movable groove and the limiting groove form a movable limiting structure.
Furthermore, the bottom groove comprises a balancing weight; the bottom groove is of a triangular structure, and the inside of the bottom groove is of an inclined structure; the balancing weight is of a spherical structure and is connected with the corner position of the main body through a traction rope to form a controllable balance structure.
Further, the mounting hole comprises a top spring; the mounting hole is of a cylindrical structure, and the outer side of the mounting hole is of an inclined structure; the middle position of the bottom end in the mounting hole is provided with a groove of an arc structure, and a top spring is arranged in the mounting hole.
Furthermore, the moving plate comprises a slot and a guide groove; the movable plate is made of a material which is easy to float and has a rectangular plate-shaped structure, and the movable plate is embedded in the inner grooves of the main bodies on the two sides; the rear end of the moving plate is provided with a spring, and the inner side of the moving plate is connected with the rectangular clamping block through a slot; the upper end and the lower end of the slot are of inclined structures; the top end of the movable plate is provided with a guide groove with a rectangular structure, and the middle position of the rear end of the movable plate is provided with a clamping groove; the movable plate moves to be a movable telescopic structure through a spring.
Furthermore, the moving block comprises a chuck; the moving block is of an L-shaped structure, and a limiting plate of a rectangular structure is arranged on the outer side of the moving block; the bottom of the moving block is made of foam; the top end of the moving block is provided with a clamping head which is in a wedge-shaped protruding structure; the dop inserts and is portable limit structure in the draw-in groove of movable plate.
Compared with the prior art, the invention has the following beneficial effects:
in the device, a bottom groove and a moving plate are arranged, wherein the bottom groove is arranged at the bottom of a main body, so that the unmanned aerial vehicle can be assisted by the bottom groove when taking off again, the bottom of the device is prevented from being adsorbed with the water surface, thereby leading the unmanned aerial vehicle not to take off rapidly, and the inner part of the bottom groove is of an inclined structure, so as to better separate the bottom of the device from the water surface, so that the device can be conveniently separated from the water surface, the balancing weight is arranged at the corner position of the main body, so that when the device is out of control or fails in the flying process, the balancing weight can be separated from the inside of the mounting hole and come out, thereby the device can carry out auxiliary correction on the falling direction through the four balancing weights in the falling process, the bottom end of the device can be contacted with the ground or the water surface, so that the device is prevented from falling to the ground, being broken and falling into the water directly when being inclined;
the movable plate is arranged in the inner groove, so that when the device falls on the water surface, the movable block can move upwards under the action of buoyancy, the movable plate can be relieved from limiting, a spring can push the two movable plates to be conveniently spliced together, the contact area between the movable plates and the water surface is enlarged, the device can stably float on the water surface, the slot on the outer side of the movable plate is used for being conveniently spliced with the clamping block, the two movable plates can be conveniently connected, the guide groove on the top end of the movable plate is used for enabling the guide plate to be inserted, the movable plate can be limited by the guide plate when moving outwards, the clamping groove on the rear end of the movable plate is used for enabling the clamping head to be inserted, the movable plate can be stably fixed by the clamping head when being embedded in the inner groove, and the problem of use is solved, when descending and carrying out the operation on the surface of water, fall into the aquatic easily, and great rocking appears in the surface of water easily, it is less with the area of contact and the kicking block of the surface of water, if set up the flight that great kicking block influenced unmanned aerial vehicle easily, and current amphibious descending unmanned aerial vehicle is when using, it makes the adsorption affinity great to break away from the surface of water to take off, be difficult to take off fast, and unmanned aerial vehicle breaks down when falling in the aquatic, can't keep unmanned aerial vehicle balanced, can't make the one side that has the kicking block stable with the surface of water contact, thereby can't avoid the problem that unmanned aerial vehicle fell into the aquatic.
Drawings
Fig. 1 is a schematic perspective view of the present invention.
Fig. 2 is a schematic bottom view of the present invention.
FIG. 3 is a schematic side view of the main body of the present invention.
Fig. 4 is a schematic bottom view of the main body of the present invention.
Fig. 5 is a partial cross-sectional structural view of the body of the present invention.
Fig. 6 is a schematic view of the enlarged part a of the present invention from fig. 5.
Fig. 7 is a perspective view of the moving plate of the present invention.
Fig. 8 is a perspective view of the moving block of the present invention.
In the drawings, the corresponding relationship between the component names and the reference numbers is as follows:
1. a main body; 101. an auxiliary member; 102. an inner tank; 103. a guide plate; 2. a moving groove; 201. an inner bore; 3. a bottom groove; 301. a balancing weight; 4. mounting holes; 401. a spring is supported; 5. moving the plate; 501. a slot; 502. a guide groove; 6. a moving block; 601. and (4) clamping the head.
Detailed Description
The embodiments of the present invention will be described in further detail with reference to the drawings and examples. The following examples are intended to illustrate the invention but are not intended to limit the scope of the invention.
In the description of the present invention, "a plurality" means two or more unless otherwise specified; the terms "upper", "lower", "left", "right", "inner", "outer", "front", "rear", "head", "tail", and the like, indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, are only for convenience in describing and simplifying the description, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed in a particular orientation, and be operated, and thus, should not be construed as limiting the invention. Furthermore, the terms "first," "second," "third," and the like are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "connected" and "connected" are to be interpreted broadly, e.g., as being fixed or detachable or integrally connected; can be mechanically or electrically connected; may be directly connected or indirectly connected through an intermediate. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
Example (b):
as shown in figures 1 to 8:
the invention provides an unmanned aerial vehicle for amphibious landing, which comprises: the device comprises a main body 1, a moving groove 2, a bottom groove 3, a mounting hole 4, a moving plate 5 and a moving block 6; the main body 1 comprises an auxiliary part 101, an inner groove 102 and a guide plate 103; the outer side of the main body 1 is of a wedge-shaped structure, and auxiliary pieces 101 of arc structures are arranged on two sides of the main body 1; an inner groove 102 with a rectangular structure is arranged in the main body 1, and a guide plate 103 with a rectangular structure is arranged at the top end of the outer side of the inner groove 102; the main body 1 is of a rectangular plate-shaped structure, and the main body 1 is connected with the bottom of the unmanned aerial vehicle in a corresponding installation mode; the moving groove 2 is arranged in the middle of the inner groove 102, the bottom end of the moving groove 2 is positioned at the bottom of the main body 1, the limiting groove on the outer side of the moving groove 2 is used for embedding the limiting plate on the outer side of the moving block 6, so that the moving block 5 is prevented from falling downwards when the moving block 5 pops up, the moving block 5 cannot be fixed again, and the inner hole 201 is used for embedding and mounting a spring, so that the moving block 5 can move outwards through the spring; the bottom groove 3 is arranged at the bottom of the main body 1 in an evenly arranged mode, and the balancing weights 301 are arranged at the corner positions of the main body 1, so that when the device loses control or breaks down in the flight process, the balancing weights 301 can be separated from the inside of the mounting holes 4, the falling direction of the device can be corrected in an auxiliary mode through the four balancing weights 301, the bottom end of the device can be in contact with the ground or the water surface, and the device is prevented from falling to the ground, breaking and falling into water in an inclined mode; the mounting holes 4 are formed in the outer sides of the two ends of the main body 1, the top spring 401 is used for enabling the balancing weight 301 to be in contact with the top spring 401 when the unmanned aerial vehicle falls in the opposite direction, and therefore the top spring 401 can rapidly eject the balancing weight 301, the balancing weight 301 can be located at the corner position of the device, and the device is rapidly controlled to be in a balance state; a spring at the rear end of the moving plate 5 is embedded in the inner hole 201, the guide plate 103 is inserted into the guide groove 502 of the moving plate 5, the guide groove 502 at the top end of the moving plate 5 is used for inserting the guide plate 103, so that the moving plate 5 can be limited by the guide plate 103 when moving outwards, and the clamping groove above the rear end of the moving plate 5 is used for inserting the clamping head 601, so that the moving plate 5 can be stably fixed by the clamping head 601 when being embedded in the inner groove 102; the moving block 6 is installed inside the moving groove 2, the limiting plate outside the moving block 6 is embedded inside the limiting groove outside the moving groove 2, and the limiting plate outside the moving block 6 is installed inside the limiting groove, so that the moving block 6 cannot be separated from the inside of the moving groove 2, and when the moving plate 5 is reset, the chuck 601 can fix the moving block again.
Wherein, the moving groove 2 comprises an inner hole 201; the moving groove 2 is of a rectangular structure, and a limit groove is arranged in the middle of the outer side of the moving groove 2; the inner hole 201 is of a circular structure, and the inner hole 201 is arranged inside the inner groove 102; the movable limiting structure is formed by the movable groove 2 and the limiting groove, the movable groove 2 is used for installing the movable block 6, so that when the movable block 6 is used, the movable block can smoothly move in the movable groove 2, and the movable block 6 can effectively control the movable plate 5.
Wherein, the bottom groove 3 comprises a balancing weight 301; the bottom groove 3 is of a triangular structure, and the inside of the bottom groove 3 is of an inclined structure; balancing weight 301 is spherical structure, and balancing weight 301 is connected through the haulage rope and main part 1's corner position and constitutes steerable balanced structure, the kerve 3 of here is used for establishing in main part 1's bottom, make unmanned aerial vehicle when taking off again, can assist through kerve 3, avoid the bottom and the surface of water absorption of this device together, thereby lead to the unable quick take off of unmanned aerial vehicle, and the inside of kerve 3 is slope column structure, be in order to can be better make this device get bottom and surface of water separation, thereby make the surface of water that breaks away from that this device can be convenient.
Wherein, the mounting hole 4 comprises a top spring 401; the mounting hole 4 is of a cylindrical structure, and the outer side of the mounting hole 4 is of an inclined structure; the inside bottom intermediate position of mounting hole 4 is equipped with the recess of arc structure, and the inside of mounting hole 4 is equipped with top spring 401, and mounting hole 4 of here is used for making balancing weight 301 imbed inside it, and the inside recess of mounting hole 4 then is used for fixing balancing weight 301, make unmanned aerial vehicle when the slope does not appear in normal flight, the phenomenon of popping out can not appear in balancing weight 301, thereby make the installation that balancing weight 301 can stabilize use.
The moving plate 5 comprises a slot 501 and a guide slot 502; the moving plate 5 is made of a rectangular plate-shaped structure and is easy to float, and the moving plate 5 is embedded in the inner grooves 102 of the main bodies 1 at two sides; the rear end of the moving plate 5 is provided with a spring, and the inner side of the moving plate 5 is connected with the rectangular fixture block through a slot 501; the upper end and the lower end of the slot 501 are of an inclined structure; a guide groove 502 with a rectangular structure is arranged at the top end of the moving plate 5, and a clamping groove is arranged in the middle of the rear end of the moving plate 5; the movable plate 5 is a movable telescopic structure through spring movement, the movable plate 5 is used for being installed in the inner groove 102, the device can fall on the water surface, the movable block 6 can move upwards under the action of buoyancy force, the movable plate 5 can be relieved for limitation, the spring can push the two movable plates 5 to be spliced together conveniently, the contact area between the movable plate and the water surface is enlarged, the device can stably float on the water surface, the inserting grooves 501 in the outer sides of the movable plates 5 are used for being spliced together with the clamping blocks conveniently, and the two movable plates 5 can be connected conveniently.
Wherein, the moving block 6 comprises a chuck 601; the moving block 6 is of an L-shaped structure, and a limiting plate of a rectangular structure is arranged on the outer side of the moving block 6; the bottom of the moving block 6 is made of foam; the top end of the moving block 6 is provided with a clamping head 601, and the clamping head 601 is of a wedge-shaped protruding structure; the clamping head 601 is inserted into the clamping groove of the moving plate 5 and is of a movable limiting structure, the moving block 6 is used for controlling the moving plate 5 to limit, when the device falls on the water surface, the bottom of the moving block 6 can receive buoyancy to move upwards, the clamping head 601 can be separated from the clamping groove, the limiting on the moving plate 5 is removed, and the moving plate 5 can be ejected out by a spring for use.
When in use: when the device is controlled to be used, when the unmanned aerial vehicle loses power on the water surface, the unmanned aerial vehicle inclines, when one side of the unmanned aerial vehicle inclines, the balancing weight 301 can be stressed to be separated from the inside of the mounting hole 4, the balancing weight 301 on the other side is contacted with the top spring 401, so that the top spring 401 can push the balancing weight 301 out of the mounting hole 4, the four balancing weights 301 can be positioned at the corner positions of the device, the unmanned aerial vehicle can be assisted to fall and correct the direction, the main body 1 can be stably contacted with the water surface, when the main body 1 is contacted with the water surface, the movable block 6 can receive buoyancy to move upwards, so that the chuck 601 can relieve the limit of the movable plate 5, the movable plate 5 can be pushed by the spring, the movable plate 5 can be separated from the inside of the inner groove 102, the two movable plates 5 can be spliced together, and the movable plate 5 can assist the, make main part 1 can increase the lifting surface with the surface of water to make the stop that this device can stabilize on the surface of water, if control unmanned aerial vehicle when the operation on the surface of water, also can make movable plate 5 and surface of water contact through same mode, thereby make the descending that unmanned aerial vehicle can stabilize on the surface of water.
The embodiments of the present invention have been presented for purposes of illustration and description, and are not intended to be exhaustive or limited to the invention in the form disclosed. Many modifications and variations will be apparent to those of ordinary skill in the art. The embodiment was chosen and described in order to best explain the principles of the invention and the practical application, and to enable others of ordinary skill in the art to understand the invention for various embodiments with various modifications as are suited to the particular use contemplated.
Claims (6)
1. The utility model provides a can be used to amphibious landing unmanned aerial vehicle which characterized in that: the method comprises the following steps: the device comprises a main body (1), a moving groove (2), a bottom groove (3), a mounting hole (4), a moving plate (5) and a moving block (6); the main body (1) comprises an auxiliary part (101), an inner groove (102) and a guide plate (103); the outer side of the main body (1) is of a wedge-shaped structure, and auxiliary pieces (101) of arc structures are arranged on two sides of the main body (1); an inner groove (102) with a rectangular structure is formed in the main body (1), and a guide plate (103) with a rectangular structure is arranged at the top end of the outer side of the inner groove (102); the main body (1) is of a rectangular plate-shaped structure, and the main body (1) is connected with the bottom of the unmanned aerial vehicle in a corresponding installation mode; the moving groove (2) is arranged in the middle of the inner part of the inner groove (102), and the bottom end of the moving groove (2) is positioned at the bottom of the main body (1); the bottom grooves (3) are arranged at the bottom of the main body (1) in a uniform arrangement mode; the mounting holes (4) are formed in the outer sides of the two ends of the main body (1); a spring at the rear end of the moving plate (5) is embedded in the inner hole (201), and a guide plate (103) is inserted into a guide groove (502) of the moving plate (5); the moving block (6) is installed inside the moving groove (2), and a limiting plate on the outer side of the moving block (6) is embedded into a limiting groove on the outer side of the moving groove (2).
2. An amphibious landing drone as claimed in claim 1, wherein: the moving groove (2) comprises an inner hole (201); the moving groove (2) is of a rectangular structure, and a limiting groove is formed in the middle position of the outer side of the moving groove (2); the inner hole (201) is of a circular structure, and the inner hole (201) is arranged inside the inner groove (102); the movable groove (2) and the limiting groove form a movable limiting structure.
3. An amphibious landing drone as claimed in claim 1, wherein: the bottom groove (3) comprises a balancing weight (301); the bottom groove (3) is of a triangular structure, and the inside of the bottom groove (3) is of an inclined structure; the balancing weight (301) is of a spherical structure, and the balancing weight (301) is connected with the corner position of the main body (1) through a traction rope to form a controllable balance structure.
4. An amphibious landing drone as claimed in claim 1, wherein: the mounting hole (4) comprises a top spring (401); the mounting hole (4) is of a cylindrical structure, and the outer side of the mounting hole (4) is of an inclined structure; the middle position of the bottom end in the mounting hole (4) is provided with a groove of an arc structure, and a top spring (401) is arranged in the mounting hole (4).
5. An amphibious landing drone as claimed in claim 1, wherein: the moving plate (5) comprises a slot (501) and a guide groove (502); the movable plate (5) is made of a rectangular plate-shaped structure and is easy to float, and the movable plate (5) is embedded in the inner grooves (102) of the main bodies (1) on the two sides; the rear end of the moving plate (5) is provided with a spring, and the inner side of the moving plate (5) is connected with the rectangular fixture block through a slot (501); the upper end and the lower end of the slot (501) are of inclined structures; the top end of the moving plate (5) is provided with a guide groove (502) with a rectangular structure, and the middle position of the rear end of the moving plate (5) is provided with a clamping groove; the moving plate (5) moves into a movable telescopic structure through a spring.
6. An amphibious landing drone as claimed in claim 1, wherein: the moving block (6) comprises a chuck (601); the moving block (6) is of an L-shaped structure, and a limiting plate of a rectangular structure is arranged on the outer side of the moving block (6); the bottom of the moving block (6) is made of foam; the top end of the moving block (6) is provided with a clamping head (601), and the clamping head (601) is of a wedge-shaped protruding structure; the clamping head (601) is inserted into the clamping groove of the moving plate (5) and is of a movable limiting structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010182927.7A CN111268123B (en) | 2020-03-16 | 2020-03-16 | Can be used to amphibious descending unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010182927.7A CN111268123B (en) | 2020-03-16 | 2020-03-16 | Can be used to amphibious descending unmanned aerial vehicle |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN111268123A true CN111268123A (en) | 2020-06-12 |
| CN111268123B CN111268123B (en) | 2022-06-24 |
Family
ID=70994471
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202010182927.7A Active CN111268123B (en) | 2020-03-16 | 2020-03-16 | Can be used to amphibious descending unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN111268123B (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112339999A (en) * | 2020-12-07 | 2021-02-09 | 丁玉玲 | Amphibious unmanned aerial vehicle with balance weight posture adjusting mechanism |
| US20210229560A1 (en) * | 2019-12-18 | 2021-07-29 | The United States Of America As Represented By The Secretary Of The Navy | Hybrid Seawater Battery for Powering an Unmanned Aerial Vehicle |
| CN114571931A (en) * | 2022-04-24 | 2022-06-03 | 浙江大学 | Amphibious unmanned aerial vehicle |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6398158B1 (en) * | 2001-06-22 | 2002-06-04 | The United States Of America As Represented By The Secretary Of The Navy | High altitude low flying platform hull |
| CN105947197A (en) * | 2016-04-28 | 2016-09-21 | 上海牧羽航空科技有限公司 | Amphibious aircraft with double-rectification planing-step structure |
| CN106741933A (en) * | 2017-02-09 | 2017-05-31 | 金陵科技学院 | A kind of amphibious unmanned plane |
| WO2017149196A1 (en) * | 2016-03-01 | 2017-09-08 | Miricle Oy | Floatplane |
| CN108284951A (en) * | 2017-12-13 | 2018-07-17 | 中国特种飞行器研究所 | A kind of Combined air cushion airvane ship |
| CN109573021A (en) * | 2018-11-27 | 2019-04-05 | 南安易盾格商贸有限公司 | A kind of amphibious self-unloading resistance-type quadrotor unmanned vehicle |
-
2020
- 2020-03-16 CN CN202010182927.7A patent/CN111268123B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6398158B1 (en) * | 2001-06-22 | 2002-06-04 | The United States Of America As Represented By The Secretary Of The Navy | High altitude low flying platform hull |
| WO2017149196A1 (en) * | 2016-03-01 | 2017-09-08 | Miricle Oy | Floatplane |
| CN105947197A (en) * | 2016-04-28 | 2016-09-21 | 上海牧羽航空科技有限公司 | Amphibious aircraft with double-rectification planing-step structure |
| CN106741933A (en) * | 2017-02-09 | 2017-05-31 | 金陵科技学院 | A kind of amphibious unmanned plane |
| CN108284951A (en) * | 2017-12-13 | 2018-07-17 | 中国特种飞行器研究所 | A kind of Combined air cushion airvane ship |
| CN109573021A (en) * | 2018-11-27 | 2019-04-05 | 南安易盾格商贸有限公司 | A kind of amphibious self-unloading resistance-type quadrotor unmanned vehicle |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20210229560A1 (en) * | 2019-12-18 | 2021-07-29 | The United States Of America As Represented By The Secretary Of The Navy | Hybrid Seawater Battery for Powering an Unmanned Aerial Vehicle |
| US11697496B2 (en) * | 2019-12-18 | 2023-07-11 | United States Of America As Represented By The Secretary Of The Navy | Hybrid seawater battery for powering an unmanned aerial vehicle |
| CN112339999A (en) * | 2020-12-07 | 2021-02-09 | 丁玉玲 | Amphibious unmanned aerial vehicle with balance weight posture adjusting mechanism |
| CN114571931A (en) * | 2022-04-24 | 2022-06-03 | 浙江大学 | Amphibious unmanned aerial vehicle |
Also Published As
| Publication number | Publication date |
|---|---|
| CN111268123B (en) | 2022-06-24 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN111268123B (en) | Can be used to amphibious descending unmanned aerial vehicle | |
| US11524797B2 (en) | Aircraft-retrieval system | |
| CN103347782B (en) | Aircraft | |
| KR101646736B1 (en) | Joined wing type unmanned aircraft | |
| CN106985997B (en) | Vibration isolation miniature four-rotor aircraft | |
| US20190016461A1 (en) | Unmanned aerial vehicle and method using the same | |
| CN202657252U (en) | Vehicle-mounted flying frame | |
| CN112758310A (en) | Multi-functional protection undercarriage of unmanned aerial vehicle | |
| CN205971884U (en) | Can protect light fixed wing uavs of carry equipment | |
| CN211108015U (en) | Unmanned aerial vehicle capable of preventing water falling | |
| CN112660407B (en) | High-pressure pneumatic boosting take-off device of light unmanned aerial vehicle | |
| CN206171815U (en) | Installation device is assisted to rotor | |
| CN210113179U (en) | Prevent reconnaissance unmanned aerial vehicle that falls with second grade floating structure | |
| CN106864736A (en) | A kind of unmanned plane protects underframe | |
| CN104229130B (en) | Pneumatic structure four rotor unmanned aircraft | |
| CN113120243B (en) | Passive mechanical general parachute of unmanned aerial vehicle | |
| CN205440795U (en) | Water aircraft | |
| KR102053889B1 (en) | Unmanned aerial vehicle for easily landing | |
| CN218703994U (en) | Unmanned aerial vehicle for water conservancy monitoring based on remote sensing image | |
| KR200394537Y1 (en) | Charging type free flight plane | |
| KR102670813B1 (en) | Detachable drone device | |
| KR102021115B1 (en) | Unmanned aerial vehicle for easily landing | |
| CN220147590U (en) | Vertical take-off and landing unmanned aerial vehicle | |
| CN211685608U (en) | Electric unmanned aerial vehicle | |
| CN211417593U (en) | Safe unmanned aerial vehicle is used in teaching |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| TA01 | Transfer of patent application right | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20220527 Address after: Room 0520, zone a, second floor, No. 8, Shengtang street, Cencun, Tianhe District, Guangzhou, Guangdong 510653 (office only) Applicant after: Guangdong Tianhao Intelligent Technology Co.,Ltd. Address before: 528400 No. 81, Xinfeng North Road, Zhongshan City, Guangdong Province Applicant before: Li Meiling |
|
| GR01 | Patent grant | ||
| GR01 | Patent grant |