CN216581017U - Marine reconnaissance of high mobility ability keeps watch on unmanned aerial vehicle - Google Patents
Marine reconnaissance of high mobility ability keeps watch on unmanned aerial vehicle Download PDFInfo
- Publication number
- CN216581017U CN216581017U CN202220155495.5U CN202220155495U CN216581017U CN 216581017 U CN216581017 U CN 216581017U CN 202220155495 U CN202220155495 U CN 202220155495U CN 216581017 U CN216581017 U CN 216581017U
- Authority
- CN
- China
- Prior art keywords
- aerial vehicle
- unmanned aerial
- main part
- wing
- vehicle main
- 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.)
- Expired - Fee Related
Links
- 210000003141 lower extremity Anatomy 0.000 claims abstract 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract description 17
- 230000000694 effects Effects 0.000 description 5
- 238000000034 method Methods 0.000 description 3
- 230000008569 process Effects 0.000 description 3
- 230000007246 mechanism Effects 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000011900 installation process Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
Images
Landscapes
- Studio Devices (AREA)
Abstract
The utility model discloses a marine reconnaissance of high mobility ability keeps watch on unmanned aerial vehicle, including the unmanned aerial vehicle main part, surface movable mounting has the camera under the unmanned aerial vehicle main part, unmanned aerial vehicle main part both sides fixed surface installs the unmanned aerial vehicle wing, the inside turbine power unit that is provided with of unmanned aerial vehicle main part, unmanned aerial vehicle main part lower surface is provided with the undercarriage, the fixed position that unmanned aerial vehicle main part lower surface is close to the undercarriage installs the glide box, the inside movable mounting of glide box has the extension to float, the undercarriage surface is close to lower limb position movable mounting and has the wheel that rises and falls, the quantity of undercarriage is three, the inside fixed mounting of unmanned aerial vehicle wing has the wing spar, the wing is installed to the wing spar surface nestification. A marine reconnaissance of high mobility ability keeps watch on unmanned aerial vehicle, enable equipment and can slide on the surface of water, also can suspend on the sea after losing power, make things convenient for salvaging of equipment to retrieve.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle field, in particular to unmanned aerial vehicle is kept watch on in marine reconnaissance of high mobility ability.
Background
The military unmanned aerial vehicle is an unmanned aerial vehicle controlled by remote control equipment or a self-contained program, and mainly comprises three types of radio remote control, automatic program control and comprehensive control according to the control mode of the unmanned aerial vehicle, equipment in the prior art has certain defects, such as 'a rapidly detachable individual combat unmanned aerial vehicle' recorded in the application No. 202020665255.0 publication No. 212354376U, which comprises a body, wherein the left side and the right side of the body are detachably connected with wings, the front side of the body is provided with a motor, the motor is connected with the body through screws, the output end of the front side of the motor is connected with a propeller, the rear side of the body is provided with a vertical tail and a horizontal tail, the vertical tail and the horizontal tail are both connected with the body through connecting pieces, the utility model discloses, the wings are conveniently detached through arranging wing fixing bolts and wing positioning grooves, when the wings are damaged and the body is intact, the wings can be rapidly replaced, the working efficiency is improved, and the firmness of the wing installation process and the overall stability of the unmanned aerial vehicle can be enhanced by arranging the wing supporting rods and the wing installation grooves; the equipment can not slide for a short time on the sea surface when in use, and can land on the sea surface, so that the unmanned aerial vehicle can not land quickly when encountering emergency and causing loss when carrying out offshore reconnaissance.
SUMMERY OF THE UTILITY MODEL
The utility model discloses a main aim at provides a marine reconnaissance of high mobility ability keeps watch on unmanned aerial vehicle, can effectively solve the problem in the background art.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides a marine reconnaissance of high mobility ability keeps watch on unmanned aerial vehicle, includes the unmanned aerial vehicle main part, unmanned aerial vehicle main part lower surface movable mounting has the camera, unmanned aerial vehicle main part both sides fixed surface installs the unmanned aerial vehicle wing, the inside turbine power unit that is provided with of unmanned aerial vehicle main part, unmanned aerial vehicle main part lower surface is provided with the undercarriage, the position fixed mounting that unmanned aerial vehicle main part lower surface is close to the undercarriage has the glide box, the inside movable mounting of glide box has the extension to float.
Preferably, the landing gear outer surface is provided with three landing wheels movably arranged at positions close to the lower edge.
Preferably, a wing beam is fixedly installed inside the wing of the unmanned aerial vehicle, a wing panel is installed on the outer surface of the wing beam in a nested mode, a threaded ring is installed at the contact position of the wing beam and the wing panel in a threaded mode, and a lightening hole is formed in the side surface of the wing panel.
Preferably, a sliding hole is formed in the front surface of the sliding box, close to the center, a limiting strip is fixedly mounted on the side surface of the sliding hole, close to the rear edge, and an electromagnet is fixedly mounted on the upper surface of the sliding box, close to the sliding hole in an embedded mode.
Preferably, a buoyancy cavity is arranged in the sliding box and close to the sliding hole, and the buoyancy cavity is in a vacuum state.
Preferably, the extension is superficial the strip with slide opening sliding connection, the extension is superficial the strip upper surface and is close to central point and puts and has seted up the spout, the spout with the electro-magnet phase-match, the spacing groove has all been seted up on extension superficial strip both sides surface, the spacing groove with spacing sliding connection, extension superficial strip side fixed surface installs the piece that rises, the quantity of the piece that rises is a plurality of, a plurality of the contained angle that rises between piece and the horizontal plane is thirty-five degrees, the unmanned aerial vehicle main part with it adopts the welded mode to connect to slide the case.
Compared with the prior art, the utility model discloses following beneficial effect has:
in the utility model, the power supply of the electromagnet is cut off through the arranged sliding box, the wings of the unmanned aerial vehicle and the extension floating strip, at the moment, the electromagnet loses magnetic force, further loses the fixing effect on the extension floating strip, the extension floating strip slides backwards under the resistance effect of water, and stops when one end of the limiting groove contacts the limiting strip, at the moment, the unmanned aerial vehicle owner continues to slide on the sea surface, the lifting piece on the lower surface of the extension floating strip contacts with the water surface, and provides lifting force for the unmanned aerial vehicle owner in the sliding process, and the sliding box is streamline as a whole, so that the resistance when the unmanned aerial vehicle owner slides can be reduced, the buoyancy cavity inside the sliding box is influenced by the buoyancy of water, and also provides lifting force for the unmanned aerial vehicle owner, in addition, the wings inside the wings of the unmanned aerial vehicle wings are provided with lightening holes, and a distance is left between the adjacent wings, so that the buoyancy of the water received by the wings of the unmanned aerial vehicle is increased, therefore, the equipment can slide on the water surface and still can be suspended on the sea surface after losing power, and the fishing and the recovery of the equipment are convenient.
Drawings
Fig. 1 is a schematic view of the overall structure of a high-mobility marine reconnaissance and surveillance unmanned aerial vehicle of the present invention;
fig. 2 is a schematic structural view of a sliding box of the high-mobility marine reconnaissance monitoring unmanned aerial vehicle of the present invention;
fig. 3 is a schematic view of a partial structure of a sliding box of the high-mobility marine reconnaissance surveillance unmanned aerial vehicle of the present invention;
fig. 4 is the utility model relates to a high mobility's marine reconnaissance is kept watch on unmanned aerial vehicle's unmanned aerial vehicle wing inner structure schematic diagram.
In the figure: 1. an unmanned aerial vehicle main body; 101. a camera; 2. a landing gear; 201. a lifting wheel; 3. a turbine power mechanism; 4. wings of the unmanned aerial vehicle; 401. a spar; 402. a fin; 403. lightening holes; 5. a slide box; 501. a slide hole; 502. a limiting strip; 503. an electromagnet; 504. a buoyant cavity; 505. a rising piece; 506. extending the floating strips; 507. a chute; 508. a limiting groove.
Detailed Description
In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand, the present invention is further described below with reference to the following embodiments.
Example one
As shown in fig. 1-4, a high-maneuverability marine reconnaissance surveillance unmanned aerial vehicle comprises an unmanned aerial vehicle main body 1, wherein a camera 101 is movably mounted on the lower surface of the unmanned aerial vehicle main body 1, wings 4 of the unmanned aerial vehicle are fixedly mounted on the surfaces of two sides of the unmanned aerial vehicle main body 1, a turbine power mechanism 3 is arranged in the unmanned aerial vehicle main body 1, a landing gear 2 is arranged on the lower surface of the unmanned aerial vehicle main body 1, a sliding box 5 is fixedly mounted on the lower surface of the unmanned aerial vehicle main body 1 at a position close to the landing gear 2, and an extension floating strip 506 is movably mounted in the sliding box 5; the landing wheels 201 are movably mounted on the outer surface of the landing gear 2 close to the lower edge, and the number of the landing gear 2 is three; a wing beam 401 is fixedly installed inside the unmanned aerial vehicle wing 4, a wing piece 402 is installed on the outer surface of the wing beam 401 in a nested mode, a threaded ring is installed at the contact position of the wing beam 401 and the wing piece 402 in a threaded mode, and a lightening hole 403 is formed in the side surface of the wing piece 402; a sliding hole 501 is formed in the front surface of the sliding box 5 close to the center, a limiting strip 502 is fixedly mounted on the side surface of the sliding hole 501 close to the rear edge, and an electromagnet 503 is fixedly mounted on the upper surface of the sliding box 5 close to the sliding hole 501 in an embedded mode; a buoyancy cavity 504 is arranged in the sliding box 5 at a position close to the sliding hole 501, and the buoyancy cavity 504 is in a vacuum state; the extension floating strip 506 is in sliding connection with the sliding hole 501, a sliding groove 507 is formed in the position, close to the center, of the upper surface of the extension floating strip 506, the sliding groove 507 is matched with the electromagnet 503, limiting grooves 508 are formed in the surfaces of the two sides of the extension floating strip 506, the limiting grooves 508 are in sliding connection with the limiting strips 502, the side surfaces of the extension floating strip 506 are fixedly provided with a plurality of lifting pieces 505, the number of the lifting pieces 505 is thirty-five degrees, the included angle between the plurality of the lifting pieces 505 and the horizontal plane is thirty-five degrees, the power supply of the electromagnet 503 is disconnected, the electromagnet 503 loses magnetic force and further loses fixing effect on the extension floating strip 506, the extension floating strip 506 slides backwards under the resistance effect of water and stops when one end of the limiting groove 508 contacts the limiting strips 502, the unmanned aerial vehicle main body 1 continues to slide on the sea surface, the lifting pieces 505 on the lower surface of the extension floating strip 506 contact with the water surface, and provide lifting force for the unmanned aerial vehicle main body 1 in the sliding process, and the whole streamline that slides case 5, can reduce the resistance when unmanned aerial vehicle main part 1 slides, and slide the buoyancy cavity 504 of case 5 inside and receive the buoyancy influence of water, the effort that rises is provided for unmanned aerial vehicle main part 1 equally, lightening hole 403 has been seted up to inside fin 402 of unmanned aerial vehicle wing 4 in addition, and vacate a section distance between the adjacent fin 402, make the buoyancy increase of the water that unmanned aerial vehicle wing 4 received, thereby make equipment can slide on the surface of water, also can suspend on the surface of water after losing power, make things convenient for salvage of equipment to retrieve, unmanned aerial vehicle main part 1 and slide case 5 adopt welded mode to connect.
Example two
As shown in fig. 1-4, when the forced landing is performed on the sea, the power supply of the electromagnet 503 is disconnected, at this time, the electromagnet 503 loses magnetic force, further loses the fixing effect on the extension floating strip 506, the extension floating strip 506 slides backwards under the action of the resistance of water, and stops when one end of the limiting groove 508 contacts the limiting strip 502, at this time, the main body 1 of the unmanned aerial vehicle continues to slide on the sea, the lifting piece 505 on the lower surface of the extension floating strip 506 contacts with the water surface, and provides the main body 1 of the unmanned aerial vehicle with a lifting force in the sliding process, the sliding box 5 is streamline as a whole, so that the resistance of the main body 1 of the unmanned aerial vehicle in sliding can be reduced, the cavity 504 inside the sliding box 5 is influenced by the buoyancy of water, and also provides the lifting force for the main body 1 of the unmanned aerial vehicle, in addition, the wings 402 inside the wings 4 of the unmanned aerial vehicle are provided with lightening holes 403, and a distance is left between the adjacent wings 402, the buoyancy of the water borne by the wings 4 of the unmanned aerial vehicle is increased, so that the equipment can slide on the water surface and still can suspend on the sea surface after losing power, and the equipment is convenient to salvage and recover.
The basic principles and the main features of the invention and the advantages of the invention have been shown and described above. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the foregoing embodiments and descriptions are provided only to illustrate the principles of the present invention without departing from the spirit and scope of the present invention. The protection scope of the present invention is defined by the appended claims and equivalents thereof, and all equivalent changes made by the structure, shape and principle of the present invention should be covered within the protection scope of the present invention.
Claims (6)
1. A high mobility's marine reconnaissance monitors unmanned aerial vehicle which characterized in that: including unmanned aerial vehicle main part (1), surface movable mounting has camera (101) under unmanned aerial vehicle main part (1), unmanned aerial vehicle main part (1) both sides fixed surface installs unmanned aerial vehicle wing (4), the inside turbine power unit (3) that is provided with of unmanned aerial vehicle main part (1), unmanned aerial vehicle main part (1) lower surface is provided with undercarriage (2), fixed position that unmanned aerial vehicle main part (1) lower surface is close to undercarriage (2) installs glide box (5), the inside movable mounting of glide box (5) has extension buoyancy (506).
2. The high mobility marine reconnaissance surveillance drone of claim 1, wherein: the landing gear (2) outer surface is close to lower limb position movable mounting has landing gear (201), landing gear (2) three in quantity.
3. The high mobility marine reconnaissance surveillance drone of claim 2, wherein: wing spar (401) is fixedly installed inside the unmanned aerial vehicle wing (4), wing panel (402) are installed on the outer surface of the wing spar (401) in a nested mode, a threaded ring is installed at the contact position of the wing spar (401) and the wing panel (402) in a threaded mode, and lightening holes (403) are formed in the side surface of the wing panel (402).
4. The high mobility marine reconnaissance surveillance drone of claim 3, wherein: the front surface of the sliding box (5) is provided with a sliding hole (501) close to the center, the side surface of the sliding hole (501) is fixedly provided with a limiting strip (502) close to the rear edge, and the upper surface of the sliding box (5) is embedded with an electromagnet (503) fixedly arranged close to the sliding hole (501).
5. The high mobility marine reconnaissance surveillance drone of claim 4, wherein: a buoyancy cavity (504) is arranged in the sliding box (5) and close to the sliding hole (501), and the buoyancy cavity (504) is in a vacuum state.
6. The high mobility marine reconnaissance surveillance drone of claim 5, wherein: the extension floats strip (506) with slide opening (501) sliding connection, extension floats strip (506) upper surface and is close to central point and puts and has seted up spout (507), spout (507) with electro-magnet (503) phase-match, spacing groove (508) have all been seted up on extension floats strip (506) both sides surface, spacing groove (508) with spacing strip (502) sliding connection, extension floats strip (506) side surface fixed mounting has piece (505) that rises, the quantity of piece (505) that rises is a plurality of, a plurality of the contained angle that rises between piece (505) and the horizontal plane is thirty-five degrees, unmanned aerial vehicle main part (1) with glide box (5) adopt the welded mode to connect.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220155495.5U CN216581017U (en) | 2022-01-20 | 2022-01-20 | Marine reconnaissance of high mobility ability keeps watch on unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220155495.5U CN216581017U (en) | 2022-01-20 | 2022-01-20 | Marine reconnaissance of high mobility ability keeps watch on unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216581017U true CN216581017U (en) | 2022-05-24 |
Family
ID=81635174
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202220155495.5U Expired - Fee Related CN216581017U (en) | 2022-01-20 | 2022-01-20 | Marine reconnaissance of high mobility ability keeps watch on unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216581017U (en) |
-
2022
- 2022-01-20 CN CN202220155495.5U patent/CN216581017U/en not_active Expired - Fee Related
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN109018271B (en) | Novel large-span hybrid drive unmanned underwater vehicle | |
| CN110217064B (en) | Amphibious submersible vehicle | |
| CN108502172A (en) | A kind of seaplane for rescue of patrolling on the sea | |
| CN216581017U (en) | Marine reconnaissance of high mobility ability keeps watch on unmanned aerial vehicle | |
| CN110775233B (en) | Bionic flexible diving device with gliding and flapping wing movement | |
| CN215155660U (en) | Unmanned aerial vehicle for water surface lifesaving | |
| CN113386964A (en) | Unmanned aerial vehicle for water surface lifesaving | |
| CN113788132A (en) | Vector-propelled hybrid drive underwater robot | |
| CN203318636U (en) | Semi-automatic remote control amphibious pneumatic lifeboat | |
| CN211139665U (en) | Fixed wing aircraft capable of vertically taking off and landing | |
| CN111572769A (en) | Coastline rubbish recovery robot | |
| CN216101397U (en) | Air-sea aircraft | |
| CN211764759U (en) | Amphibious rescue unmanned aerial vehicle in sea and air | |
| CN115675805A (en) | Cross-medium underwater vehicle carrying unmanned aerial vehicle | |
| CN210175117U (en) | Unmanned aerial vehicle takes off and land on water | |
| CN203318669U (en) | Underwater gliding propeller | |
| CN109533243A (en) | Deep-sea unmanned remote-controlled vehicle | |
| CN210653596U (en) | Underwater cruising shooting robot | |
| CN210822683U (en) | Self-propelled life saving device | |
| CN211996128U (en) | Many rotor unmanned aerial vehicle of oil-electricity hybrid | |
| US2181574A (en) | All-wing airplane with separable flotation section | |
| CN203937845U (en) | Fishing boat first aid signaling bullet | |
| CN206394899U (en) | A kind of flotation gear of unmanned plane | |
| CN205345290U (en) | Water survival device | |
| CN205186526U (en) | Airship |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20220524 |