CN106043660A - High-performance unmanned aerial vehicle applicable to seaside salt mist area - Google Patents
High-performance unmanned aerial vehicle applicable to seaside salt mist area Download PDFInfo
- Publication number
- CN106043660A CN106043660A CN201610397674.9A CN201610397674A CN106043660A CN 106043660 A CN106043660 A CN 106043660A CN 201610397674 A CN201610397674 A CN 201610397674A CN 106043660 A CN106043660 A CN 106043660A
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- CN
- China
- Prior art keywords
- wing
- airframe
- aerial vehicle
- unmanned aerial
- seashore
- 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.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/25—Fixed-wing aircraft
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
Abstract
The invention discloses a high-performance unmanned aerial vehicle applicable to a seaside salt mist area. The unmanned aerial vehicle comprises an aircraft airframe. The interior of the aircraft airframe is of a hollow structure, a master control receiver is arranged in the aircraft airframe, a reconnaissance device is connected to the surface of one end of the aircraft airframe in a rotational clamp position way, a left outer wing is connected to the surface of the left of a middle wing through a jack way, a right outer wing is connected to the surface of the right of the middle wing through the jack way, sockets are arranged on the surfaces of the right and left of the middle wing, waterproof plugs matched with the sockets are arranged on the side surfaces of the left outer wing and the right outer wing, a horizontal empennage is connected to the upper surface of a tail rod through a clamp spring, an undercarriage is connected to the lower surface of the aircraft airframe through a clamp spring, a parachute cabin cover is arranged between the aircraft airframe and the middle wing, steering engines are movably connected to the left outer wing and the right outer wing, and waterproof mechanisms are arranged on the steering engines. The high-performance unmanned aerial vehicle applicable to the seaside salt mist area has the beneficial effects that the structure is simple, practicability is high, the sealing effect is good, the operation is simple and convenient, the weight is light, the size is small, the reconnaissance coverage is wide, the timeliness is strong and the response is quick.
Description
Technical field
The present invention relates to unmanned plane seashore flight domain, particularly a kind of salt fog area, seashore High Performance Unmanned Aerial Vehicle.
Background technology
Now due to the utilization of unmanned plane is widely, and increasingly can meet the life requirement of people, but work as people
Need by the sea will feel the when of unmanned plane, unmanned plane is unable to reach the demand of people, and some unmanned plane even can be because of
Damaging for the salt fog on seashore, thus unmanned plane just has significant limitation, occurs therefore to set to reduce such thing
It is necessary for putting this device.
Summary of the invention
The invention aims to solve the problems referred to above, devise a kind of salt fog area, seashore High Performance Unmanned Aerial Vehicle.
Realizing above-mentioned purpose the technical scheme is that, a kind of salt fog area, seashore High Performance Unmanned Aerial Vehicle, including aircraft
Body, described airframe is internal is hollow-core construction, is provided with master control and receives device, described airframe in described airframe
End surface connects by the way of rotating screens ferreting device, and threaded on described airframe other end surface have tail
Bar, described airframe upper surface connects by the way of jump ring wing centre section, and described airframe and wing centre section junction are provided with one
Number sealing ring, described airframe and foot piece junction are provided with No. two sealing rings, with the side of jack in described wing centre section left-hand face
Formula connects the left outside wing, and described wing centre section right lateral surface connects by the mode of jack starboard outboard, described wing centre section left and right sides table
It is equipped with socket on face, the described left outside wing and starboard outboard side surface are equipped with the waterproof plug matched with socket, described tail
Bar upper surface jump ring connects a tailplane, and described airframe lower surface jump ring connects undercarriage, described airframe with
It is provided with umbrella hatchcover between wing centre section, the described left outside wing and starboard outboard is all connected with steering wheel, described each steering wheel is equipped with
Proof mechanism of water, described airframe, investigation device, wing centre section, the left outside wing and starboard outboard are respectively positioned on the front end that aircraft is overall, described tail
Bar is longer than airframe, and the position, centre of buoyancy of described aircraft is located proximate to fore-body position than center of gravity.
Described airframe is provided with polysulfide preserving and sealing glue-line.
A described sealing ring and No. two sealing rings are resisting salt fog corrosion, resistant to elevated temperatures Novel sealing rubber ring.
The described left outside wing and starboard outboard size, shape are the most identical.
Described umbrella hatchcover is connected by the way of jump ring with between airframe.
Described proof mechanism of water is by the rounding column-shaped projection being arranged on steering wheel, the circle that is opened on rounding column-shaped projection end face
Shape opening, the sealed folded pipe being inlaid in circular open, the connecting rod that is fixedly connected in sealed folded pipe front-end surface are common
Constitute.
The front end of described undercarriage upwarps.
Described wing centre section is provided with preserving and sealing layer with the junction of the left outside wing and starboard outboard.
Described wing centre section scribbles epoxy glue layer on the left outside wing and starboard outboard faying face.
Described wing centre section, the left outside wing and starboard outboard are single seal modules.
Utilize salt fog area, a kind of seashore High Performance Unmanned Aerial Vehicle that technical scheme makes, prevent marine moist,
Fly under corrosive salt spray, the environment such as damp and hot the problem brought, extend the service life of unmanned plane.
Accompanying drawing explanation
Fig. 1 is the structural representation of salt fog area, a kind of seashore of the present invention High Performance Unmanned Aerial Vehicle；
Fig. 2 is the top view of salt fog area, a kind of seashore of the present invention High Performance Unmanned Aerial Vehicle；
Fig. 3 is the top view of the proof mechanism of water of salt fog area, a kind of seashore of the present invention High Performance Unmanned Aerial Vehicle；
Fig. 4 is the front view of the socket of salt fog area, a kind of seashore of the present invention High Performance Unmanned Aerial Vehicle；
Fig. 5 is the top view of No. two sealing rings of salt fog area, a kind of seashore of the present invention High Performance Unmanned Aerial Vehicle；
Fig. 6 is the top view of a sealing ring of salt fog area, a kind of seashore of the present invention High Performance Unmanned Aerial Vehicle；
In figure, 1, airframe；2, ferreting device；3, foot piece；4, wing centre section；5, a sealing ring；6, No. two sealing rings；7、
The left outside wing；8, starboard outboard；9, socket；10, waterproof plug；11, tailplane；12, undercarriage；13, umbrella hatchcover；14, folding is sealed
Folded pipe；15, connecting rod.
Detailed description of the invention
Below in conjunction with the accompanying drawings the present invention is specifically described, as shown in figures 1 to 6, a kind of salt fog area, seashore high-performance without
Man-machine, including airframe (1), described airframe (1) is internal is hollow-core construction, and described airframe is provided with master control in (1)
System receives device, and described airframe (1) end surface has ferreting device (2) by rotating to connect by the way of screens, described in fly
Threaded on machine body (1) other end surface have foot piece (3), and described airframe (1) upper surface connects by the way of jump ring
Being connected to wing centre section (4), described airframe (1) and wing centre section (4) junction are provided with a sealing ring (5), described airframe (1) with
Foot piece (3) junction is provided with No. two sealing rings (6), and described wing centre section (4) left-hand face connects by the mode of jack the left outside wing
(7), described wing centre section (4) right lateral surface connects by the mode of jack and has starboard outboard (8), described wing centre section (4) surface, the left and right sides
On be equipped with socket (9), the described left outside wing (7) and starboard outboard (8) side surface are equipped with the anti-water cutting matched with socket (9)
Head (10), described foot piece (3) upper surface jump ring connects tailplane (11), and described airframe (1) lower surface jump ring connects
There is undercarriage (12), between described airframe (1) and wing centre section (4), be provided with umbrella hatchcover (13), the described left outside wing (7) and starboard outboard
(8) all it is connected with steering wheel on, described each steering wheel is equipped with proof mechanism of water, described airframe (1), investigation device
(2), wing centre section (4), the left outside wing (7) and starboard outboard (8) be respectively positioned on the front end that aircraft is overall, described foot piece (3) is longer than airframe
(1), the position, centre of buoyancy of described aircraft is located proximate to fore-body position than center of gravity；The described center of gravity of airplane is the cruise of aircraft overall loading
Mass centre under state；Described aircraft centre of buoyancy is under the aircraft body profile cruising condition after aircraft overall loading excision pack
Draining center.It practice, plane umbrella fall into water after under gravity aircraft body profile only enter the draining center of water section with
On vertical line when Aircraft Quality center will simultaneously fall in aircraft water surface attitude, just produce with under overboard state under aircraft cruising condition
Give birth to angle (in confining spectrum, i.e. aircraft waits the optimum posture salvaged when reclaiming to this angle).On described airframe (1)
It is provided with polysulfide preserving and sealing glue-line；A described sealing ring (5) and No. two sealing rings (6) are resisting salt fog corrosion, resistant to elevated temperatures
Novel sealing rubber ring；The described left outside wing (7) and starboard outboard (8) size, shape are the most identical；Described umbrella hatchcover (13) and airframe
(1) connect by the way of jump ring between；Described proof mechanism of water by the rounding column-shaped projection being arranged on steering wheel, be opened in rounding post
Circular open, the sealed folded pipe (14) being inlaid in circular open on shape projection end face, be fixedly connected on sealed folded
Connecting rod (15) in pipe (14) front-end surface collectively forms；The front end of described undercarriage (12) upwarps；Described wing centre section (4)
It is provided with preserving and sealing layer with the junction of the left outside wing (7) and starboard outboard (8)；Described wing centre section (4) and the left outside wing (7) and starboard outboard
(8) epoxy glue layer is scribbled on faying face；Described wing centre section (4), the left outside wing (7) and starboard outboard (8) are single sealed mould
Block.
The feature of the present embodiment is, centre of buoyancy and preserving and sealing to unmanned plane carry out special design.For guaranteeing that parachuting exists
Marine recovery, has carried out unmanned plane floating on water surface center of gravity, centre of buoyancy design and preserving and sealing design；The center of gravity of design unmanned plane is fixed
Being arranged in wing centre section crossbeam position, fuel tank is positioned over position of centre of gravity, makes unmanned plane will not offset in fuel consumption tailheaviness, because of body
Major part space is in front end, therefore body centre of buoyancy is in body front end, and body center of gravity is in the middle part of body, and institute's heart center of gravity is more close than centre of buoyancy
The position of fuselage afterbody, it is ensured that unmanned plane floats over sea with the maintenance long period that holds position that head slightly raises up and waits back
Receive, it is contemplated that unmanned plane sea uses environment and parachuting situation across the sea, it is desirable to unmanned plane is when the sea water short time soaks
Situation about not intaking in body, applies domestic resisting salt fog corrosion, resistant to elevated temperatures novel seal when the design of body preserving and sealing
Glue material-polysulfide preserving and sealing glue, fuselage and wing centre section installation place, for convenience wing Fast Installation/dismounting and relevant device
Maintenance and replacing, junction uses resisting salt fog corrosion, resistant to elevated temperatures Novel sealing rubber ring to seal, fuselage and empennage (vertical, level
Empennage) junction use threaded, snap close end adds resisting salt fog corrosion, the encapsulation process of resistant to elevated temperatures Novel sealing rubber ring
Method, unmanned plane floating on water surface center of gravity, centre of buoyancy design and preserving and sealing design.Unmanned plane possesses anti-damp and hot, Defend salt fog, mould proof
" three prevent " characteristic, be suitable for working under the hygrothermal environment that condition is harsh, be mainly used in and marine perform reconnaissance mission, implement
Carry out low-altitude reconnaissance on a surface target, visible ray can be carried and load is scouted in infrared reconnaissance.Unmanned plane has lightweight, volume
Little, scout broad covered area, the ageing strong and advantage such as be swift in response.
In the present embodiment, first, when unmanned plane normal flight time, the position of centre of gravity of airframe and position, centre of buoyancy
Inconsistent, position of centre of gravity is positioned at the rear side of position, centre of buoyancy, therefore body centre of buoyancy is in body front end, and body center of gravity is in the middle part of body,
Institute's heart center of gravity than centre of buoyancy near the position of fuselage afterbody, it is ensured that airframe with head slightly raise up hold position maintenance longer
Time floats over the investigation devices to be recycled such as sea and starts working, and investigation device can be with all around detected, afterwards at steering wheel
On be equipped with water-tight device, and airframe is provided with polysulfide preserving and sealing glue-line, is provided with wing centre section junction at airframe
A number sealing ring, is provided with No. two sealing rings in airframe and foot piece junction, and a sealing ring and No. two sealing rings equal
For resisting salt fog corrosion, resistant to elevated temperatures Novel sealing rubber ring, the most sufficiently protect unmanned plane, and the center of gravity position of airframe
Putting inconsistent with position, centre of buoyancy, position of centre of gravity is positioned at the rear side of position, centre of buoyancy, it is ensured that the safety of aircraft landing.
Technique scheme only embodies the optimal technical scheme of technical solution of the present invention, those skilled in the art
Some variations may made some of which part all embody the principle of the present invention, belong to protection scope of the present invention it
In.
Claims (10)
1. a seashore salt fog area High Performance Unmanned Aerial Vehicle, including airframe (1), it is characterised in that described airframe (1)
Inside is hollow-core construction, is provided with master control and receives device in described airframe (1), and described airframe (1) end surface leads to
Crossing and rotate the mode of screens and connect and have ferreting device (2), threaded on described airframe (1) other end surface have foot piece
(3), described airframe (1) upper surface connects by the way of jump ring wing centre section (4), described airframe (1) and wing centre section (4)
Junction is provided with a sealing ring (5), and described airframe (1) and foot piece (3) junction are provided with No. two sealing rings (6), described
Connect by the mode of jack in wing centre section (4) left-hand face and have the left outside wing (7), with the side of jack in described wing centre section (4) right lateral surface
Formula connects starboard outboard (8), described wing centre section (4) surface, the left and right sides is equipped with socket (9), outside the described left outside wing (7) and the right side
Being equipped with the waterproof plug (10) matched with socket (9) on the wing (8) side surface, described foot piece (3) upper surface jump ring connects to be had
Tailplane (11), described airframe (1) lower surface jump ring connects undercarriage (12), described airframe (1) and wing centre section
(4) it is provided with umbrella hatchcover (13) between, the described left outside wing (7) and starboard outboard (8) are all connected with steering wheel, described each steering wheel
On be equipped with proof mechanism of water, the equal position of described airframe (1), investigation device (2), wing centre section (4), the left outside wing (7) and starboard outboard (8)
In the front end that aircraft is overall, described foot piece (3) is longer than airframe (1), and the position, centre of buoyancy of described aircraft is than the described center of gravity of airplane
It is located proximate to fore-body position.
A kind of salt fog area, seashore the most according to claim 1 High Performance Unmanned Aerial Vehicle, it is characterised in that described airframe
(1) polysulfide preserving and sealing glue-line it is provided with.
A kind of salt fog area, seashore the most according to claim 1 High Performance Unmanned Aerial Vehicle, it is characterised in that a described sealing
Circle (5) and No. two sealing rings (6) are resisting salt fog corrosion, resistant to elevated temperatures Novel sealing rubber ring.
A kind of salt fog area, seashore the most according to claim 1 High Performance Unmanned Aerial Vehicle, it is characterised in that the described left outside wing
(7) the most identical with starboard outboard (8) size, shape.
A kind of salt fog area, seashore the most according to claim 1 High Performance Unmanned Aerial Vehicle, it is characterised in that described umbrella hatchcover
(13) it is connected by the way of jump ring with between airframe (1).
A kind of salt fog area, seashore the most according to claim 1 High Performance Unmanned Aerial Vehicle, it is characterised in that described proof mechanism of water
The circular open that by the rounding column-shaped projection being arranged on steering wheel, is opened on rounding column-shaped projection end face, it is inlaid in circle and opens
Sealed folded pipe (14) in Kou, the connecting rod (15) being fixedly connected in sealed folded pipe (14) front-end surface collectively form.
A kind of salt fog area, seashore the most according to claim 1 High Performance Unmanned Aerial Vehicle, it is characterised in that described undercarriage
(12) front end upwarps.
A kind of salt fog area, seashore the most according to claim 1 High Performance Unmanned Aerial Vehicle, it is characterised in that described wing centre section
(4) junction with the left outside wing (7) and starboard outboard (8) is provided with preserving and sealing layer.
A kind of salt fog area, seashore the most according to claim 1 High Performance Unmanned Aerial Vehicle, it is characterised in that described wing centre section (4)
Epoxy glue layer is scribbled with on the left outside wing (7) and starboard outboard (8) faying face.
A kind of salt fog area, seashore the most according to claim 1 High Performance Unmanned Aerial Vehicle, it is characterised in that described wing centre section
(4), the left outside wing (7) and starboard outboard (8) are single seal modules.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610397674.9A CN106043660A (en) | 2016-06-07 | 2016-06-07 | High-performance unmanned aerial vehicle applicable to seaside salt mist area |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610397674.9A CN106043660A (en) | 2016-06-07 | 2016-06-07 | High-performance unmanned aerial vehicle applicable to seaside salt mist area |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106043660A true CN106043660A (en) | 2016-10-26 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610397674.9A Pending CN106043660A (en) | 2016-06-07 | 2016-06-07 | High-performance unmanned aerial vehicle applicable to seaside salt mist area |
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| CN (1) | CN106043660A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114408160A (en) * | 2021-12-17 | 2022-04-29 | 海丰通航科技有限公司 | Tail stay pipe and unmanned aerial vehicle |
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2016
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| EP2930102A1 (en) * | 2014-04-08 | 2015-10-14 | Marc Arnold | Flight control augmentation system and method for high aspect ratio aircraft |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114408160A (en) * | 2021-12-17 | 2022-04-29 | 海丰通航科技有限公司 | Tail stay pipe and unmanned aerial vehicle |
| CN114408160B (en) * | 2021-12-17 | 2023-08-29 | 海丰通航科技有限公司 | Tail support pipe and unmanned aerial vehicle |
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Application publication date: 20161026 |