CN107235140A - A kind of many rotor oversea flight unmanned plane devices - Google Patents
A kind of many rotor oversea flight unmanned plane devices Download PDFInfo
- Publication number
- CN107235140A CN107235140A CN201710196144.2A CN201710196144A CN107235140A CN 107235140 A CN107235140 A CN 107235140A CN 201710196144 A CN201710196144 A CN 201710196144A CN 107235140 A CN107235140 A CN 107235140A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- floating mat
- many rotor
- plane devices
- horn
- 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.)
- Pending
Links
- 238000007667 floating Methods 0.000 claims abstract description 65
- 239000000463 material Substances 0.000 claims description 11
- 238000007789 sealing Methods 0.000 claims description 6
- 239000004677 Nylon Substances 0.000 claims description 5
- 229920001778 nylon Polymers 0.000 claims description 5
- 229920001200 poly(ethylene-vinyl acetate) Polymers 0.000 claims description 5
- 229920001169 thermoplastic Polymers 0.000 claims description 5
- 230000002093 peripheral effect Effects 0.000 claims description 2
- 238000010586 diagram Methods 0.000 description 2
- 241000239290 Araneae Species 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 239000003086 colorant Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000686 essence Substances 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- LGZXYFMMLRYXLK-UHFFFAOYSA-N mercury(2+);sulfide Chemical compound [S-2].[Hg+2] LGZXYFMMLRYXLK-UHFFFAOYSA-N 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- 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
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/34—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like comprising inflatable structural components
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
Abstract
The invention provides a kind of many rotor oversea flight unmanned plane devices, including body, the body outer circumferential side is evenly arranged with some horns, each horn and is mounted on a motor, a propeller is installed with each motor, the body outer circumferential side is additionally provided with a floating mat.The present invention passes through the floating mat on body, it is to avoid the sinking problem that unmanned plane flight air crash at sea occurs when dropping into the sea, and floating mat of the present invention can form effective combination with body, do not influence the normal operating of unmanned plane to use.Compared with prior art, the present invention can make unmanned plane fall into the sea to float on sea, so that facilitating staff carries out search-and-rescue work, it greatly improves the security reliability of unmanned plane work, while effectively prevent the problem of unmanned plane is damaged.
Description
Technical field
The present invention relates to unmanned plane, and in particular to be a kind of many rotor oversea flight unmanned plane devices, particularly one kind
At sea fly and hinder and fall into the sea for some reason, the unmanned plane device that ground crew can be facilitated to salvage.
Background technology
The many rotor unmanned aircrafts of microminiature with VTOL, steadily hovering, it is civilian take photo by plane, electric power patrol, disappear
Anti- investigation, police law execution, the marine military field such as on duty have boundless application prospect.Common unmanned rotary wing flight
Device, in flight course, by other failure factors such as main rotor, engine, operating personnel, extraneous strength, can fly control to whole
The control of system has a negative impact, and aircraft can be caused out of control, causes the phenomenon of " aircraft bombing, air crash ", especially at sea flies
When, once there is above-mentioned phenomenon, it is possible to cause airplane falling in seabed, cause the search and rescue cost of costliness and bring huge damage
Lose.
The content of the invention
Therefore, can be after falling into the sea it is an object of the invention to provide one kind, many rotors sea for facilitating ground crew to salvage
Upper flight unmanned plane device.
The purpose of the present invention is achieved through the following technical solutions.
A kind of many rotor oversea flight unmanned plane devices, including body, the body outer circumferential side are evenly arranged with some machines
It is mounted on a motor, each motor being installed with a propeller, the body periphery on arm, each horn
Side is additionally provided with a floating mat.
Preferably, and position corresponding through hole identical with the horn quantity, the horn point are provided with the floating mat
It is fixedly connected after through hole that Chuan Guo be not corresponding with body.
Preferably, the through hole junction on the horn and floating mat is additionally provided with a tight loop, can be by by the tight loop
Floating mat is fixed in body outer peripheral sidewall.
Preferably, it is provided with some locating dowels, the floating mat and is provided with and institute below the horn of the body outer circumferential side
State that locating dowel quantity is identical and the corresponding through hole in position, and the body by locating dowel correspondence be placed in through hole with it is described floating
Row is fixedly connected.
Preferably, the floating mat is strip, and it is correspondingly formed open annular after folding.
Preferably, the floatability that the floating mat is made for inflation floating mat or PVC material, nylon, thermoplastic plastic, EVA material
Floating mat.
Preferably, the floating mat is annular, oval ring or rectangle frame.
Preferably, the floatability that the floating mat is made for inflation floating mat or PVC material, nylon, thermoplastic plastic, EVA material
Floating mat.
Preferably, the horn is four, six or eight.
Preferably, the body upper is sealed by a waterproof sealing lid and fixed.
Many rotor oversea flight unmanned plane devices that the present invention is provided, pass through the floating mat on body, it is to avoid nothing
The sinking problem that the man-machine air crash of flight at sea occurs when dropping into the sea, and floating mat of the present invention can form effective knot with body
Close, do not influence the normal operating of unmanned plane to use.Compared with prior art, the present invention can make unmanned plane fall into the sea to float on sea
Face, so that facilitating staff carries out search-and-rescue work, it greatly improves the security reliability of unmanned plane work, while effectively
Prevent the problem of unmanned plane is damaged.
Brief description of the drawings
Fig. 1 is the schematic perspective view of many rotor oversea flight unmanned plane devices of the invention；
Schematic diagram after many rotor oversea flight unmanned plane device floating mats foldings of Fig. 2 present invention；
Schematic diagram after many rotor oversea flight unmanned plane device floating mats stretching, extensions of Fig. 3 present invention.
Identifier declaration in figure：Body 10, waterproof sealing lid 11, camera 12, floating mat 20, through hole 21, opening 22, horn
30th, tight loop 31, motor 40, propeller 50, support 60.
Embodiment
In order to make the purpose , technical scheme and advantage of the present invention be clearer, it is right below in conjunction with drawings and Examples
The present invention is further elaborated.It should be appreciated that the specific embodiments described herein are merely illustrative of the present invention, and
It is not used in the restriction present invention.
During for the flight at sea of current unmanned plane, cause to sink to submarine fishing inconvenience because falling and unmanned plane is easy
The problem of damage, the invention provides can be filled behind a kind of sea of falling in many rotor oversea flight unmanned planes of offshore floating
Put.
Refer to shown in Fig. 1, Fig. 1 is the schematic perspective view of many rotor oversea flight unmanned plane devices of the invention.The present invention
Described unmanned plane includes organism 10, and several horns 30 are installed with the outer circumferential side of body 10, and each horn 30
One end be connected to body 10, the other end is provided with motor 40, correspondence motor 40 and is provided with propeller 50.
A waterproof sealing lid 11 is provided with the bottom of body 10, can effectively prevent from flying by the waterproof sealing lid 11
During row or when falling into the sea, water is entered inside body 10, and causes unmanned plane to damage.In addition, being set on waterproof sealing lid 11
A handle is equipped with, in order to which user carries.
Support 60 is installed with the bottom of body 10, bottom surface is can be formed in order to the takeoff and landing of unmanned plane
On support.
The side correspondence of body 10 is also equipped with a camera 12, in order to carry out detection work in high-altitude flight.
The present invention is provided with a floating mat 20 in the outer circumferential side correspondence of body 10, and the floating mat 20 can be inflation floating mat 20,
Can also be other non-inflatable floating mats, the floatability floating mat being such as made up of PVC material, nylon, thermoplastic plastic, EVA materials.
The shape of wherein floating mat 20 is strip, and several through holes 21 (see Fig. 3), the through hole 21 are correspondingly arranged on above
Quantity and position and body 10 on the position of horn 30 and quantity be in one-to-one relationship.Floating mat 20 is around one split ring of formation
Shape, and it is formed between the two ends of the strip opening 22 (see Fig. 2).
After floating mat 20 is folded into shape as shown in Figure 2, correspondence is coated on the outer circumferential side of body 10, and horn 30 is distinguished
It is fixedly connected after through corresponding through hole 21 with body 10.And in order to ensure floating mat 20 be fixed on body 10 side wall it is firm
Reliably, one tight loop 31 can be set in horn 30 and the junction of body 10, can be by floating mat 20, horn 30 by the tight loop 31
And the three of body 10 is fixed together.And the correspondence of opening 22 formed on floating mat 20 is then located at the position of camera 12, with
Exempt to block camera 12.
Be illustrated in the present embodiment by taking six rotor wing unmanned aerial vehicles as an example, in other embodiments or four rotors,
Eight rotors or other multi-rotor unmanned aerial vehicles, should not be construed the limit value to the present invention herein.
It should be noted that the shape of body 10 can be circular, oval, square or other shapes in the present embodiment,
And accordingly, the shape of floating mat 20 can be corresponded to around the outer circumferential side of body 10.
In another embodiment, floating mat 20 need not be fixedly mounted on body 10 by horn 30, the embodiment
Described in the correspondence of floating mat 20 be fixedly mounted on the lower section of horn 30, be also the annular that correspondence is formed around the bottom of body 10.
In the embodiment, several locating dowels, the floating mat 20 are provided with below the horn 30 of the outer circumferential side of body 10
On be provided with the corresponding through hole 21 in and position identical with the locating dowel quantity, and the body 10 passes through locating dowel correspondence holding
It is fixedly connected in through hole 21 with the floating mat 20.
The bottom shape of wherein body 10 is different, and the shape of correspondence floating mat 20 also corresponds to difference, is arranged on the periphery of body 10
The locating dowel quantity of side-lower is more than three, and preferably six, it is mainly fixed by floating mat correspondence, and now selected
Floating mat for closing ring-type, be primarily to facilitate fixation.
Floating mat is fixedly mounted on body by the present invention through the above way, occurs what is fallen into the sea during unmanned plane during flying
During situation, by the buoyancy of floating mat unmanned plane can be made to swim in sea and be unlikely to sinking.In addition, working for convenience
Personnel can accurately find the unmanned plane floated across the sea, and floating mat can be fabricated to the eye-catching color of comparison, such as red,
Other colors such as Chinese red, yellow, white.
If using inflation floating mat, can correspond on floating mat set inflation connect mouth, not only can manually blow inflation but also can
To use inflator or air compressor machine air-blowing, airing form is versatile and flexible.If it is floating that the material that using to float is made
Row, then can be without inflation.
The floating mat of the present invention can easily be inserted on the spider of unmanned vehicle and directly can also be coordinated by horn
Fixed, it, which is operated, installs very convenient；Under different use environments, can also according to the weight of aircraft, adjustment floating mat
Volume size, so as to increase the functional reliability of different weight aircraft.
Unmanned vehicle of the present invention has advantage simple in construction, easy to operate, can greatly improve many gyroplanes and exist
Aeromarine security reliability, once there is air crash, drops marine, the buoyancy produced by floating mat device, can facilitate work
Make personnel to search, salvage, substantially increase the offshore applications field of many rotor unmanned aircrafts.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all essences in the present invention
Any modifications, equivalent substitutions and improvements made within refreshing and principle etc., should be included in the scope of the protection.
Claims (10)
1. a kind of many rotor oversea flight unmanned plane devices, it is characterised in that including body (10), body (10) outer circumferential side
It is evenly arranged with some horns (30), each horn (30) and is mounted on a motor (40), each motor (40)
On be installed with a propeller (50), body (10) outer circumferential side is additionally provided with a floating mat (20).
2. many rotor oversea flight unmanned plane devices as claimed in claim 1, it is characterised in that set on the floating mat (20)
There is and position corresponding through hole (21) identical with the horn (30) quantity, the horn (30) is each passed through corresponding lead to
Hole (21) is fixedly connected with body (10) afterwards.
3. many rotor oversea flight unmanned plane devices as claimed in claim 2, it is characterised in that the horn (30) and floating mat
(20) through hole (21) junction on is additionally provided with a tight loop (31), can be fixed on floating mat (20) by the tight loop (31)
In body (10) outer peripheral sidewall.
4. many rotor oversea flight unmanned plane devices as claimed in claim 1, it is characterised in that body (10) outer circumferential side
Horn (30) below be provided with some locating dowels, the floating mat (20) and be provided with and position identical with the locating dowel quantity
Corresponding through hole (21), and the body (10) is correspondingly placed in by locating dowel in through hole (21) and the floating mat (20) is fixed
Connection.
5. many rotor oversea flight unmanned plane devices as described in Claims 1 to 4 is any, it is characterised in that the floating mat
(20) it is strip, it is correspondingly formed open annular after folding.
6. many rotor oversea flight unmanned plane devices as claimed in claim 5, it is characterised in that the floating mat (20) is inflation
The floatability floating mat that floating mat or PVC material, nylon, thermoplastic plastic, EVA material are made.
7. many rotor oversea flight unmanned plane devices as described in Claims 1 to 4 is any, it is characterised in that the floating mat
(20) it is annular, oval ring or rectangle frame.
8. many rotor oversea flight unmanned plane devices as claimed in claim 7, it is characterised in that the floating mat (20) is inflation
The floatability floating mat that floating mat or PVC material, nylon, thermoplastic plastic, EVA material are made.
9. many rotor oversea flight unmanned plane devices as claimed in claim 1, it is characterised in that the horn (30) is four
It is individual, six or eight.
10. many rotor oversea flight unmanned plane devices as claimed in claim 1, it is characterised in that body (10) top
Sealed and fixed by a waterproof sealing lid (11).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710196144.2A CN107235140A (en) | 2017-03-29 | 2017-03-29 | A kind of many rotor oversea flight unmanned plane devices |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710196144.2A CN107235140A (en) | 2017-03-29 | 2017-03-29 | A kind of many rotor oversea flight unmanned plane devices |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107235140A true CN107235140A (en) | 2017-10-10 |
Family
ID=59983449
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710196144.2A Pending CN107235140A (en) | 2017-03-29 | 2017-03-29 | A kind of many rotor oversea flight unmanned plane devices |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107235140A (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2013189036A (en) * | 2012-03-12 | 2013-09-26 | Kitakyushu Foundation For The Advancement Of Industry Science & Technology | Flying object for measuring |
| CN105711824A (en) * | 2014-12-22 | 2016-06-29 | 鹦鹉股份有限公司 | ROTARY WING DRONE provided with accessory enabling amphibious type rotary wing drone |
| WO2016163482A1 (en) * | 2015-04-07 | 2016-10-13 | 株式会社日本自動車部品総合研究所 | Mobile unit |
| CN206719534U (en) * | 2017-03-29 | 2017-12-08 | 深圳市科卫泰实业发展有限公司 | A kind of more rotor oversea flight unmanned plane devices |
-
2017
- 2017-03-29 CN CN201710196144.2A patent/CN107235140A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2013189036A (en) * | 2012-03-12 | 2013-09-26 | Kitakyushu Foundation For The Advancement Of Industry Science & Technology | Flying object for measuring |
| CN105711824A (en) * | 2014-12-22 | 2016-06-29 | 鹦鹉股份有限公司 | ROTARY WING DRONE provided with accessory enabling amphibious type rotary wing drone |
| WO2016163482A1 (en) * | 2015-04-07 | 2016-10-13 | 株式会社日本自動車部品総合研究所 | Mobile unit |
| CN206719534U (en) * | 2017-03-29 | 2017-12-08 | 深圳市科卫泰实业发展有限公司 | A kind of more rotor oversea flight unmanned plane devices |
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| 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 | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20171010 |