CN107097948A - A kind of multi-rotor unmanned aerial vehicle - Google Patents
A kind of multi-rotor unmanned aerial vehicle Download PDFInfo
- Publication number
- CN107097948A CN107097948A CN201610116777.3A CN201610116777A CN107097948A CN 107097948 A CN107097948 A CN 107097948A CN 201610116777 A CN201610116777 A CN 201610116777A CN 107097948 A CN107097948 A CN 107097948A
- Authority
- CN
- China
- Prior art keywords
- unmanned aerial
- aerial vehicle
- rotor
- protective cover
- rotor unmanned
- 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
- 230000001681 protective effect Effects 0.000 claims abstract description 32
- 239000002775 capsule Substances 0.000 claims abstract description 12
- 239000002131 composite material Substances 0.000 claims abstract description 7
- 239000006260 foam Substances 0.000 claims abstract description 7
- 230000005611 electricity Effects 0.000 claims description 5
- 230000004224 protection Effects 0.000 claims description 5
- 239000000203 mixture Substances 0.000 claims description 2
- 239000011800 void material Substances 0.000 claims 1
- 238000010276 construction Methods 0.000 abstract description 2
- 230000006386 memory function Effects 0.000 abstract description 2
- 230000003139 buffering effect Effects 0.000 abstract 1
- 230000007613 environmental effect Effects 0.000 abstract 1
- 238000005507 spraying Methods 0.000 abstract 1
- 230000000694 effects Effects 0.000 description 2
- 230000006870 function Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000007493 shaping process Methods 0.000 description 2
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000003337 fertilizer Substances 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical group C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/20—Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/006—Safety devices
-
- 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
- B64C27/10—Helicopters with two or more rotors arranged coaxially
-
- 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)
- Catching Or Destruction (AREA)
Abstract
A kind of multi-rotor unmanned aerial vehicle, it is related to a kind of round pie protective cover and aerated capsule being made with one-shot forming foam composite material, the multi-rotor unmanned aerial vehicle of radar avoiding device, can be close to building, trees, avoid colliding falling of causing with it and ruin machine accident, outside is cased with aerated capsule, buffering can be mitigated to hit, suspended window breaker, deliver buoyant apparatus, available for hanging traction construction operation, fishing tackle fishing gear can be hung, also suspended spraying operation equipment, it also is adapted for the operations such as express delivery, such as install radar avoiding device additional, cavern can be navigated within, between building, it can also be returned if any memory function by Reciprocal course.Branched this gyroplane can be serially connected with vertical direction or connect into relatively large multi-rotor unmanned aerial vehicle in the horizontal direction and be combined into the unmanned plane of train shape, can greatly expand multi-rotor unmanned aerial vehicle application, Environmental Safety.
Description
Technical field：
A kind of multi-rotor unmanned aerial vehicle, belongs to unmanned field of aircraft.
Background technology：
The circular peripheral-mill of the aerial blocks of revolution at a high speed in multi-rotor unmanned aerial vehicle shape such as day, so it should be specifically noted that
Safety in use, rotor and building, trees collision and the causing accident that machine ruins of falling happens occasionally, right
We are equally wrapped using domestic fan with protective cover for this, are become round pie, can be played good effect,
Unmanned plane can be close to building, trees, and can expand multi-rotor unmanned aerial vehicle and use scope, outside it
We also cover aerated capsule can reducing collisions, rise cushioning effect, available for high building fire fighting, mount window breaker,
Fire distinguisher, fire extinguisher bomb etc. are delivered, available for hanging traction construction operation, fishing tackle fishing gear can be hung, sprayed
Apply fertilizer agricultural machinery, also is adapted for express transportation, such as installs radar avoiding device additional and have memory function, returned by Reciprocal course
Function is returned, can be navigated between cavern, building, in the upper surface of this multi-rotor unmanned aerial vehicle with protective cover
Center and lower surface center are provided with implement quick-attaching couple, can be quickly by multiple multi-rotor unmanned aerial vehicles in vertical direction
Be serially connected or connect into large-scale multi-rotor unmanned aerial vehicle in the horizontal direction, can also be combined into train type without
It is man-machine to expand application.
The content of the invention：
Goal of the invention：The round pie protective cover and gas-filled protective glue being made with one-shot forming foam composite material
The multi-rotor unmanned aerial vehicle of capsule, and have a radar avoiding device, can close to building and trees, and walk cave,
Ability between grove, building, can rapidly by multiple multi-rotor unmanned aerial vehicle strings and be connected into larger many rotors nobody
Machine, has been widely used in each side tool of national economy.
What the present invention was realized in：It is made up of protection capsule, the one-shot forming foam composite material inflated
Upper protective cover, lower protective cover, it is intermediate supports circle, cross rotor bar, coaxial anti-oar rotor head, upper quick
Connector, lower quick connector, the mechanical, electrical tune device of reception, LED light, radar avoiding device, secondary electricity
The multi-rotor unmanned aerial vehicle of pond composition, it is characterised in that upper protective cover is netted dome shape, leaves two large holes
Hole, facilitates the installation of secondary cell, and quick connector is installed in centre, and lower protective cover is also netted dome shape,
Lower protective cover center is provided with lower quick connector, and upper protective cover is connected to one with lower protective cover by bracing ring
Rise, cross rotor bar is connected on intermediate supports circle by the end of bar, four coaxial anti-oar rotor head peaces
On cross rotor bar, the mechanical, electrical tune device of reception, two are installed in the centre of cross rotor bar
Primary cell, radar avoiding device, LED light are arranged on intermediate supports circle, the outer cover of intermediate supports circle
There is gas-filled protective capsule, receive mechanical, electrical tune device, radar avoiding device, LED light, coaxial anti-oar rotor
Head, secondary cell are electrically connected, and the protection capsule of inflation is the capsule that bicycle high pressure inflator is inflated, once
Upper protective cover that shaping foam composite is made, lower protective cover, intermediate supports circle material therefor is also for once
Shaping foam composite, the material of cross rotor bar is carbon fiber pipe, and lower implement quick-attaching couple also can root
According to needing to install electronic discharge mechanism, lower hung article can be quickly thrown.
The advantage of this programme is the unmanned transporter of simple structure, multipurpose, low cost, function admirable.
Brief description of the drawings：
Fig. 1, a kind of multi-rotor unmanned aerial vehicle top view
Fig. 2, a kind of multi-rotor unmanned aerial vehicle front view
Fig. 3, a kind of multi-rotor unmanned aerial vehicle remove top view after upper protective cover
Fig. 4, be Fig. 3 A-A cross section views
Fig. 5, lower protective cover top view
Fig. 6, lower protective cover B-B cross section views
Fig. 7, intermediate supports circle top view
Fig. 8, intermediate supports circle C-C cross section views
Fig. 9, situation together will be concatenated above and below 2 (or branched) multi-rotor unmanned aerial vehicles
Figure 10, horizontal direction connect into large-scale multi-rotor unmanned aerial vehicle situation
Figure 11, the situation for connecting into train type unmanned plane
In figure：Protective cover, 2 gas-filled protective capsules, 3 intermediate supports circles, 4 times protective covers, 5 times protections on 1
Supporting leg, 6LED indicator lamps, 7 radar avoiding devices on cover, 8 electricity adjust devices, 9 receivers, 10 secondary cells,
12 coaxial anti-oar rotor heads, 13 poles, 14 cross rotor bars, quick connector on 15,16 times it is quick
Connector, the dop of 17 intermediate supports circles, 18 and load connect auxiliary, 19 multi-rotor unmanned aerial vehicles
Embodiment：
Embodiment 1：Quick connector on protective cover installed above 15 on 1,4 times protective covers, 16 times it is quick
Connector is linked together, and 6LED indicator lamps, 7 radar avoiding devices, 14 are installed on 3 intermediate supports circles
Cross rotor bar is connected by the dop of 17 intermediate supports circles with 3 intermediate supports circles, in the rotation of 14 cross
12 coaxial anti-oar rotor heads, 9 receivers, 8 electricity are installed on wing bar and adjust device, 10 secondary cells, will be protected on 1
Shield, 4 times protective covers, 3 intermediate supports circles are installed together, 12 coaxial anti-oar rotor heads, 9 receivers,
8 electricity adjust device, 10 secondary cells, 7 radar avoiding devices, 6LED indicator lamps to electrically connect, 2 gas-filled protective capsules
It is enclosed on the outside of 3 intermediate supports circles.
Claims (2)
1. a kind of multi-rotor unmanned aerial vehicle is by the protection capsule inflated, upper protective cover, lower protective cover, intermediate supports
Circle, cross rotor bar, contrarotation rotor head, upper quick connector, lower quick connector, receiver,
Electricity adjusts device, LED light, radar avoiding device, the multi-rotor unmanned aerial vehicle of secondary battery composition, its feature
It is：Upper protective cover is the netted circular enclosure that is made of one-shot forming foam composite material, leave above two compared with
Macroscopic void, facilitates secondary cell to install, and centre is provided with quick connector, and lower protective cover is also one-shot forming
The netted circular enclosure that foam composite material is made, lower protective cover center is provided with lower quick connector, upper protection
Cover is linked together with lower protective cover by intermediate supports circle, and cross rotor bar is connected to by the end of bar
On intermediate supports circle, four coaxial anti-oar rotor heads are arranged on cross rotor bar, in cross rotor bar
Centre be provided with reception it is mechanical, electrical tune device, secondary cell, radar avoiding device, LED light install
On intermediate supports circle, gas-filled protective capsule is cased with outside intermediate supports circle, mechanical, electrical tune device, radar is received and keeps away
Device, LED light, coaxial anti-oar rotor head, secondary cell is allowed to electrically connect.
2. a kind of multi-rotor unmanned aerial vehicle according to claim 1 is further characterized in that：With combining and tear open
Unload auxiliary, can be achieved many unmanned planes quickly connect string and or plane combination, adapt to different use conditions and
Flight is required.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610116777.3A CN107097948A (en) | 2016-02-23 | 2016-02-23 | A kind of multi-rotor unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610116777.3A CN107097948A (en) | 2016-02-23 | 2016-02-23 | A kind of multi-rotor unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107097948A true CN107097948A (en) | 2017-08-29 |
Family
ID=59658576
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610116777.3A Pending CN107097948A (en) | 2016-02-23 | 2016-02-23 | A kind of multi-rotor unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107097948A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107585298A (en) * | 2016-07-06 | 2018-01-16 | 珠海天空速递有限公司 | Aerial deformable multi-rotor unmanned aerial vehicle |
| FR3092824A1 (en) * | 2019-02-20 | 2020-08-21 | Airbus Operations | system comprising an air inlet for an aircraft engine and an inflatable protection for said air inlet |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20120136797A (en) * | 2011-06-10 | 2012-12-20 | 드림스페이스월드주식회사 | Safety cover for unmanned vehicle |
| CN104192304A (en) * | 2014-09-17 | 2014-12-10 | 深圳大学 | Rotor robot system for environment and pedestrian safety |
| CN104443411A (en) * | 2014-10-27 | 2015-03-25 | 成都好飞机器人科技有限公司 | Quad-rotor unmanned aerial vehicle with anti-collision protective device |
| CN204548499U (en) * | 2015-02-01 | 2015-08-12 | 范磊 | Modularization combined type many rotors hybrid power aircraft |
| CN105292474A (en) * | 2015-11-06 | 2016-02-03 | 中国航空工业经济技术研究院 | Aerial queue type agricultural unmanned aerial vehicle system |
| CN205366068U (en) * | 2016-02-23 | 2016-07-06 | 陈志石 | Unmanned aerial vehicle with multiple rotor wings |
-
2016
- 2016-02-23 CN CN201610116777.3A patent/CN107097948A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20120136797A (en) * | 2011-06-10 | 2012-12-20 | 드림스페이스월드주식회사 | Safety cover for unmanned vehicle |
| CN104192304A (en) * | 2014-09-17 | 2014-12-10 | 深圳大学 | Rotor robot system for environment and pedestrian safety |
| CN104443411A (en) * | 2014-10-27 | 2015-03-25 | 成都好飞机器人科技有限公司 | Quad-rotor unmanned aerial vehicle with anti-collision protective device |
| CN204548499U (en) * | 2015-02-01 | 2015-08-12 | 范磊 | Modularization combined type many rotors hybrid power aircraft |
| CN105292474A (en) * | 2015-11-06 | 2016-02-03 | 中国航空工业经济技术研究院 | Aerial queue type agricultural unmanned aerial vehicle system |
| CN205366068U (en) * | 2016-02-23 | 2016-07-06 | 陈志石 | Unmanned aerial vehicle with multiple rotor wings |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107585298A (en) * | 2016-07-06 | 2018-01-16 | 珠海天空速递有限公司 | Aerial deformable multi-rotor unmanned aerial vehicle |
| FR3092824A1 (en) * | 2019-02-20 | 2020-08-21 | Airbus Operations | system comprising an air inlet for an aircraft engine and an inflatable protection for said air inlet |
| EP3699096A1 (en) * | 2019-02-20 | 2020-08-26 | Airbus Operations (S.A.S.) | System comprising an air intake of an aircraft engine and inflatable protection for said air intake |
| US11377224B2 (en) | 2019-02-20 | 2022-07-05 | Airbus Operations Sas | System comprising an air intake of an aircraft engine and an inflatable protection item for said air intake |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN201469941U (en) | Fire extinguisher for wind generating set | |
| CN201309590Y (en) | Air tanker | |
| CN107097948A (en) | A kind of multi-rotor unmanned aerial vehicle | |
| CN204606224U (en) | A kind of unmanned plane landing damping device | |
| CN202569554U (en) | Tumbler aircraft toy | |
| CN103252032B (en) | Intelligent forest fire extinguishing aerial bomb integrated loading module | |
| CN202686759U (en) | Four-wing flight vehicle | |
| CN205366068U (en) | Unmanned aerial vehicle with multiple rotor wings | |
| CN103033103A (en) | Closed explosion-proof container | |
| CN104575879B (en) | The anti-unfirmly closing device of a kind of extra-high voltage combined insulator | |
| CN205239919U (en) | A explosive barrel combined type duct for having more unmanned plant protection of rotor machine | |
| CN105836147B (en) | A kind of rotor wing unmanned aerial vehicle protective device | |
| CN204587308U (en) | Aircraft seeding mounting apparatus | |
| CN203100594U (en) | Closed anti-explosion tank | |
| CN210096729U (en) | High-altitude flight fire-fighting device | |
| CN204637367U (en) | A kind of automobile of self-extinguishing | |
| CN203079642U (en) | Working bucket with fall protection device and high-altitude vehicle | |
| CN202491924U (en) | Airplane anti-falling and self-rescuing device | |
| CN102921125A (en) | Direct emission type remote fire extinguishing bomb | |
| CN205574292U (en) | Rotor unmanned aerial vehicle protection device | |
| CN106275408A (en) | A kind of rotor wing unmanned aerial vehicle | |
| CN208216990U (en) | A kind of efficient emergency broken window multi-rotor unmanned aerial vehicle system | |
| CN106314780A (en) | Unmanned aerial vehicle (UAV) for logistics | |
| CN206511113U (en) | A kind of multi-rotor unmanned aerial vehicle damping undercarriage | |
| CN205615700U (en) | Soft protective sheath of multiaxis aircraft |
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: 20220719 Address after: 519000 zone a, floor 1, building 1, No. 728, Jinhu Road, Sanzao Town, Jinwan District, Zhuhai City, Guangdong Province Applicant after: SINO-AMERICAN AERIAL ROBOT (ZHUHAI) CO.,LTD. Address before: 519041 No. 437-1-302, Huayang Road, Jinhai coast, Sanzao Town, Jinwan District, Zhuhai City, Guangdong Province Applicant before: Chen Zhishi |
|
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170829 |