CN105691600A - Multi-rotor unmanned aerial vehicle - Google Patents
Multi-rotor unmanned aerial vehicle Download PDFInfo
- Publication number
- CN105691600A CN105691600A CN201511035454.3A CN201511035454A CN105691600A CN 105691600 A CN105691600 A CN 105691600A CN 201511035454 A CN201511035454 A CN 201511035454A CN 105691600 A CN105691600 A CN 105691600A
- Authority
- CN
- China
- Prior art keywords
- unmanned aerial
- lower arm
- wing unmanned
- rotor wing
- arm rod
- 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
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/34—Alighting gear characterised by elements which contact the ground or similar surface wheeled type, e.g. multi-wheeled bogies
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
- B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
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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
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C2025/325—Alighting gear characterised by elements which contact the ground or similar surface specially adapted for helicopters
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Transportation (AREA)
- Toys (AREA)
Abstract
The invention discloses a multi-rotor unmanned aerial vehicle. The multi-rotor unmanned aerial vehicle comprises a vehicle body, rotors and support legs; the support legs consist of upper arm rods and lower arm rods; the upper arm rods and the lower arm rods are hinged through hinge shafts; and electronic wheels are arranged in the hinged places between the upper arm rods and the lower arm rods. The multi-rotor unmanned aerial vehicle further comprises a control mechanism for controlling the lower arm rods to swing up and down around the hinge shafts for unfolding and folding. The multi-rotor unmanned aerial vehicle has special mechanical arms, is simple in structure and light in weight, and has the aerial transportation capacity; and meanwhile, the multi-rotor unmanned aerial vehicle also has a land walking function.
Description
Technical field
The present invention relates to a kind of many rotor wing unmanned aerial vehicles。
Background technology
Current many rotor wing unmanned aerial vehicles generally comprise fuselage, rotor and leg, and general described leg is substantially fixing, so existing many rotor wing unmanned aerial vehicles do not have land walking function substantially。It addition, current many rotor wing unmanned aerial vehicles generally do not have mechanical arm for capturing article, because the structure of mechanical arm is complicated, certainly will cause that the weight of many rotor wing unmanned aerial vehicles increases, and from causing that unmanned plane is difficult to take off。
For the problems referred to above, the present inventor devises a kind of many rotor wing unmanned aerial vehicles with transporting capacity, to solve the problems referred to above。
Summary of the invention
In view of this, it is an object of the invention to provide a kind of many rotor wing unmanned aerial vehicles, these many rotor wing unmanned aerial vehicles have special mechanical arm, its simple in construction, lightweight, have therefore possessed air transport ability, and many rotor wing unmanned aerial vehicles of the present invention also have land walking function simultaneously。
The present invention solves the problems referred to above by techniques below means:
The many rotor wing unmanned aerial vehicles of one of the present invention, including fuselage, rotor and leg, described leg is made up of upper armed lever and lower arm rod, and described upper armed lever and lower arm rod are hinged by jointed shaft, and the hinged place between described upper armed lever and lower arm rod is provided with electric wheels；Also include the controlling organization taken down the exhibits for controlling described lower arm rod to swing up and down around described jointed shaft。
Further, described controlling organization includes electric expansion bar, and the two ends of described electric expansion bar are hinged with described upper armed lever and lower arm rod respectively。
Further, the end of described lower arm rod is provided with coupler body。
Further, described leg at least provided with three, the rotationally symmetrical setting of lower arm rod of described three legs, and can simultaneously to place folding。
Further, the top of described upper armed lever and fuselage are rotatably assorted。
Further, the top of described upper armed lever is fixed with a rotating shaft, and described fuselage bottom is provided with and circumferentially rotates, with described rotating shaft, the bearing coordinated。
Further, described rotating shaft top is provided with gear, and described fuselage bottom is additionally provided with the motor for controlling rotating shaft angle, and described motor is coordinated with the gear drive at described rotating shaft top by the gear being arranged on above power output shaft。
Beneficial effects of the present invention: many rotor wing unmanned aerial vehicles of the present invention, including fuselage, rotor and leg, described leg is made up of upper armed lever and lower arm rod, and described upper armed lever and lower arm rod are hinged by jointed shaft, and the hinged place between described upper armed lever and lower arm rod is provided with electric wheels；Also include the controlling organization taken down the exhibits for controlling described lower arm rod to swing up and down around described jointed shaft。Many rotor wing unmanned aerial vehicles of the present invention have special mechanical arm, its simple in construction, lightweight, have therefore possessed air transport ability, and many rotor wing unmanned aerial vehicles of the present invention also have land walking function simultaneously。
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the invention will be further described。
Fig. 1 is the Facad structure schematic diagram of the many rotor wing unmanned aerial vehicles of the present invention, eliminates the support in front in figure；
Fig. 2 is the side structure schematic diagram of the many rotor wing unmanned aerial vehicles of the present invention；
Fig. 3 is the structure for amplifying schematic diagram in Tu2Zhong A district。
Detailed description of the invention
Below with reference to accompanying drawing, the present invention is described in detail:
As shown in Figures 1 to 3, the many rotor wing unmanned aerial vehicles of one of the present invention, including fuselage 1, rotor 2 and leg 3, described leg 3 is made up of upper armed lever 31 and lower arm rod 32, described upper armed lever 31 and lower arm rod 32 are hinged by jointed shaft 33, and the hinged place between described upper armed lever 31 and lower arm rod 32 is provided with electric wheels 34；Also include the controlling organization 35 taken down the exhibits for controlling described lower arm rod to swing up and down around described jointed shaft 33, described controlling organization 35 includes electric expansion bar, the two ends of described electric expansion bar are hinged with described upper armed lever and lower arm rod respectively, described leg is at least provided with three, the rotationally symmetrical setting of lower arm rod of described three legs, and can simultaneously to place folding。When landing time lower arm rod 32 can upwards folding, make electric wheels 34 contact ground, and then realize the land walking of unmanned plane；When needs air transport article, then multiple lower arm rods 32 can be opened folding together to grab article simultaneously。Due to the present invention by the support of unmanned plane and the mechanical arm organically structure capturing article, thus not dramatically increasing the weight of unmanned plane。
Many rotor wing unmanned aerial vehicles of the present invention have special mechanical arm, its simple in construction, lightweight, have therefore possessed air transport ability, and many rotor wing unmanned aerial vehicles of the present invention also have land walking function simultaneously。
As the further improvement of technique scheme, the end of described lower arm rod is provided with coupler body 36。Article can be caught on, it is prevented that article come off in the air by arranging coupler body 36。
Further improvement as technique scheme, the top of described upper armed lever and fuselage are rotatably assorted, the top of described upper armed lever is fixed with a rotating shaft 37, described fuselage bottom is provided with and circumferentially rotates the bearing 38 coordinated with described rotating shaft, described rotating shaft top is provided with gear 39, described fuselage bottom is additionally provided with the motor 4 for controlling rotating shaft angle, and described motor is coordinated with the gear drive at described rotating shaft top by the gear being arranged on above power output shaft。By motor can the rotation of drive shaft, and then control the direction of electric wheels 34, to be arranged by above-mentioned improvement so that the unmanned plane of the present invention is provided with turning function when land walking。
What finally illustrate is, above example is only in order to illustrate technical scheme and unrestricted, although the present invention being described in detail with reference to preferred embodiment, it will be understood by those within the art that, technical scheme can be modified or equivalent replacement, without deviating from objective and the scope of technical solution of the present invention, it all should be encompassed in the middle of scope of the presently claimed invention。
Claims (7)
1. rotor wing unmanned aerial vehicle more than a kind, it is characterized in that: include fuselage, rotor and leg, described leg is made up of upper armed lever and lower arm rod, and described upper armed lever and lower arm rod are hinged by jointed shaft, and the hinged place between described upper armed lever and lower arm rod is provided with electric wheels；Also include the controlling organization taken down the exhibits for controlling described lower arm rod to swing up and down around described jointed shaft。
2. many rotor wing unmanned aerial vehicles according to claim 1, it is characterised in that: described controlling organization includes electric expansion bar, and the two ends of described electric expansion bar are hinged with described upper armed lever and lower arm rod respectively。
3. many rotor wing unmanned aerial vehicles according to claim 2, it is characterised in that: the end of described lower arm rod is provided with coupler body。
4. many rotor wing unmanned aerial vehicles according to claim 3, it is characterised in that: described leg at least provided with three, the rotationally symmetrical setting of lower arm rod of described three legs, and can simultaneously to place folding。
5. many rotor wing unmanned aerial vehicles according to claim 4, it is characterised in that: the top of described upper armed lever and fuselage are rotatably assorted。
6. many rotor wing unmanned aerial vehicles according to claim 5, it is characterised in that: the top of described upper armed lever is fixed with a rotating shaft, and described fuselage bottom is provided with and circumferentially rotates, with described rotating shaft, the bearing coordinated。
7. many rotor wing unmanned aerial vehicles according to claim 6, it is characterized in that: described rotating shaft top is provided with gear, described fuselage bottom is additionally provided with the motor for controlling rotating shaft angle, and described motor is coordinated with the gear drive at described rotating shaft top by the gear being arranged on above power output shaft。
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201511035454.3A CN105691600A (en) | 2015-12-31 | 2015-12-31 | Multi-rotor unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201511035454.3A CN105691600A (en) | 2015-12-31 | 2015-12-31 | Multi-rotor unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105691600A true CN105691600A (en) | 2016-06-22 |
Family
ID=56226867
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201511035454.3A Withdrawn CN105691600A (en) | 2015-12-31 | 2015-12-31 | Multi-rotor unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105691600A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106827992A (en) * | 2017-03-07 | 2017-06-13 | 上海机电工程研究所 | Land and air double-used six rotorcraft device |
| CN106927034A (en) * | 2017-03-23 | 2017-07-07 | 东莞职业技术学院 | It is a kind of with self-protection function and can fast lifting unmanned plane |
| CN107117291A (en) * | 2017-04-26 | 2017-09-01 | 浙江大学 | A kind of power-assisted transport foot stool and the unmanned plane with the foot stool |
| CN107379909A (en) * | 2017-07-27 | 2017-11-24 | 韩朝锋 | A kind of flight meal delivery robot |
| CN107902090A (en) * | 2017-10-18 | 2018-04-13 | 安徽工程大学 | A kind of transport of unmanned vehicle is jettisoninged mechanism |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN203111294U (en) * | 2013-01-18 | 2013-08-07 | 西北农林科技大学 | Agricultural remote control mobile robot platform capable of rotating omni-directionally and lifting |
| CN203623975U (en) * | 2014-01-01 | 2014-06-04 | 许洪 | Improved aircraft |
| KR20140115711A (en) * | 2013-03-22 | 2014-10-01 | 김명호 | Aerial Vehicle With Mltipurpose Grip Type Taking Off an Landing Devic |
| CN204368417U (en) * | 2014-11-28 | 2015-06-03 | 吉林大学 | Novel four rotor amphibious robots |
| CN204713431U (en) * | 2015-04-24 | 2015-10-21 | 深圳一电科技有限公司 | Carry device and unmanned plane |
-
2015
- 2015-12-31 CN CN201511035454.3A patent/CN105691600A/en not_active Withdrawn
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN203111294U (en) * | 2013-01-18 | 2013-08-07 | 西北农林科技大学 | Agricultural remote control mobile robot platform capable of rotating omni-directionally and lifting |
| KR20140115711A (en) * | 2013-03-22 | 2014-10-01 | 김명호 | Aerial Vehicle With Mltipurpose Grip Type Taking Off an Landing Devic |
| CN203623975U (en) * | 2014-01-01 | 2014-06-04 | 许洪 | Improved aircraft |
| CN204368417U (en) * | 2014-11-28 | 2015-06-03 | 吉林大学 | Novel four rotor amphibious robots |
| CN204713431U (en) * | 2015-04-24 | 2015-10-21 | 深圳一电科技有限公司 | Carry device and unmanned plane |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106827992A (en) * | 2017-03-07 | 2017-06-13 | 上海机电工程研究所 | Land and air double-used six rotorcraft device |
| CN106927034A (en) * | 2017-03-23 | 2017-07-07 | 东莞职业技术学院 | It is a kind of with self-protection function and can fast lifting unmanned plane |
| CN106927034B (en) * | 2017-03-23 | 2019-02-01 | 东莞职业技术学院 | It is a kind of with self-protection function and can fast lifting unmanned plane |
| CN107117291A (en) * | 2017-04-26 | 2017-09-01 | 浙江大学 | A kind of power-assisted transport foot stool and the unmanned plane with the foot stool |
| CN107117291B (en) * | 2017-04-26 | 2023-09-15 | 浙江大学 | Helping hand transportation foot rest and have unmanned aerial vehicle of this foot rest |
| CN107379909A (en) * | 2017-07-27 | 2017-11-24 | 韩朝锋 | A kind of flight meal delivery robot |
| CN107379909B (en) * | 2017-07-27 | 2019-10-29 | 潘浩然 | A kind of flight meal delivery robot |
| CN107902090A (en) * | 2017-10-18 | 2018-04-13 | 安徽工程大学 | A kind of transport of unmanned vehicle is jettisoninged mechanism |
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| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20160622 |
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| WW01 | Invention patent application withdrawn after publication |