CN110606190A - Four rotor unmanned aerial vehicle of collapsible arm - Google Patents
Four rotor unmanned aerial vehicle of collapsible arm Download PDFInfo
- Publication number
- CN110606190A CN110606190A CN201910987971.2A CN201910987971A CN110606190A CN 110606190 A CN110606190 A CN 110606190A CN 201910987971 A CN201910987971 A CN 201910987971A CN 110606190 A CN110606190 A CN 110606190A
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- China
- Prior art keywords
- horn
- unmanned aerial
- aerial vehicle
- motor
- machine body
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- 230000000694 effects Effects 0.000 abstract description 5
- 238000000034 method Methods 0.000 abstract description 4
- 230000008569 process Effects 0.000 abstract description 2
- 230000009471 action Effects 0.000 description 4
- 230000008602 contraction Effects 0.000 description 3
- 230000007306 turnover Effects 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000012876 topography Methods 0.000 description 1
Classifications
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- 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
- B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of 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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
Abstract
The invention provides a quad-rotor unmanned aerial vehicle with foldable arms, which comprises: the surface of the machine body is square; the four arms are respectively connected to the four sides of the machine body and are connected with the machine body through springs and hinges; and the propeller is arranged on the horn and consists of a motor bracket, a motor fixed on the motor bracket and a blade connected with the motor. The folding arm of the unmanned aerial vehicle has a simple structure, can realize the function of deforming the folding arm in the flying process of the unmanned aerial vehicle without an additional driver, has good deformation effect, can also keep the advantages of long endurance, large load and high stability through the narrow space which can not be penetrated by the existing generally non-deformable quatrotor, and can play an important role in tasks such as rescue, survey and the like.
Description
Technical Field
The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to a quad-rotor unmanned aerial vehicle with foldable arms.
Background
An unmanned aircraft, abbreviated as drone and in english as UAV, is an aircraft that is operated by means of a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. The unmanned aerial vehicle is wide in application field at present and has general application in military use, civil use and other aspects. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In civil aspects, unmanned aerial vehicles are widely applied to aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, movie and television shooting and the like.
In some operation tasks, for example disaster relief, military reconnaissance, scientific surveying, because the environment is comparatively complicated, unmanned aerial vehicle will face the test through narrow and small topography at the operation in-process, because above operation task has higher requirements to functions such as unmanned aerial vehicle's continuation of the journey load stability simultaneously again, consequently, the volume that reduces unmanned aerial vehicle in a taste improves its flexibility inadvisable.
Disclosure of Invention
The invention is made to solve the above problems, and an object of the invention is to provide a quad-rotor unmanned aerial vehicle with foldable arms.
The invention provides a quad-rotor unmanned aerial vehicle with foldable arms, which is characterized by comprising the following components: the surface of the machine body is square; the four arms are respectively connected to the four sides of the machine body and are connected with the machine body through springs and hinges; and the propeller is arranged on the horn and consists of a motor bracket, a motor fixed on the motor bracket and a blade connected with the motor.
In the four rotor unmanned aerial vehicle with foldable arms provided by the invention, the four rotor unmanned aerial vehicle can also have the following characteristics: wherein, the screw propeller is a ducted screw propeller.
In the four rotor unmanned aerial vehicle with foldable arms provided by the invention, the four rotor unmanned aerial vehicle can also have the following characteristics: wherein, the support is composed of two crossbeams which are mutually vertical in a cross shape.
Action and Effect of the invention
According to the four-rotor unmanned aerial vehicle with the foldable horn, the horn is connected with the body through the spring and the hinge, so that the extension and contraction of the spring and the turnover of the hinge can be controlled by controlling the thrust of the propeller, and the folding and unfolding of the horn can be further controlled; because the screw comprises motor support, motor and paddle, so can the motor independently drive the paddle rotatory, need not extra driver, saved the cost.
Therefore, the four-rotor unmanned aerial vehicle with the foldable arms is simple in structure, the function of deforming the foldable arms in the flight process of the unmanned aerial vehicle can be realized without an additional driver, and the deformation effect is good. In addition, the time required by the opening and closing deformation of the horn is short, the size of the folded horn is reduced by 50% relative to the size of the stretched horn, so that the size of the folded horn is reduced, the advantages of long endurance, large load and high stability can be kept through a narrow space which can not be penetrated by the existing universal non-deformable four-axis gyroplane, and the folded horn can play an important role in tasks such as rescue, survey and the like.
Drawings
Fig. 1 is a schematic structural view of a quad-rotor drone with foldable arms according to an embodiment of the invention;
fig. 2 is a structural side view of a quad-rotor drone with foldable horn according to an embodiment of the present invention.
Detailed Description
In order to make the technical means and functions of the present invention easy to understand, the present invention is specifically described below with reference to the embodiments and the accompanying drawings.
Example (b):
fig. 1 is a schematic structural view of a quad-rotor drone with a foldable horn according to an embodiment of the present invention, and fig. 2 is a side structural view of the quad-rotor drone with a foldable horn according to an embodiment of the present invention.
As shown in fig. 1 and 2, a four-rotor drone 100 with foldable arms of the present embodiment includes: fuselage 10, horn 20, and propeller 30.
The surface of the body 10 is square.
The number of the horn 20 is 4, which is respectively connected to four sides of the body 10 and is symmetrical about the center of the body 10, and is connected to the body 10 by the spring 40 and the hinge 50, the spring 40 and the hinge 50 pull the horn 10 to a vertical position when the propeller 30 stops operating, and the horn 10 is unfolded again when the propeller 30 starts and the thrust of the propeller 30 exceeds the tension of the spring 40.
The surface of the horn 20 is square and has the same side length as the surface of the body 10, and the size of the folded horn 20 is half of the size of the extended horn 20, that is, the size is reduced by 50%.
The hinge 50 is disposed at the connection position of the fuselage 10 and the horn 20, and under the expansion and contraction of the spring 40 and the turning action of the hinge 50, the horn 20 can be turned over under the thrust action of the propeller 30, thereby completing the folding and unfolding of the horn 20.
The propeller 30 is mounted on the arm 10 and is composed of a motor bracket 301, a motor (not shown) fixed on the motor bracket 301, and a blade 302 connected to the motor, and the rotation of the blade 302 is driven by the motor.
In this embodiment, the propeller 30 is a ducted propeller, and the support 301 is composed of two cross-shaped cross beams perpendicular to each other.
The working principle of the four-rotor unmanned aerial vehicle with the foldable horn is as follows:
in the four-rotor unmanned plane with foldable horn 100 of the present invention, when the motor stops operating, the propeller 30 stops operating, at this time, the thrust provided by the propeller 30 is zero, the horn 20 will be pulled to the vertical position to realize folding under the action of the spring 40 and the hinge 50, when the motor operates, the propeller 30 starts and when the thrust of the propeller 30 exceeds the tension of the spring 40, the horn 20 will be unfolded again.
Effects and effects of the embodiments
According to the four-rotor unmanned aerial vehicle with the foldable horn, the horn is connected with the body through the spring and the hinge, so that the extension and contraction of the spring and the turnover of the hinge can be controlled by controlling the thrust of the propeller, and the folding and unfolding of the horn can be further controlled; because the screw comprises motor support, motor and paddle, so can independently drive the paddle rotation through the motor, need not extra driver, save the cost.
According to the collapsible four rotor unmanned aerial vehicle of horn that this embodiment relates to, because the screw that adopts is duct formula screw, so efficiency is higher, and the mobility is stronger.
Consequently, the collapsible four rotor unmanned aerial vehicle of horn of this embodiment simple structure need not extra driver and just can realize the function that unmanned aerial vehicle flight in-process folding horn warp, and warp respond well. In addition, the time required by the opening and closing deformation of the horn is short, the size of the folded horn is reduced by 50% relative to the size of the stretched horn, so that the size of the folded horn is reduced, the advantages of long endurance, large load and high stability can be kept through a narrow space which can not be penetrated by the existing universal non-deformable four-axis gyroplane, and the folded horn can play an important role in tasks such as rescue, survey and the like.
The above embodiments are preferred examples of the present invention, and are not intended to limit the scope of the present invention.
Claims (3)
1. The utility model provides a four rotor unmanned aerial vehicle of collapsible horn which characterized in that includes:
the surface of the machine body is square;
the four machine arms are respectively connected to the four sides of the machine body and are connected with the machine body through springs and hinges; and
the propeller is arranged on the horn and consists of a motor support, a motor fixed on the motor support and a paddle connected with the motor.
2. The horn-foldable quad-rotor drone of claim 1, characterized in that:
wherein, the screw propeller is a ducted screw propeller.
3. The horn-foldable quad-rotor drone of claim 1, characterized in that:
the motor support is composed of two cross-shaped cross beams which are perpendicular to each other.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2019215955564 | 2019-09-24 | ||
| CN201921595556 | 2019-09-24 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110606190A true CN110606190A (en) | 2019-12-24 |
Family
ID=68894866
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910987971.2A Pending CN110606190A (en) | 2019-09-24 | 2019-10-17 | Four rotor unmanned aerial vehicle of collapsible arm |
| CN201921743552.6U Active CN210852883U (en) | 2019-09-24 | 2019-10-17 | Four rotor unmanned aerial vehicle of collapsible arm |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921743552.6U Active CN210852883U (en) | 2019-09-24 | 2019-10-17 | Four rotor unmanned aerial vehicle of collapsible arm |
Country Status (1)
| Country | Link |
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| CN (2) | CN110606190A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113753229A (en) * | 2021-10-09 | 2021-12-07 | 吉林大学 | Foldable fixed-wing four-rotor composite unmanned aerial vehicle and control method thereof |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110606190A (en) * | 2019-09-24 | 2019-12-24 | 复旦大学 | Four rotor unmanned aerial vehicle of collapsible arm |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN205633049U (en) * | 2016-04-08 | 2016-10-12 | 四川克瑞斯航空科技有限公司 | Collapsible many rotor unmanned aerial vehicle of horn |
| CN205738051U (en) * | 2016-06-30 | 2016-11-30 | 北方天途航空技术发展（北京）有限公司 | Unmanned plane horn Kuai Zhe mechanism |
| CN205854486U (en) * | 2016-06-28 | 2017-01-04 | 赵一凡 | A kind of four collapsible unmanned planes of rotor |
| CN107416198A (en) * | 2017-07-20 | 2017-12-01 | 珠海磐磊智能科技有限公司 | Aircraft and its flying method |
| CN108116668A (en) * | 2017-11-24 | 2018-06-05 | 南京航空航天大学 | The land and air double-used more rotor manned aircraft of full electricity |
| CN207595251U (en) * | 2017-08-10 | 2018-07-10 | 昊翔电能运动科技(昆山)有限公司 | More duct unmanned vehicles |
| CN208085997U (en) * | 2018-03-20 | 2018-11-13 | 河北云奥电子科技有限公司 | The unmanned plane that a kind of horn is scalable, folds |
| US20190243385A1 (en) * | 2016-10-18 | 2019-08-08 | Deakin University | Thrust vectored multicopters |
| CN210852883U (en) * | 2019-09-24 | 2020-06-26 | 复旦大学 | Four rotor unmanned aerial vehicle of collapsible arm |
-
2019
- 2019-10-17 CN CN201910987971.2A patent/CN110606190A/en active Pending
- 2019-10-17 CN CN201921743552.6U patent/CN210852883U/en active Active
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN205633049U (en) * | 2016-04-08 | 2016-10-12 | 四川克瑞斯航空科技有限公司 | Collapsible many rotor unmanned aerial vehicle of horn |
| CN205854486U (en) * | 2016-06-28 | 2017-01-04 | 赵一凡 | A kind of four collapsible unmanned planes of rotor |
| CN205738051U (en) * | 2016-06-30 | 2016-11-30 | 北方天途航空技术发展（北京）有限公司 | Unmanned plane horn Kuai Zhe mechanism |
| US20190243385A1 (en) * | 2016-10-18 | 2019-08-08 | Deakin University | Thrust vectored multicopters |
| CN107416198A (en) * | 2017-07-20 | 2017-12-01 | 珠海磐磊智能科技有限公司 | Aircraft and its flying method |
| CN207595251U (en) * | 2017-08-10 | 2018-07-10 | 昊翔电能运动科技(昆山)有限公司 | More duct unmanned vehicles |
| CN108116668A (en) * | 2017-11-24 | 2018-06-05 | 南京航空航天大学 | The land and air double-used more rotor manned aircraft of full electricity |
| CN208085997U (en) * | 2018-03-20 | 2018-11-13 | 河北云奥电子科技有限公司 | The unmanned plane that a kind of horn is scalable, folds |
| CN210852883U (en) * | 2019-09-24 | 2020-06-26 | 复旦大学 | Four rotor unmanned aerial vehicle of collapsible arm |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113753229A (en) * | 2021-10-09 | 2021-12-07 | 吉林大学 | Foldable fixed-wing four-rotor composite unmanned aerial vehicle and control method thereof |
Also Published As
| Publication number | Publication date |
|---|---|
| CN210852883U (en) | 2020-06-26 |
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