CN112550690A - Unmanned aerial vehicle driving system protector - Google Patents
Unmanned aerial vehicle driving system protector Download PDFInfo
- Publication number
- CN112550690A CN112550690A CN202011428220.6A CN202011428220A CN112550690A CN 112550690 A CN112550690 A CN 112550690A CN 202011428220 A CN202011428220 A CN 202011428220A CN 112550690 A CN112550690 A CN 112550690A
- Authority
- CN
- China
- Prior art keywords
- sliding sleeve
- unmanned aerial
- aerial vehicle
- buckle
- sliding
- 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
- 230000001012 protector Effects 0.000 title description 3
- 238000003780 insertion Methods 0.000 claims abstract description 4
- 230000037431 insertion Effects 0.000 claims abstract description 4
- 238000000926 separation method Methods 0.000 claims abstract description 4
- 230000005489 elastic deformation Effects 0.000 claims description 9
- 229910000838 Al alloy Inorganic materials 0.000 claims description 3
- 238000003197 gene knockdown Methods 0.000 abstract description 2
- 230000007547 defect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
Images
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
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
-
- 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)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Vibration Dampers (AREA)
Abstract
The invention discloses a protection device for an unmanned aerial vehicle power system, which comprises a sliding sleeve, a sliding sheet, a buckle and a fixed rod, wherein the sliding sleeve is fixedly connected with the sliding sheet; the buckle comprises a buckle head and a buckle groove which can realize assembly and separation by utilizing insertion fit; the sliding sleeve is an arc hollow strip panel, one end of the sliding sleeve is open, and the other end of the sliding sleeve is closed; one end of the fixed rod is fixedly connected with the inner wall of the sliding sleeve, and the other end of the fixed rod is fixedly connected with the arm of the unmanned aerial vehicle; the sliding sheet is an arc strip sheet plate, is arranged in the sliding sleeve, and one end of the sliding sheet extends out of the opening end of the sliding sleeve and can freely slide relative to the sliding sleeve; the catching groove with the blind end of sliding sleeve links firmly, and the discount links firmly with the gleitbretter one end of keeping away from the sliding sleeve blind end. The invention can be arranged on each arm of the unmanned aerial vehicle to protect each propeller of the unmanned aerial vehicle, and the problem of crash caused by the fact that blades of the unmanned aerial vehicle knock down branches is prevented.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to a protection device for a power system of an unmanned aerial vehicle.
Background
An unmanned plane is an unmanned plane which is operated by radio remote control equipment and a self-contained program control device, or is completely or intermittently and autonomously operated by a vehicle-mounted computer, and can be divided into military, civil and civil aspects according to the application field.
The great comprehensive guard shield of quality is generally not add to the propeller to current unmanned aerial vehicle, all can have trees all around when flying, and the paddle of the unmanned aerial vehicle that then has is when the flight is rotatory, because traditional paddle does not have protector, when unmanned aerial vehicle's paddle fell the branch, the branch can injure or damage unmanned aerial vehicle's paddle to make unmanned aerial vehicle have the hidden danger of crash.
Disclosure of Invention
The invention aims to solve the technical problem of providing a protection device for an unmanned aerial vehicle power system aiming at the defects related in the background technology.
The invention adopts the following technical scheme for solving the technical problems:
a protection device for an unmanned aerial vehicle power system comprises a sliding sleeve, a sliding sheet, a buckle and a fixed rod;
the buckle comprises a buckle head and a buckle groove which can realize assembly and separation by utilizing insertion fit; the buckle head is provided with an elastic deformation part and can be inserted into the buckle groove by utilizing the elastic deformation of the elastic deformation part;
the sliding sleeve is an arc hollow strip panel, one end of the sliding sleeve is open, and the other end of the sliding sleeve is closed;
one end of the fixed rod is fixedly connected with the inner wall of the sliding sleeve, and the other end of the fixed rod is fixedly connected with the arm of the unmanned aerial vehicle, so that the sliding sleeve is sleeved outside a propeller at the tail end of the arm of the unmanned aerial vehicle;
the sliding piece is an arc strip-shaped piece plate, is arranged in the sliding sleeve, and one end of the sliding piece extends out of the opening end of the sliding sleeve and can freely slide relative to the sliding sleeve;
the buckle groove is fixedly connected with the closed end of the sliding sleeve, and the buckle head is fixedly connected with one end of the sliding sheet far away from the closed end of the sliding sleeve; when gleitbretter roll-off sliding sleeve made discount and catching groove link to each other, sliding sleeve, gleitbretter, discount, catching groove formed and centers on the ring guard flap at its center with unmanned aerial vehicle horn end screw.
As a further optimization scheme of the unmanned aerial vehicle power system protection device, the sliding sleeve, the sliding sheet, the buckle and the fixed rod are made of aluminum alloy, and the unmanned aerial vehicle power system protection device is firm and light.
Compared with the prior art, the invention adopting the technical scheme has the following technical effects:
the invention can be arranged on each arm of the unmanned aerial vehicle to protect each propeller of the unmanned aerial vehicle, and the problem of crash caused by the fact that blades of the unmanned aerial vehicle knock down branches is prevented.
Drawings
FIG. 1 is a schematic view of the present invention with the fixing rod removed;
FIG. 2 is a schematic view of the present invention mounted on a boom of an unmanned aerial vehicle;
fig. 3 is a schematic structural view of the quad-rotor drone of the present invention.
In the figure, 1-sliding sleeve, 2-sliding sheet, 3-buckle slot of buckle, 4-buckle head of buckle, 5-fixed rod, 6-unmanned aerial vehicle arm.
Detailed Description
The technical scheme of the invention is further explained in detail by combining the attached drawings:
the present invention may be embodied in many different forms and should not be construed as limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the scope of the invention to those skilled in the art. In the drawings, components are exaggerated for clarity.
As shown in fig. 1 and 2, the invention discloses a protection device for an unmanned aerial vehicle power system, which comprises a sliding sleeve, a sliding sheet, a buckle and a fixed rod;
the buckle comprises a buckle head and a buckle groove which can realize assembly and separation by utilizing insertion fit; the buckle head is provided with an elastic deformation part and can be inserted into the buckle groove by utilizing the elastic deformation of the elastic deformation part;
the sliding sleeve is an arc hollow strip panel, one end of the sliding sleeve is open, and the other end of the sliding sleeve is closed;
one end of the fixed rod is fixedly connected with the inner wall of the sliding sleeve, and the other end of the fixed rod is fixedly connected with the arm of the unmanned aerial vehicle, so that the sliding sleeve is sleeved outside a propeller at the tail end of the arm of the unmanned aerial vehicle;
the sliding piece is an arc strip-shaped piece plate, is arranged in the sliding sleeve, and one end of the sliding piece extends out of the opening end of the sliding sleeve and can freely slide relative to the sliding sleeve;
the buckle groove is fixedly connected with the closed end of the sliding sleeve, and the buckle head is fixedly connected with one end of the sliding sheet far away from the closed end of the sliding sleeve; when gleitbretter roll-off sliding sleeve made discount and catching groove link to each other, sliding sleeve, gleitbretter, discount, catching groove formed and centers on the ring guard flap at its center with unmanned aerial vehicle horn end screw.
The sliding sleeve, the sliding sheet, the buckle and the fixed rod are all made of aluminum alloy, and are firm and light.
As shown in fig. 3, the propeller protection device can be arranged on each arm of the unmanned aerial vehicle to protect each propeller of the unmanned aerial vehicle, so that the problem of crash caused by the fact that blades of the unmanned aerial vehicle collide with branches is solved.
It will be understood by those skilled in the art that, unless otherwise defined, all terms (including technical and scientific terms) used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. It will be further understood that terms, such as those defined in commonly used dictionaries, should be interpreted as having a meaning that is consistent with their meaning in the context of the prior art and will not be interpreted in an idealized or overly formal sense unless expressly so defined herein.
The above-mentioned embodiments, objects, technical solutions and advantages of the present invention are further described in detail, it should be understood that the above-mentioned embodiments are only illustrative of the present invention and are not intended to limit the present invention, and any modifications, equivalents, improvements and the like made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (2)
1. A protection device for an unmanned aerial vehicle power system is characterized by comprising a sliding sleeve, a sliding sheet, a buckle and a fixed rod;
the buckle comprises a buckle head and a buckle groove which can realize assembly and separation by utilizing insertion fit; the buckle head is provided with an elastic deformation part and can be inserted into the buckle groove by utilizing the elastic deformation of the elastic deformation part;
the sliding sleeve is an arc hollow strip panel, one end of the sliding sleeve is open, and the other end of the sliding sleeve is closed;
one end of the fixed rod is fixedly connected with the inner wall of the sliding sleeve, and the other end of the fixed rod is fixedly connected with the arm of the unmanned aerial vehicle, so that the sliding sleeve is sleeved outside a propeller at the tail end of the arm of the unmanned aerial vehicle;
the sliding piece is an arc strip-shaped piece plate, is arranged in the sliding sleeve, and one end of the sliding piece extends out of the opening end of the sliding sleeve and can freely slide relative to the sliding sleeve;
the buckle groove is fixedly connected with the closed end of the sliding sleeve, and the buckle head is fixedly connected with one end of the sliding sheet far away from the closed end of the sliding sleeve; when gleitbretter roll-off sliding sleeve made discount and catching groove link to each other, sliding sleeve, gleitbretter, discount, catching groove formed and centers on the ring guard flap at its center with unmanned aerial vehicle horn end screw.
2. The unmanned aerial vehicle power system protection device of claim 1, wherein the sliding sleeve, sliding piece, buckle, and fixing rod are made of aluminum alloy.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011428220.6A CN112550690A (en) | 2020-12-07 | 2020-12-07 | Unmanned aerial vehicle driving system protector |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011428220.6A CN112550690A (en) | 2020-12-07 | 2020-12-07 | Unmanned aerial vehicle driving system protector |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN112550690A true CN112550690A (en) | 2021-03-26 |
Family
ID=75060726
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202011428220.6A Pending CN112550690A (en) | 2020-12-07 | 2020-12-07 | Unmanned aerial vehicle driving system protector |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN112550690A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104986331A (en) * | 2015-07-27 | 2015-10-21 | 致导科技（北京）有限公司 | Unmanned aerial vehicle rotor wing protection frame and unmanned aerial vehicle |
| KR20160098807A (en) * | 2015-02-11 | 2016-08-19 | 금오공과대학교 산학협력단 | A drone having high accessibility |
| CN205525010U (en) * | 2016-03-07 | 2016-08-31 | 李霞林 | Unmanned aerial vehicle frame with wing protect function |
| CN106218895A (en) * | 2015-05-12 | 2016-12-14 | 空中客车运营简化股份公司 | It is furnished with the lane device of the interregional independent activities wall body that can connect safely of at least two making housing |
| CN207433796U (en) * | 2017-11-23 | 2018-06-01 | 宜昌兴邦无人机科技有限公司 | A kind of unmanned plane with rotor protective device |
| CN108248820A (en) * | 2016-12-28 | 2018-07-06 | 昊翔电能运动科技(昆山)有限公司 | A kind of split type foldable machine paddle fender bracket and its application method |
-
2020
- 2020-12-07 CN CN202011428220.6A patent/CN112550690A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20160098807A (en) * | 2015-02-11 | 2016-08-19 | 금오공과대학교 산학협력단 | A drone having high accessibility |
| CN106218895A (en) * | 2015-05-12 | 2016-12-14 | 空中客车运营简化股份公司 | It is furnished with the lane device of the interregional independent activities wall body that can connect safely of at least two making housing |
| CN104986331A (en) * | 2015-07-27 | 2015-10-21 | 致导科技（北京）有限公司 | Unmanned aerial vehicle rotor wing protection frame and unmanned aerial vehicle |
| CN205525010U (en) * | 2016-03-07 | 2016-08-31 | 李霞林 | Unmanned aerial vehicle frame with wing protect function |
| CN108248820A (en) * | 2016-12-28 | 2018-07-06 | 昊翔电能运动科技(昆山)有限公司 | A kind of split type foldable machine paddle fender bracket and its application method |
| CN207433796U (en) * | 2017-11-23 | 2018-06-01 | 宜昌兴邦无人机科技有限公司 | A kind of unmanned plane with rotor protective device |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN205418138U (en) | Triaxial optoelectronic pod | |
| KR101773674B1 (en) | Structure for inserting and removal battery and drone including the same | |
| GB0106990D0 (en) | A system for airborne launch of an aircraft from a larger carrier aircraft | |
| KR101822386B1 (en) | Wireless charging system of drone | |
| CN112550690A (en) | Unmanned aerial vehicle driving system protector | |
| CN105856248A (en) | Low-detectability air-defense robot | |
| WO2021056925A1 (en) | Unmanned aircraft for automatically intercepting and capturing unmanned aerial vehicle | |
| CN207292417U (en) | One kind is easy to clean type unmanned plane propeller | |
| CN110553548A (en) | anti-unmanned aerial vehicle system based on fixed wing platform | |
| CN213008741U (en) | Unmanned aerial vehicle shock attenuation protector for surveying and mapping is photographic | |
| CN104309806A (en) | Cruise missile carrier vehicle | |
| CN205499331U (en) | For military use unmanned vehicles of portable connection wing | |
| CN200945932Y (en) | Solar energy folding type bird-shaped flying screen | |
| CN220577527U (en) | Unmanned aerial vehicle screw safety cover | |
| CN207417153U (en) | It is a kind of can anticollision Intelligent unattended machine | |
| CN215155762U (en) | Back-emitting fulcrum structure of retractable unmanned aerial vehicle body | |
| CN205345313U (en) | Unmanned aerial vehicle | |
| CN214824132U (en) | A unmanned aerial vehicle for forest is put out a fire | |
| CN220662887U (en) | Unmanned aerial vehicle is with defending device | |
| CN111688945A (en) | Unmanned aerial vehicle strutting arrangement | |
| CN218858715U (en) | Anti-interference unmanned aerial vehicle structure assembly of integral type | |
| CN205589525U (en) | Be used for wireless broadcast unmanned aerial vehicle | |
| CN216509005U (en) | Combined type opening cover suitable for assembling and disassembling special-shaped antenna | |
| CN213384700U (en) | Model airplane protector | |
| CN205345334U (en) | Unmanned aerial vehicle rotor |
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 | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20210326 |
|
| WD01 | Invention patent application deemed withdrawn after publication |