CN107813953A - A kind of folding device for unmanned plane robot - Google Patents
A kind of folding device for unmanned plane robot Download PDFInfo
- Publication number
- CN107813953A CN107813953A CN201710941065.XA CN201710941065A CN107813953A CN 107813953 A CN107813953 A CN 107813953A CN 201710941065 A CN201710941065 A CN 201710941065A CN 107813953 A CN107813953 A CN 107813953A
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- China
- Prior art keywords
- fixed
- alignment pin
- rack
- protective cover
- hinged
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- 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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Links
- 230000001681 protective effect Effects 0.000 claims abstract description 23
- 208000020442 loss of weight Diseases 0.000 claims description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 6
- 229910052742 iron Inorganic materials 0.000 description 3
- 238000010521 absorption reaction Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000005381 potential energy Methods 0.000 description 2
- 238000003756 stirring Methods 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000003814 drug Substances 0.000 description 1
- 229940079593 drug Drugs 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
Classifications
-
- 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
- B64D47/00—Equipment not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Manipulator (AREA)
Abstract
The invention discloses a kind of folding device for unmanned plane robot, including upper junction plate and lower connecting plate, two upper connecting rods are hinged with the lower surface of the upper junction plate, it is hinged with two lower links on the upper surface of the lower connecting plate, one end of the lower link and upper connecting rod is hinged by jointed shaft respectively；Vertical rack is formed on the lower surface of upper junction plate between the upper connecting rod; vertical sheath body is formed on the upper surface of lower connecting plate between lower link; the side vertical inner wall of sheath body is provided with vertical electromagnet; one side wall of rack is provided with the vertical irony portion coordinated with the electromagnet; protective cover is formed on the outer wall of sheath body; gear in the protective cover provided with fulcrum and fixed sleeve in the middle part of the fulcrum; the both ends of fulcrum are fixed and are plugged with torsion spring, and one end of the torsion spring is fixed on the inwall of protective cover.The present invention is convenient to be folded, and realizes that the volume of support reduces, so as to convenience in transport.
Description
Technical field：
The present invention relates to the technical field of robot, is specifically related to a kind of folding device for unmanned plane robot.
Background technology：
The use range of unmanned plane has spread over military affairs, scientific research, civilian three big field at present, specifically electric power, communication,
Meteorology, agricultural, ocean, exploration, photograph, take precautions against natural calamities, enforcing the drug law, border patrol, the field such as public security anti-terrorism are widely used.Unmanned plane passes through
Carry sensor and realize the function such as image real-time Transmission and high-risk areas detection, be satellite remote sensing and traditional air remote sensing field
Powerful auxiliary equipment.The mode that sensor is carried on unmanned plane is usually to utilize mounting bracket thereon, but existing nothing
Mounting bracket on man-machine exist volume it is big, not foldable the shortcomings that, so as to cause transport inconvenience.
In view of it is above-mentioned the defects of, the design people, be actively subject to research and innovation, to found a kind of being used for for new structure
The folding device of unmanned plane robot, make it with more the value in industry.
The content of the invention：
The purpose of the present invention aims to solve the problem that the problem of prior art is present, there is provided the convenient body for folding, realizing support of one kind
Product reduces, so as to the folding device for unmanned plane robot of convenience in transport.
It is described the present invention relates to a kind of folding device for unmanned plane robot, including upper junction plate and lower connecting plate
Two upper connecting rods are hinged with the lower surface of upper junction plate, two lower links, institute are hinged with the upper surface of the lower connecting plate
It is hinged by jointed shaft respectively to state one end of lower link and upper connecting rod, upper connecting rod is fixed with upper positioning at jointed shaft
To sell, extension spring is fixed between the upper alignment pin of two upper connecting rods, lower link is fixed with lower alignment pin at jointed shaft,
Tension spring is fixed between the lower alignment pin of two lower links；
Form vertical rack on the lower surface of upper junction plate between the upper connecting rod, the lower connection between lower link
Vertical sheath body is formed on the upper surface of plate, the sheath body is relative with the rack, and the side vertical inner wall of sheath body is provided with
Vertical electromagnet, a side wall of rack are provided with the vertical irony portion coordinated with the electromagnet, on the outer wall of sheath body into
Type has protective cover, the gear of fulcrum and fixed sleeve in the middle part of the fulcrum is provided with the protective cover, the both ends of fulcrum are fixed
Torsion spring is plugged with, one end of the torsion spring is fixed on the inwall of protective cover, and fluting is formed on the housing sidewall in protective cover,
The gear is engaged with the fluting and rack.
By above-mentioned technical proposal, the present invention is when needing to fold, by upper junction plate and lower connecting plate mutually to pressure, then on
Connecting rod and lower link are mutually drawn close in the presence of jointed shaft, and upper extension spring and tension spring trail, and rack, which moves down, is plugged on sheath body
Interior, electromagnet, which is powered, adsorbs the iron portion on rack, realizes that rack is fixed in sheath body, completes to fold, can effectively reduce body
Product.Support after folding can also install sensor, when needing the height to support to be adjusted, need to only power off electromagnet
The absorption to rack is released, then stirs the gear in protective cover so that gear turns while being meshed through fluting with rack
It is dynamic to drive racks turn, so as to adjust the distance between upper junction plate and lower connecting plate, said gear with rack engagement rotation
When drive fulcrum, torsion spring fulcrum close to rack while drives torsion spring deformation storage elastic potential energy, works as support height
After the completion of regulation, electromagnet is powered adsorbs the fixed height so as to locating support by rack, then bleeds off gear, is resetted in torsion spring
Drive under, gear leaves rack and inverts reset.
By such scheme, the convenient body for folding, realizing support of the folding device for unmanned plane robot of the invention
Product reduces, so as to convenience in transport.
One kind as such scheme preferably, the upper alignment pin plugged and fixed at the middle part of upper connecting rod, upper alignment pin
Two opposing sidewalls that upper connecting rod is stretched out at both ends are simultaneously respectively fixed with extension spring, between two of upper alignment pin both ends upper extension springs into
Type has a upper gap, and for lower alignment pin plugged and fixed at the middle part of lower link, the both ends of lower alignment pin stretch out lower link two are relative
Side wall is simultaneously respectively fixed with tension spring, forms lower gap between two tension springs at lower alignment pin both ends, the rack can be worn
Cross the upper gap and lower gap.
Preferably, two upper connecting rods and two lower links are hinged on one kind as such scheme by hinged seat respectively
The lower surface of upper junction plate and the upper surface of lower connecting plate, the end of lower link form notch, and the end of upper connecting rod forms
Journal stirrup, the journal stirrup are plugged in the notch, the jointed shaft be plugged on journal stirrup and notch in.
One kind as such scheme preferably offers gathering hole in a side wall of the protective cover.
Preferably, the both ends of the fulcrum and the inwall of protective cover are spaced apart for one kind as such scheme.
As such scheme one kind preferably, if formed on the upper junction plate and lower connecting plate taper loss of weight mouth and
Dry mounting hole.
Described above is only the general introduction of technical solution of the present invention, in order to better understand the technological means of the present invention,
And can be practiced according to the content of specification, below with presently preferred embodiments of the present invention and coordinate accompanying drawing describe in detail as after.
Brief description of the drawings：
The following drawings is only intended to, in doing schematic illustration and explanation to the present invention, not delimit the scope of the invention.Wherein：
Fig. 1 is the structural representation of the present invention；
Fig. 2 is the partial sectional view of the present invention；
Fig. 3 is the cross section structure diagram of containment vessel in the present invention；
Fig. 4 is the structural representation of upper extension spring and tension spring in the present invention；
Fig. 5 is the structural representation of upper junction plate in the present invention.
Embodiment：
With reference to the accompanying drawings and examples, the embodiment of the present invention is described in further detail.Implement below
Example is used to illustrate the present invention, but is not limited to the scope of the present invention.
Referring to Fig. 1, Fig. 5, a kind of folding device for unmanned plane robot of the present invention, including upper junction plate 11
With lower connecting plate 12, taper loss of weight mouth 13 and some mounting holes 14 are formed on the upper junction plate 11 and lower connecting plate 12,
Two upper connecting rods 21 are hinged with the lower surface of upper junction plate 11, is hinged with two and connects on the upper surface of the lower connecting plate 12
One end of bar 22, the lower link 22 and upper connecting rod 21 is hinged by jointed shaft 23 respectively, and upper connecting rod 21 is close to be hinged
Alignment pin 31 is fixed with axle 23, extension spring 41, lower link are fixed between the upper alignment pin 31 of two upper connecting rods 21
22 are fixed with lower alignment pin 32 at jointed shaft 23, and tension spring is fixed between the lower alignment pin 32 of two lower links 22
42。
Referring to Fig. 4, the upper plugged and fixed of alignment pin 31 is stretched out at the middle part of upper connecting rod 21, the both ends of upper alignment pin 31
Two opposing sidewalls of connecting rod 21 are simultaneously respectively fixed with extension spring 41, are molded between two upper extension springs 41 at the upper both ends of alignment pin 31
There is upper gap 34, the lower plugged and fixed of alignment pin 32 stretches out lower link 22 at the middle part of lower link 22, the both ends of lower alignment pin 32
Two opposing sidewalls are simultaneously respectively fixed with tension spring 42, and lower gap is formed between two tension springs 42 at the lower both ends of alignment pin 32
43。
Referring to Fig. 1, two upper connecting rods 21 and two lower links 22 are hinged on upper junction plate by hinged seat 15 respectively
11 lower surface and the upper surface of lower connecting plate 12, the end of lower link 22 form notch 221, the end shaping of upper connecting rod 21
There is journal stirrup 211, the journal stirrup 211 is plugged in the notch 221, and the jointed shaft 23 is plugged on journal stirrup 211 and notch 221
It is interior.
Referring to Fig. 2 to Fig. 4, vertical rack 5 is formed on the lower surface of the upper junction plate 11 between the upper connecting rod 21,
The rack 5 may pass through the upper gap 34 and lower gap 43, is molded on the upper surface of the lower connecting plate 12 between lower link 22
There is vertical sheath body 6, the sheath body 6 is relative with the rack 5, and the side vertical inner wall of sheath body 6 is provided with vertical electromagnet
71, a side wall of rack 5 is provided with the vertical irony portion 72 coordinated with the electromagnet 71, is formed on the outer wall of sheath body 6
Protective cover 61, gathering hole 611 is offered in a side wall of the protective cover 61, fulcrum 7 and fixed sleeve are provided with protective cover 61
Gear 8 at the middle part of fulcrum 7, the both ends of fulcrum 7, which are fixed, is plugged with torsion spring 9, the both ends of fulcrum 7 and the inwall of protective cover 61
Spaced apart, one end of the torsion spring 9 is fixed on the inwall of protective cover 61, in the side wall of case 6 in protective cover 61 into
Type has fluting 62, and the gear 8 is engaged with the fluting 62 and rack 5.
The present invention is when needing to fold, by upper junction plate 11 and lower connecting plate 12 mutually to pressure, then upper connecting rod 21 and lower company
Bar 22 is mutually drawn close in the presence of jointed shaft 23, and upper extension spring 41 and tension spring 42 trail, and rack 5, which moves down, is plugged on sheath body 6
Interior, electromagnet 71, which is powered, adsorbs the iron portion 72 on rack 5, realizes that rack 5 is fixed in sheath body 6, completes to fold, can be effective
Reduce volume.Support after folding can also install sensor, when needing the height to support to be adjusted, only need to make electromagnetism
The power-off of iron 71 releases the absorption to rack 5, then stirs the gear 8 in protective cover 61 so that gear 8 passes through fluting 62 and rack
5 carry-over bars of rotational band while be meshed 5 rotate, above-mentioned so as to adjust the distance between upper junction plate 11 and lower connecting plate 12
Gear 8 drives fulcrum 7 to rotate when with 5 engagement rotation of rack, torsion spring 9 to rack 5 close to while fulcrum 7 drive torsion spring 9
Deformation storage elastic potential energy, after the completion of support height regulation, electromagnet 71 is powered to adsorbing rack 5 and fixed so as to locating support
Height, then bleed off gear 8, torsion spring 9 reset drive under, gear 8 leaves rack 5 and inverts reset.
In summary, the folding device for unmanned plane robot of the invention is convenient folds, and realizes that the volume of support subtracts
It is small, so as to convenience in transport.
Folding device provided by the present invention for unmanned plane robot, it is only the embodiment of the present invention, but
Protection scope of the present invention is not limited thereto, any one skilled in the art the invention discloses technology model
In enclosing, change or replacement can be readily occurred in, should all be covered within the scope of the present invention.Therefore, protection scope of the present invention
It should be based on the protection scope of the described claims.
Claims (6)
- A kind of 1. folding device for unmanned plane robot, it is characterised in that：Including upper junction plate (11) and lower connecting plate (12), two upper connecting rods are hinged with the lower surface of the upper junction plate (11) (21), it is hinged with two lower links (22) on the upper surface of the lower connecting plate (12), the lower link and upper connecting rod (21) One end is hinged by jointed shaft (23) respectively, and upper connecting rod (21) is fixed with alignment pin close to jointed shaft (23) place (31) extension spring (41), is fixed between the upper alignment pin (31) of two upper connecting rods (21), lower link (22) is close to be hinged Axle (23) place is fixed with lower alignment pin (32), and tension spring is fixed between the lower alignment pin (32) of two lower links (22) (42)；Vertical rack (5), lower link (22) are formed on the lower surface of upper junction plate (11) between the upper connecting rod (21) Between lower connecting plate (12) upper surface on form vertical sheath body (6), the sheath body with the rack (5) relatively, set The side vertical inner wall of shell (6) is provided with vertical electromagnet (71), and a side wall of rack (5) is provided with and the electromagnet (71) the vertical irony portion (72) coordinated, protective cover (61) is formed on the outer wall of sheath body (6), branch is provided with the protective cover The gear (8) of axle (7) and fixed sleeve in the middle part of the fulcrum, the both ends of fulcrum (7), which are fixed, is plugged with torsion spring (9), the torsion One end of spring is fixed on the inwall of protective cover (61), and fluting (62), the tooth are formed in case (6) side wall in protective cover Wheel (8) is engaged with the fluting (62) and rack (5).
- 2. the folding device according to claim 1 for unmanned plane robot, it is characterised in that：The upper alignment pin (31) for plugged and fixed at the middle part of upper connecting rod (21), two opposing sidewalls of upper connecting rod (21) are stretched out at the both ends of upper alignment pin (31) And extension spring (41) is respectively fixed with, gap (34) is formed between extension spring on two (41) at upper alignment pin (31) both ends, For lower alignment pin (32) plugged and fixed at the middle part of lower link (22), the both ends of lower alignment pin (32) stretch out two of lower link (22) Opposing sidewalls are simultaneously respectively fixed with tension spring (42), between being formed down between two tension springs (42) at lower alignment pin (32) both ends Gap (43), the rack (5) may pass through the upper gap (34) and lower gap (43).
- 3. the folding device according to claim 1 for unmanned plane robot, it is characterised in that：Two upper connecting rods (21) and two lower links (22) are hinged on lower surface and the lower connecting plate of upper junction plate (11) by hinged seat (15) respectively (12) upper surface, the end of lower link (22) form notch (221), and the end of upper connecting rod (21) forms journal stirrup (211), The journal stirrup is plugged in the notch (221), and the jointed shaft (23) is plugged on journal stirrup (211) and notch (221) is interior.
- 4. the folding device according to claim 1 for unmanned plane robot, it is characterised in that：The protective cover (61) A side wall on offer gathering hole (611).
- 5. the folding device according to claim 1 for unmanned plane robot, it is characterised in that：The fulcrum (7) The inwall at both ends and protective cover (61) is spaced apart.
- 6. the folding device according to claim 1 for unmanned plane robot, it is characterised in that：The upper junction plate (11) taper loss of weight mouth (13) and some mounting holes (14) and on lower connecting plate (12) are formed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710941065.XA CN107813953B (en) | 2017-10-11 | 2017-10-11 | A kind of folding device for unmanned plane robot |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710941065.XA CN107813953B (en) | 2017-10-11 | 2017-10-11 | A kind of folding device for unmanned plane robot |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107813953A true CN107813953A (en) | 2018-03-20 |
| CN107813953B CN107813953B (en) | 2019-10-15 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710941065.XA Active CN107813953B (en) | 2017-10-11 | 2017-10-11 | A kind of folding device for unmanned plane robot |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107813953B (en) |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204802081U (en) * | 2015-06-11 | 2015-11-25 | 邓钰朗 | Miniature aircraft of taking photo by plane |
| WO2017069320A1 (en) * | 2015-10-19 | 2017-04-27 | 한국항공우주연구원 | Free-fall type aerial photographing device using free rotation of helicopter |
| CN106741911A (en) * | 2016-12-30 | 2017-05-31 | 歌尔股份有限公司 | Robot unmanned plane |
-
2017
- 2017-10-11 CN CN201710941065.XA patent/CN107813953B/en active Active
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204802081U (en) * | 2015-06-11 | 2015-11-25 | 邓钰朗 | Miniature aircraft of taking photo by plane |
| WO2017069320A1 (en) * | 2015-10-19 | 2017-04-27 | 한국항공우주연구원 | Free-fall type aerial photographing device using free rotation of helicopter |
| CN106741911A (en) * | 2016-12-30 | 2017-05-31 | 歌尔股份有限公司 | Robot unmanned plane |
Also Published As
| Publication number | Publication date |
|---|---|
| CN107813953B (en) | 2019-10-15 |
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| TA01 | Transfer of patent application right | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20190918 Address after: 318050, Feng Jiang Road, Luqiao District, Zhejiang, Taizhou, No. 316 Applicant after: Xu Xian Fu Address before: 523000 Guangdong province Dongguan City Songshan Lake high tech Industrial Zone Building 406 industrial development productivity Applicant before: Dongguan Lianzhou Intellectual Property Operation Management Co.,Ltd. |
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