CN208102347U - A kind of unmanned plane to be charged using high-voltage line - Google Patents
A kind of unmanned plane to be charged using high-voltage line Download PDFInfo
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- CN208102347U CN208102347U CN201820374123.5U CN201820374123U CN208102347U CN 208102347 U CN208102347 U CN 208102347U CN 201820374123 U CN201820374123 U CN 201820374123U CN 208102347 U CN208102347 U CN 208102347U
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- 210000001699 lower leg Anatomy 0.000 claims abstract description 13
- 230000005540 biological transmission Effects 0.000 claims abstract description 11
- 239000000523 sample Substances 0.000 claims abstract description 10
- 238000003466 welding Methods 0.000 claims description 9
- 238000003780 insertion Methods 0.000 claims description 8
- 230000037431 insertion Effects 0.000 claims description 8
- 230000006698 induction Effects 0.000 abstract description 3
- 238000000034 method Methods 0.000 description 4
- 238000007689 inspection Methods 0.000 description 3
- 229910000838 Al alloy Inorganic materials 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 239000010949 copper Substances 0.000 description 2
- 238000005520 cutting process Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 244000309464 bull Species 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
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Abstract
The utility model discloses a kind of unmanned planes to be charged using high-voltage line,Its structure includes fuselage,Right flank,Right-hand screw paddle,Right connecting rod,Fixed block,Right crus of diaphragm frame,Fixing sleeve,Left foot frame,Transmission pole,Positive terminal,Vertical bar,Negative terminal,Left-hand airscrew,Left connecting rod,Left wing,The lower surface of fuselage and the upper surface of fixed block are bonding,A kind of unmanned plane to be charged using high-voltage line of the utility model,Control right-hand screw paddle and left-hand airscrew rotation,Increase unmanned plane,Positive terminal and negative terminal contact the function of reaching charging with high-voltage line,Unmanned plane after taking off,Probe induction ground is at a distance from unmanned plane,Range sensor control motor powers on,Motor drives shaft rotation,Shaft drives left gear and right gear to rotate by lower gear,Left gear and right gear pass through left-hand rotation bar and right-hand rotation bar drive left-hand airscrew and the rotation of right-hand screw paddle,The draw-in and draw-off function of foot prop is preferable,Foot prop is not easy to be wound into high-voltage line,Practicability is higher.
Description
Technical field
The utility model is a kind of unmanned plane to be charged using high-voltage line, belongs to power patrol unmanned machine field.
Background technique
In recent years, with the high speed development of China's power grid construction, electric inspection process is converted to machine by manual inspection step by step
Inspection.
Prior art discloses application No. is：201720566791.3 it is a kind of using high-voltage line charging unmanned plane include
Drone body, the battery compartment inside drone body, and the undercarriage below drone body, it is described to rise and fall
Frame includes two stocks being parallel to each other, and stock side wall is equipped with insulated connecting rod, the end and unmanned plane bottom surface two of insulated connecting rod
Side is connected, but the draw-in and draw-off function of the prior art foot prop is poor, causes foot prop to be easy to be wound into high-voltage line, falls unmanned plane
Fall behind damage, practicability is lower.
Utility model content
In view of the deficienciess of the prior art, the utility model aim be to provide it is a kind of using high-voltage line charging nobody
Machine, it is poor with the draw-in and draw-off function for solving prior art foot prop, cause foot prop to be easy to be wound into high-voltage line, is damaged after falling unmanned plane
It is bad, the lower problem of practicability.
To achieve the goals above, the utility model is to realize by the following technical solutions：It is a kind of to utilize high-voltage line
The unmanned plane of charging, structure include fuselage, right flank, right-hand screw paddle, right connecting rod, fixed block, right crus of diaphragm frame, fixing sleeve, left foot
Frame, transmission pole, positive terminal, vertical bar, negative terminal, left-hand airscrew, left connecting rod, left wing, the lower surface of the fuselage and solid
The upper surface for determining block is bonding, and the left surface of the right flank is mutually welded with the outer surface of fuselage, the outer surface of the right-hand screw paddle
It is connected with right connecting rod front, the right surface of the right flank is installed on the outer surface of right connecting rod and uses vertical welding,
The right crus of diaphragm frame insertion is installed on the right surface of fixed block and is gap-matched, and the outer surface of the fixing sleeve is installed on solid
Determine the inner surface of block and be gap-matched, the left foot frame insertion is installed on the left surface of fixed block and is matched using gap
It closes, the inner surface of the fixing sleeve and the outer surface of transmission pole fit, the left surface of the transmission pole and the outer surface of vertical bar
Vertical welding, the outer surface of the vertical bar are installed on the inner surface of negative terminal and are gap-matched, the left-hand airscrew
Outer surface and the front of left connecting rod mutually weld, the outer surface of the fuselage is connected with the right surface of left wing, the fixation
Block includes shell, range sensor, left gear, probe, fixed frame, right gear, right-hand rotation bar, shaft, motor, lower gear, left-hand rotation
Bar, bearing, the outer surface of the bearing are installed on the inner surface of shell and are gap-matched, outside the range sensor
The inner surface of surface and fixed frame fits, and the lower surface of the left gear is meshed with the left surface of lower gear, the distance
Sensor is electrically connected with probe, and the inner surface of the right gear is installed on the outer surface of right-hand rotation bar and is gap-matched, institute
Shaft insertion is stated to be installed on the upper surface of motor and be gap-matched, the outer surface of the left-hand rotation bar and the inner surface of bearing
It fits.
Further, the outer surface of the left connecting rod is installed on the left surface of left wing and using vertical welding.
Further, the inner surface of the positive terminal is installed on the outer surface of vertical bar and is gap-matched.
Further, the right crus of diaphragm frame insertion is installed on the right surface of shell and is gap-matched.
Further, the right connecting rod is the cylindrical structure of diameter 2CM, high 20CM.
Further, the positive terminal uses copper material, and resistance is smaller, reduces electrical loss.
Further, the right crus of diaphragm frame uses aluminum alloy material, and hardness is higher, is unlikely to deform.
Beneficial effect
A kind of unmanned plane to be charged using high-voltage line of the utility model, is controlled right-hand screw paddle and left-hand airscrew rotation, makes nothing
Man-machine rising, positive terminal and negative terminal contact the function of reaching charging, the unmanned plane after taking off, probe induction with high-voltage line
Ground is at a distance from unmanned plane, and range sensor control motor powers on, and motor drives shaft rotation, and shaft passes through lower gear
Left gear and right gear rotation are driven, left gear and right gear pass through left-hand rotation bar and right-hand rotation bar drive left-hand airscrew and right-hand screw paddle
The draw-in and draw-off function of rotation, foot prop is preferable, and foot prop is not easy to be wound into high-voltage line, and practicability is higher.
Detailed description of the invention
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other spies of the utility model
Sign, objects and advantages will become more apparent upon：
Fig. 1 is a kind of structural schematic diagram of the unmanned plane using high-voltage line charging of the utility model；
Fig. 2 is the schematic diagram of the section structure of the utility model fixed block.
In figure：Fuselage -1, right flank -2, right-hand screw paddle -3, right connecting rod -4, fixed block -5, right crus of diaphragm frame -6, fixing sleeve -7,
Left foot frame -8, transmission pole -9, positive terminal -10, vertical bar -11, negative terminal -12, left-hand airscrew -13, left connecting rod -14, a left side
The wing -15, range sensor -502, left gear -503, probe -504, fixed frame -505, right gear -506, is turned right at shell -501
Bar -507, shaft -508, motor -509, lower gear -510, left-hand rotation bar -511, bearing -512.
Specific embodiment
To be easy to understand the technical means, creative features, achievement of purpose, and effectiveness of the utility model, below
In conjunction with specific embodiment, the utility model is further described.
Fig. 1, Fig. 2 are please referred to, the utility model provides a kind of unmanned air vehicle technique scheme to charge using high-voltage line：Its structure
Including fuselage 1, right flank 2, right-hand screw paddle 3, right connecting rod 4, fixed block 5, right crus of diaphragm frame 6, fixing sleeve 7, left foot frame 8, transmission pole 9,
Positive terminal 10, vertical bar 11, negative terminal 12, left-hand airscrew 13, left connecting rod 14, left wing 15, the lower surface of the fuselage 1 with
The upper surface of fixed block 5 is bonding, and the left surface of the right flank 2 is mutually welded with the outer surface of fuselage 1, the right-hand screw paddle 3
Outer surface is connected with right 4 front of connecting rod, and the right surface of the right flank 2 is installed on the outer surface of right connecting rod 4 and use
Vertical welding, the right crus of diaphragm frame 6 is embedded in the right surface for being installed on fixed block 5 and is gap-matched, outside the fixing sleeve 7
Surface is installed on the inner surface of fixed block 5 and is gap-matched, and the left foot frame 8 is embedded in the left-handed watch for being installed on fixed block 5
It face and is gap-matched, the outer surface of the inner surface and transmission pole 9 of the fixing sleeve 7 fits, a left side for the transmission pole 9
The outer surface vertical welding on surface and vertical bar 11, the outer surface of the vertical bar 11 are installed on the inner surface of negative terminal 12 and adopt
With clearance fit, the front of the outer surface of the left-hand airscrew 13 and left connecting rod 14 is mutually welded, the outer surface of the fuselage 1 with
The right surface of left wing 15 is connected, the fixed block 5 include shell 501, range sensor 502, left gear 503, probe 504,
Fixed frame 505, right gear 506, right-hand rotation bar 507, shaft 508, motor 509, lower gear 510, left-hand rotation bar 511, bearing 512, institute
The outer surface for stating bearing 512 is installed on the inner surface of shell 501 and is gap-matched, outside the range sensor 502
Surface and the inner surface of fixed frame 505 fit, and the lower surface of the left gear 503 is meshed with the left surface of lower gear 510,
The range sensor 502 is electrically connected with probe 504, and the inner surface of the right gear 506 is installed on the outer surface of right-hand rotation bar 507
And it is gap-matched, the shaft 508 is embedded in the upper surface for being installed on motor 509 and is gap-matched, the left side
The outer surface of bull stick 511 and the inner surface of bearing 512 fit, and the outer surface of the left connecting rod 14 is installed on a left side for left wing 15
Surface and vertical welding is used, the inner surface of the positive terminal 10 is installed on the outer surface of vertical bar 11 and is matched using gap
It closes, the right crus of diaphragm frame 6 is embedded in the right surface for being installed on shell 501 and is gap-matched, and the right connecting rod 4 is diameter
The cylindrical structure of 2CM, high 20CM, the positive terminal 10 use copper material, and resistance is smaller, reduce electrical loss, the right crus of diaphragm
Frame 6 uses aluminum alloy material, and hardness is higher, is unlikely to deform.
Left gear 503 described in this patent refers to the machinery member for having gear continuously to engage passing movement and power on wheel rim
Part, there have been transform into the principle of cutting method and the special purpose machine tool using this principle cutting very early for application of the gear in transmission
With the successive appearance of cutter, with the development of production, the stationarity of gear operation is taken seriously, and the shaft 508 is as its name suggests
Be connect zero main part of product must use, for moment of flexure had not only been born in rotation work again receiving torque axis.
Carry out using when control right-hand screw paddle 3 and left-hand airscrew 13 rotate, increase unmanned plane, positive terminal 10 and negative
Extreme son 12 contact the function of reaching charging with high-voltage line, the unmanned plane after taking off, pop one's head in 504 incude ground and unmanned plane away from
From range sensor 502 controls motor 509 and powers on, and motor 509 drives shaft 508 to rotate, and shaft 508 passes through lower gear
510 drive left gear 503 and right gear 506 to rotate, and left gear 503 and right gear 506 pass through left-hand rotation bar 511 and right-hand rotation bar 507
Left-hand airscrew 13 and right-hand screw paddle 3 is driven to rotate.
The draw-in and draw-off function that the utility model solves prior art foot prop is poor, and foot prop is caused to be easy to be wound into high-voltage line,
It is damaged after falling unmanned plane, the lower problem of practicability, the utility model is combined with each other by above-mentioned component, this is practical new
A kind of unmanned plane to be charged using high-voltage line of type, is controlled right-hand screw paddle and left-hand airscrew rotation, increase unmanned plane, positive terminal
Contact the function of reaching charging with high-voltage line with negative terminal, the unmanned plane after taking off, probe induction ground and unmanned plane away from
From range sensor control motor powers on, and motor drives shaft rotation, and shaft drives left gear and right tooth by lower gear
Wheel rotation, left gear and right gear drive left-hand airscrew and the rotation of right-hand screw paddle by left-hand rotation bar and right-hand rotation bar, foot prop
Draw-in and draw-off function is preferable, and foot prop is not easy to be wound into high-voltage line, and practicability is higher.
The basic principles and main features of the present invention and the advantages of the present invention have been shown and described above, for
For those skilled in the art, it is clear that the present invention is not limited to the details of the above exemplary embodiments, and without departing substantially from this
In the case where the spirit or essential attributes of utility model, the utility model can be realized in other specific forms.Therefore, no matter
From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the utility model is by institute
Attached claim rather than above description limit, it is intended that will fall within the meaning and scope of the equivalent elements of the claims
All changes are embraced therein.It should not treat any reference in the claims as limiting related right
It is required that.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should
It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
The other embodiments being understood that.
Claims (5)
1. a kind of unmanned plane to be charged using high-voltage line, it is characterised in that：Its structure includes fuselage (1), right flank (2), right-hand screw
Paddle (3), right connecting rod (4), fixed block (5), right crus of diaphragm frame (6), fixing sleeve (7), left foot frame (8), transmission pole (9), positive terminal
(10), vertical bar (11), negative terminal (12), left-hand airscrew (13), left connecting rod (14), left wing (15), under the fuselage (1)
The upper surface on surface and fixed block (5) is bonding, and the left surface of the right flank (2) and the outer surface of fuselage (1) are mutually welded, described
The outer surface of right-hand screw paddle (3) is connected with right connecting rod (4) front, and the right surface of the right flank (2) is installed on right connecting rod
(4) outer surface and vertical welding is used, right crus of diaphragm frame (6) insertion is installed on the right surface of fixed block (5) and uses
Clearance fit, the outer surface of the fixing sleeve (7) are installed on the inner surface of fixed block (5) and are gap-matched, the left side
Foot prop (8) insertion is installed on the left surface of fixed block (5) and is gap-matched, the inner surface and biography of the fixing sleeve (7)
The outer surface of defeated bar (9) fits, the left surface of the transmission pole (9) and the outer surface vertical welding of vertical bar (11), described perpendicular
The outer surface of bar (11) is installed on the inner surface of negative terminal (12) and is gap-matched, outside the left-hand airscrew (13)
Surface and the front of left connecting rod (14) are mutually welded, and the outer surface of the fuselage (1) is connected with the right surface of left wing (15), institute
Stating fixed block (5) includes shell (501), range sensor (502), left gear (503), probe (504), fixed frame (505), the right side
Gear (506), right-hand rotation bar (507), shaft (508), motor (509), lower gear (510), left-hand rotation bar (511), bearing (512),
The outer surface of the bearing (512) is installed on the inner surface of shell (501) and is gap-matched, the range sensor
(502) inner surface of outer surface and fixed frame (505) fits, the lower surface and lower gear (510) of the left gear (503)
Left surface be meshed, the range sensor (502) be electrically connected with probe (504), and the inner surface of the right gear (506) is pacified
It outer surface loaded on right-hand rotation bar (507) and is gap-matched, shaft (508) insertion is installed on the upper of motor (509)
It surface and is gap-matched, the outer surface of the left-hand rotation bar (511) and the inner surface of bearing (512) fit.
2. a kind of unmanned plane to be charged using high-voltage line according to claim 1, it is characterised in that：The left connecting rod
(14) outer surface is installed on the left surface of left wing (15) and using vertical welding.
3. a kind of unmanned plane to be charged using high-voltage line according to claim 1, it is characterised in that：The positive terminal
(10) inner surface is installed on the outer surface of vertical bar (11) and is gap-matched.
4. a kind of unmanned plane to be charged using high-voltage line according to claim 1, it is characterised in that：The right crus of diaphragm frame (6)
Insertion is installed on the right surface of shell (501) and is gap-matched.
5. a kind of unmanned plane to be charged using high-voltage line according to claim 1, it is characterised in that：The right connecting rod
It (4) is diameter 2CM, the cylindrical structure of high 20CM.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820374123.5U CN208102347U (en) | 2018-03-19 | 2018-03-19 | A kind of unmanned plane to be charged using high-voltage line |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820374123.5U CN208102347U (en) | 2018-03-19 | 2018-03-19 | A kind of unmanned plane to be charged using high-voltage line |
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| Publication Number | Publication Date |
|---|---|
| CN208102347U true CN208102347U (en) | 2018-11-16 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201820374123.5U Active CN208102347U (en) | 2018-03-19 | 2018-03-19 | A kind of unmanned plane to be charged using high-voltage line |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110316337A (en) * | 2019-03-25 | 2019-10-11 | 西安水泽动力科技有限公司 | A kind of multifunction changable pitch master and slave type underwater robot |
| CN112693583A (en) * | 2020-12-18 | 2021-04-23 | 浙江科技学院 | Single-motor-driven full-freedom underwater micro unmanned aerial vehicle |
-
2018
- 2018-03-19 CN CN201820374123.5U patent/CN208102347U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110316337A (en) * | 2019-03-25 | 2019-10-11 | 西安水泽动力科技有限公司 | A kind of multifunction changable pitch master and slave type underwater robot |
| CN110316337B (en) * | 2019-03-25 | 2022-07-12 | 青岛觉海科技有限公司 | Multifunctional variable-pitch primary-secondary underwater robot |
| CN112693583A (en) * | 2020-12-18 | 2021-04-23 | 浙江科技学院 | Single-motor-driven full-freedom underwater micro unmanned aerial vehicle |
| CN112693583B (en) * | 2020-12-18 | 2021-12-21 | 浙江科技学院 | Single-motor-driven full-freedom underwater micro unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20190528 Address after: 435400 No. 2 Beichuan Road, Wuxue City, Huanggang City, Hubei Province Patentee after: HUBEI YUCHAI ENGINE CO.,LTD. Address before: 362314 No. 29, Lingjiao Waijiao, Yunan Village, Jintao Town, Nanan City, Quanzhou City, Fujian Province Patentee before: Li Changgeng |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20231222 Address after: 435499 No. 2, North Side, West End of Beichuan Road, Wuxue City, Huanggang City, Hubei Province Patentee after: Hubei Yufa Feifang Agricultural Technology Co.,Ltd. Address before: 435400 No. 2 Beichuan Road, Wuxue City, Huanggang City, Hubei Province Patentee before: HUBEI YUCHAI ENGINE CO.,LTD. |
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| TR01 | Transfer of patent right |