CN106276725A - Unmanned aerial vehicle for engineering - Google Patents
Unmanned aerial vehicle for engineering Download PDFInfo
- Publication number
- CN106276725A CN106276725A CN201610458565.3A CN201610458565A CN106276725A CN 106276725 A CN106276725 A CN 106276725A CN 201610458565 A CN201610458565 A CN 201610458565A CN 106276725 A CN106276725 A CN 106276725A
- Authority
- CN
- China
- Prior art keywords
- unmanned vehicle
- supporting body
- construction
- engineering
- balance
- 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
- 238000010276 construction Methods 0.000 claims abstract description 56
- 230000005484 gravity Effects 0.000 claims description 12
- 230000004308 accommodation Effects 0.000 claims description 7
- 239000000463 material Substances 0.000 claims description 6
- 238000005303 weighing Methods 0.000 claims description 2
- 238000005516 engineering process Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 2
- 238000005299 abrasion Methods 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 210000000744 eyelid Anatomy 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000005065 mining Methods 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B66—HOISTING; LIFTING; HAULING
- B66F—HOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD
- B66F11/00—Lifting devices specially adapted for particular uses not otherwise provided for
- B66F11/04—Lifting devices specially adapted for particular uses not otherwise provided for for movable platforms or cabins, e.g. on vehicles, permitting workmen to place themselves in any desired position for carrying out required operations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
Abstract
The invention discloses an unmanned aerial vehicle for engineering, which is used for construction at a height far away from the ground and comprises a flight module and a construction module, wherein the flight module comprises a bearing body, a supporting rod, a rotating piece and a driving component, the supporting rod is connected with the bearing body, the rotating piece is arranged on the supporting rod and far away from the bearing body, the driving component drives the rotating piece to rotate, and the construction module comprises a applying piece and at least one balancing piece which are oppositely arranged on the bearing body, so that when the unmanned aerial vehicle for engineering flies at the height, a balance range can be kept in a space for construction. The invention can solve the problem that the prior operation personnel is high in complexity and danger and is easy to cause accidents when carrying out construction operation at high altitude.
Description
Technical field
The present invention relates to a kind of unmanned vehicle, espespecially a kind of engineering unmanned vehicle.
Background technology
Along with capital construction, commercial building and all can flourish, super high-rise building or skyscraper building
The most of common occurrence, in addition to the technique of Building technology and engineering design, the high building exterior wall after completion is overhauled, clearly
Clean or layout etc., is also the work of high-tech and high risk.
In prior art, having mining height working platform person, such as TaiWan, China new patent announces M487337
Number, disclose one and have ambulant Foldable aloftwork platform, mainly include a support foot rest, a folding
Device, an atmospheric pressure pole device, H type ladder and a job platform, this support foot rest is provided with multiple pillar,
Bottom is provided with roller group, and this folding device is mounted on this support foot rest, and this atmospheric pressure pole device is articulated in this
On kickstand and this folding device, this H type ladder is hubbed on this support foot rest, and this job platform is provided with many
Individual handle assembly, this job platform is mounted on this folding device, is filled by this atmospheric pressure pole device, this folding
Put and this H type ladder, this job platform can be made to rise to certain altitude sealed fixing, make the operating personnel can be in
High aerial work.Or, also have employing rope technique person, such as TaiWan, China new patent M405878
Number, disclose a kind of double cable-styled security master cable eyelid retractor, mainly include fixing seat and an anti-fall part of slip, should
Fixing seat bottom portion includes a locking hole, and this fixing seat top includes that a plate, plate both sides respectively set a body.
The anti-fall part of this slip includes a block, and top sets a clasp, for linking a safety rope, and each pivot in block both sides
If a fin, the section of each fin respectively forms a tool frame jaggy and encloses, and each airfoil root respectively protrudes out one and convex supports
Portion, and on the rotation path of each convex supporting part, set a stop tab, each to a predetermined angular for each fin swing
Convex supporting part can be butted on stop tab just.Whereby, fixing seat is available for two security master cables and stretches through and link, when wherein
One security master cable is tired etc. and cannot bear work high above the ground personnel and accidental falling occurs because of corrosion, abrasion or metal
Time to impulse force produced by it, still have another security master cable can provide support.
So, the most above-mentioned whichever, all operating personnel must construct in high vacancy, still possess a certain degree of
Danger, and in case of environmental factors is disturbed, not only work efficiency and progress can be affected, and work peace accident
Risk can increase.
Summary of the invention
The main object of the present invention, is to provide a kind of engineering unmanned vehicle, solves conventional operation people
Member is when eminence carries out construction operation, and complexity is higher with danger, and the problem easily causing accident.
For reaching above-mentioned purpose, the present invention provides a kind of engineering unmanned vehicle, is in order to one remotely
The height in face is constructed, and it includes a flight module and a construction module, and this flight module includes one
Supporting body, a support bar, a revolving part and one drive assembly, and this support bar is connected to this supporting body, should
Revolving part is arranged at this support bar away from this supporting body, and this driving assembly drives this revolving part by this support bar
Rotating to allow this flight module must be in this altitude, this construction module be arranged at this supporting body, and includes one
The laterally projecting construction part and at least of a working side outside this supporting body is located at this supporting body and towards this carrying
What external one was different with this working side balances the balance element that side is laterally projecting, and wherein, this construction part is with this extremely
A few balance element is respectively provided with construction end and the balance end away from this supporting body, makes this engineering fly with nobody
Row carrier, when this altitude, obtains and keeps a range of balance to construct in space.
Wherein, the Resultant force of the center of gravity of this construction part and this at least one balance element is positioned at this engineering and uses unmanned flight
The center of carrier.
Wherein, this at least one balance element includes one first balance element and one second balance element, this construction part,
This first balance element is positioned in this engineering unmanned vehicle with the Resultant force of the center of gravity of this second balance element
The heart.
Wherein, further include a control module being electrically connected at this driving assembly, to control this flight module.
Wherein, further including an external cable being electrically connected at this control module, this external cable electrically connects
It is connected to a power supply unit being arranged at ground and inputs an electric power to this control module.
Wherein, the bracing frame of a bottom surface being arranged at this supporting body is further included.
Wherein, a video lens being arranged at this supporting body this construction part adjacent is further included.
Wherein, this supporting body has further included an accommodation space, the material needed for this construction part accommodating.
As shown in the above description, the invention have the characteristics that:
One, unmanned vehicle is utilized to need not take advantage of manned feature, can be one away from the height on ground
Construct, to increase safety during construction.
Two, it is respectively arranged at this supporting body by this construction part and this at least one balance element, and makes the present invention
Balance stabilized flight can be kept.
Describe the present invention below in conjunction with the drawings and specific embodiments, but not as to the present invention's
Limit.
Accompanying drawing explanation
Fig. 1 is the schematic perspective view of first embodiment of the invention.
Fig. 2 is the partial exploded view of first embodiment of the invention.
Fig. 3 is the schematic perspective view of second embodiment of the invention.
Fig. 4 is the functional block diagram of the present invention.
Wherein, reference:
10 flight modules
11 supporting bodies
12 support bars
13 revolving parts
14 drive assembly
15 accommodation spaces
20 construction modules
21 construction parts
211 construction ends
22 balance elements
221 balance end
222 first balance elements
223 second balance elements
30 control modules
40 external cables
50 power supply units
60 bracing frames
70 video lenses
Detailed description of the invention
Relate to detailed description of the invention and technology contents, show and just coordinate graphic being described as follows:
Refer to shown in Fig. 1 and Fig. 2, for a kind of engineering unmanned vehicle, be in order to one remotely
The height in face is constructed, and it includes flight module 10 and a construction module 20, this flight module
10 include that supporting body 11, support bar 12, revolving part 13 and drives assembly 14 (being shown in Fig. 4),
This support bar 12 is connected to this supporting body 11, and this revolving part 13 is arranged at this support bar 12 away from this carrying
Body 11, and driven by this driving assembly 14 and rotate, with allow this flight module 10 must in this altitude,
In the present embodiment, this support bar 12 and this revolving part 13 are with multiple relative and set and illustrate, but
It is not limited.This construction module 20 is arranged at this supporting body 11, including a construction part 21 and at least
Balance element 22, this construction part 21 is laterally projecting towards the working side outside this supporting body 11, this at least one balance
Part 22 is located at this supporting body 11 and laterally dashes forward in the balance side different with this working side outside this supporting body 11
Go out, and this supporting body 11 has further included an accommodation space 15, the material needed for this construction part 21 accommodating,
This accommodation space 15 can be connected with this construction part 21, and sustainable supply material is to this construction part 21, or
This construction part 21 of person can stretch in this accommodation space 15, to pick material, but is not limited.Yu Ben
In embodiment, this construction part 21, this working side and this at least one balance element 22, this balance side are phases each other
To setting, the right present invention is not limited to this, if the center of gravity of this construction part 21 and this at least one balance element 22
The Resultant force of center of gravity be positioned at the center of this engineering unmanned vehicle, make the present invention can keep balancing also
Stabilized flight.Additionally, this construction part 21 is respectively provided with away from this carrying with this at least one balance element 22
One construction end 211 and a balance end 221 of body 11, makes this engineering unmanned vehicle at this altitude
Time, obtain and keep a range of balance to construct in space.
Continuous collocation is refering to shown in Fig. 3, and for second embodiment of the invention, in this embodiment, this is at least one flat
Weighing apparatus part 22 includes one first balance element 222 and one second balance element 223, the center of gravity of this construction part 21,
The center of gravity of this first balance element 222 is similarly positioned in this engineering with the Resultant force of the center of gravity of this second balance element 223
With the center of unmanned vehicle, to reach the purpose of balance, make smooth flight of the present invention, and in space
Keeping a range of balance to construct, in the present embodiment, the quantity of this at least one balance element 22 is two,
And setting up and down, but be not limited thereto, can also arrange, as long as making the Resultant force of center of gravity be positioned at this left and right
The center of engineering unmanned vehicle.
Additionally, collocation is refering to Fig. 4, the present invention has further included control module 30, external cable 40,
Bracing frame 60 and a video lens 70, this control module 30 is electrically connected at this driving assembly 14, with control
Make this flight module 10, it is possible to collocation is arranged at this video recording mirror of this supporting body 11 this construction part 21 adjacent
70, to confirm construction area and the situation of this construction part 21 construction, this external cable 40 is electrically connected with
It is arranged at ground in one or persistently inputs an electric power to this control less than the power supply unit 50 of position of this height
Molding block 30, works long hours required electric power supplying the present invention.This bracing frame 60 is then arranged at this
One bottom surface of supporting body 11, for the present invention stop construction and landing time, can steadily safety be placed in ground
On, damage without making this supporting body 11 maybe this construction module 20 touch ground.
In sum, the invention have the characteristics that:
One, utilize unmanned vehicle to need not take advantage of manned feature, can enter away from the height on ground one
Row construction, to increase safety during construction.
Two, the Resultant force by the center of gravity of this construction part and the center of gravity of this at least one balance element is positioned at this engineering and uses
The center of unmanned vehicle, makes the present invention can keep balance stabilized flight.
Three, by this accommodation space can and sustainable supply material to this construction part, and improve this construction part work
The time made.
Four, this control module is arranged in pairs or groups this video lens, can confirm that the construction area of this construction part and this execute
The situation of workpiece construction.
Five, it is electrically connected at this power supply unit by this external cable, works long hours institute supplying the present invention
The electric power needed.
Certainly, the present invention also can have other various embodiments, without departing substantially from present invention spirit and the feelings of essence thereof
Under condition, those of ordinary skill in the art can make various corresponding change and deformation according to the present invention, but this
A little corresponding changes and deformation all should belong to the protection domain of the claims in the present invention.
Claims (8)
1. an engineering unmanned vehicle, is that it is special in order to construct away from the height on ground one
Levying and be, this engineering unmanned vehicle includes:
One flight module, including a supporting body, one is connected to the support bar of this supporting body, one is arranged at this
Strut drives this revolving part to rotate to allow this fly away from the revolving part and of this supporting body by this support bar
Row module must be in the driving assembly of this altitude；And
The one construction module being located at this supporting body, laterally projecting towards the working side outside this supporting body including one
Construction part is located at this supporting body and towards the balance side different with this working side outside this supporting body with at least one
Laterally projecting balance element, wherein, this construction part and this at least one balance element are respectively provided with away from this supporting body
An a construction end and balance end, make this engineering unmanned vehicle when this altitude, must be in space
Middle holding one range of balance is to construct.
Engineering unmanned vehicle the most according to claim 1, it is characterised in that this construction part and
The Resultant force of the center of gravity of this at least one balance element is positioned at the center of this engineering unmanned vehicle.
Engineering unmanned vehicle the most according to claim 1, it is characterised in that this is at least one flat
Weighing apparatus part includes one first balance element and one second balance element, this construction part, this first balance element with this second
The Resultant force of the center of gravity of balance element is positioned at the center of this engineering unmanned vehicle.
Engineering unmanned vehicle the most according to claim 1, it is characterised in that further included one
It is electrically connected at the control module of this driving assembly, to control this flight module.
Engineering unmanned vehicle the most according to claim 4, it is characterised in that further included one
Being electrically connected at the external cable of this control module, this external cable is electrically connected at a confession being arranged at ground
Electric unit and input an electric power to this control module.
Engineering unmanned vehicle the most according to claim 1, it is characterised in that further included one
It is arranged at the bracing frame of a bottom surface of this supporting body.
Engineering unmanned vehicle the most according to claim 1, it is characterised in that further included one
It is arranged at the video lens of this supporting body this construction part adjacent.
Engineering unmanned vehicle the most according to claim 1, it is characterised in that this supporting body is more
Include an accommodation space, the material needed for this construction part accommodating.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| TW104120635A TWI590988B (en) | 2015-06-26 | 2015-06-26 | Unmanned aerial vehicle used in engineering |
| TW104120635 | 2015-06-26 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106276725A true CN106276725A (en) | 2017-01-04 |
Family
ID=57651388
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610458565.3A Pending CN106276725A (en) | 2015-06-26 | 2016-06-22 | Unmanned aerial vehicle for engineering |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN106276725A (en) |
| TW (1) | TWI590988B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108888167A (en) * | 2018-09-04 | 2018-11-27 | 蔡鹏翔 | A kind of high-altitude cleaning unmanned plane and the method using high-altitude cleaning unmanned plane progress building high-altitude cleaning |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202699027U (en) * | 2012-07-13 | 2013-01-30 | 长春工程学院 | Remote-control automatic window cleaner |
| CN103112587A (en) * | 2013-02-27 | 2013-05-22 | 曾小敏 | Aircraft |
| CN103253373A (en) * | 2012-02-21 | 2013-08-21 | 吴泽邦 | Multifunctional unmanned machine platform capable of feeding water continuously for in-air fire-fighting rescue and rescue method thereof |
| TWM490346U (en) * | 2014-06-27 | 2014-11-21 | Univ Chien Hsin Sci & Tech | Wing protection mechanism of rotary wing aircraft |
| CN104210659A (en) * | 2014-09-15 | 2014-12-17 | 金陵科技学院 | Unmanned aerial vehicle for high-rise building cleaning |
| CN204210732U (en) * | 2014-11-05 | 2015-03-18 | 国网辽宁省电力有限公司检修分公司 | A kind of four rotor wing unmanned aerial vehicles for removing the flammable foreign matter in high-altitude |
-
2015
- 2015-06-26 TW TW104120635A patent/TWI590988B/en not_active IP Right Cessation
-
2016
- 2016-06-22 CN CN201610458565.3A patent/CN106276725A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103253373A (en) * | 2012-02-21 | 2013-08-21 | 吴泽邦 | Multifunctional unmanned machine platform capable of feeding water continuously for in-air fire-fighting rescue and rescue method thereof |
| CN202699027U (en) * | 2012-07-13 | 2013-01-30 | 长春工程学院 | Remote-control automatic window cleaner |
| CN103112587A (en) * | 2013-02-27 | 2013-05-22 | 曾小敏 | Aircraft |
| TWM490346U (en) * | 2014-06-27 | 2014-11-21 | Univ Chien Hsin Sci & Tech | Wing protection mechanism of rotary wing aircraft |
| CN104210659A (en) * | 2014-09-15 | 2014-12-17 | 金陵科技学院 | Unmanned aerial vehicle for high-rise building cleaning |
| CN204210732U (en) * | 2014-11-05 | 2015-03-18 | 国网辽宁省电力有限公司检修分公司 | A kind of four rotor wing unmanned aerial vehicles for removing the flammable foreign matter in high-altitude |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108888167A (en) * | 2018-09-04 | 2018-11-27 | 蔡鹏翔 | A kind of high-altitude cleaning unmanned plane and the method using high-altitude cleaning unmanned plane progress building high-altitude cleaning |
Also Published As
| Publication number | Publication date |
|---|---|
| TWI590988B (en) | 2017-07-11 |
| TW201700352A (en) | 2017-01-01 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170104 |