CN109131499A - Printer application method - Google Patents
Printer application method Download PDFInfo
- Publication number
- CN109131499A CN109131499A CN201810997671.8A CN201810997671A CN109131499A CN 109131499 A CN109131499 A CN 109131499A CN 201810997671 A CN201810997671 A CN 201810997671A CN 109131499 A CN109131499 A CN 109131499A
- Authority
- CN
- China
- Prior art keywords
- guide runner
- guide
- threaded rod
- motor
- slider
- 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.)
- Withdrawn
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B41—PRINTING; LINING MACHINES; TYPEWRITERS; STAMPS
- B41J—TYPEWRITERS; SELECTIVE PRINTING MECHANISMS, i.e. MECHANISMS PRINTING OTHERWISE THAN FROM A FORME; CORRECTION OF TYPOGRAPHICAL ERRORS
- B41J29/00—Details of, or accessories for, typewriters or selective printing mechanisms not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62B—HAND-PROPELLED VEHICLES, e.g. HAND CARTS OR PERAMBULATORS; SLEDGES
- B62B3/00—Hand carts having more than one axis carrying transport wheels; Steering devices therefor; Equipment therefor
- B62B3/02—Hand carts having more than one axis carrying transport wheels; Steering devices therefor; Equipment therefor involving parts being adjustable, collapsible, attachable, detachable or convertible
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62B—HAND-PROPELLED VEHICLES, e.g. HAND CARTS OR PERAMBULATORS; SLEDGES
- B62B3/00—Hand carts having more than one axis carrying transport wheels; Steering devices therefor; Equipment therefor
- B62B3/04—Hand carts having more than one axis carrying transport wheels; Steering devices therefor; Equipment therefor involving means for grappling or securing in place objects to be carried; Loading or unloading equipment
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62B—HAND-PROPELLED VEHICLES, e.g. HAND CARTS OR PERAMBULATORS; SLEDGES
- B62B5/00—Accessories or details specially adapted for hand carts
- B62B5/0026—Propulsion aids
- B62B5/0033—Electric motors
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Steering Controls (AREA)
Abstract
The invention discloses printer application methods, including fuselage and the first guide runner of the fuselage inner opening to the left is set, the first slider guide is slidably connected in first guide runner, the first threaded rod extended up and down after the first slider guide screw-internal thread fit connection, the first threaded rod top end has been connected by power the first motor, first motor outer surface is embedded in the first guide runner top inner wall and connection fixed thereto, the second guide runner of opening to the left is equipped in first slider guide, symmetrical second slider guide in front and back is slidably connected in second guide runner.
Description
Technical field
The present invention relates to printer technology fields, specifically printer application method.
Background technique
With the reach of science, social progress, country is promoting always the development of advanced technology, wherein in printer skill
A problem is always existed in art field leads to device precisely due to general printer is not provided with the device of convenient movement
It is mobile difficult, and printer is a kind of office appliance of precision, and extremely soft carrying is needed in handling process, the present invention
Device solve this problem in that.
Summary of the invention
Technical problem to be solved by the invention is to provide printer application methods, are able to solve above-mentioned show in the art
The problem of.
The present invention is achieved through the following technical solutions: printer of the invention, including fuselage and setting are in institute
The first guide runner of fuselage inner opening to the left is stated, is slidably connected with the first slider guide in first guide runner, described
The first threaded rod extended up and down after the connection of one slider guide screw-internal thread fit, the first threaded rod top end are connected by power
There is the first motor, first motor outer surface is embedded in the first guide runner top inner wall and company fixed thereto
It connects, the second guide runner of opening to the left is equipped in first slider guide, before being slidably connected in second guide runner
Symmetrical second slider guide afterwards, second slider guide left end are stretched out outside second guide runner and are fixedly connected with extension up and down
Connecting rod, the supporting rod that symmetrical above and below and left and right extends is fixedly connected on the end face of the connecting rod left end, described second leads
Sliding block screw-internal thread fit is connected with the second threaded rod that front and back extends, and the second screw thread rod rear end end has been connected by power second
Motor, second motor outer surface is embedded in the inner wall of second guide runner rear end and connection fixed thereto, described
It is equipped in fuselage bottom end face and is located at the first downward cavity of the first guide runner bottom opening, the first cavity right end is set
There is the second cavity that Open Side Down, is communicated in the first cavity right end inner wall equipped with third guide runner, first cavity top
Be rotatably assorted the first rotation axis for being connected with that front and back is symmetrical and extends up and down on portion's inner wall, and the first rotation axis bottom end is solid
Surely it is connected with disk, the disk is rotatably assorted far from first cavity center end is connected with the main shaft that front and back extends, described
Main shaft is fixedly connected with steered wheel far from first cavity end, and left and right is fixedly connected on the end face of the disk left end and is extended
The first turning-bar, the second turning-bar that front and back extends is hingedly connected between two first turning-bars, the third is led
Third slider guide is slidably connected in sliding slot, the third slider guide screw-internal thread fit is connected with the third spiral shell that front and back extends
Rasp bar, the third screw thread rod rear end end have been connected by power third motor, and third motor outer surface is embedded at institute
It states in the inner wall of third guide runner rear end and connection fixed thereto, third slider guide left end end face is described to open equipped with open slot
Be rotatably assorted the second rotation axis for being connected with and extending up and down in mouth slot, turns between second rotation axis and second turning-bar
It is dynamic to be connected with connecting plate, it is equipped with first be slidably connected with second rotation axis up and down in the connecting plate
Sliding rail is equipped with the second sliding rail positioned at first sliding rail left end, first cavity top in the connecting plate up and down
It is fixedly connected with the fixed link for running through second sliding rail and being slidably connected therewith, it is dynamic to be equipped with driving in second cavity
Force mechanisms, the interior balancing device being equipped with positioned at the first guide runner right end of the fuselage；
Described method includes following steps:
Firstly, first slider guide is located at the first guide runner bottommost, two second slider guides when original state
It is separated from each other, the steered wheel is in horizontal state to the left, and second turning-bar is in horizontality, and the third is led
Sliding block is located in the middle part of the third guide runner, and the connecting plate is in horizontal left and right state；
Then, when the work is required, starting the driving motor first moves integrally device, electronic by starting the third
Machine drives the third threaded rod rotation, is moved forward and backward the third slider guide, drives the connecting plate to rotate, by described
Second turning-bar and first turning-bar drive the disk rotational, to adjust deflecting roller steering, have reached change device
The problem of direction, finally moves integrally device to institute's printer to be transported, after finally adjusting good position, starting described second
Motor drives the second threaded rod rotation, keeps two second slider guides close to each other, beats the clamping board clamping
Print machine finally starts first motor and drives the first threaded rod rotation, make first slider guide integrally move up from
And printer is carried to suitable position；
Finally, start the 4th motor wherein during needing center-of-gravity regulating and drive the 4th threaded rod rotation,
Keep the balancing gravity block mobile to the 4th guide runner right end, anti-locking apparatus inclination.
It may be preferred that second threaded rod front and back end screw thread is reversed, it is easy to implement Automatic-clamping and relaxation printer.
It may be preferred that the balancing device includes the 4th guide runner being arranged in the fuselage, the 4th guide runner
It is inside slidably connected with balancing gravity block, the balancing gravity block screw-internal thread fit is connected with the 4th screw thread that left and right extends
Bar, the 4th threaded rod left end end have been connected by power the 4th motor, and the 4th motor outer surface is embedded at described
In 4th guide runner left end inner wall and connection fixed thereto, prevent deviation of gravity center device unstable.
It may be preferred that the driving power mechanism includes being rotatably assorted to connect to be arranged between two second cavitys
The drive shaft that front and back extends, drive shaft front and back end are fixedly connected with power wheel, have been connected by power drive in the drive shaft
Dynamic motor, consequently facilitating the movement of device.
It may be preferred that being equipped with processor in the fuselage, dynamics display screen is equipped in fuselage right end end face, thus just
Stablize in device and clamps printer.
The beneficial effects of the present invention are: first slider guide is located at first guide runner due in the initial state
Bottommost, two second slider guides are separated from each other, and the steered wheel is in horizontal state to the left, and described second turns to
Bar is in horizontality, and the third slider guide is located in the middle part of the third guide runner, and the connecting plate is in horizontal left and right shape
State, consequently facilitating the care and maintenance of device.
When the work is required, starting the driving motor first moves integrally device, electronic by starting the third
Machine drives the third threaded rod rotation, is moved forward and backward the third slider guide, drives the connecting plate to rotate, by described
Second turning-bar and first turning-bar drive the disk rotational, to adjust deflecting roller steering, have reached change device
The problem of direction, finally moves integrally device to institute's printer to be transported, after finally adjusting good position, starting described second
Motor drives the second threaded rod rotation, keeps two second slider guides close to each other, beats the clamping board clamping
Print machine finally starts first motor and drives the first threaded rod rotation, make first slider guide integrally move up from
And printer is carried to suitable position, to promote carrying effect.
Wherein during needing center-of-gravity regulating, starts the 4th motor and drives the 4th threaded rod rotation,
Keep the balancing gravity block mobile to the 4th guide runner right end, anti-locking apparatus inclination, thus lifting device practical performance.
The configuration of the present invention is simple, it is easy to operate, by using the fuselage being integrated in one, it is respectively set certainly in fuselage bottom
Dynamic identification steering mechanism and driving power mechanism, turn to convenient for automatically moving for device with automatic identification, and be arranged in fuselage
Soft clamp system, internal setting can automatic center-of-gravity regulating mechanism, so that Lifting Convey tonnage range, ingenious in design,
Equipment is light and handy, Intelligent portable, and environmental protection is excellent.
Detailed description of the invention
The present invention is described in detail by following specific embodiments and drawings for ease of explanation,.
Fig. 1 is overall structure diagram inside printer application method of the invention；
Fig. 2 is the partial enlargement structural representation of A in Fig. 1；
Fig. 3 is the schematic cross-section of B in Fig. 2.
Specific embodiment
As shown in Figure 1, Figure 2 and Figure 3, printer application method of the invention, including fuselage 100 and setting are in the machine
The first guide runner 101 of 100 inner opening of body to the left is slidably connected with the first slider guide in first guide runner 101
103, the first threaded rod 102 extended up and down after 103 screw-internal thread fit of the first slider guide connection, first threaded rod
102 top ends have been connected by power the first motor 117, and 117 outer surface of the first motor is embedded at first slide guide
In 101 top inner wall of slot and connection fixed thereto, it is equipped with the second guide runner 104 of opening to the left in first slider guide 103,
Symmetrical second slider guide 106 in front and back is slidably connected in second guide runner 104, second slider guide 106 is left
End is stretched out outside second guide runner 104 and is fixedly connected with the connecting rod 107 extended up and down, the 107 left end end of connecting rod
The supporting rod 140 that symmetrical above and below and left and right extends is fixedly connected on face, 106 screw-internal thread fit of the second slider guide is connected with
The second threaded rod 105 that front and back extends, the 105 rear end end of the second threaded rod have been connected by power the second motor, and described the
Two motor outer surfaces are embedded in the 104 rear end inner wall of the second guide runner and connection fixed thereto, 100 bottom of fuselage
It is equipped in end face and is located at the first downward cavity 119 of 101 bottom opening of the first guide runner, 119 right end of the first cavity
Equipped with the second cavity 110 that Open Side Down, communicate in the 119 right end inner wall of the first cavity equipped with third guide runner 128, it is described
Be rotatably assorted the first rotation axis 118 for being connected with that front and back is symmetrical and extends up and down in first cavity, 119 top inner wall, and described first
118 bottom end of rotation axis is fixedly connected with disk 121, and the disk 121 is matched far from 119 center-side of the first cavity rotation
It closes and is connected with the main shaft 122 that front and back extends, the main shaft 122 is fixedly connected with steered wheel far from 119 end of the first cavity
120, the first turning-bar 133 that left and right extends, two first turning-bars are fixedly connected on the 121 left end end face of disk
It is hingedly connected with the second turning-bar 132 that front and back extends between 133, the is slidably connected in the third guide runner 128
Three slider guides 127,127 screw-internal thread fit of third slider guide are connected with the third threaded rod 129 that front and back extends, the third
129 rear end end of threaded rod has been connected by power third motor 134, and 134 outer surface of third motor is embedded at described
In three guide runners, 128 rear end inner wall and connection fixed thereto, the 127 left end end face of third slider guide is equipped with open slot 126, institute
State the second rotation axis 130 for being rotatably assorted in open slot 126 and being connected with and extending up and down, second rotation axis 130 and described the
It is rotatably assorted between two turning-bars 132 and is connected with connecting plate 123, be equipped with and described second up and down in the connecting plate 123
The first sliding rail 125 that rotation axis 130 is slidably connected, is equipped with that be located at described first sliding in the connecting plate 123 up and down
Second sliding rail 124 of 125 left end of rail, is fixedly connected at the top of first cavity 119 through second sliding rail 124 and therewith
The fixed link 131 of sliding connection, second cavity 110 is interior to be equipped with driving power mechanism, is equipped with position in the fuselage 100
In the balancing device of 101 right end of the first guide runner.
Valuably, the 105 front and back end screw thread of the second threaded rod is reversed, is easy to implement Automatic-clamping and relaxation printer.
Valuably, the balancing device includes the 4th guide runner 114 being arranged in the fuselage 100, and the described 4th leads
Balancing gravity block 115 is slidably connected in sliding slot 114,115 screw-internal thread fit of balancing gravity block is connected with left and right and prolongs
The 4th threaded rod 113 stretched, the 113 left end end of the 4th threaded rod have been connected by power the 4th motor 116, the 4th electricity
116 outer surface of motivation is embedded in the 114 left end inner wall of the 4th guide runner and connection fixed thereto, prevents deviation of gravity center device
It is unstable.
Valuably, the driving power mechanism includes being rotatably assorted connection setting between two second cavitys 110
Front and back extend drive shaft 109, the 109 front and back end of drive shaft is fixedly connected with power wheel 108, the drive shaft 109
On be connected by power driving motor, consequently facilitating the movement of device.
Valuably, it is equipped with processor 111 in the fuselage 100, is equipped with dynamics display screen in the 100 right end end face of fuselage
112, consequently facilitating device, which is stablized, clamps printer.
Described method includes following steps:
Firstly, when original state, first slider guide 103 is located at 101 bottommost of the first guide runner, two described second
Slider guide 106 is separated from each other, and the steered wheel 120 is in horizontal state to the left, and second turning-bar 132 is in level
State, the third slider guide 127 are located at 128 middle part of third guide runner, and the connecting plate 123 is in horizontal left and right shape
State；
Then, when the work is required, starting the driving motor first moves integrally device, electronic by starting the third
Machine 134 drives the third threaded rod 129 to rotate, and is moved forward and backward the third slider guide 127, drives the connecting plate 123
Rotation drives the disk 121 to rotate, to adjust steering by second turning-bar 132 and first turning-bar 133
Wheel 120 turns to, and has reached the problem of changing device direction, finally moves integrally device to institute's printer to be transported, finally
After adjusting good position, starts second motor and second threaded rod 105 is driven to rotate, make two second slider guides
106 is close to each other, so that the grip block 140 is clamped printer, finally starts first motor 117 and drive first spiral shell
Rasp bar 102 rotates, and makes first slider guide 103 is whole to move up printer being carried to suitable position；
Finally, starting the 4th motor 116 wherein during needing center-of-gravity regulating and driving the 4th threaded rod
113 rotations keep the balancing gravity block 115 mobile to 114 right end of the 4th guide runner, anti-locking apparatus inclination.
The beneficial effects of the present invention are: first slider guide is located at first guide runner due in the initial state
Bottommost, two second slider guides are separated from each other, and the steered wheel is in horizontal state to the left, and described second turns to
Bar is in horizontality, and the third slider guide is located in the middle part of the third guide runner, and the connecting plate is in horizontal left and right shape
State, consequently facilitating the care and maintenance of device.
When the work is required, starting the driving motor first moves integrally device, electronic by starting the third
Machine drives the third threaded rod rotation, is moved forward and backward the third slider guide, drives the connecting plate to rotate, by described
Second turning-bar and first turning-bar drive the disk rotational, to adjust deflecting roller steering, have reached change device
The problem of direction, finally moves integrally device to institute's printer to be transported, after finally adjusting good position, starting described second
Motor drives the second threaded rod rotation, keeps two second slider guides close to each other, beats the clamping board clamping
Print machine finally starts first motor and drives the first threaded rod rotation, make first slider guide integrally move up from
And printer is carried to suitable position, to promote carrying effect.
Wherein during needing center-of-gravity regulating, starts the 4th motor and drives the 4th threaded rod rotation,
Keep the balancing gravity block mobile to the 4th guide runner right end, anti-locking apparatus inclination, thus lifting device practical performance.
The configuration of the present invention is simple, it is easy to operate, by using the fuselage being integrated in one, it is respectively set certainly in fuselage bottom
Dynamic identification steering mechanism and driving power mechanism, turn to convenient for automatically moving for device with automatic identification, and be arranged in fuselage
Soft clamp system, internal setting can automatic center-of-gravity regulating mechanism, so that Lifting Convey tonnage range, ingenious in design,
Equipment is light and handy, Intelligent portable, and environmental protection is excellent.
The above description is merely a specific embodiment, but scope of protection of the present invention is not limited thereto, any
The change or replacement expected without creative work, should be covered by the protection scope of the present invention.Therefore, of the invention
Protection scope should be determined by the scope of protection defined in the claims.
Claims (4)
1. including fuselage and the first guide runner of the fuselage inner opening to the left, feature is arranged in printer application method
Be: being slidably connected with the first slider guide in first guide runner, the first slider guide screw-internal thread fit connection with
The first threaded rod extended up and down afterwards, the first threaded rod top end have been connected by power the first motor, first electricity
Motivation outer surface is embedded in the first guide runner top inner wall and connection fixed thereto, is equipped with and opens in first slider guide
Mouth the second guide runner to the left, is slidably connected with symmetrical second slider guide in front and back in second guide runner, and described the
Two slider guide left ends are stretched out outside second guide runner and are fixedly connected with the connecting rod extended up and down, connecting rod left end end
The supporting rod that symmetrical above and below and left and right extends is fixedly connected on face, the second slider guide screw-internal thread fit is connected with front and back and prolongs
The second threaded rod stretched, the second screw thread rod rear end end have been connected by power the second motor, the second motor appearance
Face is embedded in the inner wall of second guide runner rear end and connection fixed thereto, is equipped with described in being located in the fuselage bottom end face
The first downward cavity of first guide runner bottom opening, the first cavity right end is equipped with the second cavity that Open Side Down, described
It is communicated in first cavity right end inner wall equipped with third guide runner, is rotatably assorted on the first cavity top inner wall and is connected with front and back
The first rotation axis symmetrically and up and down extended, the first rotation axis bottom end are fixedly connected with disk, and the disk is separate
First cavity center end, which is rotatably assorted, is connected with the main shaft that front and back extends, and the main shaft is fixed far from first cavity end
Be connected with steered wheel, be fixedly connected on the end face of the disk left end left and right extend the first turning-bar, two described first
It is hingedly connected with the second turning-bar that front and back extends between turning-bar, is slidably connected with third in the third guide runner and leads
Sliding block, the third slider guide screw-internal thread fit are connected with the third threaded rod that front and back extends, the third screw thread rod rear end end
End has been connected by power third motor, third motor outer surface be embedded in the inner wall of third guide runner rear end and with
Be fixedly connected, third slider guide left end end face is equipped with open slot, and being rotatably assorted in the open slot, it is downward to be connected with
The second rotation axis stretched is rotatably assorted between second rotation axis and second turning-bar and is connected with connecting plate, the company
It is equipped with the first sliding rail for being slidably connected with second rotation axis in fishplate bar up and down, in the connecting plate up and down
Equipped with the second sliding rail for being located at first sliding rail left end, first cavity top is fixedly connected with through second sliding rail
And the fixed link being slidably connected therewith, second cavity is interior to be equipped with driving power mechanism, is equipped with and is located in the fuselage
The balancing device of the first guide runner right end；
Described method includes following steps:
Firstly, first slider guide is located at the first guide runner bottommost, two second slider guides when original state
It is separated from each other, the steered wheel is in horizontal state to the left, and second turning-bar is in horizontality, and the third is led
Sliding block is located in the middle part of the third guide runner, and the connecting plate is in horizontal left and right state；
Then, when the work is required, starting the driving motor first moves integrally device, electronic by starting the third
Machine drives the third threaded rod rotation, is moved forward and backward the third slider guide, drives the connecting plate to rotate, by described
Second turning-bar and first turning-bar drive the disk rotational, to adjust deflecting roller steering, have reached change device
The problem of direction, finally moves integrally device to institute's printer to be transported, after finally adjusting good position, starting described second
Motor drives the second threaded rod rotation, keeps two second slider guides close to each other, beats the clamping board clamping
Print machine finally starts first motor and drives the first threaded rod rotation, make first slider guide integrally move up from
And printer is carried to suitable position；
Finally, start the 4th motor wherein during needing center-of-gravity regulating and drive the 4th threaded rod rotation,
Keep the balancing gravity block mobile to the 4th guide runner right end, anti-locking apparatus inclination
Printer application method according to claim 1, it is characterised in that: second threaded rod front and back end screw thread is anti-
To.
2. printer application method according to claim 1, it is characterised in that: the balancing device includes being arranged described
The 4th guide runner in fuselage, is slidably connected with balancing gravity block in the 4th guide runner, in the balancing gravity block
It is threadedly engaged and is connected with the 4th threaded rod that left and right extends, it is electronic that the 4th threaded rod left end end has been connected by power the 4th
Machine, the 4th motor outer surface is embedded in the inner wall of the 4th guide runner left end and connection fixed thereto.
3. printer application method according to claim 1, it is characterised in that: the driving power mechanism includes that rotation is matched
The drive shaft that the front and back that connection is arranged between two second cavitys extends is closed, end is fixedly connected before and after the drive shaft
Dynamic wheel has been connected by power driving motor in the drive shaft.
4. printer application method according to claim 1, it is characterised in that: processor is equipped in the fuselage, it is described
Dynamics display screen is equipped in fuselage right end end face.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810997671.8A CN109131499A (en) | 2018-08-29 | 2018-08-29 | Printer application method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810997671.8A CN109131499A (en) | 2018-08-29 | 2018-08-29 | Printer application method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109131499A true CN109131499A (en) | 2019-01-04 |
Family
ID=64829132
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810997671.8A Withdrawn CN109131499A (en) | 2018-08-29 | 2018-08-29 | Printer application method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109131499A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110203121A (en) * | 2019-05-14 | 2019-09-06 | 嘉兴笼列电子商务有限公司 | A kind of vaccine tote box |
-
2018
- 2018-08-29 CN CN201810997671.8A patent/CN109131499A/en not_active Withdrawn
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110203121A (en) * | 2019-05-14 | 2019-09-06 | 嘉兴笼列电子商务有限公司 | A kind of vaccine tote box |
| CN110203121B (en) * | 2019-05-14 | 2021-01-15 | 浙江麦知网络科技有限公司 | Bacterin transports case |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20190104 |