CN106985994A - A kind of air force ship brake apparatus - Google Patents
A kind of air force ship brake apparatus Download PDFInfo
- Publication number
- CN106985994A CN106985994A CN201710295442.7A CN201710295442A CN106985994A CN 106985994 A CN106985994 A CN 106985994A CN 201710295442 A CN201710295442 A CN 201710295442A CN 106985994 A CN106985994 A CN 106985994A
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- China
- Prior art keywords
- pedal
- expansion link
- air force
- keep plate
- force ship
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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.)
- Pending
Links
- 230000000694 effects Effects 0.000 abstract description 11
- 238000000034 method Methods 0.000 abstract description 8
- 230000033001 locomotion Effects 0.000 description 6
- 238000005516 engineering process Methods 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000005183 dynamical system Methods 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H25/00—Steering; Slowing-down otherwise than by use of propulsive elements; Dynamic anchoring, i.e. positioning vessels by means of main or auxiliary propulsive elements
- B63H25/44—Steering or slowing-down by extensible flaps or the like
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Braking Elements And Transmission Devices (AREA)
Abstract
The invention discloses a kind of air force ship brake apparatus, by air force ship direct of travel, it is made up of the transfer for being symmetricly set on the air force ship left and right sides；Pedal is located in driving cabin, is fixedly connected with pedal arm one end；The pedal arm other end passes through the movable axle sleeve being connected with cabin truss, and the other end of the Flexible Reset part with being fixedly connected on towards fore direction one end on cabin truss is fixedly connected, while being also hinged with the front end expansion link towards stern direction；Front end expansion link is with setting one end of rear end expansion link to be on the quarter connected by hydraulic tube；Fixed plate is fixedly connected with stern transom plate bottom on the quarter, is hinged with keep plate；The rear end expansion link other end is hinged with keep plate, and driving keep plate is spun upside down；The present invention drives keep plate to push to form resistance and turned to and braked by pedal, obtains the flexibly and effectively reduction air force ship speed of a ship or plane, realizes the technique effect that low speed is turned and braked.
Description
Technical field
The present invention relates to ships and light boats control device, a kind of air force ship brake apparatus is specifically related to, belongs to air and moves
Power ship control technology field.
Background technology
Air force ship is that one kind utilizes aerodynamic principle, and dynamical system and steering are placed on hull
Portion, many landform vehicles that can be navigated by water in the complicated interfaces such as shallow water, marsh and wetland.Air force ship is abroad
Through widely using, in China due to technology restriction, air force ship is also in development and development phase.
There is following defect in actual applications in current air force ship：
1. air force ship does not have brake apparatus.Air force ship fully relies on resistance that hull contacts with the water surface to realize
Braking, whole braking procedure is longer, when there is emergency case, it is impossible to which braking in time, security is relatively low.
2. can not effective brake in air force ship steering procedure.The change that existing air force ship relies only on rudder angle comes
Realize that hull is turned to, steering flexibility ratio is relatively low, and rudder for ship does not have braking effect in steering procedure, only relies on rotation speed of the fan
Change and be difficult to reduce the speed of a ship or plane in time or braked to adjust in the headway of ships and light boats, steering procedure, it is impossible to realize low speed spirit
It is living to turn to.
The content of the invention
It is an object of the invention to provide a kind of air force ship brake apparatus, to solve existing air force ship presence
It can not brake in time, and can not the low speed technological deficiency and problem that flexibly turn to.
To reach above-mentioned purpose, the present invention is achieved by the following technical programs：
A kind of air force ship brake apparatus, it is left by being symmetricly set on air force ship by air force ship direct of travel
The transfer 1 of right both sides is constituted；
The transfer 1 includes：Pedal 11, pedal arm 12, Flexible Reset part 13, movable axle sleeve 14, front end are stretched
Bar 15, hydraulic tube 16, rear end expansion link 17, fixed plate 18 and keep plate 19；
The pedal 11 is located in driving cabin, is fixedly connected with described one end of pedal arm 12；The other end of pedal arm 12
Through the movable axle sleeve 14 being connected with cabin truss, described in being fixedly connected on towards fore direction one end on cabin truss
The other end of Flexible Reset part 13 is fixedly connected, while being also hinged with the front end expansion link 15 towards stern direction；It is described
Front end expansion link 15 is with setting one end of the rear end expansion link 17 to be on the quarter connected by the hydraulic tube 16；It is described solid
Fixed board 18 is fixedly connected with stern transom plate bottom on the quarter, is hinged with the keep plate 19；The other end of rear end expansion link 17 and institute
State keep plate 19 to be hinged, drive the keep plate 19 to spin upside down.
The purpose of the present invention can also further be realized by following technical measures：
Further, the air force ship brake apparatus also includes：Brake pedal 2；The brake pedal 2 is located at left side
Pedal 11 and right side pedal 11 between, and half mulching is on the pedal 11 in left side and the pedal 11 on right side.
Further, the movable axle sleeve 14 is equal to the pedal 11 apart from the vertical of hull bottom apart from the vertical range of hull bottom
/ 3rd of distance.
Further, the hydraulic tube 16 is the hydraulic tube that two ends are connected with single-acting expansion hydro-cylinder 161, its hydraulic cylinder
The spring for reset is also set with piston rod in 161.
Further, the transfer 1 also includes rear end expansion link retainer ring 110；The rear end expansion link retainer ring
110 are made up of fixed support 1101 and retainer ring 1102；Described one end of fixed support 1101 is fixedly connected with stern stern transom plate,
The other end is hinged with retainer ring 1102；The rear end expansion link 17 passes through retainer ring 1102, and is fixedly connected with retainer ring 1102.
Further, the keep plate 19 also includes fixed-hinged support 1901；The fixed-hinged support 1901 is arranged at institute
State in the table plane of keep plate 19；The rear end expansion link 17 is hinged by fixed-hinged support 1901 with the keep plate 19.
Further, the keep plate 19 is plough type keep plate.
Further, the keep plate 19 is the plough type keep plate that surface is provided with anti-skid stud.
Compared with prior art, the beneficial effects of the invention are as follows：
In the present invention, pedal drives keep plate activity by expansion link, tramples degree according to pedal and realizes to keep plate
Different degrees of pushes, and increases the resistance of air force ship, so that realizing flexibly and effectively reduces the speed of a ship or plane of air force ship, it is real
Now braking and low speed are turned.
In the present invention, the brake pedal by half mulching on the pedal on left side and right side, can be to the pedals of both sides
Control simultaneously, realize in case of emergency quick and flexible braking.
In the present invention, rear end expansion link is consolidated by installing rear end expansion link retainer ring on stern transom plate on the quarter additional
It is fixed, the change of expansion link angle in rear end in braking procedure is adapted to, braking effect is improved.
In the present invention, movable axle sleeve is arranged to pedal apart from the three of hull bottom vertical range apart from the vertical range of hull bottom
/ mono-, the flexibility that pedal is trampled can be improved, so as to improve the flexibility of keep plate motion, braking effect is improved.
In the present invention, fixed-hinged support is set on keep plate, and is hinged by fixed-hinged support with rear end expansion link,
Keep plate activity point of view can be controlled, and does not produce and rocks, braking effect is improved.
In the present invention, using plough type keep plate, the increase braking when marshland shape is dynamic of air force ship can be caused
Effect.
In the present invention, using the plough type keep plate with anti-skid stud, air force ship can be caused in ice formation ground shape
Increase braking effect when dynamic.
Brief description of the drawings
Fig. 1 is the front view of air force ship brake apparatus of the present invention；
Fig. 2 is the top view of air force ship brake apparatus of the present invention；
Fig. 3 is air force ship brake apparatus pedal of the present invention and the partial schematic diagram of pedal arm section；
Fig. 4 is the partial schematic diagram of pedal part of the air force ship brake apparatus of the present invention with brake pedal；
Fig. 5 is the partial top view of air force ship brake apparatus of the present invention on the quarter；
Fig. 6 is the partial side view of air force ship brake apparatus of the present invention on the quarter；
Fig. 7 is air force ship brake apparatus hydraulic tube organigram of the present invention.
Wherein, 1- transfers, 11- pedals, 12- pedal arms, 13- Flexible Reset parts, 14- activity axle sleeves, 15- front ends
Expansion link, 16- hydraulic tubes, 161- single-action telescopic hydraulic cylinders, 17- rear ends expansion link, 18- fixed plates, 19- keep plates；
1901- fixed-hinged supports, 110- rear ends expansion link retainer ring；1101- fixed supports；1102- retainer rings.
Embodiment
The invention will be further described with specific embodiment below in conjunction with the accompanying drawings.
As shown in Figure 1, Figure 2 and Figure 3, the air force ship brake apparatus that the present invention is provided, by air force ship traveling side
To being made up of the transfer 1 for being symmetricly set on the air force ship left and right sides；
Transfer 1 includes：Pedal 11, pedal arm 12, Flexible Reset part 13, movable axle sleeve 14, front end expansion link 15,
Hydraulic tube 16, rear end expansion link 17, fixed plate 18 and keep plate 19；
Pedal 11 is located in driving cabin, is fixedly connected with the one end of pedal arm 12；The other end of pedal arm 12 is passed through and cabin purlin
The movable axle sleeve 14 of frame connection, it is another with the Flexible Reset part 13 that is fixedly connected on towards fore direction one end on cabin truss
End is fixedly connected, while being also hinged with the front end expansion link 15 towards stern direction；After front end expansion link 15 and setting on the quarter
One end of end expansion link 17 is connected by hydraulic tube 16；Fixed plate 18 is fixedly connected with stern transom plate bottom on the quarter, with keep plate
19 are hinged；The other end of rear end expansion link 17 is hinged with keep plate 19, and driving keep plate 19 is spun upside down.
Air force ship brake apparatus be by be arranged on hull each side one group of transfer 1 turned to and
Control for brake.Provided with two pedals 11 in left and right in driver's cabin, when needing to be turned to, human pilot tramples stepping on for respective direction
Plate 11, pedal 11 can drive pedal arm 12 to move, because pedal arm 12 is to be fixed on by movable axle sleeve 14 on cabin truss,
So when pedal 11 is pressed down, pedal arm 12 can be that fulcrum carries out lever motion with movable axle sleeve 14, so as to drive reset bullet
Property part 13 is stretched and front end expansion link 15 shrinks, and front end expansion link 15 and rear end expansion link 17 are connected by hydraulic tube 16
, thus front end expansion link 15 shrink after by hydraulic tube 16 by pressure transmission to rear end expansion link 17, now rear end expansion link
17, which can be stressed, influences to be stretched, so as to promote keep plate 19 to push, due to only pushing side keep plate 19 and opposite side
Keep plate 19 is in initial level state, so keep plate 19 pushes collateral resistance increase, air force ship can slow down and to the party
To steering.When needing to stop turning to, human pilot unclamps pedal 11, and Flexible Reset part 13 can be returned to just from extended state
Beginning state, drives front end expansion link 15 to stretch, the stretching, extension of front end expansion link 15 can drive the contraction of rear end expansion link 17, final band
Dynamic keep plate 19 recovers initial level state, and air force ship can just recover normally travel.In order to preferably realize pedal arm
12 lever motion, improves the operability of keep plate 19, and the vertical height that can fix movable axle sleeve 14 is arranged to pedal
11 to 1/3rd of hull bottom vertical height.
When in case of emergency, human pilot can step on both sides pedal 11 simultaneously, by both sides keep plate 19 with present
Pressure, while increasing two collateral resistances, realizes braking in time.
Because the lever principle manipulation keep plate 19 using pedal arm 12 is pushed, trampling by pedal 11 can be very good
Amplitude is realized to control keep plate 19 to push amplitude and flexibly controls the steering of air force ship and brake.
As shown in figure 4, air force ship brake apparatus also includes：Brake pedal 2；Brake pedal 2 is located at the pedal in left side
11 and right side pedal 11 between, and half mulching is on the pedal 11 in left side and the pedal 11 on right side.
When being braked due to trampling both sides pedal 11 simultaneously, it may appear that trample amplitude difference, keep plate 19 pushes amplitude
Difference, causes the collateral resistance of hull two different, the situation for causing hull control unstable in braking procedure.Between both sides pedal 11
Increase by one can control the brake pedal 2 that both sides pedal 11 is pushed simultaneously, when needing brake hard, and only need to trample braking steps on
Plate 2, because the half mulching of brake pedal 2 is on both sides pedal 11, it is possible to drive both sides pedal 11 while pushing, simultaneously
Both sides pedal 11 is not interfered with individually to trample yet.
As shown in Figure 5 and Figure 6, transfer 1 also includes rear end expansion link retainer ring 110；Rear end expansion link retainer ring 110
It is made up of fixed support 1101 and retainer ring 1102；Fixed support one end is fixedly connected with stern stern transom plate, and the other end is with consolidating
Determine ring 1102 to be hinged；Rear end expansion link 17 passes through retainer ring 1102, and is fixedly connected with retainer ring 1102；Keep plate 19 is also wrapped
Include：Fixed-hinged support 1901；Fixed-hinged support 1901 is arranged at the surface of keep plate 19；Rear end expansion link 17 passes through fixed-hinged support
1901 are hinged with keep plate 19.
During keep plate 19 pushes and recovered horizontality, rear end expansion link 17 needs certain angle change
Keep plate 19 can be coordinated to be moved well, if simply fixed to rear end expansion link 17, only be allowed to fixed, then
The movement effects of keep plate 19 can be influenceed, so as to influence braking and turning efficiency.Increase a rear end expansion link retainer ring 110,
Allow rear end expansion link 17 to pass through the retainer ring 1102 being hinged on fixed support 1101, pass through fixed support 1101 and retainer ring
Movement angle between 1102 adapts to and controlled the angle change of the rear end expansion link 17 in the motion process of keep plate 19, simultaneously
Rear end expansion link 17 can be controlled to occur without displacement.
Simultaneously in order to preferably coordinate keep plate 19 and rear end expansion link 17 to move, fixation is provided with braking plate surface
Hinged-support 1901, rear end expansion link 17 is hinged by fixed-hinged support with keep plate 19 so that rear end expansion link 17 and keep plate
Can more flexibly it be moved between 19.
As shown in fig. 7, hydraulic tube 16 is the hydraulic tube that two ends are connected with single-acting expansion hydro-cylinder 161, its hydraulic cylinder 161
In piston rod on be also set with spring for reset.
In addition to the implementation, the present invention can also have other embodiment, all use equivalent substitution or equivalent transformation shape
Into technical scheme, all fall within the protection domain of application claims.
Claims (8)
1. a kind of air force ship brake apparatus, it is characterised in that by air force ship direct of travel, by being symmetricly set on air
The transfer (1) of the power-driven light boat left and right sides is constituted；
The transfer (1) includes：It is pedal (11), pedal arm (12), Flexible Reset part (13), movable axle sleeve (14), preceding
Hold expansion link (15), hydraulic tube (16), rear end expansion link (17), fixed plate (18) and keep plate (19)；
The pedal (11) is located in driving cabin, is fixedly connected with the pedal arm (12) one end；The pedal arm (12) is another
End is through the movable axle sleeve (14) being connected with cabin truss, with being fixedly connected on towards fore direction one end on cabin truss
The other end of the Flexible Reset part (13) is fixedly connected, while also being cut with scissors with the front end expansion link (15) towards stern direction
Connect；The front end expansion link (15) is with setting one end of the rear end expansion link (17) on the quarter to pass through the hydraulic tube (16)
It is connected；The fixed plate (18) is fixedly connected with stern transom plate bottom on the quarter, is hinged with the keep plate (19)；Stretch the rear end
Contracting bar (17) other end is hinged with the keep plate (19), drives the keep plate (19) to spin upside down.
2. air force ship brake apparatus as claimed in claim 1, it is characterised in that also including brake pedal (2)；The system
Dynamic pedal (2) is located between the pedal (11) in left side and the pedal (11) on right side, and half mulching left side pedal (11) with
And on the pedal (11) on right side.
3. air force ship brake apparatus as claimed in claim 1 or 2, it is characterised in that the transfer (1) also includes
Rear end expansion link retainer ring (110)；The rear end expansion link retainer ring (110) is by fixed support (1101) and retainer ring
(1102) constitute；Described fixed support (1101) one end is fixedly connected with stern stern transom plate, and the other end is cut with scissors with retainer ring (1102)
Connect；The rear end expansion link (17) passes through retainer ring (1102), and is fixedly connected with retainer ring (1102).
4. air force ship brake apparatus as claimed in claim 1 or 2, it is characterised in that movable axle sleeve (14) distance
The vertical range of hull bottom is equal to the pedal (11) apart from 1/3rd of the vertical range of hull bottom.
5. air force ship brake apparatus as claimed in claim 1 or 2, it is characterised in that the keep plate (19) also includes
Fixed-hinged support (1901)；The fixed-hinged support (1901) is arranged in the keep plate (19) table plane；Stretch the rear end
Contracting bar (17) is hinged by fixed-hinged support (1901) with the keep plate (19).
6. air force ship brake apparatus as claimed in claim 1 or 2, it is characterised in that the keep plate (19) is plough type
Keep plate.
7. air force ship brake apparatus as claimed in claim 1 or 2, it is characterised in that the keep plate (19) is surface
Plough type keep plate provided with anti-skid stud.
8. air force ship brake apparatus as claimed in claim 1 or 2, it is characterised in that the hydraulic tube (16) is two ends
The hydraulic tube of single-acting expansion hydro-cylinder 161 is connected with, the bullet for reset is also set with the piston rod in its hydraulic cylinder 161
Spring.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710295442.7A CN106985994A (en) | 2017-04-28 | 2017-04-28 | A kind of air force ship brake apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710295442.7A CN106985994A (en) | 2017-04-28 | 2017-04-28 | A kind of air force ship brake apparatus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106985994A true CN106985994A (en) | 2017-07-28 |
Family
ID=59418362
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710295442.7A Pending CN106985994A (en) | 2017-04-28 | 2017-04-28 | A kind of air force ship brake apparatus |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106985994A (en) |
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| JPH07196093A (en) * | 1994-10-27 | 1995-08-01 | Yamaha Motor Co Ltd | Water leisure boat |
| CN2425852Y (en) * | 1999-09-27 | 2001-04-04 | 陆银河 | Ship safety butter |
| CN2554087Y (en) * | 2002-06-19 | 2003-06-04 | 胡德贵 | Double-oar motorboat without rudder |
| US7007621B1 (en) * | 2004-10-15 | 2006-03-07 | Todd Bootes | Braking system for a personal watercraft |
| US7168384B1 (en) * | 2006-01-13 | 2007-01-30 | Willis Charles M | Personal water craft brake apparatus |
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| CN201971147U (en) * | 2011-04-14 | 2011-09-14 | 蒋同跃 | Marine hydraulic braking and steering gear |
| CN202193170U (en) * | 2011-07-05 | 2012-04-18 | 赵凤银 | Ship, naval vessel or submarine with speed reducing and turn damping board device |
| CN102963517A (en) * | 2012-12-06 | 2013-03-13 | 王军辉 | Ship with bilateral two-way power-assisted brake propeller |
| CN204362538U (en) * | 2014-12-23 | 2015-06-03 | 湖北工业大学 | A kind of novel hydraulic braking in a turn system for boat tractor |
| US9180953B1 (en) * | 2014-04-29 | 2015-11-10 | Roger Durand | Airboat braking system |
| CN204846333U (en) * | 2015-06-15 | 2015-12-09 | 帅晓华 | Pedal bionical fish pectoral fin quant propeller |
| CN105292426A (en) * | 2014-07-02 | 2016-02-03 | 鲁一南 | Multifunctional ship speed controlling fin |
| CN105579339A (en) * | 2013-08-21 | 2016-05-11 | 夸德罗弗伊尔生产和服务有限责任公司 | Vessel control system with movable underwater wings |
| CN105620702A (en) * | 2016-01-18 | 2016-06-01 | 虞静丽 | Improved electric ship provided with brake device and used for municipal administration |
| CN106184689A (en) * | 2016-07-31 | 2016-12-07 | 王立新 | Naval vessels brake flap |
| CN206939024U (en) * | 2017-04-28 | 2018-01-30 | 江苏科技大学 | A kind of air force ship brake apparatus |
-
2017
- 2017-04-28 CN CN201710295442.7A patent/CN106985994A/en active Pending
Patent Citations (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH07196093A (en) * | 1994-10-27 | 1995-08-01 | Yamaha Motor Co Ltd | Water leisure boat |
| CN2425852Y (en) * | 1999-09-27 | 2001-04-04 | 陆银河 | Ship safety butter |
| CN2554087Y (en) * | 2002-06-19 | 2003-06-04 | 胡德贵 | Double-oar motorboat without rudder |
| US7007621B1 (en) * | 2004-10-15 | 2006-03-07 | Todd Bootes | Braking system for a personal watercraft |
| US7168384B1 (en) * | 2006-01-13 | 2007-01-30 | Willis Charles M | Personal water craft brake apparatus |
| CN101580110A (en) * | 2008-05-13 | 2009-11-18 | 北京新漩世为科技有限公司 | Power-assisted steering device of ship |
| CN102100137A (en) * | 2010-12-15 | 2011-06-22 | 杨太平 | Brake steering mechanism based on wheel-controlled single side separation |
| CN201971147U (en) * | 2011-04-14 | 2011-09-14 | 蒋同跃 | Marine hydraulic braking and steering gear |
| CN202193170U (en) * | 2011-07-05 | 2012-04-18 | 赵凤银 | Ship, naval vessel or submarine with speed reducing and turn damping board device |
| CN102963517A (en) * | 2012-12-06 | 2013-03-13 | 王军辉 | Ship with bilateral two-way power-assisted brake propeller |
| CN105579339A (en) * | 2013-08-21 | 2016-05-11 | 夸德罗弗伊尔生产和服务有限责任公司 | Vessel control system with movable underwater wings |
| US9180953B1 (en) * | 2014-04-29 | 2015-11-10 | Roger Durand | Airboat braking system |
| CN105292426A (en) * | 2014-07-02 | 2016-02-03 | 鲁一南 | Multifunctional ship speed controlling fin |
| CN204362538U (en) * | 2014-12-23 | 2015-06-03 | 湖北工业大学 | A kind of novel hydraulic braking in a turn system for boat tractor |
| CN204846333U (en) * | 2015-06-15 | 2015-12-09 | 帅晓华 | Pedal bionical fish pectoral fin quant propeller |
| CN105620702A (en) * | 2016-01-18 | 2016-06-01 | 虞静丽 | Improved electric ship provided with brake device and used for municipal administration |
| CN106184689A (en) * | 2016-07-31 | 2016-12-07 | 王立新 | Naval vessels brake flap |
| CN206939024U (en) * | 2017-04-28 | 2018-01-30 | 江苏科技大学 | A kind of air force ship brake apparatus |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
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| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170728 |
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| RJ01 | Rejection of invention patent application after publication |