CN203638088U - Rotor craft - Google Patents
Rotor craft Download PDFInfo
- Publication number
- CN203638088U CN203638088U CN201320661184.7U CN201320661184U CN203638088U CN 203638088 U CN203638088 U CN 203638088U CN 201320661184 U CN201320661184 U CN 201320661184U CN 203638088 U CN203638088 U CN 203638088U
- Authority
- CN
- China
- Prior art keywords
- housing
- slide plate
- plate body
- rotor craft
- battery cover
- 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.)
- Expired - Lifetime
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- 238000003780 insertion Methods 0.000 claims description 34
- 230000037431 insertion Effects 0.000 claims description 34
- 238000007373 indentation Methods 0.000 claims description 16
- 230000006978 adaptation Effects 0.000 claims description 4
- 238000009434 installation Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 238000005452 bending Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 238000001746 injection moulding Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
- 230000033764 rhythmic process Effects 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
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- Battery Mounting, Suspending (AREA)
Abstract
The utility model provides a rotor craft, comprising a shell and a landing gear, wherein a locating cavity is arranged on the shell; an inserting section inserted into the locating cavity to fix the landing gear on the shell in advance is arranged on the landing gear; the landing gear is screwed and fastened with the shell. The rotor craft disclosed by the utility model is convenient and fast to install.
Description
Technical field
The utility model relates to vehicle technology field, relates in particular to a kind of rotor craft.
Background technology
In the prior art, rotor craft comprises housing and the alighting gear being connected with housing.But alighting gear relies on multiple screws and housing locking conventionally, at least needing to make a call to 2 screws could locate.In the time using many screws, need pretension screw, then adjust the position of alighting gear, then screw is screwed tight completely.Therefore how to assemble easily alighting gear and housing is problem demanding prompt solution.
Utility model content
Main purpose of the present utility model is to provide a kind of rotor craft, is intended to improve the assembling convenience of alighting gear and housing.
The utility model provides a kind of rotor craft, comprise housing and alighting gear, described housing is provided with positioning chamber, and described alighting gear is provided with and inserts in described positioning chamber described alighting gear to be pre-fixed to the insertion section on described housing, and described alighting gear and described housing are spirally connected fastening.
Preferably, the two opposite side walls of the insertion section of described alighting gear is respectively provided with at least one location indentations, and described housing is provided with the fitting projection engaging with described location indentations in the position of the described location indentations of correspondence.
Preferably, described alighting gear comprises support beam and crossbeam for contacting with ground, and one end of described support beam is connected with described crossbeam, and the other end of described support beam is installed with described insertion section, and described crossbeam is the high shape that arches upward in low centre, two ends.
Preferably, the two ends of described crossbeam are respectively connected with a described support beam, are connected to two the described support beam opposite tilts setting on same described crossbeam.
Preferably, the junction of described insertion section and described support beam is provided with reinforced rib; The junction of described crossbeam and described support beam is provided with reinforced rib.
Preferably, described housing be provided with have uncovered battery cavities and with the described uncovered battery cover component coordinating, one end of described battery cover component and described housing by bearing pin be rotatablely connected, the other end and described housing be fixed.
Preferably, described battery cover component comprises battery cover body, pressing plate and slide plate, the handle that described slide plate comprises slide plate body and is connected with described slide plate body, described battery cover body is provided with the resigning hole of the slide rail of described slide plate body being installed and being stretched out for described handle, and described pressing plate is packed on described battery cover body and by spacing described slide plate on described slide rail; Described slide plate body can slide along described slide rail in the time that described handle is subject to External Force Acting, and described housing is provided with the recess that slips into or exit for described slide plate.
Preferably, described pressing plate comprises the cantilever beam that pressing plate body and one end connect and can rotate relative to described pressing plate body under external force with described pressing plate body, described cantilever beam is provided with positioning convex, described slide plate body be provided with can with the first detent of described positioning convex adaptation and the second detent; Described slide plate body slips into the state of described recess, described positioning convex and described the first detent clamping; Described slide plate body exits the state of described recess, described positioning convex and described the second detent clamping.
Preferably, on described battery cover body, be also provided with registration mast, described pressing plate body is provided with the knock hole coordinating with described registration mast.
Preferably, described housing is provided with oar arm and range light, and described range light is installed in the bottom of described oar arm.
Rotor craft disclosed in the utility model, by the insertion section of alighting gear is inserted in the positioning chamber of housing, thereby plays the effect pre-fixing.Only need update can complete pre-fixing of alighting gear and housing, and this alighting gear and housing can not relatively move or swing under the effect pre-fixing, thus on this basis pre-fixing the urgent screw for fastening alighting gear and housing easily.Therefore the utlity model has advantage quick and easy for installation, and only need an installation personnel to install, reach and save artificial object.
Brief description of the drawings
Fig. 1 is the local structure schematic diagram of the utility model rotor craft;
Fig. 2 is the structural representation of the alighting gear in Fig. 1;
Fig. 3 is the structure for amplifying schematic diagram in dashed region in Fig. 2;
Fig. 4 is and the assembling schematic diagram of the battery cover component of Fig. 1 adaptation;
Fig. 5 is the blast structural representation of the battery cover component of Fig. 4;
Fig. 6 is the longitudinal sectional view of the battery cover component of Fig. 4.
Realization, functional characteristics and the advantage of the utility model object, in connection with embodiment, are described further with reference to accompanying drawing.
Detailed description of the invention
Should be appreciated that specific embodiment described herein is only in order to explain the utility model, and be not used in restriction the utility model, the technical characterictic in the utility model can combination in any not conflicting in the situation that.
Understand for unified, now define the direction of taking off of rotor craft for upwards (top), the direction of landing is downward (end).
Please refer to Fig. 1, this rotor craft, comprises housing 1 and alighting gear 2.Housing 1 is provided with positioning chamber 11, and alighting gear 2 is provided with the insertion section 21 suitable with positioning chamber 11.In assembling, first the insertion section of alighting gear 2 21 is inserted in positioning chamber 11 to alighting gear 2 and housing 1 are pre-fixed, and then alighting gear 2 and housing 1 are spirally connected fastening.
The utility model is by the insertion section of alighting gear 2 21 is inserted in the positioning chamber 11 of housing 1, thereby plays the effect pre-fixing.Only need update can complete pre-fixing of alighting gear 2 and housing 1, and this alighting gear 2 can not relatively move or swing under the effect pre-fixing with housing 1, thereby can be easily on this basis pre-fixing urgent for fastening alighting gear 2 screw with housing 1, therefore the utlity model has advantage quick and easy for installation, and only need an installation personnel to install, reach and save artificial object.
The positioning chamber 11 of housing 1 can be the bottom of being located at housing 1, also can be located at the sidepiece of housing 1, also can be located at the top of housing 1.Meanwhile, in positioning chamber 11, insert for the insertion section 21 of alighting gear 2 uncovered can be towards vertical direction, also can be towards horizontal direction.Particularly, in the present embodiment, positioning chamber 11 is located at the bottom of housing 1, meanwhile, and this positioning chamber 11 uncovered towards horizontal direction.Therefore, the insertion section 21 of alighting gear 2 is horizontal, with from this positioning chamber 11 of uncovered insertion of positioning chamber 11.Particularly, in order to make insertion section 21 for level, can be by the end bending of alighting gear 2 to form insertion section 21, or use the mode such as weld, be spirally connected that insertion section 21 is fixed on alighting gear 2.In other embodiments, also positioning chamber 11 can be arranged to the side of housing 1, and downward uncovered, the insertion section 21 of alighting gear 2 is through the uncovered positioning chamber 11 that inserts from the bottom up of positioning chamber 11.
Please in the lump referring to Fig. 2 and Fig. 3, go out positioning chamber 11 in order to make the insertion section 21 of alighting gear 2 insert to be not easy to slippage after positioning chamber 11, preferably, in the two opposite side walls of the insertion section 21 of alighting gear 2, be respectively provided with two location indentations 211; Housing 1 is provided with the fitting projection (invisible in Fig. 1) engaging with location indentations 211 in the position of corresponding location indentations 211.In fitting process, insert in the process of positioning chamber 11 of housing 1 in the insertion section 21 of alighting gear 2, the location indentations 211 of insertion section 21 can fasten with fitting projection, thereby the insertion section 21 that makes alighting gear 2 insert after positioning chamber 11 not can automatic trip from, thereby make alighting gear 2 and housing 1 to pre-fix effect more stable, and can inform that operator insertion section 21 is inserted in positioning chamber 11 and put in place.
The opposing sidewalls of the horizontal direction of the insertion section 21 of alighting gear 2 can be provided with location indentations 211; The opposing sidewalls that can be also the above-below direction of the insertion section 21 of alighting gear 2 is provided with location indentations 211; Can certainly on above-mentioned position, be provided with location indentations 211, location indentations 211 is around insertion section 21 1 circles simultaneously.Further, the location indentations 211 on the one-sided wall of the insertion section 21 of alighting gear 2 can be set to one or more, in the present embodiment, is only arranged on the horizontal direction of insertion section 21 and as two as example, describes in detail taking location indentations 211.
Particularly, in this rotor craft, alighting gear 2 comprises support beam 22 and crossbeam 23, and crossbeam 23 is for contacting with ground in the time that aircraft lands, and support beam 22 makes aircraft and ground keep certain distance for supporting aircraft.Wherein one end of support beam 22 is connected with crossbeam 23, and the other end of support beam 22 is installed with insertion section 21.Particularly, in the present embodiment, the end bending of this support beam 22 forms this insertion section 21 after flattening, and insertion section 21 is one-body molded with support beam 22.In this programme the crossbeam 23 of alighting gear 2 and ground to contact optimum be line contact, still in actual injection molding process, the contraction during due to material cooled, can make crossbeam 23 be out of shape and become the shape that arches upward.When this crossbeam 23 that is the shape that arches upward is when upwards arching upward, crossbeam 23 has two contact points with ground, when rotor craft is stopped, keeps balance not affect; But when crossbeam 23 is when arching upward, between crossbeam 23 and ground, only have a contact point downwards, can not effectively ensure balance when rotor craft is stopped.Therefore, unsettled phenomenon occurs when occurring that rotor craft is stopped, so in the present embodiment, the crossbeam 23 of alighting gear 2 is to be the high shape that arches upward in low centre, two ends, the state upwards arching upward.
In the present embodiment, further, the two ends of same crossbeam 23 are respectively connecting a support beam 22; In other embodiment, also can be set to 23 only with one support beams 22 of a crossbeam and be connected, can be now that one end of crossbeam 23 is connected with one end of support beam 22, can be also the middle part that one end of support beam 22 is connected to crossbeam 23.Further, in the present embodiment, two support beams, the 22 opposite tilt settings that are connected with the two ends of same crossbeam 23 respectively, thus make in the time that aircraft lands, the extending direction of the direction of the impulsive force being subject to and support beam 22 at an angle, can cushion the effect of landing impulsive force.Particularly, two opposite tilt crossbeams 23 can be 70 degree, 60 degree, 50 degree equal angles with the angle of support beam 22 respectively.
In order to make the structure of alighting gear more stable, intensity is better, is provided with reinforced rib 24 in insertion section 21 and the junction of support beam 22.Further, be also provided with reinforced rib 25 in crossbeam 23 and the junction of support beam 22.
In the present embodiment, for the ease of the dismounting of battery, also improve the structure of equipped with battery part.
Incorporated by reference to referring to Fig. 1 and Fig. 4, in this rotor craft, housing 1 be provided with have the battery cavities 12 of uncovered (in figure not mark) and with this uncovered battery cover component coordinating 6.Battery cavities 12 is for holding battery, uncovered for packing into and take out for battery on battery cavities 12.One end of battery cover component 6 and housing 1 by bearing pin 5 be rotatablely connected, the other end and housing 1 be fixed.
Particularly, housing 1 in form battery cavities 12 a sidewall marginating compartment be provided with two axis pin bases 121, the two ends of bearing pin 5 can be inserted respectively in these two axis pin bases 121 to make bearing pin 5 fixing with housing 1.Battery cover component 6 comprises battery cover body 3, wherein, battery cover body 3 side of two axis pin bases 121 in corresponding housing 1 is provided with bearing pin pipe 31, bearing pin 5 can be through two axis pin bases 121 and this bearing pin pipe 31 so that battery cover component 6 be rotatably connected with housing 1.Housing 1 by bearing pin 5 pivot joints, makes battery cover component 6 and housing 1 can thoroughly not separate in the time of released state with battery cover component 6, has avoided battery cover 3 to lose in the time having changed battery; Battery cover component 6 need to being fastened while putting to pre-fixing of housing 1, also only needing to rotate battery cover component 6 can be fastened on battery cover component 6 on the position of these battery cavities 12 correspondences accurately, thereby has the effect of quick assembling.
Please in the lump referring to Fig. 5 and Fig. 6, further, battery cover component 6 also comprises pressing plate 4 and slide plate 7, the handle 711 that slide plate 7 comprises slide plate body 71 and is connected with slide plate body 71, and battery cover body 3 is provided with the resigning hole 34 of the slide rail 33 of slide plate body 71 being installed and being stretched out for handle 711.Pressing plate 4 is packed on battery cover body 3 and by slide plate 7 and is limited on slide rail 33.Particularly, on battery cover body 3, convex with erection column 32(double-screw bolt), pressing plate 4 is provided with the mounting hole corresponding with erection column 32, and screw passes mounting hole and is screwed in erection column 32 so that pressing plate 4 is fixedly connected with erection column 32.Slide plate body 71 can slide along slide rail 33 in the time that handle 711 is subject to External Force Acting.Housing 1 is provided with the recess 122 that slips into or exit for slide plate 7, and, in the time that a part for slide plate body 71 is inserted into recess 122, battery cover component 6 locks together with housing 1; In the time that slide plate body 71 exits from recess 122, battery cover component 6 can rotate relatively with housing 1.
In prior art, there is the multiple slide plate 7 that makes to remain on the state that slips into recess 122, keep battery cover component 6 and housing 1 at the state of locking together, only enumerate a kind of technical scheme simple in structure at this, and do not enumerate.In the present embodiment, pressing plate 4 comprises pressing plate body 41 and cantilever beam 413.One end of this cantilever beam 413 is connected with pressing plate body 41, and can rotate relative to pressing plate body 41 under external force.Cantilever beam 413 is provided with positioning convex 411, slide plate body 71 be provided with can with the first detent 712 of positioning convex 411 adaptations and the second detent 713.Due to the easy deformation of cantilever beam 413, the pressure of the positioning convex 411 that therefore can reduce pressing plate 4 to slide plate body 71, thus make the movement of slide plate 7 lighter.Slip into the state of the recess 122 of housing 1 at slide plate body 71, positioning convex 411 and the first detent 712 clamp; Exit the state of the recess 122 of housing 1 at slide plate body 71, positioning convex 411 and the second detent 713 clamp.Due in the time that this positioning convex 411 slips into the first detent 712 or the second detent 713, obvious generation pause and transition in rhythm or melody sense is moved and put in place with reminding user, thereby can avoid that the distance of user's moving slide board 7 is excessive or miles of relative movement is not enough.
The shape of location protrusion 411 can be multiple, and in the present embodiment, it is the strip extending perpendicular to slide plate body 71 direction of slips that location protrudes 411; In other embodiments, location protrudes 411 also can adopt point-like, polygon-shaped etc.
In order to make the installation of pressing plate 4 more quick and convenient, preferably, on battery cover body 3, be also provided with registration mast 35, pressing plate 4 is provided with the knock hole 414 coordinating with registration mast 35.When mounted, the knock hole of pressing plate 4 414 is aimed to registration mast 35 and inserted, then pressing plate 4 is screwed tight on erection column 32.
For the circuit that makes this rotor craft is easier to cabling.Preferably, housing 1 is provided with oar arm 13 and range light (not shown), and range light is installed in the bottom of oar arm 13.In prior art, the end of oar arm 13 is provided with the motor that drives screw propeller, therefore, in oar arm 13, is provided with circuit.The bottom that range light is installed in to oar arm 13 can be easy to when aerial in rotary-wing flight be observed by operator on the one hand; Can directly the circuit of range light be connected on the other hand to the circuit for motor power supply in oar arm, the supply line that is located at the range light of oar arm 13 belows can simplify, and avoided the interference to housing 1 circuit configuration, and producers is more easy to operate.
The foregoing is only preferred embodiment of the present utility model; not thereby limit the scope of the claims of the present utility model; every equivalent structure or conversion of equivalent flow process that utilizes the utility model specification sheets and accompanying drawing content to do; or be directly or indirectly used in other relevant technical fields, be all in like manner included in scope of patent protection of the present utility model.
Claims (10)
1. a rotor craft, comprise housing and alighting gear, it is characterized in that, described housing is provided with positioning chamber, described alighting gear is provided with and inserts in described positioning chamber described alighting gear to be pre-fixed to the insertion section on described housing, and described alighting gear and described housing are spirally connected fastening.
2. rotor craft according to claim 1, it is characterized in that, the two opposite side walls of the insertion section of described alighting gear is respectively provided with at least one location indentations, and described housing is provided with the fitting projection engaging with described location indentations in the position of the described location indentations of correspondence.
3. rotor craft according to claim 1, it is characterized in that, described alighting gear comprises support beam and crossbeam for contacting with ground, one end of described support beam is connected with described crossbeam, the other end of described support beam is installed with described insertion section, and described crossbeam is the high shape that arches upward in low centre, two ends.
4. rotor craft according to claim 3, is characterized in that, the two ends of described crossbeam are respectively connected with a described support beam, is connected to two the described support beam opposite tilts setting on same described crossbeam.
5. rotor craft according to claim 4, is characterized in that, the junction of described insertion section and described support beam is provided with reinforced rib; The junction of described crossbeam and described support beam is provided with reinforced rib.
6. according to the rotor craft described in claim 1 to 5 any one, it is characterized in that, described housing be provided with have uncovered battery cavities and with the described uncovered battery cover component coordinating, one end of described battery cover component and described housing by bearing pin be rotatablely connected, the other end and described housing be fixed.
7. rotor craft according to claim 6, it is characterized in that, described battery cover component comprises battery cover body, pressing plate and slide plate, the handle that described slide plate comprises slide plate body and is connected with described slide plate body, described battery cover body is provided with the resigning hole of the slide rail of described slide plate body being installed and being stretched out for described handle, and described pressing plate is packed on described battery cover body and by spacing described slide plate on described slide rail; Described slide plate body can slide along described slide rail in the time that described handle is subject to External Force Acting, and described housing is provided with the recess that slips into or exit for described slide plate.
8. rotor craft according to claim 7, it is characterized in that, described pressing plate comprises the cantilever beam that pressing plate body and one end connect and can rotate relative to described pressing plate body under external force with described pressing plate body, described cantilever beam is provided with positioning convex, described slide plate body be provided with can with the first detent of described positioning convex adaptation and the second detent; Described slide plate body slips into the state of described recess, described positioning convex and described the first detent clamping; Described slide plate body exits the state of described recess, described positioning convex and described the second detent clamping.
9. rotor craft according to claim 8, is characterized in that, on described battery cover body, is also provided with registration mast, and described pressing plate body is provided with the knock hole coordinating with described registration mast.
10. according to the rotor craft described in claim 1 to 5 any one, it is characterized in that, described housing is provided with oar arm and range light, and described range light is installed in the bottom of described oar arm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320661184.7U CN203638088U (en) | 2013-10-24 | 2013-10-24 | Rotor craft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320661184.7U CN203638088U (en) | 2013-10-24 | 2013-10-24 | Rotor craft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203638088U true CN203638088U (en) | 2014-06-11 |
Family
ID=50869355
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320661184.7U Expired - Lifetime CN203638088U (en) | 2013-10-24 | 2013-10-24 | Rotor craft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203638088U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105083540A (en) * | 2015-06-24 | 2015-11-25 | 广州飞米电子科技有限公司 | Aircraft, aircraft body and foot stand |
| CN105691599A (en) * | 2016-01-20 | 2016-06-22 | 广东司马航模实业有限公司 | Undercarriage disassembly and assembly structure of aircraft |
| WO2016161975A1 (en) * | 2015-04-08 | 2016-10-13 | 优利科技有限公司 | Aircraft fuselage and aircraft with same |
| CN106275461A (en) * | 2016-08-26 | 2017-01-04 | 深圳电航空技术有限公司 | The battery box structure of unmanned plane and unmanned plane |
| EP3239044A1 (en) * | 2014-10-27 | 2017-11-01 | Guangzhou Xaircraft Technology Co., Ltd. | Rotorcraft and assembly and disassembly structure for foot stand and airframe of rotorcraft |
| WO2017185487A1 (en) * | 2016-04-28 | 2017-11-02 | 深圳市龙云创新航空科技有限公司 | Battery fixing and mounting structure for battery self-dismounting unmanned aerial vehicle |
-
2013
- 2013-10-24 CN CN201320661184.7U patent/CN203638088U/en not_active Expired - Lifetime
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3239044A1 (en) * | 2014-10-27 | 2017-11-01 | Guangzhou Xaircraft Technology Co., Ltd. | Rotorcraft and assembly and disassembly structure for foot stand and airframe of rotorcraft |
| WO2016161975A1 (en) * | 2015-04-08 | 2016-10-13 | 优利科技有限公司 | Aircraft fuselage and aircraft with same |
| CN105083540A (en) * | 2015-06-24 | 2015-11-25 | 广州飞米电子科技有限公司 | Aircraft, aircraft body and foot stand |
| CN105083540B (en) * | 2015-06-24 | 2017-04-05 | 广州飞米电子科技有限公司 | Aircraft, aircraft body and foot rest |
| CN105691599A (en) * | 2016-01-20 | 2016-06-22 | 广东司马航模实业有限公司 | Undercarriage disassembly and assembly structure of aircraft |
| CN105691599B (en) * | 2016-01-20 | 2018-10-16 | 广东司马航模实业有限公司 | A kind of undercarriage disassembly and assembly structure of aircraft |
| WO2017185487A1 (en) * | 2016-04-28 | 2017-11-02 | 深圳市龙云创新航空科技有限公司 | Battery fixing and mounting structure for battery self-dismounting unmanned aerial vehicle |
| CN106275461A (en) * | 2016-08-26 | 2017-01-04 | 深圳电航空技术有限公司 | The battery box structure of unmanned plane and unmanned plane |
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Legal Events
| Date | Code | Title | Description |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20160303 Address after: Baoan District Shiyan street Shenzhen city Guangdong province 518108 Songbai road Tangtou junctions electric science and Technology Park Patentee after: SHENZHEN AEE TECHNOLOGY Co.,Ltd. Address before: 518108 Guangdong city of Shenzhen province Nanshan District Xili Sunshine Industrial Zone Electric Science and Technology Park Patentee before: SHENZHEN AEE TECHNOLOGY Co.,Ltd. |
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| TR01 | Transfer of patent right |
Effective date of registration: 20191219 Address after: Room 812, enterprise service center, No. 17, section 3, west section of Changjiang North Road, Lingang Economic Development Zone, Yibin City, Sichuan Province Patentee after: Sichuan Yidian Aviation Technology Co.,Ltd. Address before: Baoan District Shiyan street Shenzhen city Guangdong province 518108 Songbai road Tangtou junctions electric science and Technology Park Patentee before: SHENZHEN AEE TECHNOLOGY Co.,Ltd. |
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| TR01 | Transfer of patent right | ||
| CX01 | Expiry of patent term |
Granted publication date: 20140611 |
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| CX01 | Expiry of patent term |