CN108100220A - Flight controller stent and GPS antenna supporting rack assembly - Google Patents
Flight controller stent and GPS antenna supporting rack assembly Download PDFInfo
- Publication number
- CN108100220A CN108100220A CN201711256682.2A CN201711256682A CN108100220A CN 108100220 A CN108100220 A CN 108100220A CN 201711256682 A CN201711256682 A CN 201711256682A CN 108100220 A CN108100220 A CN 108100220A
- Authority
- CN
- China
- Prior art keywords
- plate
- flight controller
- gps antenna
- frustum
- supporting rack
- 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
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims abstract description 11
- 238000005192 partition Methods 0.000 claims description 24
- 238000001746 injection moulding Methods 0.000 claims description 4
- 229910000831 Steel Inorganic materials 0.000 claims description 3
- 239000000203 mixture Substances 0.000 claims description 3
- 239000010959 steel Substances 0.000 claims description 3
- 230000002035 prolonged effect Effects 0.000 claims 1
- 238000004519 manufacturing process Methods 0.000 abstract description 9
- 239000011435 rock Substances 0.000 abstract description 4
- 210000002683 foot Anatomy 0.000 description 15
- 238000005516 engineering process Methods 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 238000012545 processing Methods 0.000 description 4
- 238000009434 installation Methods 0.000 description 3
- 208000020442 loss of weight Diseases 0.000 description 3
- 238000005507 spraying Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000004458 analytical method Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 239000002917 insecticide Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/36—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like adapted to receive antennas or radomes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/12—Supports; Mounting means
- H01Q1/1242—Rigid masts specially adapted for supporting an aerial
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
Abstract
The invention discloses a kind of flight controller stents and GPS antenna supporting rack assembly, flight controller stent is double-deck box structure, GPS antenna supporting rack is installed at the middle part of flight controller rack plate top surface, the GPS antenna supporting rack is made of bearing, upright bar and pedestal, the bearing is disc structure, the first up big and down small frustum is provided in the center of rest base, the upper end of upright bar is inserted in by first frustum, the lower end of upright bar is provided with pedestal, which is made of the support feet of the second intermediate frustum and periphery.The flight controller stent of the present invention using boxlike double-layer structure, it is not only simple in structure, occupy little space, production cost it is low, and installed convenient for flight controller, be not susceptible to rock, reliability is splendid.GPS antenna supporting rack is arranged on flight controller stent, and connection is firm, and stability is good.
Description
Technical field
The invention belongs to technical field of agricultural machinery, specifically, the flight controller more particularly on vehicle-mounted sprayer
Stent and GPS antenna supporting rack assembly.
Background technology
With the development of society, the progress of science and technology, farmland sprays insecticide progressively completed by unmanned spraying machine on a large scale.
Flight controller and GPS antenna are the important components on vehicle-mounted sprayer, are typically mounted on the stent specially made.It is existing
Flight controller stent and the GPS antenna supporting rack individual independent as two, it is complicated, occupied space is big, production cost
Height is not only not easy to install, and stability is poor, and flight controller and GPS antenna easily rock.
The content of the invention
In view of the drawbacks described above of the prior art, the technical problems to be solved by the invention are to provide a kind of flight controller
Stent and GPS antenna supporting rack assembly.
Technical scheme is as follows：A kind of flight controller stent and GPS antenna supporting rack assembly, are controlled including flight
Device stent and GPS antenna supporting rack processed, it is characterised in that：The flight controller stent has top plate and bottom plate, the top of top
Plate is parallel with the bottom plate of lower section, left plate is fixedly connected between the top plate and the left end of both bottom plates, in the upper of left plate
Portion offers bar hole, is fixedly connected with right plate between top plate and the right end of both bottom plates, and left plate and right plate are and top plate
Perpendicular, the position of middle and lower part is provided with partition plate between the top plate and bottom plate, and the left and right ends of the partition plate are vertically fixed on
On corresponding side plate, the partition plate will be separated into two layers of cassette space, and upper strata cassette space up and down between top plate and bottom plate
Front and back end is open, is respectively equipped with front vertical plate and back vertical plate in the front and back end of lower floor's cassette space, the upper end of each riser and partition plate
Plane perpendicular is fixed, and the lower end of each riser and the front end of bottom plate or rear end are fixed, the left and right ends of each riser respectively with respective side
The medial surface of plate is mutually fixed, and door v notch v, the bottom of the rear end of the left plate are equipped in the lower part of the left plate or right plate
Portion integrally extends backwards, forms the first convex block, and the left part of the partition plate rear end integrally extends backwards, forms the second convex block；
GPS antenna supporting rack is installed at the middle part of the top plate top surface, the GPS antenna supporting rack is by bearing, upright bar and bottom
Seat composition, the bearing are disc structure, the first up big and down small frustum are provided in the center of rest base, first frustum
The upper end of upright bar is inserted in, and the first frustum and upright bar are fixed together；The lower end of the upright bar is provided with pedestal, it should
Pedestal is made of the support feet of the second intermediate frustum and periphery, and second frustum is up-small and down-big, and second frustum is by upright bar
Lower end be inserted in, the second frustum and upright bar are fixed together, second frustum periphery set there are four press circumference
Equally distributed support feet, the root of the support feet are mutually fixed with the second frustum, and each support feet passes through bolt and top
Plate is mutually fixed.
Using above technical scheme, partition plate will be separated into two layers of cassette space up and down, upper strata boxlike between top plate and bottom plate
The posture instrument of flight controller in space is installed, the battery of flight controller, posture instrument and battery are installed in lower floor's cassette space
Layering installation, connection and reasonable arrangement, orderly, connection convenience.The front and back end of upper strata cassette space is open, and it is quick to be conducive to posture instrument
It is packed into；Door v notch v is equipped in the lower part of left plate or right plate, this v notch v is that battery is packed into lower floor's cassette space
Entrance.The top of left plate offers bar hole, which is not only convenient for arrangement cable, and can play loss of weight,
To reduce the weight of entire stent, and save production cost.In addition, the first convex block and the second convex block are formed at the left back end of stent
Grasping part, the grasping part can be used for clamping reserve battery, and the battery that can also directly use flight controller is mounted on
In above-mentioned grasping part, so not only lower floor's boxlike space-saving out can be arranged other parts, and electricity of being more convenient for
The installation or replacement in pond.It can be seen that flight controller stent uses box structure, one side moulding is simple, compact-sized, accounts for
Small with space, making easy to process, production cost is low；On the other hand, flight controller install convenient, stability and reliability
It is good.
GPS antenna supporting rack is arranged on flight controller stent, and the two engagement is close, compact.Bearing is for branch
The fixed GPS antenna of support, bearing is disc structure, big with the contact area of GPS antenna, can ensure that GPS antenna firmly installs.GPS
Antenna support frame is simple in structure, it is easy to process make, assemble it is convenient, can effectively save production cost；GPS antenna supporting rack passes through
Four support feets are connected with flight controller stent, and stability is good, and for spraying machine in operation process, GPS antenna supporting rack will not
It rocks and loosens；Meanwhile good reliability of the present invention, it can fully ensure that the stability of the GPS antenna in the present invention
And fixing.
Heat emission hole is equipped at the middle part of the bottom plate, which is ellipse or circular.On the one hand more than structure radiates
Hole battery can be worked caused by heat Quick diffusing go out, be conducive to battery performance and for a long time use, separately
On the one hand, heat emission hole can play loss of weight, further to mitigate the weight of stent.
Strip hole is equipped in the centre position of the front vertical plate and back vertical plate.On the one hand strip hole is conducive to radiate and subtract
The weight of light front and rear riser；On the other hand it is convenient for outlet.
For the structural strength, water-resistance and shock resistance of lifting bracket, the top plate, bottom plate, left plate, right plate, every
Plate, front vertical plate and back vertical plate are made of aviation laminate.
In order to facilitate processing and fabricating, first convex block is rectangle, and first convex block and left plate are in the same plane；
Second convex block is rectangle, and second convex block and partition plate are in the same plane.
In order to simplify structure, convenient for assembly, and it is firm to ensure that upright bar is connected with frustum, the upper end of the upright bar and the first cone
By being tightly fixed between platform and between the lower end of upright bar and the second frustum.
The upright bar is steel straight tube structure, and such one side convenient material drawing, production cost is low, processing and fabricating is easy；Separately
On the one hand, the structural strength of upright bar is reliable, will not deform or damage.
In order to facilitate processing and fabricating, production cost is reduced, first frustum is structure as a whole with bearing, and passes through injection
Shaping.
In order to facilitate processing and fabricating, production cost is reduced, second frustum is structure as a whole with support feet, and passes through note
It is moulded into type.
Advantageous effect：The flight controller stent of the present invention is using boxlike double-layer structure, upper sheaf space Installation posture instrument, under
Sheaf space install battery, it is not only simple in structure, occupy little space, production cost it is low, and convenient for flight controller install, stablize
Performance is good, is not susceptible to rock, reliability is splendid；GPS antenna supporting rack is arranged on flight controller stent, and connection is firm,
Stability is good, in spraying machine operation process, will not generate the danger rocked, loosen or even come off, reliability is splendid.
Description of the drawings
Fig. 1 is the stereogram at the preceding visual angle of flight controller stent.
Fig. 2 is the stereogram of flight controller stent back angle.
Fig. 3 is the structure diagram that GPS antenna supporting rack is set on flight controller stent.
Fig. 4 is the structure diagram of GPS antenna supporting rack.
Fig. 5 is the top view of pedestal.
Specific embodiment
The invention will be further described with reference to the accompanying drawings and examples：
As shown in Figure 1, Figure 2, Figure 3 shows, flight controller stent of the invention is by top plate 1, bottom plate 2, left plate 3, right plate
4th, the compositions such as partition plate 5, front vertical plate 6 and back vertical plate 7.Wherein, the top plate 1 of top and the bottom plate 2 of lower section are parallel, the top plate 1
It is preferably made with bottom plate 2 of aviation laminate.Heat emission hole 2a is equipped at the middle part of bottom plate 2, heat emission hole 2a is ellipse or circle
Shape.Left plate 3 is fixedly connected between the left end of 2 the two of the top plate 1 and bottom plate, is consolidated between the right end of 2 the two of top plate 1 and bottom plate
Surely right plate 4 is connected, left plate 3 and right plate 4 be preferably made of aviation laminate, and left plate 3 and right plate 4 are and top plate
1 is perpendicular.Bar hole 3b is offered on the top of the left plate 3, bar hole 3b is not only convenient for outlet, but also loss of weight can be played
Effect.
As shown in Figure 1, Figure 2, Figure 3 shows, the position of middle and lower part is provided with partition plate 5 between top plate 1 and bottom plate 2, and the partition plate 5 is excellent
Made of aviation laminate, partition plate 5 is parallel with top plate 1 for choosing.The left end of partition plate 5 is fixed on the inner plate surface of left plate 3, partition plate
5 right end is fixed on the inner plate surface of right plate 4.The partition plate 5 will be separated into two layers of boxlike up and down between top plate 1 and bottom plate 2
Space, and the front and back end of upper strata cassette space is open, upper strata cassette space is used to install the posture instrument of flight controller, lower cassette
Formula space is used to install the battery of flight controller.Front vertical plate 6 and back vertical plate are respectively equipped in the front and back end of lower floor's cassette space
7, the front vertical plate 6 and back vertical plate 7 are preferably made of aviation laminate.Strip hole N is equipped in the centre position of each riser, it is each vertical
The upper end of plate and the plane perpendicular of partition plate 5 are fixed, and lower end and the front end of bottom plate 2 or rear end of each riser are fixed, a left side for each riser
Right both ends are mutually fixed respectively with the medial surface of corresponding side plate.
As shown in Figure 1, Figure 2, Figure 3 shows, door v notch v M is equipped in the lower part of left plate 3 or right plate 4, is lacked by this shape
Battery can be packed into lower floor's cassette space by mouth M.In the present embodiment, door v notch v M is arranged on right plate 4.The left side
The bottom of 3 rear end of plate integrally extends backwards, and it is rectangle, the first convex block 3a and left side to form the first convex block 3a, the first convex block 3a
Plate 3 is in the same plane.The left part of 5 rear end of partition plate integrally extends backwards, forms the second convex block 5a, the second convex block 5a and is
Rectangle, the second convex block 5a and partition plate 5 are in the same plane.First convex block 3a and the second convex block 5a forms grasping part, can
For clamping battery or reserve battery.
As shown in Fig. 3, Fig. 4, Fig. 5, GPS antenna supporting rack, the GPS antenna supporting rack are installed at the middle part of 1 top surface of top plate
It is made of upright bar 10, bearing 8 and pedestal.Wherein, bearing 8 is disc structure, and GPS antenna is fixedly connected at the top of the bearing 8,
The center of 8 bottom of bearing is provided with the first up big and down small frustum 9, and first frustum 9 is structure as a whole with bearing 8, and leads to
Cross injection molding.The upper end of upright bar 10 is inserted in by the first frustum 9, and by being tightly fixed between the first frustum 9 and upright bar 10.
The upright bar 10 is steel straight tube structure, and upright bar 10 and bearing 8 are perpendicular.
As shown in Fig. 3, Fig. 4, Fig. 5, the lower end of upright bar 10 is provided with pedestal, the pedestal is by intermediate 11 He of the second frustum
The support feet 12 of periphery forms, and the second frustum 11 is structure as a whole with support feet 12, and passes through injection molding.Second frustum
11 is up-small and down-big, which is inserted in the lower end of upright bar 10, is consolidated between the second frustum 11 and upright bar 10 by tight fit
It is fixed.It is set in the periphery of the second frustum 11 there are four the support feet 12 by even circumferential distribution, this four support feets 12 are same
In horizontal plane, the direction of the width of support feet 12 from cantilever end toward root gradually increases, and the root of support feet 12 and the second cone
Platform 11 is connected as a single entity.Mounting hole is both provided in each support feet 12, bolt passes through mounting hole and top in support feet 12
Support feet 12 and top plate 1 are fixed together by the via on plate 1.
The preferred embodiment of the present invention described in detail above.It should be appreciated that those of ordinary skill in the art without
Creative work is needed according to the present invention can to conceive and makes many modifications and variations.Therefore, all technologies in the art
Personnel are available by logical analysis, reasoning, or a limited experiment on the basis of existing technology under this invention's idea
Technical solution, all should be in the protection domain being defined in the patent claims.
Claims (9)
1. a kind of flight controller stent and GPS antenna supporting rack assembly, support including flight controller stent and GPS antenna
Frame, it is characterized in that：The flight controller stent has top plate (1) and bottom plate (2), the top plate (1) of top and the bottom plate of lower section
(2) it is parallel, left plate (3) is fixedly connected between the top plate (1) and the left end of both bottom plates (2), in the upper of left plate (3)
Portion offers bar hole (3b), and right plate (4), left plate (3) are fixedly connected between top plate (1) and the right end of both bottom plates (2)
Perpendicular with top plate (1) with right plate (4), the position of middle and lower part is provided with partition plate between the top plate (1) and bottom plate (2)
(5), the left and right ends of the partition plate (5) are vertically fixed on corresponding side plate, the partition plate (5) by top plate (1) and bottom plate (2) it
Between be separated into two layers of cassette space up and down, and the front and back end of upper strata cassette space is open, in the front and back end of lower floor's cassette space point
Not She You front vertical plate (6) and back vertical plate (7), the upper end of each riser and the plane perpendicular of partition plate (5) fix, the lower end of each riser with
The front end or rear end of bottom plate (2) are fixed, and the left and right ends of each riser are mutually fixed respectively with the medial surface of corresponding side plate, on the left side
The lower part of side plate (3) or right plate (4) is equipped with door v notch v (M), and the bottom of the rear end of the left plate (3) is integrally prolonged backwards
It stretches, forms the first convex block (3a), the left part of partition plate (5) rear end integrally extends backwards, forms the second convex block (5a)；
GPS antenna supporting rack is installed at the middle part of the top plate (1) top surface, the GPS antenna supporting rack is by bearing (8), upright bar
(10) and pedestal composition, the bearing (8) are disc structure, and the center of bearing (8) bottom is provided with up big and down small first
The upper end of upright bar (10) is inserted in by frustum (9), first frustum (9), and the first frustum (9) and upright bar (10) are fixedly connected on one
It rises；The lower end of the upright bar (10) is provided with pedestal, the pedestal is by intermediate the second frustum (11) and the support feet of periphery
(12) form, second frustum (11) is up-small and down-big, which is inserted in the lower end of upright bar (10), the second frustum
(11) it is fixed together with upright bar (10), is distributed in the periphery setting of second frustum (11) there are four even circumferential is pressed
Support feet (12), root and the second frustum (11) of the support feet (12) mutually fix, and each support feet (12) passes through
Bolt is mutually fixed with top plate (1).
2. flight controller stent according to claim 1 and GPS antenna supporting rack assembly, it is characterized in that：The upright bar
(10) consolidated between upper end and the first frustum (9) and between the lower end of upright bar (10) and the second frustum (11) by tight fit
It is fixed.
3. flight controller stent according to claim 1 or 2 and GPS antenna supporting rack assembly, it is characterized in that：It is described vertical
Bar (10) is steel straight tube structure.
4. flight controller stent according to claim 3 and GPS antenna supporting rack assembly, it is characterized in that：Described first
Frustum (9) is structure as a whole with bearing (8), and passes through injection molding.
5. flight controller stent according to claim 3 and GPS antenna supporting rack assembly, it is characterized in that：Described second
Frustum (11) is structure as a whole with support feet (12), and passes through injection molding.
6. flight controller stent according to claim 1 and GPS antenna supporting rack assembly, it is characterized in that：At the bottom
The middle part of plate (2) is equipped with heat emission hole (2a), which is ellipse or circular.
7. flight controller stent according to claim 1 and GPS antenna supporting rack assembly, it is characterized in that：Before described
The centre position of riser (6) and back vertical plate (7) is equipped with strip hole (N).
8. flight controller stent and GPS antenna supporting rack assembly according to claim 1 or 6 or 7, it is characterized in that：Institute
Top plate (1), bottom plate (2), left plate (3), right plate (4), partition plate (5), front vertical plate (6) and back vertical plate (7) are stated by aviation layer
Plate is made.
9. flight controller stent according to claim 8 and GPS antenna supporting rack assembly, it is characterized in that：Described first
Convex block (3a) is rectangle, and first convex block (3a) and left plate (3) are in the same plane；Second convex block (5a) is square
Shape, second convex block (5a) and partition plate (5) are in the same plane.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711256682.2A CN108100220A (en) | 2017-12-03 | 2017-12-03 | Flight controller stent and GPS antenna supporting rack assembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711256682.2A CN108100220A (en) | 2017-12-03 | 2017-12-03 | Flight controller stent and GPS antenna supporting rack assembly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108100220A true CN108100220A (en) | 2018-06-01 |
Family
ID=62209057
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711256682.2A Pending CN108100220A (en) | 2017-12-03 | 2017-12-03 | Flight controller stent and GPS antenna supporting rack assembly |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108100220A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114524184A (en) * | 2022-02-21 | 2022-05-24 | 东风汽车集团股份有限公司 | Rotor lamination supports transfer device |
Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2134720Y (en) * | 1992-05-26 | 1993-05-26 | 烟台开发区意埃伊股份有限公司 | Small vertical pole type antenna orientation regulating mechanism |
| CN201937005U (en) * | 2011-03-22 | 2011-08-17 | 北京航空航天大学 | Telescopic antenna grounding device |
| CN202496039U (en) * | 2012-03-05 | 2012-10-17 | 中国人民武装警察部队后勤学院附属医院 | Vehicle communication device integration box |
| CN203467083U (en) * | 2013-06-27 | 2014-03-05 | 成都网动光电子技术股份有限公司 | Temperature regulation box of radio frequency transceiver |
| CN203967563U (en) * | 2014-06-24 | 2014-11-26 | 华东控股集团温州电气有限公司 | A kind of voltage switchgear |
| CN104859858A (en) * | 2015-06-10 | 2015-08-26 | 安静 | Agricultural pesticide application unmanned aerial vehicle |
| CN105539870A (en) * | 2016-01-08 | 2016-05-04 | 苏州大势智慧信息科技有限公司 | Swinging camera oblique photographing device carried on unmanned aerial vehicle |
| CN106428567A (en) * | 2016-10-10 | 2017-02-22 | 浙江同创无人机科技有限公司 | Pest control device adopting combination of unmanned aerial vehicle and pecans |
| CN206371629U (en) * | 2016-12-28 | 2017-08-04 | 戴福良 | Multifunctional router receiver |
| CN206544599U (en) * | 2016-12-27 | 2017-10-10 | 南昌工程学院 | A kind of efficient VTOL carrying air-drop unmanned plane |
| CN107416195A (en) * | 2017-07-03 | 2017-12-01 | 北京航空航天大学 | A kind of imitative hawk grasping system of aerial operation multi-rotor aerocraft |
-
2017
- 2017-12-03 CN CN201711256682.2A patent/CN108100220A/en active Pending
Patent Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2134720Y (en) * | 1992-05-26 | 1993-05-26 | 烟台开发区意埃伊股份有限公司 | Small vertical pole type antenna orientation regulating mechanism |
| CN201937005U (en) * | 2011-03-22 | 2011-08-17 | 北京航空航天大学 | Telescopic antenna grounding device |
| CN202496039U (en) * | 2012-03-05 | 2012-10-17 | 中国人民武装警察部队后勤学院附属医院 | Vehicle communication device integration box |
| CN203467083U (en) * | 2013-06-27 | 2014-03-05 | 成都网动光电子技术股份有限公司 | Temperature regulation box of radio frequency transceiver |
| CN203967563U (en) * | 2014-06-24 | 2014-11-26 | 华东控股集团温州电气有限公司 | A kind of voltage switchgear |
| CN104859858A (en) * | 2015-06-10 | 2015-08-26 | 安静 | Agricultural pesticide application unmanned aerial vehicle |
| CN105539870A (en) * | 2016-01-08 | 2016-05-04 | 苏州大势智慧信息科技有限公司 | Swinging camera oblique photographing device carried on unmanned aerial vehicle |
| CN106428567A (en) * | 2016-10-10 | 2017-02-22 | 浙江同创无人机科技有限公司 | Pest control device adopting combination of unmanned aerial vehicle and pecans |
| CN206544599U (en) * | 2016-12-27 | 2017-10-10 | 南昌工程学院 | A kind of efficient VTOL carrying air-drop unmanned plane |
| CN206371629U (en) * | 2016-12-28 | 2017-08-04 | 戴福良 | Multifunctional router receiver |
| CN107416195A (en) * | 2017-07-03 | 2017-12-01 | 北京航空航天大学 | A kind of imitative hawk grasping system of aerial operation multi-rotor aerocraft |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114524184A (en) * | 2022-02-21 | 2022-05-24 | 东风汽车集团股份有限公司 | Rotor lamination supports transfer device |
| CN114524184B (en) * | 2022-02-21 | 2023-12-19 | 东风汽车集团股份有限公司 | Rotor lamination supports transfer device |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN203015508U (en) | Inner steel frame fast combined sector-shaped flower box | |
| CN108100220A (en) | Flight controller stent and GPS antenna supporting rack assembly | |
| CN205129867U (en) | Move stable food delivery robot | |
| CN205238055U (en) | Food delivery robot | |
| USD898623S1 (en) | Four wheel towable utility cart | |
| CN204958127U (en) | Three -dimensional storage rack of staircase guide rail | |
| CN108082509A (en) | Flight controller stent and machine body assembly | |
| CN206443426U (en) | A kind of detachable combination suspends bookshelf | |
| CN205513654U (en) | Multi -functional paper baby's bed accessory | |
| CN102771330A (en) | Assembled stereoscopic flowerpot | |
| CN208344441U (en) | A kind of vehicle frame and the electric bicycle with the vehicle frame | |
| CN205674921U (en) | A kind of lightweight backrest dinner table board | |
| CN203646152U (en) | Podium type combination flower box | |
| CN202722115U (en) | Assembled stereoscopic flowerpot | |
| US20080089973A1 (en) | Potter's wheel | |
| CN108174542A (en) | Flight controller box | |
| CN203153205U (en) | Three-layer scrollable flower shelf | |
| CN209410100U (en) | Grid dispenses utensil in preceding guarantor | |
| CN209058540U (en) | Bilayer promotion basket | |
| CN209151715U (en) | A kind of high-stability hexagon flower box structure | |
| CN209975058U (en) | Integrative cotton sock machine frame | |
| CN207753820U (en) | A kind of modified single-point balance sound rack | |
| CN206561404U (en) | Parts transport frock | |
| CN208881463U (en) | A kind of novel bamboo and wood decorative lamp frame | |
| CN215819473U (en) | Double-deck support frame of growing seedlings of chinese herbal medicine |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20180601 |
|
| WD01 | Invention patent application deemed withdrawn after publication |