CN109319085A - Based shell, rack and unmanned plane - Google Patents
Based shell, rack and unmanned plane Download PDFInfo
- Publication number
- CN109319085A CN109319085A CN201710647702.2A CN201710647702A CN109319085A CN 109319085 A CN109319085 A CN 109319085A CN 201710647702 A CN201710647702 A CN 201710647702A CN 109319085 A CN109319085 A CN 109319085A
- Authority
- CN
- China
- Prior art keywords
- electronic device
- unmanned plane
- shell
- mounting hole
- top 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.)
- Pending
Links
- 230000013011 mating Effects 0.000 claims abstract description 25
- 238000009434 installation Methods 0.000 claims description 41
- 230000005389 magnetism Effects 0.000 claims description 3
- 230000005611 electricity Effects 0.000 claims 1
- 108090000565 Capsid Proteins Proteins 0.000 description 6
- 239000007788 liquid Substances 0.000 description 6
- 238000012423 maintenance Methods 0.000 description 3
- 238000001816 cooling Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000007689 inspection Methods 0.000 description 2
- 238000005192 partition Methods 0.000 description 2
- 230000002093 peripheral effect Effects 0.000 description 2
- 238000009423 ventilation Methods 0.000 description 2
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005662 electromechanics Effects 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 239000000696 magnetic material Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 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
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/068—Fuselage sections
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Casings For Electric Apparatus (AREA)
Abstract
The present invention provides a kind of based shells, the based shell includes the base enclosure ontology being fixedly connected for the fuselage with unmanned plane and the top cover that is detachably connected with the base enclosure ontology, the mounting hole of the electronic device on fuselage described in face is opened up at the top of the base enclosure ontology, the top cover is set on the mounting hole.The convenience of electronic device dismounting can be improved in unmanned plane of the invention, when needing replacing or overhauling electronic device, top cover is taken out out of mating groove, electronic device is removed from bottom plate again and is taken out by mounting hole, when electronic device reinstalls bottom plate, electronic device is put into accommodating chamber by mounting hole and is placed on bottom plate and is fixedly mounted, compared with prior art, when avoiding replacement electronic device, it needs to dismantle complete machine, the efficiency of unmanned plane replacement electronic device is improved, and reduces the cost of the efficiency of unmanned plane replacement electronic device.
Description
Technical field
The invention belongs to unmanned plane during flying device technical field more particularly to a kind of based shells, rack and unmanned plane.
Background technique
Unmanned plane refers to the not manned vehicle controlled using wireless remote control device and electronic device, such as nobody is directly
The machine of liter, unmanned fixed-wing aircraft, unmanned gyroplane etc..In recent years, with Development of UAV, because it is with maneuverability, reaction
Quickly, unmanned flight, operation requires low advantage, and unmanned plane has been widely used in agricultural plant protection, photography of taking photo by plane, electric power patrol
Inspection, environmental monitoring, forest fire protection and disaster inspection effectively overcome the deficiency that manned aircraft carries out aerial work.
Unmanned plane shell is typically secured to the outside of unmanned aerial vehicle body to protect the internal structure being equipped on unmanned plane, nothing
Man-machine shell is fixed on unmanned aerial vehicle body by fastener, and such fixed structure dismounting trouble has seriously affected unmanned electromechanics
The efficiency of replacement and the maintenance of sub-device.
Summary of the invention
The purpose of the present invention is to provide a kind of unmanned planes, can be improved the efficiency of replacement and the maintenance of electronic device.
The invention is realized in this way a kind of based shell, the based shell includes for the fixed company of fuselage with unmanned plane
The base enclosure ontology connect and the top cover being detachably connected with the base enclosure ontology open up described in face at the top of the base enclosure ontology
The mounting hole of electronic device on fuselage, the top cover are set on the mounting hole.
It should be understood that the base enclosure ontology includes upper housing, the mounting hole is set to the upper housing, the upper housing
The mounting hole periphery is provided with the first magnetic part, is correspondingly arranged on the top cover for magnetic with first magnetic part
Second magnetic part of connection.
It should be understood that first magnetic part is magnet, second magnetic part is made of ferrimagnet.
It should be understood that the upper housing offers with the structure matching of the top cover and for accommodating matching for the top cover
Slot is closed, the mounting hole is set to the slot bottom of the mating groove and runs through the slot bottom of the mating groove, and first magnetic part is solid
Due to the slot bottom of the mating groove.
The present invention also provides a kind of racks, including above-mentioned fuselage and based shell.
It should be understood that the fuselage includes bottom plate and is arranged in parallel with the bottom plate and is fixedly mounted with the bottom plate
Top plate, the top plate and the bottom plate are collectively formed one for accommodating the installation space of the electronic device, and the top plate opens up
One bit-avoiding slot, the bit-avoiding slot connection installation space and the bit-avoiding slot and the electronic device and the mounting hole are just
To setting.
It should be understood that the bit-avoiding slot is through one end close to the electronic device of the top plate.
The present invention also provides a kind of unmanned planes, including above-mentioned rack and electronic device.
It should be understood that the unmanned plane includes housing unit, the housing unit include the based shell and with it is described
The installation shell of based shell being fixedly connected, the installation shell include be symmetrically arranged on the upper housing two sides and with the top
The two connection shells and be set between the two connection shells and be used to connect two attachment beams for connecting shells that plate is fixedly connected.
It should be understood that the bottom of the mating groove is additionally provided with the screw hole for installing the connection shell, the base enclosure
Body is fixedly connected and is covered on top plate and the bottom plate with the top plate by the mounting shell.
The present invention compared with the existing technology have the technical effect that based shell of the invention can be improved electronic device dismounting
Convenience is taken out top cover, then electronic device is taken from bottom plate when needing replacing or overhauling electronic device out of mating groove
It is taken out down and by mounting hole, when electronic device reinstalls bottom plate, electronic device is put into accommodating chamber by mounting hole and is placed in bottom plate
Upper fixed installation when avoiding replacement electronic device, needs to dismantle complete machine, improves unmanned plane more compared with prior art
The efficiency of electronic device is changed, and reduces the cost of the efficiency of unmanned plane replacement electronic device.
Detailed description of the invention
In order to illustrate the technical solution of the embodiments of the present invention more clearly, below will be to the embodiment of the present invention or the prior art
Attached drawing needed in description is briefly described, it should be apparent that, drawings described below is only of the invention
Some embodiments for those of ordinary skill in the art without creative efforts, can also be according to this
A little attached drawings obtain other attached drawings.
Fig. 1 is the perspective view of unmanned plane provided in an embodiment of the present invention.
Fig. 2 is the exploded view of unmanned plane provided in an embodiment of the present invention.
Fig. 3 is the part-structure perspective view of unmanned plane provided in an embodiment of the present invention.
Fig. 4 is fuselage, horn, undercarriage, installation shell and Power Component provided in an embodiment of the present invention.
Fig. 5 is that undercarriage provided in an embodiment of the present invention, horn, Power Component close the perspective view of part airframe structure.
Fig. 6 is the perspective view of housing unit provided in an embodiment of the present invention.
Fig. 7 is the perspective view of connection shell provided in an embodiment of the present invention.
Fig. 8 is the perspective view of base enclosure ontology provided in an embodiment of the present invention.
Description of symbols:
Specific embodiment
The embodiment of the present invention is described below in detail, examples of the embodiments are shown in the accompanying drawings, wherein from beginning to end
Same or similar label indicates same or similar element or element with the same or similar functions.Below with reference to attached
The embodiment of figure description is exemplary, it is intended to is used to explain the present invention, and is not considered as limiting the invention.
In order to make the objectives, technical solutions, and advantages of the present invention clearer, with reference to the accompanying drawings and embodiments, right
The present invention is further elaborated.
As depicted in figs. 1 and 2, the embodiment of the present invention provide a kind of unmanned plane include fuselage 100, with fuselage 100 is fixed pacifies
The electronic device 800 of dress, the multiple horns 200 being fixedly connected with the fuselage 100, two rising and falling of being fixedly connected with fuselage 100
Frame 300, the housing unit 400 for being covered on fuselage 100, be installed on horn 200 100 end of separate fuselage Power Component
500, it is installed on fuselage 100 and is used for the liquid storage container 600 of storage solutions, is installed on fuselage 100 and for being power packages
The battery 700 that part 500 is powered.
Further, as shown in Figures 2 and 3, fuselage 100 includes fuselage body 110 and fixes company with fuselage body 110
The installing frame 120 for connecing and being used to store, fuselage body 110 include the bottom plate 113 and top plate 111 for being arranged in parallel and being fixedly connected,
Top plate 111 and bottom plate 113 are collectively formed one for accommodating the installation space 114 of electronic device 800, and electronic device 800 is in installation
It is fixedly connected with bottom plate 113 in space 114, top plate 111 opens up a bit-avoiding slot 112 and communicates with installation space 114 to be filled with supplied for electronic
It sets 800 to be put into installation space 114 or take out out of installation space 114, the setting of 112 face electronic device 800 of bit-avoiding slot；Installing frame
120 are arranged in frame-type and are fixedly connected in the one end of installing frame 120 insertion installation space 114 and with bottom plate 113, installing frame
A partition 123 is provided in 120, installing frame 120 has the first installation cavity 121 and the second installation cavity 122 for storage, partition
123 are spaced apart the first installation cavity 121 and the second installation cavity 122, and battery 700 is installed in the first installation cavity 121, and liquid storage holds
Device 600 is installed in the second installation cavity 122, and the bottom of liquid storage container 600 is fixedly connected with the top of bottom plate 113.
Further, multiple horns 200 are distributed in around fuselage 100 that (unmanned plane in the present embodiment is with four horns
200 are illustrated, but are not limited thereto), and horn 200 is fixedly connected with fuselage 100, specifically, as shown in Figure 2 and Figure 5,
200 one end of horn is protruded into installation space 114 and is fixedly connected with bottom plate 113, and the side of horn 200 and installing frame 120
Side wall is fixedly connected, and top plate 111 covers the top connect with horn 200.
Further, four Power Components 500, which correspond, is installed on four ends of the horn 200 far from fuselage 100, and four
A Power Component 500 is electrically connected for providing the Power Component 500 of flying power with battery 700, and four Power Components 500 are equal
The flight stake situation for controlling unmanned plane is connect with 800 signal of electronic device.
Certainly, in other embodiments of the present invention, a horn 200 is at least arranged in unmanned plane, and Power Component 500 is corresponding extremely
One is arranged less.
Further, as shown in Fig. 2, each Power Component 500 includes propeller 510 and drives company with propeller 510
It connecing and drives the rotation of propeller 510 to provide the driver 520 of flying power, driver 520 is fixedly installed on horn 200,
Battery 700 is electrically connected with driver 520 and provides electric energy for driver 520, and electronic device 800 is connect with 520 signal of driver,
Electronic device 800 controls the flight condition of unmanned plane by control driver 520.
Further, two undercarriages 300 are both secured to the lower section of fuselage 100 to guarantee the stabilization of unmanned plane takeoff and landing
Property, specifically, as shown in Figure 1, undercarriage 300 include for support face contact and support fuselage 100 support portion 310 and
Respectively at the first connecting portion 320 and second connecting portion 330 that 310 both ends of support portion and support portion 310 are wholely set, the first connection
Portion 320 is fixedly connected with the one end of fuselage 100, and second connecting portion 330 is fixedly connected with the other end of fuselage 100.Specifically
Ground, first connecting portion 320 are fixedly connected with the side wall of installing frame 120, and the bottom of second connecting portion 330 and bottom plate 113 is fixed to be connected
Connect, unmanned plane is placed on supporting surface by two undercarriages 300, by 100 bottom surface of fuselage close to supporting surface, two undercarriages 300 it
Between apart from flaring be arranged, supporting surface and two undercarriages 300 collectively form triangular support configurations more stably to support fuselage
100。
Further, as shown in fig. 6, housing unit 400 includes the installation shell 410 and based shell 420 being fixedly connected, such as
Shown in Fig. 4, installation shell 410 includes symmetrically arranged two connection shell 411 and is set between two connection shells 411 and connect with two
The attachment beam 414 that shell 411 is fixedly connected, two connection shells 411 are arranged in arcuate, as shown in fig. 7, connection 411 bottom margin of shell
Extend and formed the connecting plate 412 to fit with 111 plate face of top plate to side, connection 411 top edge of shell extends simultaneously to side
Fixed part 413 is formed, installation shell 410 is fixedly connected by connecting plate 412 with top plate 111, and installation shell 410 passes through fixed part
413 are fixedly connected with based shell 420, and the end that two connection shells 411 tilt extended and separate top plate 111 is close to each other,
Two connection shells 411 are provided with antenna mounting groove 414, and antenna mounting groove 414, which also tilts, to be extended, antenna mounting groove 414
The plate face of inclined surface and top plate 111 is arranged in angle, and the angular range of the angle is more than or equal to 30 ° and to be less than or equal to
70 °, stability, the reliability of the transmission of wireless signal are improved for enhancing the intensity of wireless signal.
Further, as shown in Fig. 2, based shell 420 include base enclosure ontology 421 and with detachably connect on base enclosure ontology 421
The top cover 429 connect, as shown in figure 8, it is in the upper housing 425 and procapsid 422 being extended that base enclosure ontology 421, which includes, and on
Shell 425 is wholely set with procapsid 422, upper housing 425 and extending direction and procapsid 422 extending direction substantially hang down
Directly.Specifically, the extending direction of upper housing 425 is roughly parallel to the plate face of top plate 111, and the extending direction of procapsid 422 is substantially
Perpendicular to the plate face of top plate 111.
Based shell 420 is fixedly connected with top plate 111 and is covered on top plate 111 and bottom plate 113 by installing shell 410,
Based shell 420 and bottom plate 113 are collectively formed to accommodate the accommodating chamber of electronic device 800 (figure is unlabeled), specifically, upper housing
425, procapsid 422 and top cover 429 and bottom plate 113 surround accommodating chamber jointly, and the top center position of upper housing 425 opens up one and matches
Slot 427 is closed to accommodate top cover 429 and multiple screw hole 427a to be fixedly connected with installation shell 410, screw hole 427a, which is set to, to be matched
The bottom of slot 427 is closed, connects the fixed part 413 of shell 411 and the screw hole 427a of upper housing 425 by determining part (not shown) lock
It fastening, the structure of mating groove 427 and the structure matching of top cover 429 are arranged, specifically, the shape and top cover 429 of mating groove 427
Shape match setting, the thickness matching of the depth of mating groove 427 and top cover 429 is arranged, and top cover 429 and base enclosure ontology 421 can
Dismantling connection also opens up one at mating groove 427, on upper housing 425 and communicates the simultaneously disengaging of electronic devices 800 receiving with accommodating chamber
The mounting hole 426 of chamber specifically opens up a mounting hole to pass through when the installation of electronic devices 800 in the bottom of mating groove 427
426, the aperture of mounting hole 426 is less than the size of the slot bottom of mating groove 427, and mounting hole 426 runs through the slot bottom of mating groove 427, peace
Dress hole 426 is connected to setting, and mounting hole 426 and bit-avoiding slot 112 and electronics with accommodating chamber, bit-avoiding slot 112 and installation space 114
Device 800 is set to the peripheral position of mounting hole 426 to positive setting, screw hole 427a.
Further, in being fixedly installed in the slot bottom of mating groove 427 multiple first magnetic parts (figure unlabeled), and first
Magnetic part is set to the peripheral position of mounting hole 427, and the first magnetic part is magnet, and top cover 429 is fixedly installed with and the first magnetism
Part is arranged in a one-to-one correspondence and the second magnetic part made of magnetic material (figure is unlabeled), the second magnetic part are ferrimagnet system
At the polarity of, the pole of the second magnetic part and the first magnetic part to anti-, when top cover 429 is installed, multiple second magnetic parts of top cover 429
It corresponds and installs with multiple first magnetic parts in mating groove 427, the second magnetic part is attracting by magnetic force with the first magnetic part
It and is that top cover 429 is fixedly installed in mating groove 427, and is covered on mounting hole 426.
When electronic device 800 is installed, electronic device 800 is put into accommodating chamber by mounting hole 426, after bit-avoiding slot 112
It is installed on bottom plate 113, and electronic device 800 is installed in installation space 114；When electronic device 800 is dismantled, make the second magnetism
Part separates with the first magnetic part and takes out top cover 429 out of mating groove 427, and taking on bottom plate 113 electronic device 800 and passes through
Bit-avoiding slot 112, then electronic device 800 is taken out from mounting hole 426, electronics can be improved in the based shell 420 of the embodiment of the present invention
The convenience of device dismounting needs to dismantle complete machine when avoiding replacement electronic device 800, improves unmanned plane replacement electronics
The efficiency of device 800, and reduce the cost of the efficiency of unmanned plane replacement electronic device 800.
Further, the two sides of procapsid 422 are respectively provided with a ventilation culvert that electronic device 800 is communicated and led to accommodating chamber
Road 423, when unmanned plane during flying, since the operation of electronic device 800 can generate a large amount of heat, there is two ventilations culvert in extraneous cold space
Road 423 enters in accommodating chamber with the cooling of electronic devices 800.
The convenience of the dismounting of electronic device 800 can be improved in the unmanned plane of the embodiment of the present invention, when needing replacing or overhaul
When electronic device 800, top cover 429 is taken out out of mating groove 427, then electronic device 800 is removed from bottom plate 113 and by pacifying
It fills hole 426 to take out, when electronic device 800 reinstalls bottom plate 113, electronic device 800 is put into accommodating chamber by mounting hole 426 and is placed
It is fixedly mounted on bottom plate 113, compared with prior art, when avoiding replacement electronic device 800, needs to dismantle complete machine, mention
The high efficiency of unmanned plane replacement electronic device 800, and reduce the cost of the efficiency of unmanned plane replacement electronic device 800.
When top cover 429 is installed, the second magnetic part can the second magnetic part of automatic absorbing close to the first magnetic part, the first magnetic part
And adsorb top cover 429, only need to adjust top cover 429 keeps top cover 429 and mating groove 427 right in the position of mating groove 427 and angle
Positive installation, greatly improve the efficiency of installation makes the first magnetic part separate and move with the second magnetic part when top cover 429 is dismantled
Top cover 429 is opened, the disassembly of top cover 429 is very convenient, it does not need to collect the connector for being used for top cover 429 and base enclosure ontology 421,
Compared with traditional technology, the top cover 429 of the embodiment of the present invention and the disassembly efficiency of base enclosure ontology 421 are high, top cover 429 and base enclosure sheet
Body 421 passes through the magnetic connection of the second magnetic part and the first magnetic part, can be realized repeated disassembled and assembled, and convenient for disassembly and assembly.
When due to failure air crash occurs for unmanned plane, top plate 111 and bottom plate 113 can fill the electronics in installation space 114
Set 800 to play a protective role, avoid loading directly impact electronic device 800 and electronic device 800 is caused to damage, with reduce maintenance at
This.
Installing frame 120 is inserted into installation space 114 and is fixedly connected with bottom plate 113, can optimize the installation space of unmanned plane
114, and at least mountable two kinds different size objects of the first installation cavity 121 and the second installation cavity 122 that installing frame 120 is arranged,
Second installation cavity 122 is set between the first installation cavity 121 and electronic device 800, and further, battery 700 is installed on first
Installation cavity 121, liquid storage container 600 are installed in the second installation cavity 122, and battery 700 and electronic device 800 generate at work
Heat after the heat that liquid absorption battery 700 and electronic device 800 in liquid storage container 600 generate, when fluid removal, takes away heat
Amount can play the role of cooling down for battery 700 and electronic device 800, to extend the service life of unmanned plane.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all in essence of the invention
Made any modifications, equivalent replacements, and improvements etc., should all be included in the protection scope of the present invention within mind and principle.
Claims (10)
1. a kind of based shell, which is characterized in that the based shell includes the base enclosure sheet being fixedly connected for the fuselage with unmanned plane
Body and the top cover being detachably connected with the base enclosure ontology open up the electricity on fuselage described in face at the top of the base enclosure ontology
The mounting hole of sub-device, the top cover are set on the mounting hole.
2. based shell as described in claim 1, which is characterized in that the base enclosure ontology includes upper housing, and the mounting hole is set
In the upper housing, the upper housing is provided with the first magnetic part in the mounting hole periphery, is correspondingly arranged on the top cover
The second magnetic part for being connect with the first magnetic part magnetism.
3. based shell as claimed in claim 2, which is characterized in that first magnetic part is magnet, second magnetic part
It is made of ferrimagnet.
4. based shell as claimed in claim 2, which is characterized in that the upper housing offers the structure matching with the top cover
And the mating groove for accommodating the top cover, the mounting hole are set to the slot bottom of the mating groove and through the mating grooves
Slot bottom, first magnetic part are fixed on the slot bottom of the mating groove.
5. a kind of rack, including fuselage according to any one of claims 1-4 and based shell.
6. rack as claimed in claim 5, which is characterized in that the fuselage includes bottom plate and is arranged in parallel simultaneously with the bottom plate
The top plate being fixedly mounted with the bottom plate, the top plate and the bottom plate are collectively formed one for accommodating the peace of the electronic device
Space is filled, the top plate opens up a bit-avoiding slot, the bit-avoiding slot connection installation space and the bit-avoiding slot and the electronics
Device and the equal face setting of the mounting hole.
7. rack as claimed in claim 6, which is characterized in that the bit-avoiding slot is filled through the top plate close to the electronics
The one end set.
8. a kind of unmanned plane, including such as the described in any item racks of claim 5-7 and electronic device.
9. unmanned plane as claimed in claim 8, which is characterized in that the unmanned plane includes housing unit, the housing unit
Including the based shell and with the installation shell of the based shell being fixedly connected, the installation shell include be symmetrically arranged on institute
State upper housing two sides and with the top plate is fixedly connected two connect shell and be set between the two connection shells and for connecting
Connect the attachment beam of the two connection shells.
10. unmanned plane as claimed in claim 9, which is characterized in that the bottom of the mating groove is additionally provided with for installing
The screw hole of connection shell is stated, the based shell is fixedly connected with the top plate by the mounting shell and is covered on top plate and the bottom
On plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710647702.2A CN109319085A (en) | 2017-08-01 | 2017-08-01 | Based shell, rack and unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710647702.2A CN109319085A (en) | 2017-08-01 | 2017-08-01 | Based shell, rack and unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109319085A true CN109319085A (en) | 2019-02-12 |
Family
ID=65245995
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710647702.2A Pending CN109319085A (en) | 2017-08-01 | 2017-08-01 | Based shell, rack and unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109319085A (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103818544A (en) * | 2014-01-24 | 2014-05-28 | 深圳一电科技有限公司 | Unmanned aerial vehicle, unmanned aerial vehicle body and manufacturing method thereof |
| CN105752340A (en) * | 2016-04-07 | 2016-07-13 | 广州极飞电子科技有限公司 | Unmanned aerial vehicle |
| CN205418056U (en) * | 2016-03-29 | 2016-08-03 | 零度智控（北京）智能科技有限公司 | Unmanned aerial vehicle of unmanned aerial vehicle shell and applied this unmanned aerial vehicle shell |
| WO2016161975A1 (en) * | 2015-04-08 | 2016-10-13 | 优利科技有限公司 | Aircraft fuselage and aircraft with same |
| CN106218881A (en) * | 2016-08-30 | 2016-12-14 | 辽宁壮龙无人机科技有限公司 | Vertical layout fuel power four rotor flying platform |
| CN106828867A (en) * | 2016-12-30 | 2017-06-13 | 易瓦特科技股份公司 | Noise-proofing formula unmanned plane |
| CN207346070U (en) * | 2017-08-01 | 2018-05-11 | 广州极飞科技有限公司 | Based shell, rack and unmanned plane |
-
2017
- 2017-08-01 CN CN201710647702.2A patent/CN109319085A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103818544A (en) * | 2014-01-24 | 2014-05-28 | 深圳一电科技有限公司 | Unmanned aerial vehicle, unmanned aerial vehicle body and manufacturing method thereof |
| WO2016161975A1 (en) * | 2015-04-08 | 2016-10-13 | 优利科技有限公司 | Aircraft fuselage and aircraft with same |
| CN205418056U (en) * | 2016-03-29 | 2016-08-03 | 零度智控（北京）智能科技有限公司 | Unmanned aerial vehicle of unmanned aerial vehicle shell and applied this unmanned aerial vehicle shell |
| CN105752340A (en) * | 2016-04-07 | 2016-07-13 | 广州极飞电子科技有限公司 | Unmanned aerial vehicle |
| CN106218881A (en) * | 2016-08-30 | 2016-12-14 | 辽宁壮龙无人机科技有限公司 | Vertical layout fuel power four rotor flying platform |
| CN106828867A (en) * | 2016-12-30 | 2017-06-13 | 易瓦特科技股份公司 | Noise-proofing formula unmanned plane |
| CN207346070U (en) * | 2017-08-01 | 2018-05-11 | 广州极飞科技有限公司 | Based shell, rack and unmanned plane |
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