CN207346069U - It is a kind of for the installing frame of unmanned plane, rack and unmanned plane - Google Patents
It is a kind of for the installing frame of unmanned plane, rack and unmanned plane Download PDFInfo
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- CN207346069U CN207346069U CN201720954595.3U CN201720954595U CN207346069U CN 207346069 U CN207346069 U CN 207346069U CN 201720954595 U CN201720954595 U CN 201720954595U CN 207346069 U CN207346069 U CN 207346069U
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- unmanned plane
- installing frame
- rack
- plate
- side plate
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- 239000007788 liquid Substances 0.000 claims abstract description 15
- 229920002635 polyurethane Polymers 0.000 claims abstract description 8
- 239000004814 polyurethane Substances 0.000 claims abstract description 8
- 238000009434 installation Methods 0.000 claims description 22
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 9
- 239000004917 carbon fiber Substances 0.000 claims description 9
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 9
- 239000000758 substrate Substances 0.000 claims description 9
- 238000005096 rolling process Methods 0.000 claims description 5
- 238000004891 communication Methods 0.000 claims description 3
- 239000006260 foam Substances 0.000 claims description 3
- -1 acyl Imines Chemical class 0.000 claims 1
- 239000000463 material Substances 0.000 abstract description 16
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 abstract description 9
- 229910052799 carbon Inorganic materials 0.000 abstract description 9
- 239000000835 fiber Substances 0.000 abstract description 9
- 238000005265 energy consumption Methods 0.000 abstract description 5
- 238000000034 method Methods 0.000 abstract description 4
- 238000013461 design Methods 0.000 abstract description 3
- 229920007790 polymethacrylimide foam Polymers 0.000 abstract description 3
- 230000002787 reinforcement Effects 0.000 abstract description 2
- 230000013011 mating Effects 0.000 description 4
- 238000007689 inspection Methods 0.000 description 2
- 238000005728 strengthening Methods 0.000 description 2
- 108090000565 Capsid Proteins Proteins 0.000 description 1
- 230000005540 biological transmission Effects 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
- 238000005516 engineering process Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 230000006872 improvement Effects 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
- 238000005192 partition Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000009423 ventilation Methods 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
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Abstract
The utility model belongs to unmanned air vehicle technique field, a kind of installing frame for unmanned plane is provided, rack and unmanned plane, including rack, the liquid storage container and battery part being connected in the rack, installing frame is also associated with the rack, the installing frame is included by the fixed frame that carbon fibre material plate forms and is connected in the rack and the mounting bracket for being connected on the fixed frame and being equally made of carbon fibre material plate, the liquid storage container is spacing to be connected on the fixed frame, the battery part is spacing to be connected on the mounting bracket, it is also formed with being filled with the cavity of the filled layer of polymethacrylimide foam or polyurethane material on the inside of the carbon fibre material plate；So design can solve the problems, such as that the mode of reinforcement structure in existing unmanned plane structure adds the weight and energy consumption of itself.
Description
Technical field
The utility model belongs to unmanned air vehicle technique field, more particularly to a kind of for the installing frame of unmanned plane, rack and nothing
It is man-machine.
Background technology
Unmanned plane refers to the not manned vehicle being controlled using wireless remote control device and the control device of itself, with
Development of UAV, because of it, to have the advantages that maneuverability, unmanned flight, operation require low, and unmanned plane has been widely used in agriculture
Industry plant protection, photography of taking photo by plane, electric inspection process, environmental monitoring, forest fire protection and disaster inspection etc., effectively overcome manned fly
Machine carries out the deficiency of aerial work.Applied unmanned plane generally requires carrying power tool, and fuselage intensity requirement is high.
But in existing unmanned plane structure, fuselage intensity is strengthened using the size for the self structure for increasing unmanned plane,
This solution increases increase energy consumption while unmanned plane own wt.
Utility model content
The purpose of this utility model is to provide a kind of installing frame for unmanned plane, it is intended to solves existing unmanned plane knot
The mode of reinforcement structure adds the problem of weight and energy consumption of itself in structure.
The utility model so solves：A kind of installing frame for unmanned plane, including carbon fiber board and filled layer, institute
State carbon fiber board and be equipped with hollow cavity, the filled layer is filled in the cavity of the carbon fiber board.
Further, the filled layer is polymethacrylimide foam or polyurethanes filled layer.
Further, the carbon fiber board includes fixed frame and the mounting bracket being connected on the fixed frame, the cavity
Arranged on the fixed frame and the mounting bracket.
Further, the fixed frame including being in for the substrate being connected on the fuselage and along the both sides of the substrate
Outwardly extending first extension board of V-type and the second extension board, the mounting bracket include the first side plate and the second side being oppositely arranged
Plate, and the end plate being connected on first side plate and the second side plate end face, first side plate deviate from the end plate
Side connect the end of first extension board, second side plate is away from the side of end plate connection second extension
The end of plate, the cavity are arranged on first extension board, second extension board, first side plate and second side plate
On.
Further, mounting groove is defined in the installing frame, is also associated between the fixed frame and the mounting bracket
By the mounting groove be separated into the first installation straight slot and second installation straight slot every beam.
The utility model also provides a kind of rack, including foregoing installing frame.
The utility model also provides a kind of unmanned plane, including foregoing rack, the liquid storage container that is connected in the rack
With battery part, in the first installation straight slot that the liquid storage container is spacing to be connected on the installing frame, the spacing company of battery part
It is connected in the second installation straight slot on the installing frame.
Further, the interior rolling group for being also associated with being slidably connected easy to the liquid storage container of the first installation straight slot
Part, limit assembly easy to lock the battery part is also associated with the second installation straight slot and easy to the battery part and institute
State the plug-assembly of fuselage electrical connection.
Further, the rack includes the fuselage main body connected for the installing frame and is connected to the fuselage main body
On housing unit, the upper surface of the housing unit and the upper surface of the liquid storage container and/or the battery part are stream
Line curved surface.
Further, the fuselage main body includes top plate and the bottom plate being oppositely arranged with the top plate, and is connected to institute
State between top plate and the bottom plate and accommodate control system and the middle roll-over of communication module, the fuselage bottom are also associated with being used for
The undercarriage for protecting the unmanned plane to rise and fall.
The technique effect that installing frame provided by the utility model for unmanned plane has compared with the prior art is：It is logical
The material selection carbon fibre material plate of installing frame is crossed, so that meet the structural strength of unmanned plane entirety, while carbon fiber material
Be additionally provided with cavity on the inside of flitch, and in cavity light filling filled layer, and then can ensure the quality of whole installing frame more
Gently, so as to reduce the total quality of unmanned plane, and then energy consumption during reduction unmanned plane during flying.
Brief description of the drawings
, below will be to embodiment or the prior art in order to illustrate more clearly of the technical scheme in the embodiment of the utility model
Attached drawing is briefly described needed in description, it should be apparent that, drawings in the following description are only that this practicality is new
Some embodiments of type, for those of ordinary skill in the art, without having to pay creative labor, can be with
Other attached drawings are obtained according to these attached drawings.
Fig. 1 is the overall structure stereogram for the unmanned plane that the utility model embodiment provides；
Fig. 2 is that the overall structure for the unmanned plane that the utility model embodiment provides removes the stereogram after battery part；
Fig. 3 is unmanned plane that the utility model embodiment provides from the stereogram for looking up direction visual angle；
Fig. 4 is the semi-cutaway for the unmanned plane that the utility model embodiment provides；
Fig. 5 be the utility model embodiment provide unmanned plane in installing frame in one direction on structure chart；
Fig. 6 be in the unmanned plane that the utility model embodiment provides installing frame along the structure chart on another direction；
Fig. 7 be in the unmanned plane that the utility model embodiment provides installing frame along the structure chart on another direction；
Fig. 8 is the semi-cutaway of installing frame in the unmanned plane that the utility model embodiment provides.
Wherein, fuselage 1, fuselage body 10, middle roll-over 11, top plate 12, bottom plate 13, installing frame 14, fixed frame 141, substrate
1411st, the first extension board 1412, the second extension board 1413, mounting bracket 142, end plate 1421, the first side plate 1422, the second side plate
1423rd, protection department 1424, partition plate 143, first install straight slot 144, second and install straight slot 145, rolling assembly 144, limit assembly
145th, plug-assembly 146, first installs straight slot 147, second and installs straight slot 148, cavity 149；
Horn 2, housing unit 3, installation housing 31, based shell 32, base enclosure body 321, head cover 322, procapsid 3211, on
Housing 3212, mounting hole 3213, mating groove 3214, magnet ring 3215, ventilation duct 3210；
Undercarriage 4, Power Component 5, liquid storage container 6, battery part 7, antenna module 8, connecting portion 81, first antenna portion 82,
Second antenna part 83.
Embodiment
In order to make the purpose of the utility model, technical solutions and advantages more clearly understood, below in conjunction with attached drawing and implementation
Example, is further elaborated the utility model.It should be appreciated that specific embodiment described herein is only explaining
The utility model, is not used to limit the utility model.
It should be noted that when element is referred to as " being fixed on " or " being arranged at " another element, it can be directly another
On one element or it is connected on another element.When an element is known as " being connected to " another element, it can
To be directly to another element or be indirectly connected on another element.
It is to be appreciated that term " length ", " width ", " on ", " under ", "front", "rear", "left", "right", " vertical ",
The orientation or position relationship of the instruction such as " level ", " top ", " bottom " " interior ", " outer " are to be closed based on orientation shown in the drawings or position
System, is for only for ease of and describes the utility model and simplified description, rather than the device or element of instruction or hint meaning are necessary
With specific orientation, with specific azimuth configuration and operation, therefore it is not intended that limitation to the utility model.
In addition, term " first ", " second " are only used for description purpose, and it is not intended that instruction or hint relative importance
Or the implicit quantity for indicating indicated technical characteristic.Thus, define " first ", the feature of " second " can be expressed or
Implicitly include one or more this feature.In the description of the utility model, " multiple " are meant that two or two
More than, unless otherwise specifically defined.
Attached drawing 1 be refer to shown in Fig. 8, in the utility model embodiment, there is provided a kind of unmanned plane, including 1 He of rack
Along the outwardly extending multiple horns 2 of the rack 1, be connected in the rack 1 and in streamline curved surface housing unit 3, be connected to this
1 bottom of rack is used to ensureing that the unmanned plane to rise and fall the undercarriage 4 of stability, is also connected to the Power Component 5 of 2 end of horn,
The liquid storage container 6 and battery part 7 being connected in the rack 1, and control system.It is remote that the Power Component 5 is fixed on the horn 2
The end of the rack 1, it is to provide power to the flight of unmanned plane that it, which is acted on,.The liquid storage container 6 is equipped in rack 1 and interior is suitable for
Article to be sprayed or to be transported is contained, which is fixed in rack 1 to provide power, control system for Power Component 5
System is fixed in rack 1, for controlling the flight attitude of the aircraft.
Installing frame 14 forms for carbon fibre material plate or carbon fibre material plate wraps up Polymethacrylimide (PMI) bubble
The filled layer of foam or polyurethanes (PU) material forms；In other words, formed with cavity 149, chamber on the inside of carbon fibre material plate
Filled with Polymethacrylimide (PMI) foam or polyurethanes (PU) material in body 149), thus, reduce peace
Increase the intensity of installing frame 14 while 14 weight that frames up.
The installing frame for unmanned plane of design above, by the material selection carbon fibre material plate of installing frame 14, and then
So that meeting the structural strength of unmanned plane entirety, while cavity 149 is additionally provided with the inside of carbon fibre material plate, and filling in cavity
The polymethacrylimide foam of lightweight or the filled layer of polyurethane material, and then can ensure whole installing frame 14
Quality it is lighter, so as to reduce the total quality of unmanned plane, and then energy consumption when reducing unmanned plane during flying.
Meanwhile the installing frame 14 for spacing linkage function component is connected with the rack 1, which is preferably to wrap
Liquid storage container 6 and battery part 7 are included, which includes the fixed frame 141 being connected in the rack 1 and be connected to the fixed frame
Mounting bracket 142 on 141, the cavity 149 are arranged on the fixed frame 141 and the mounting bracket 142, also spacing connection on the horn 2
There is antenna module 8, which is connected on the horn 2 and close to the side of the rack 1, while the mounting bracket 142 is upper
End upwardly extends the protection department 1424 for being useful for protecting the antenna module 8, and the height of the protection department 1424 is more than the antenna module 8
Height.
More than design unmanned plane, by being connected to antenna module 8 is spacing on horn 2, while in the upper of mounting bracket 142
End upwardly extends the protection department 1424 for being useful for protecting the antenna module 8, and the height of the protection department 1424 is more than the antenna
The height of component 8, and then when unmanned plane during flying is overturn, which can protect the antenna module 8 collision damage occur
It is bad.
Specifically, as shown in Figure 1 to Figure 3, in the utility model embodiment, rack 1 includes fuselage body 10 and connection
In the installing frame 14 of fuselage body 10, wherein, fuselage body 10 includes top plate 11, bottom plate 12 and middle roll-over 13, top plate 11 with
Bottom plate 12 is oppositely arranged, and middle roll-over 13 is arranged between top plate 11 and bottom plate 12 and is connected with the top plate 11 and bottom plate 12.It is preferred that
Ground, 11 front end of top plate are provided with installation gap, and thus, 10 front end of fuselage body is formed as unlimited accommodating chamber, control system (example
It is like flying to control the electronic devices such as device, communication module) it can be contained in accommodating chamber.
Specifically, as shown in Figures 5 to 7, in the utility model embodiment, which is connected to the fuselage sheet
On body 10, which is connected on the fixed frame 141, is also associated between the mounting bracket 142 and fixed frame 141 every beam
143.The fixed frame 141, mounting bracket 142 and it can be integrally formed every beam 143.Wherein, which includes substrate 1411
And the first extension board 1412 and the second extension board 1413 obliquely extended from the opposite both sides of the substrate 1411.The substrate
1411 are connected with roll-over in this 13, and 1412 and second extension board 1413 of the first extension board is V-shaped along the both sides of the substrate 1411
Set, while perforation is equipped with 1412 and second extension board 1413 of the first extension board.The mounting bracket 142 includes opposite the
1422 and second side plate 1423 of side plate, and the end plate being connected on 1422 and second side plate of the first side plate, 1423 end face
1421.First side plate 1422 connects the end of first extension board 1412, second side plate away from the side of the end plate 1421
1423 connect the end of second extension board 1413,1422 and second side plate of the first side plate away from the side of the end plate 1421
1423 upper end upwardly extends to form the protection department 1424.The installing frame 14 limits mounting groove, should be connected to this every beam 143
The mounting groove interval is divided into the first installation straight slot 147 and the second installation straight slot between first side plate 1422 and the second side plate 1423
148.The battery part 7 can be installed on the second installation straight slot 148, which can be installed on the first installation straight slot 147
On.The cavity is arranged on first extension board 1412, the second extension board 1413, the first side plate 1422 and the second side plate 1423.
Specifically, as shown in figure 5, in the utility model embodiment, which further includes rolling assembly 144, limit
Hyte part 145 and plug-assembly 146.The rolling assembly 144 is linked in the first installation straight slot 147, and for being slidably connected
The liquid storage container 6.The limit assembly 145 is fixed in the second installation straight slot 148, and for locking the battery part 7.The plug
Component 146 is connected in the second installation straight slot 148, and is electrically connected for battery part 7 with rack 1.
The plug-assembly 146 includes modular plug and signal lamp module, and signal lamp module is oppositely arranged end with modular plug
1421 both sides of plate and signal lamp module is electrically connected with modular plug, further, mating groove are provided with the end plate 1421, are coordinated
Be suitable for the connecting line for housing signal lamp module and modular plug on groove, be additionally provided with the outside of 1421 upper end of end plate strengthening portion with
Strengthen 1421 intensity of end plate, signal lamp module can be matched between end plate 1421 and strengthening portion.
Specifically, as shown in Figure 6 and Figure 7, in the utility model embodiment, in the present embodiment, 142 lower end of mounting bracket
Extend extension, extend and crossed beam trunking 14231 is provided with end surface, crossed beam trunking 14231 connects the mating groove, by plug group
The power cord drawn in part 146 can be arranged in crossed beam trunking 14231.
In the present embodiment, as shown in Figure 6 and Figure 7, extension is extended in 142 lower end of mounting bracket, extends and is set on end surface
Crossed beam trunking 14231 is equipped with, crossed beam trunking 14231 connects the mating groove, can be arranged at by the power cord drawn in plug-assembly 146
In crossed beam trunking 14231.
In the present embodiment, as shown in figure 4, the unmanned plane further includes antenna module 8, antenna module 8 is fixed on horn 2
Think unmanned plane positioning, transmission information.The protection department for protective cover antenna module 8 is extended in 142 upper end of mounting bracket at the same time
1424。
In the present embodiment, which includes the spacing connecting portion 81 being connected on the horn 2, is connected to the company
The top of socket part 81 and the first antenna portion 82 that upwardly extends and it is connected to the bottom of the connecting portion 81 and extend downwardly second
Antenna part 83, the first antenna portion 82 and second antenna part 83 are located along the same line.And the height of the protection department 1424
More than the height in the first antenna portion 82.
Specifically, as shown in figure 4, in the utility model embodiment, 1424 height of protection department being somebody's turn to do is more than antenna module 8
Height, when unmanned plane is overturn, protection department 1424 prevents antenna module 8 from damaging.
The above is only the preferred embodiment of the utility model only, is not intended to limit the utility model, all at this
All any modification, equivalent and improvement made within the spirit and principle of utility model etc., should be included in the utility model
Protection domain within.
Claims (9)
- A kind of 1. installing frame for unmanned plane, it is characterised in that：Including carbon fiber board and filled layer, the carbon fiber board is equipped with Hollow cavity, the filled layer are filled in the cavity of the carbon fiber board, and the carbon fiber board includes fixed frame and is connected to Mounting bracket on the fixed frame, the cavity are arranged on the fixed frame and the mounting bracket.
- 2. it is used for the installing frame of unmanned plane as claimed in claim 1, it is characterised in that：The filled layer is polymethyl acyl Imines foam or polyurethanes filled layer.
- 3. it is used for the installing frame of unmanned plane as claimed in claim 1 or 2, it is characterised in that：The fixed frame is included for even The substrate that is connected on fuselage and along V-shaped outwardly extending first extension board in both sides of the substrate and the second extension board, it is described Mounting bracket includes the first side plate and the second side plate being oppositely arranged, and is connected to first side plate and the second side plate end End plate on face, first side plate connect the end of first extension board, second side away from the side of the end plate Backboard connects the end of second extension board from the side of the end plate, and the cavity is arranged on first extension board, described On second extension board, first side plate and second side plate.
- 4. it is used for the installing frame of unmanned plane as claimed in claim 3, it is characterised in that：Installation is defined in the installing frame Groove, is also associated with the mounting groove being separated into the first installation straight slot and the second installation between the fixed frame and the mounting bracket Straight slot every beam.
- A kind of 5. rack, it is characterised in that：Including such as claim 1-4 any one of them installing frame.
- A kind of 6. unmanned plane, it is characterised in that：Including rack as claimed in claim 5, the liquid storage being connected in the rack Container and battery part, in the first installation straight slot that the liquid storage container is spacing to be connected on the installing frame, the battery part limit Position is connected in the second installation straight slot on the installing frame.
- 7. unmanned plane as claimed in claim 6, it is characterised in that：It is also associated with the first installation straight slot easy to described The rolling assembly that liquid storage container is slidably connected, is also associated with easy to lock the spacing of the battery part in the second installation straight slot Component and the plug-assembly being electrically connected easy to the battery part with fuselage.
- 8. unmanned plane as claimed in claim 7, it is characterised in that：The rack includes the fuselage for installing frame connection Main body and the housing unit being connected in the fuselage main body, the upper surface of the housing unit and the liquid storage container and/or The upper surface of the battery part is streamline curved surface.
- 9. unmanned plane as claimed in claim 7, it is characterised in that：The fuselage main body includes top plate and opposite with the top plate The bottom plate of setting, and be connected between the top plate and the bottom plate and accommodate control system and the middle roll-over of communication module, The fuselage bottom is also associated with the undercarriage for protecting the unmanned plane to rise and fall.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720954595.3U CN207346069U (en) | 2017-08-01 | 2017-08-01 | It is a kind of for the installing frame of unmanned plane, rack and unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720954595.3U CN207346069U (en) | 2017-08-01 | 2017-08-01 | It is a kind of for the installing frame of unmanned plane, rack and unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207346069U true CN207346069U (en) | 2018-05-11 |
Family
ID=62360403
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720954595.3U Active CN207346069U (en) | 2017-08-01 | 2017-08-01 | It is a kind of for the installing frame of unmanned plane, rack and unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207346069U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111099026A (en) * | 2019-12-17 | 2020-05-05 | 湖北吉利太力飞车有限公司 | Supporting structure of power battery system of electric aircraft |
| WO2021120659A1 (en) * | 2019-12-19 | 2021-06-24 | 广州极飞科技有限公司 | Self-driving control apparatus and driverless apparatus provided with same |
| RU2777941C1 (en) * | 2019-12-19 | 2022-08-12 | Гуанчжоу Иксэркрафт Текнолоджи Ко., Лтд. | Device for controlling autonomous driving and a device for unmanned driving associated with it |
-
2017
- 2017-08-01 CN CN201720954595.3U patent/CN207346069U/en active Active
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111099026A (en) * | 2019-12-17 | 2020-05-05 | 湖北吉利太力飞车有限公司 | Supporting structure of power battery system of electric aircraft |
| CN111099026B (en) * | 2019-12-17 | 2022-06-14 | 湖北吉利太力飞车有限公司 | Supporting structure of power battery system of electric aircraft |
| WO2021120659A1 (en) * | 2019-12-19 | 2021-06-24 | 广州极飞科技有限公司 | Self-driving control apparatus and driverless apparatus provided with same |
| JP2022532713A (en) * | 2019-12-19 | 2022-07-19 | 広州極飛科技股▲ふん▼有限公司 | Automatic operation control device and unmanned operation device equipped with it |
| RU2777941C1 (en) * | 2019-12-19 | 2022-08-12 | Гуанчжоу Иксэркрафт Текнолоджи Ко., Лтд. | Device for controlling autonomous driving and a device for unmanned driving associated with it |
| JP7269375B2 (en) | 2019-12-19 | 2023-05-08 | 広州極飛科技股▲ふん▼有限公司 | Automatic operation control device and unmanned operation device equipped with it |
| AU2020408484B2 (en) * | 2019-12-19 | 2023-07-13 | Guangzhou Xaircraft Technology Co., Ltd. | Self-driving control device and unmanned driving device with the same |
| US12009569B2 (en) | 2019-12-19 | 2024-06-11 | Guangzhou Xaircraft Technology Co., Ltd. | Self-driving control device and unmanned driving device with the same |
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Address after: 510000 Block C, 115 Gaopu Road, Tianhe District, Guangzhou City, Guangdong Province Patentee after: XAG Co., Ltd. Address before: 510000, Guangdong, Guangzhou, Gaotang Tianhe District Software Park Road, No. 1, 3A01 Patentee before: Guangzhou Xaircraft Technology Co.,Ltd. |
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| CP03 | Change of name, title or address |