CN207346070U - Based shell, rack and unmanned plane - Google Patents

Based shell, rack and unmanned plane Download PDF

Info

Publication number
CN207346070U
CN207346070U CN201720954592.XU CN201720954592U CN207346070U CN 207346070 U CN207346070 U CN 207346070U CN 201720954592 U CN201720954592 U CN 201720954592U CN 207346070 U CN207346070 U CN 207346070U
Authority
CN
China
Prior art keywords
electronic device
unmanned plane
shell
mounting hole
head 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.)
Active
Application number
CN201720954592.XU
Other languages
Chinese (zh)
Inventor
肖锭锋
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Guangzhou Xaircraft Technology Co Ltd
Original Assignee
Guangzhou Xaircraft Technology Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Guangzhou Xaircraft Technology Co Ltd filed Critical Guangzhou Xaircraft Technology Co Ltd
Priority to CN201720954592.XU priority Critical patent/CN207346070U/en
Application granted granted Critical
Publication of CN207346070U publication Critical patent/CN207346070U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Casings For Electric Apparatus (AREA)

Abstract

The utility model provides a kind of based shell, the based shell includes being used for the base enclosure body being fixedly connected with the fuselage of unmanned plane and the head cover being detachably connected with the base enclosure body, the mounting hole of the electronic device described in face on fuselage is opened up at the top of the base enclosure body, the head cover is arranged on the mounting hole.The unmanned plane of the utility model can improve the convenience of electronic device dismounting, when needing replacing or overhauling electronic device, head 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 host cavity and is positioned on bottom plate by mounting hole and is fixedly mounted, compared with prior art, when avoiding replacement electronic device, need to dismantle complete machine, improve unmanned plane and replace the efficiency of electronic device, and reduce the cost that unmanned plane replaces the efficiency of electronic device.

Description

Based shell, rack and unmanned plane
Technical field
The utility model belongs to unmanned plane during flying device technical field, more particularly to a kind of based shell, rack and unmanned plane.
Background technology
Unmanned plane refers to the not manned vehicle being controlled using wireless remote control device and electronic device, such as nobody is straight 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 housing is typically secured to the outside of unmanned aerial vehicle body to protect the internal structure being equipped on unmanned plane, nothing Man-machine housing is fixed on unmanned aerial vehicle body by fastener, and such a fixed structure dismounting trouble, has seriously affected unmanned electromechanics The efficiency of replacement and the maintenance of sub-device.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane, it is possible to increase the effect of replacement and the maintenance of electronic device Rate.
The utility model is realized in this way a kind of based shell, the based shell includes being used to consolidate with the fuselage of unmanned plane Surely the base enclosure body connected and the head cover being detachably connected with the base enclosure body, open up face at the top of the base enclosure body The mounting hole of electronic device on the fuselage, the head cover are arranged on the mounting hole.
It should be understood that the base enclosure body includes upper shell, the mounting hole is arranged on the upper shell, the upper shell The mounting hole periphery is provided with the first magnetic part, is correspondingly arranged and is useful for and first magnetic part magnetism on the head cover 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 shell is offered with the structure matching of the head cover and for accommodating matching somebody with somebody for the head cover Groove is closed, the mounting hole is arranged at the slot bottom of the mating groove and consolidates through the slot bottom of the mating groove, first magnetic part Due to the slot bottom of the mating groove.
The utility model also provides a kind of rack, including above-mentioned fuselage and based shell.
It should be understood that the fuselage include bottom plate and be arranged in parallel with the bottom plate and with the bottom plate be fixedly mounted Top plate, the top plate are collectively forming an installation space for being used to accommodate the electronic device with the bottom plate, 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 of the close electronic device of the top plate.
The utility model also provides a kind of unmanned plane, 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 housing being fixedly connected of based shell, it is described installation housing include be symmetrically arranged on the upper shell both sides and with the top The two connection shells and be arranged between the two connection shells and for the tie-beams of the connection shells of connection two 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 by the mounting shell be fixedly connected with the top plate and be covered on top plate and the bottom plate on.
The utility model has the technical effect that relative to the prior art:The based shell of the utility model can improve electronics dress Put the convenience of dismounting, when needing replacing or overhauling electronic device, head cover taken out out of mating groove, then by electronic device from Remove on bottom plate and taken out by mounting hole, when electronic device reinstalls bottom plate, electronic device is put into host cavity by mounting hole and is put It is placed on bottom plate and is fixedly mounted, compared with prior art, it is necessary to which complete machine is dismantled when avoiding replacement electronic device, improves Unmanned plane replaces the efficiency of electronic device, and reduces the cost that unmanned plane replaces the efficiency of electronic device.
Brief description of the drawings
In order to illustrate more clearly of the technical solution of the utility model embodiment, below will to the utility model embodiment or Attached drawing needed to be used in the description of the prior art is briefly described, it should be apparent that, drawings described below is only Some embodiments of the utility model, for those of ordinary skill in the art, without creative efforts, Other attached drawings can also be obtained according to these attached drawings.
Fig. 1 is the stereogram for the unmanned plane that the utility model embodiment provides.
Fig. 2 is the exploded view for the unmanned plane that the utility model embodiment provides.
Fig. 3 is the part-structure stereogram for the unmanned plane that the utility model embodiment provides.
Fig. 4 is fuselage, horn, undercarriage, installation housing and the Power Component that the utility model embodiment provides.
Fig. 5 is the solid that undercarriage, horn, the Power Component that the utility model embodiment provides close part airframe structure Figure.
Fig. 6 is the stereogram for the housing unit that the utility model embodiment provides.
Fig. 7 is the stereogram for the connection shell that the utility model embodiment provides.
Fig. 8 is the stereogram for the base enclosure body that the utility model embodiment provides.
Description of reference numerals:
Embodiment
The embodiment of the utility model is described below in detail, the example of the embodiment is shown in the drawings, wherein from beginning Same or similar element is represented to same or similar label eventually or there is same or like element.Below by ginseng The embodiment for examining attached drawing description is exemplary, it is intended to for explaining the utility model, and it is not intended that to the utility model Limitation.
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.
As depicted in figs. 1 and 2, the utility model embodiment provides a kind of unmanned plane and includes fuselage 100, consolidates with fuselage 100 Dingan County dress electronic device 800, be fixedly connected with the fuselage 100 multiple horns 200, be fixedly connected with fuselage 100 two Undercarriage 300, the housing unit 400 for being covered on fuselage 100, be installed on horn 200 100 end of remote fuselage power packages Part 500, the liquid storage container 600 for being installed on fuselage 100 and being used for storage solutions, be installed on fuselage 100 and for being power The battery 700 that component 500 is powered.
Further, as shown in Figures 2 and 3, fuselage 100 includes fuselage body 110 and fixes with fuselage body 110 to connect The installing frame 120 stored is connect and is used for, fuselage body 110 includes the bottom plate 113 and top plate 111 for being arranged in parallel and being fixedly connected, Top plate 111 is collectively forming an installation space 114 for being used to accommodate electronic device 800 with bottom plate 113, and electronic device 800 is in installation Is fixedly connected with bottom plate 113 in space 114, top plate 111 opens up a bit-avoiding slot 112 and communicated with installation space 114 to be filled with supplied for electronic Put 800 to be put into installation space 114 or take out out of installation space 114,112 face electronic device 800 of bit-avoiding slot is set;Installing frame 120 set 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 plate 123 is provided with 120, installing frame 120 has the first installation cavity 121 and the second installation cavity 122 for storing, partition plate 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 illustrate, 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 stretched into installation space 114 and is fixedly connected with bottom plate 113, and the sidepiece 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 away from fuselage 100, and four A Power Component 500 is electrically connected the Power Component 500 for providing flying power with battery 700, and four Power Components 500 are equal The flight stake situation of control unmanned plane is connected to 800 signal of electronic device.
Certainly, in the utility model other embodiment, unmanned plane at least sets a horn 200, and Power Component 500 is right One should at least be set.
Further, as shown in Fig. 2, each Power Component 500 includes propeller 510 and drive with propeller 510 to connect Connecing and drive propeller 510 to rotate 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 connected with 520 signal of driver, Electronic device 800 is by controlling driver 520 to control the flight condition of unmanned plane.
Further, two undercarriages 300 are both secured to the lower section of fuselage 100 to ensure the stabilization of unmanned plane takeoff and landing Property, specifically, as shown in Figure 1, undercarriage 300 include be used for contacted with supporting surface and support fuselage 100 supporting part 310 and Respectively at the first connecting portion 320 and second connecting portion 330 that 310 both ends of supporting part and supporting part 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, which is fixed, to be connected Connect, unmanned plane is positioned 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 set, 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 housing 410 and based shell 420 being fixedly connected, such as Shown in Fig. 4, installation housing 410 includes symmetrically arranged two connection shells 411 and is arranged between two connection shells 411 and is connected with two The tie-beam 414 that shell 411 is fixedly connected, two connection shells 411 are set 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 housing 410 is fixedly connected by connecting plate 412 with top plate 111, and installation housing 410 passes through fixed part 413 are fixedly connected with based shell 420, and the end that two connection shells 411 tilt extended and remote top plate 111 is close to each other, Two connection shells 411 are both provided with antenna mounting groove 414, and antenna mounting groove 414, which also tilts, to be extended, antenna mounting groove 414 Inclined plane and the plate face of top plate 111 are set in angle, and the angular range of the angle is more than or equal to 30 ° and is less than or equal to 70 °, for strengthening the intensity of wireless signal to improve the stability of the transmission of wireless signal, reliability.
Further, as shown in Fig. 2, based shell 420 includes base enclosure body 421 and with detachably connecting on base enclosure body 421 The head cover 429 connect, as shown in figure 8, base enclosure body 421 is included in extended upper shell 425 and procapsid 422, and on Housing 425 is wholely set with procapsid 422, upper shell 425 and the extending direction of extending direction and procapsid 422 substantially hang down Directly.Specifically, the extending direction of upper shell 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 by installing housing 410 with top plate 111 and is covered on top plate 111 and bottom plate 113, Based shell 420 is collectively forming with bottom plate 113 to accommodate the host cavity (the non-label of figure) of electronic device 800, specifically, upper shell 425th, procapsid 422 and head cover 429 surround host cavity jointly with bottom plate 113, and the crown center position of upper shell 425 opens up one and matches somebody with somebody Close groove 427 with accommodate head cover 429 and it is multiple be fixedly connected installation housing 410 screw hole 427a, screw hole 427a, which is arranged at, to be matched somebody with somebody The bottom of groove 427 is closed, the fixed part 413 of shell 411 is connected and is locked with the screw hole 427a of upper shell 425 by determining part (not shown) Fastening, the structure of mating groove 427 is set with the structure matching of head cover 429, specifically, shape and the head cover 429 of mating groove 427 Form fit set, the depth of mating groove 427 and the thickness matching of head cover 429 are set, and head cover 429 can with base enclosure body 421 Dismantling connection also opens up one at mating groove 427, on upper shell 425 and the simultaneously disengaging of electronic devices 800 collecting is communicated with host cavity The mounting hole 426 of chamber, specifically, in the bottom of mating groove 427 open up one installed with electronic devices 800 when the mounting hole that passes through 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 connects setting, and mounting hole 426 and bit-avoiding slot 112 and electronics with host cavity, bit-avoiding slot 112 and installation space 114 Device 800 aligns setting, and screw hole 427a is arranged at the peripheral position of mounting hole 426.
Further, in being installed with multiple first magnetic parts (figure non-label), and first in the slot bottom of mating groove 427 Magnetic part is arranged at the peripheral position of mounting hole 427, and the first magnetic part is magnet, and head cover 429 is installed with and the first magnetism Part corresponds setting and the second magnetic part (the non-label of figure) made of magnetic material, and the second magnetic part is ferrimagnet system Into, the pole of the second magnetic part and the first magnetic part polarity to anti-, when head cover 429 is installed, multiple second magnetic parts of head cover 429 Correspond and install with multiple first magnetic parts in mating groove 427, the second magnetic part is attracting by magnetic force with the first magnetic part And be that head cover 429 is fixedly installed in mating groove 427, and be covered on mounting hole 426.
When electronic device 800 is installed, electronic device 800 is put into host cavity 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 head 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 at mounting hole 426, the based shell 420 of the utility model embodiment can improve The convenience of electronic device dismounting, it is necessary to which complete machine is dismantled when avoiding replacement electronic device 800, improves unmanned plane replacement The efficiency of electronic device 800, and reduce the cost that unmanned plane replaces the efficiency of electronic device 800.
Further, the both sides of procapsid 422 are respectively provided with one and are communicated with host cavity and lead to the ventilation culvert of electronic device 800 Road 423, during unmanned plane during flying, since the operation of electronic device 800 can produce substantial amounts of heat, there is two ventilations culvert in extraneous cold space Road 423 enters in host cavity to be cooled down with electronic devices 800.
The unmanned plane of the utility model embodiment can improve the convenience of the dismounting of electronic device 800, when needing replacing or When overhauling electronic device 800, head cover 429 is taken out out of mating groove 427, then electronic device 800 is removed simultaneously from bottom plate 113 Taken out by mounting hole 426, when electronic device 800 reinstalls bottom plate 113, electronic device 800 is put into host cavity simultaneously by mounting hole 426 It is positioned on bottom plate 113 and is fixedly mounted, compared with prior art, avoids when replacing electronic device 800, it is necessary to which complete machine is torn open Unload, improve unmanned plane replace electronic device 800 efficiency, and reduce unmanned plane replace electronic device 800 efficiency into This.
When head 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 head cover 429, only need to adjust head cover 429 makes head cover 429 and mating groove 427 right in the position of mating groove 427 and angle Positive installation, greatly improves the efficiency of installation, when head cover 429 is dismantled, the first magnetic part is separated and is moved with the second magnetic part Head cover 429 is opened, the dismounting of head cover 429 is very convenient, and need not collect the connector for head cover 429 and base enclosure body 421, Compared with conventional art, the head cover 429 of the utility model embodiment is high with the disassembly efficiency of base enclosure body 421, head cover 429 and base Shell body 421 can realize repeated disassembled and assembled by the magnetic connection of the second magnetic part and the first magnetic part, 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 Put 800 to play a protective role, avoid loading directly impact electronic device 800 and cause electronic device 800 to damage, with reduce maintenance into 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 the first installation cavity 121 of the setting of installing frame 120 and the second installation cavity 122 can at least install two kinds of different size objects, Second installation cavity 122 is arranged 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 produce at work Heat, after the heat that liquid absorption battery 700 and electronic device 800 in liquid storage container 600 produce, during 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 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)

1. a kind of based shell, it is characterised in that the based shell includes being used for the base enclosure sheet being fixedly connected with the fuselage of unmanned plane Body and the head cover being detachably connected with the base enclosure body, the electricity described in face on fuselage is opened up at the top of the base enclosure body The mounting hole of sub-device, the head cover are arranged on the mounting hole;
The base enclosure body includes upper shell, and the mounting hole is arranged on the upper shell, and the upper shell is in mounting hole week While being provided with the first magnetic part, it is correspondingly arranged and is useful for and magnetic the second magnetism being connected of first magnetic part on the head cover Part.
2. based shell as claimed in claim 1, it is characterised in that first magnetic part is magnet, second magnetic part It is made of ferrimagnet.
3. based shell as claimed in claim 1, it is characterised in that the upper shell offers the structure matching with the head cover And for accommodating the mating groove of the head cover, the mounting hole is arranged at the slot bottom of the mating groove and through the mating groove Slot bottom, first magnetic part are fixed on the slot bottom of the mating groove.
4. a kind of rack, including fuselage as claimed in claim 3 and based shell.
5. rack as claimed in claim 4, it is characterised 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 are collectively forming a peace for being used to accommodate the electronic device with the bottom plate Space is filled, the top plate opens up a bit-avoiding slot, and the bit-avoiding slot connects the installation space and the bit-avoiding slot and the electronics Device and the equal face of the mounting hole are set.
6. rack as claimed in claim 5, it is characterised in that the close electronics dress of the bit-avoiding slot through the top plate The one end put.
7. a kind of unmanned plane, including such as claim 5-6 any one of them rack and electronic device.
8. unmanned plane as claimed in claim 7, it is characterised in that the unmanned plane includes housing unit, the housing unit The installation housing being fixedly connected including the based shell and with the based shell, the installation housing include being symmetrically arranged on institute State upper shell both sides and with the top plate is fixedly connected two is connected shell and is arranged between the two connection shells and for connecting Connect the tie-beam of the two connection shells.
9. unmanned plane as claimed in claim 8, it is characterised in that the bottom of the mating groove is additionally provided with described for installing The screw hole of shell is connected, 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.
CN201720954592.XU 2017-08-01 2017-08-01 Based shell, rack and unmanned plane Active CN207346070U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720954592.XU CN207346070U (en) 2017-08-01 2017-08-01 Based shell, rack and unmanned plane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720954592.XU CN207346070U (en) 2017-08-01 2017-08-01 Based shell, rack and unmanned plane

Publications (1)

Publication Number Publication Date
CN207346070U true CN207346070U (en) 2018-05-11

Family

ID=62360500

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201720954592.XU Active CN207346070U (en) 2017-08-01 2017-08-01 Based shell, rack and unmanned plane

Country Status (1)

Country Link
CN (1) CN207346070U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109319085A (en) * 2017-08-01 2019-02-12 广州极飞科技有限公司 Based shell, rack and unmanned plane

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109319085A (en) * 2017-08-01 2019-02-12 广州极飞科技有限公司 Based shell, rack and unmanned plane

Similar Documents

Publication Publication Date Title
US10093418B2 (en) Unmanned aerial vehicle
CN107207087B (en) Unmanned aerial vehicle
CN103350752A (en) Four-rotor aircraft
CN205854465U (en) A kind of low windage unmanned plane
US20160229530A1 (en) Unmanned aerial vehicle protective frame configuration
CN107223108B (en) Power supply module, unmanned vehicle and remote-controlled movement device
CN205469856U (en) Power supply module , Unmanned vehicles and remote control mobile device
CN213139140U (en) But autogiration's remote sensing survey and drawing unmanned aerial vehicle
CN207346070U (en) Based shell, rack and unmanned plane
CN207346071U (en) Unmanned plane and based shell
CN111619783A (en) Unmanned aerial vehicle with collapsible unmanned aerial vehicle support piece
CN207060390U (en) Unmanned plane and unmanned plane frame
CN116039981B (en) Adaptive multi-module assembled unmanned aerial vehicle
CN207346069U (en) It is a kind of for the installing frame of unmanned plane, rack and unmanned plane
CN207060392U (en) Unmanned plane
CN205418094U (en) Push -button aircraft
CN109319085A (en) Based shell, rack and unmanned plane
CN206569278U (en) A kind of unmanned aerial vehicle onboard disassembly and assembly structure and unmanned plane
CN210912856U (en) Unmanned vehicles's wing arm subassembly and unmanned vehicles
CN207060375U (en) A kind of unmanned plane
CN207550497U (en) A kind of unmanned plane
CN106531925A (en) Power cabin
CN220263107U (en) Portable unmanned aerial vehicle attack system
CN214808420U (en) Model aeroplane and model ship aircraft based on solar energy power supply
CN206031751U (en) Unmanned aerial vehicle that can quick assembly disassembly

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant
CP03 Change of name, title or address
CP03 Change of name, title or address

Address after: 510000 Block C, 115 Gaopu Road, Tianhe District, Guangzhou City, Guangdong Province

Patentee after: Guangzhou Jifei Technology Co.,Ltd.

Address before: 510000, Guangdong, Guangzhou, Gaotang Tianhe District Software Park Road, No. 1, 3A01

Patentee before: Guangzhou Xaircraft Technology Co.,Ltd.