CN209008869U - Unmanned plane gondola mounting structure and unmanned machine equipment - Google Patents

Unmanned plane gondola mounting structure and unmanned machine equipment Download PDF

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Publication number
CN209008869U
CN209008869U CN201821292278.0U CN201821292278U CN209008869U CN 209008869 U CN209008869 U CN 209008869U CN 201821292278 U CN201821292278 U CN 201821292278U CN 209008869 U CN209008869 U CN 209008869U
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CN
China
Prior art keywords
unmanned plane
quickly disassembling
mounting structure
shell
carry
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Active
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CN201821292278.0U
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Chinese (zh)
Inventor
卢致辉
车嘉兴
李杨
黄少龙
杨春春
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Zhejiang Kebit Technology Co Ltd
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Zhejiang Kebit Technology Co Ltd
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Priority to CN201821292278.0U priority Critical patent/CN209008869U/en
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Abstract

The utility model is suitable for unmanned vehicle technical field, provide a kind of unmanned plane gondola mounting structure and unmanned machine equipment, unmanned plane gondola mounting structure includes multiple second device for quickly disassembling be removably mounted to the first device for quickly disassembling of unmanned plane lower end, be removably mounted to the loading plate component of the lower end of the first device for quickly disassembling, and being removably mounted to the lower end of loading plate component;Second device for quickly disassembling includes the second airborne end, and the second airborne end is for installing outer load equipment.The utility model is by being arranged loading plate component in the lower end of the first device for quickly disassembling, multiple second device for quickly disassembling are connected with loading plate component, second device for quickly disassembling can install outer load equipment, it is thus achieved that multiple outer load equipment can be installed on the basis of the first device for quickly disassembling, improve the carry ability of unmanned plane, multiple outer installations for carrying equipment are capable of providing that unmanned plane is more or more preferably function, meet currently to the higher requirement of unmanned plane.

Description

Unmanned plane gondola mounting structure and unmanned machine equipment
Technical field
The utility model belongs to unmanned vehicle technical field, in particular to a kind of unmanned plane gondola mounting structure and nobody Machine equipment.
Background technique
Unmanned plane be it is a kind of by radio robot or airborne computer stored program controlled manipulated it is not manned fly Row device, unmanned plane structure is simple, use cost is low, can not only complete the task of manned aircraft execution, be more suitable for someone The task that aircraft should not execute plays the role of very big in burst thing emergency, early warning.With unmanned air vehicle technique continuous development and Maturation has been widely used in taking photo by plane, the fields such as field is searched and rescued, mapping, has greatly expanded the purposes of unmanned plane itself.To take photo by plane For, carry part is carried using unmanned plane, such as video camera, high speed camera filming apparatus, it is more manned take photo by plane for, cost is lower And safety is higher, can be widely applied to national ecological environmental protection, mineral resources exploration, marine environmental monitoring, land use Investigation, water resources development, crop growth monitoring and the yield by estimation, agricultural operation, Natural calamity monitoring and assessment, urban planning and city The fields such as political affairs management, forest disease and pest protection and monitoring, public safety, Defence business, digital earth and advertisement photography, have The wide market demand.
Unmanned plane, which carries carry part, to be realized by the way that the gondola mounting structure of uav bottom is arranged in.However, existing Unmanned plane gondola mounting structure can only install and carry equipment outside one, a such as video camera can not be carried out carrying outside two simultaneously and be set The transmission of standby installation and two-path video signal, limits the use of unmanned plane, causes a degree of wasting of resources. Therefore, it is necessary to a kind of unmanned plane gondola mounting structure that can carry two or more outer load equipment simultaneously be provided, with full The higher use demand of sufficient unmanned plane.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane gondola mounting structures, it is intended to solve hanging for existing unmanned plane The lower technical problem of cabin carry ability.
The utility model is realized in this way a kind of unmanned plane gondola mounting structure, for installing outer carry on unmanned plane Equipment, comprising:
First device for quickly disassembling is removably mounted to the lower end of unmanned plane;
Loading plate component is removably mounted to the lower end of first device for quickly disassembling;
Multiple second device for quickly disassembling are removably mounted to the lower end of the loading plate component;
Second device for quickly disassembling includes the second airborne end, and the second airborne end carries equipment for installing outside one.
It further include the communication switching unit for being installed on the lower end of the loading plate component, the communication switching unit is set to more Between a second device for quickly disassembling, and communication connection is distinguished with multiple outer load equipment.
First device for quickly disassembling includes the first carry end for being installed on the lower end of the unmanned plane and detachable installation In the first airborne end at first carry end, the loading plate component is installed on the lower end at the described first airborne end;
Second device for quickly disassembling further includes the second carry end, and the second airborne end and second carry end are detachable Connection, second carry end is installed on the lower end of the loading plate component.
The first airborne end includes first shell, and it is sliding that first is respectively provided in the opposite both ends of the surface of the first shell Opposite two the first side walls of rail, first carry end are equipped with the first sliding groove entered for first sliding rail;
The second airborne end includes second shell, is respectively provided with the second sliding rail on the opposite both ends of the second shell, Opposite two second sidewalls at second carry end are equipped with the second sliding slot entered for second sliding rail.
Also be respectively provided with the first telescopic buckle in the opposite both ends of the surface of the first shell, the first shell it is other End face is equipped with the first button portion for controlling first telescopic buckle;The first side wall at first carry end is equipped with The first card hole for passing through or retracting for first telescopic buckle;
The second telescopic buckle, the other end of the second shell are also respectively provided on the opposite both ends of the second shell Face is equipped with the second button portion for controlling second telescopic buckle;The second sidewall at second carry end, which is equipped with, to be supplied The second card hole that second telescopic buckle is passed through or retracted.
First carry end includes the first power supply output module and the first communication output module, the first airborne end packet It includes and is set to the intracorporal first communication input module of the first shell and the first Power Entry Module, the first communication output mould Block is docked with the first communication input module, and the first power supply output module is docked with first Power Entry Module;
Second carry end includes second source output module and the second communication output module, the second airborne end packet It includes and is set to the intracorporal second communication input module of the second shell and second source input module, the second communication output mould Block is docked with the second communication input module, and the second source output module is docked with the second source input module.
First device for quickly disassembling is identical as the structure of second device for quickly disassembling.
The loading plate component includes the upper plate for being installed on the lower end at first carry end and second device for quickly disassembling The lower plate of connection and the side plate being connected between the upper plate and lower plate, limit a chamber between the upper plate, lower plate and side plate Body.
The upper plate is equipped with upper through-hole, and the lower plate is equipped with the first lower through-hole and multiple second lower through-holes, in the cavity Equipped with connection and power supply line, through-hole is stretched out in one end of the connection and power supply line, and the other end of the connection is stretched The other end of first lower through-hole out, the power supply line stretches out second lower through-hole.
The another object of the utility model is to provide a kind of unmanned machine equipment, including above-mentioned described unmanned plane gondola peace Assembling structure.
The beneficial effect of unmanned plane gondola mounting structure provided by the utility model and unmanned machine equipment compared with the existing technology Fruit is: by the way that loading plate component is arranged in the lower end of first device for quickly disassembling, connecting multiple second with loading plate component Device for quickly disassembling, every one second device for quickly disassembling, which can be installed, carries equipment outside one, it is thus achieved that in first device for quickly disassembling On the basis of multiple outer load equipment can be installed, improve the carry ability of unmanned plane, multiple outer installations for carrying equipment are capable of providing Unmanned plane is more or more preferably function, meets currently to the higher requirement of unmanned plane.
Detailed description of the invention
Fig. 1 is the decomposition texture schematic diagram of unmanned plane gondola mounting structure provided by the embodiment of the utility model;
Fig. 2 is that the part-structure of loading plate component in unmanned plane gondola mounting structure provided by the embodiment of the utility model shows It is intended to;
Fig. 3 is the structural representation at the first carry end in unmanned plane gondola mounting structure provided by the embodiment of the utility model Figure;
Fig. 4 is another angle at the first carry end in unmanned plane gondola mounting structure provided by the embodiment of the utility model Structural schematic diagram;
Fig. 5 is the structural representation at the first airborne end in unmanned plane gondola mounting structure provided by the embodiment of the utility model Figure;
Fig. 6 is the structural representation at the second carry end in unmanned plane gondola mounting structure provided by the embodiment of the utility model Figure;
Fig. 7 is another angle at the second carry end in unmanned plane gondola mounting structure provided by the embodiment of the utility model Structural schematic diagram;
Fig. 8 is the structural representation at the second airborne end in unmanned plane gondola mounting structure provided by the embodiment of the utility model Figure;
Fig. 9 is that the communication line and power circuit in unmanned plane gondola mounting structure provided by the embodiment of the utility model show It is intended to.
Meaning marked in the figure are as follows:
Unmanned plane gondola mounting structure 100;
First device for quickly disassembling 1, the first carry end 11, the first holding part 111, the first communication output module 112, the first power supply Output module 113, the first side wall 114, first sliding groove 115, the first card hole 116;
First airborne end 12, first shell 121, the first communication input module 122, the first Power Entry Module 123, first Sliding rail 124, the first telescopic buckle 125, the first button portion 126;
Second device for quickly disassembling 2, the second carry end 21, the second holding part 211, the second communication output module 212, second source Output module 213, second sidewall 214, second sliding slot 215, the second card hole 216;
Second airborne end 22, second shell 221, the second communication input module 222, second source input module 223, second Sliding rail 224, the second telescopic buckle 225, the second button portion 226;
Loading plate component 3, upper plate 31, lower plate 32, side plate 33, stiffening plate 34, upper through-hole 35, the first lower through-hole 36, second Lower through-hole 37, cavity 38;
Communication switching unit 4, protective shell 41, interchanger 42.
Specific 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, the present invention will be further described in detail.It should be appreciated that specific embodiment described herein is only to explain this Utility model is not used to limit the utility model.
It should be noted that when component is referred to as " being fixed on " or " being set to " another component, it can directly or It connects on another component.When a component is known as " being connected to " another component, it be can be directly or indirectly It is connected on another component.The orientation or positional relationship of the instructions such as term " on ", "lower", "left", "right" is based on attached drawing Shown in orientation or positional relationship, be merely for convenience of describing, rather than the device or element of indication or suggestion meaning must have There is specific orientation, be constructed and operated in a specific orientation, therefore should not be understood as the limitation to this patent.Term " first ", " second " is used merely to facilitate description purpose, is not understood to indicate or imply relative importance or implicitly indicates technical characteristic Quantity.The meaning of " plurality " is two or more, unless otherwise specifically defined.
In order to illustrate technical solution described in the utility model, carried out specifically below in conjunction with specific accompanying drawings and embodiments It is bright.
Referring to Fig. 1, the utility model provides a kind of unmanned plane gondola mounting structure 100, for installing on unmanned plane Outer load equipment, comprising: the first device for quickly disassembling 1, loading plate component 3 and multiple second device for quickly disassembling 2, wherein the first device for quickly disassembling 1 It is removably installed in the lower end of unmanned plane, loading plate component 3 is removably installed in the lower end of the first device for quickly disassembling 1, multiple Second device for quickly disassembling 2 is further removably installed in the lower end of loading plate component 3, and the second device for quickly disassembling 2 is for installing outer load Equipment, so that multiple second device for quickly disassembling 2 can install multiple outer load equipment, such as the second device for quickly disassembling 2 includes holder hole location, is used It is connect in holder.The unmanned plane gondola mounting structure 100 of the utility model is not limited to install the bat such as video camera by holder It takes the photograph device to take photo by plane, outer load equipment can also be the optoelectronic devices such as rangefinder or thermal infrared imager, and certainly outer load equipment can also To be the non-optoelectronic device for transmitting or not needing communication signal remote control without signal, such as one of them the second device for quickly disassembling 2 Upper installation video camera can install reserve battery component on another second device for quickly disassembling 2 and provide for video camera even unmanned plane Power supply improves the cruise duration of video camera or unmanned plane.
Unmanned plane gondola mounting structure 100 provided by the utility model is held by the setting in the lower end of the first device for quickly disassembling 1 Support plate component 3 is detachably connected multiple second device for quickly disassembling 2 with loading plate component 3, and every one second device for quickly disassembling 2 can The outer load equipment of installation improves nobody it is thus achieved that can install multiple outer load equipment on the basis of the first device for quickly disassembling 1 The carry ability of machine, multiple outer installations for carrying equipment are capable of providing that unmanned plane is more or more preferably function, meet currently to nobody The higher requirement of machine.
As a preferred embodiment, the first device for quickly disassembling 1 is identical with the structure of the second device for quickly disassembling 2, and such benefit is First device for quickly disassembling 1 and the second device for quickly disassembling 2 may be used interchangeably, and outer load equipment can be installed on the first device for quickly disassembling 1, can also To be installed on the second device for quickly disassembling 2, it is often more important that, it, can be by 1 He of the first device for quickly disassembling when only needing to carry equipment outside one It is dismantled between loading plate component 3, outer load equipment is directly mounted on the first device for quickly disassembling 1, outer with existing UAV flight one The usage mode for carrying equipment is identical.Therefore, the unmanned plane gondola mounting structure 100 of the utility model can carry outside one carrying Flexible choice uses between equipment and multiple outer load equipment.
Referring specifically to Fig. 1, in the present embodiment, the quantity of the second device for quickly disassembling 2 is 2, is respectively arranged at loading plate component 3 Lower end two sides, a communication switching unit 4, the shunting for communication signal are additionally provided between two second device for quickly disassembling 2.It is logical Interrogating conversion equipment 4 includes interchanger 42 and the protective shell 41 for protecting the interchanger 42, and interchanger 42 passes through protective shell 41 It is installed on the lower end of loading plate component 3.
Please refer to Fig. 1 and Fig. 2, loading plate component 3 include upper plate 31, lower plate 32 and be connected to upper plate 31 and lower plate 32 it Between multiple side plates 33, a cavity 38 is limited between upper plate 31, lower plate 32 and side plate 33.Multiple add is also provided in lower plate 32 Strong plate 34 is used to support the cavity 38 and guarantees the bearing strength of upper plate 31 and lower plate 32.Upper plate 31 is equipped with upper through-hole 35, under Plate 32 is equipped with the first lower through-hole 36 of corresponding communication switching unit 4 and the second lower through-hole 37 of the second device for quickly disassembling of multiple correspondences 2, First lower through-hole 36 is installed on lower plate 32 by protective shell 41 for installing protective shell 41, interchanger 42.Electricity is equipped in cavity 38 Source line and connection (not shown), one end of power supply line stretch out in through-hole 35, and the other end of power supply line stretches out in multiple second Lower through-hole 37, one end of connection stretch out in through-hole 35, and the other end stretches out in the first lower through-hole 36 and is connected to interchanger 42, That is, upper through-hole 35, the first lower through-hole 36, the second lower through-hole 37 and cavity 38 for power supply line and connection from unmanned plane at most The shunting of a outer electric power and signal for carrying equipment.
Fig. 1, Fig. 3 is please referred to include the first carry end 11 to 5, first device for quickly disassembling 1 and be installed on the first carry end 11 The airborne end 12 of interior first, the lower end of unmanned plane are connect with the first carry end 11, for example, passing through screw (not shown) and setting respectively The screw hole cooperation set on the lower end and the first carry end 11 of unmanned plane is installed, loading plate component 3 and the first airborne end 12 Between connect, equally can be through screw and the spiral shell that is separately positioned in the upper cover and the first airborne end 12 of loading plate component 3 It is installed in hole.
First airborne end 12 includes first shell 121, and is set to the first communication input of side in first shell 121 Module 122 and the first Power Entry Module 123, one end of the first communication input module 122 and the first Power Entry Module 123 One end is separately connected connection and power supply line in supreme through-hole 35.Is respectively provided in the opposite both ends of the surface of first shell 121 One sliding rail 124 and the first telescopic buckle 125, other end are equipped with the first button for controlling first telescopic buckle 125 Portion 126, specifically, the first button portion 126 are the first inclined-planes (not shown) by being set in first shell 121 to stretch with first 125 connection of contracting buckle, the first button portion 126 can drive the first telescopic buckle 125 to withdraw or pop up.
First carry end 11 includes the first holding part 111, is equipped with the first communication output module in the first holding part 111 112 and the first power supply output module 113, one end of the first communication output module 112 and one end of the first power supply output module 113 It is connected to unmanned plane, two opposite the first side walls 114 positioned at 111 side of the first holding part, which are equipped with, supplies two first sliding rails First card hole 116 of 124 first sliding grooves 115 entered and corresponding first telescopic buckle 125.
When pressing the first button portion 126, the first telescopic buckle 125 on the first airborne end 12 is withdrawn, sliding along first First sliding rail 124 at the first airborne end 12 is pushed by slot 115, after the first telescopic buckle 125 reaches the first card hole 116, is released The first button portion 126 is put, the first telescopic buckle 125 is popped up and is sticked in the first card hole 116, also, the first communication output The other end of module 112 is docked with the other end of the first communication input module 122, the other end of the first power supply output module 113 It is docked with the other end of second source input module 223, it is thus achieved that the first carry end 11 and the first airborne end 12 is removable Connection and communication connection and electric connection are unloaded, electric power and communication signal from unmanned plane can be transferred to the first airborne end 12, please refer to Fig. 9 (solid arrow indicates that power circuit, dotted arrow indicate communication line in figure).
Similarly, referring to Figure 1, Fig. 6 to 8, the second device for quickly disassembling 2 includes the second carry end 21 and is installed on the second carry The second airborne end 22 in end 21, the lower plate 32 of loading plate component 3 are connect with the second carry end 21, for example, passing through screw and spiral shell Hole is coupled, and is repeated no more.
Second airborne end 22 includes second shell 221, and is set to the second communication input of side in second shell 221 Module 222 and second source input module 223, one end of the second communication input module 222 and second source input module 223 One end is connected to outer load equipment.The second sliding rail 224 and the second flexible card are respectively provided in the opposite both ends of the surface of second shell 221 Button 225, other end are equipped with the second button portion 226 for controlling second telescopic buckle 225, similarly, the second button Portion 226 is the second inclined-plane (not shown) by being set in second shell 221 to connect with the second telescopic buckle 225, and second presses Button portion 226 can drive the second telescopic buckle 225 to withdraw or pop up.
Second carry end 21 includes the second holding part 211, is equipped with the second communication output module in the second holding part 211 212 and second source output module 213, one end of the second communication output module 212 is connected to communication conversion module, second source One end of output module 213 is connected to the power supply line in the second lower through-hole 37.Positioned at the two opposite of 211 side of the second holding part Second sidewall 214 is equipped with the of the second sliding slot 215 and corresponding second telescopic buckle 225 entered for two second sliding rails 224 Two card holes 216.
When pressing the second button portion 226, the second telescopic buckle 225 on the second airborne end 22 is withdrawn, sliding along second Second sliding rail 224 at the second airborne end 22 is pushed by slot 215, after the second telescopic buckle 225 reaches the second card hole 216, is released The second button portion 226 is put, the second telescopic buckle 225 is popped up and is sticked in the second card hole 216, also, the second communication output The other end of module 212 is docked with the other end of the second communication input module 222, the other end of second source output module 213 It is docked with the other end of second source input module 223, it is thus achieved that the second carry end 21 and the second airborne end 22 is removable Connection and communication connection and electric connection are unloaded, electric power and communication signal from unmanned plane can be further transferred to the second machine It carries end 22 and is transferred to outer load equipment, please refer to Fig. 9.
As illustrated in figures 4 and 7, the front end of first sliding groove 115 and second sliding slot 215 can be set to horn-like, in order to The entrance of one sliding rail 124 and the second sliding rail 224.
First Power Entry Module 123, the first power supply output module 113, second source input module 223 and second source Output module 213 is the transmitting for electric current, and it is logical that the first communication input module 122, first communicates output module 112, second News input module 222 and the second communication output module 212 are the transmitting for communication signal.
According to above mentioned, the first airborne end 12 is installed in the first carry end 11 and two second airborne ends 22 are installed on After in two second carry ends 21, equipment, such as two video cameras are can be realized on a unmanned plane while carried outside installation two, and Signal transmission route between two video cameras is independent of each other, while carrying out shooting transmission and control etc..
First device for quickly disassembling 1 and the second device for quickly disassembling 2 be it is identical, therefore, the second airborne end 22 can be installed on first On carry end 11, and second source input module 223 can be docked with the first power supply output module 113, the second communication input Module 222 can be docked with the first communication output module 112, at this point, the usually used mode as unmanned plane, only carries one Outer load equipment.
The utility model also provides a kind of unmanned machine equipment, hangs including unmanned plane and the unmanned plane for being mounted on unmanned lower end Cabin mounting structure, referring to unmanned plane structure for pod described in above-described embodiment.
The above is only the preferred embodiment of the utility model only, is not intended to limit the utility model, all at this Made any modifications, equivalent replacements, and improvements etc., should be included in the utility model within the spirit and principle of utility model Protection scope within.

Claims (10)

1. a kind of unmanned plane gondola mounting structure, for installing outer load equipment on unmanned plane characterized by comprising
First device for quickly disassembling is removably mounted to the lower end of unmanned plane;
Loading plate component is removably mounted to the lower end of first device for quickly disassembling;
Multiple second device for quickly disassembling are removably mounted to the lower end of the loading plate component;
Second device for quickly disassembling includes the second airborne end, and the second airborne end is for installing outer load equipment.
2. unmanned plane gondola mounting structure as described in claim 1, which is characterized in that further include being installed on the carrying board group The communication switching unit of the lower end of part, the communication switching unit be set to multiple second device for quickly disassembling between, and with it is multiple The outer load equipment distinguishes communication connection.
3. unmanned plane gondola mounting structure as described in claim 1, which is characterized in that first device for quickly disassembling includes installation In the lower end of the unmanned plane the first carry end and be removably mounted to the first airborne end at first carry end, it is described Loading plate component is installed on the lower end at the described first airborne end;
Second device for quickly disassembling further includes the second carry end, and the second airborne end detachably connects with second carry end It connects, second carry end is installed on the lower end of the loading plate component.
4. unmanned plane gondola mounting structure as claimed in claim 3, which is characterized in that the first airborne end includes first shell Body is respectively provided with the first sliding rail, opposite two the first side walls at first carry end in the opposite both ends of the surface of the first shell It is equipped with the first sliding groove entered for first sliding rail;
The second airborne end includes second shell, and the second sliding rail is respectively provided on the opposite both ends of the second shell, described Opposite two second sidewalls at the second carry end are equipped with the second sliding slot entered for second sliding rail.
5. unmanned plane gondola mounting structure as claimed in claim 4, which is characterized in that the opposite both ends of the first shell The first telescopic buckle is also respectively provided on face, other two end face of the first shell is equipped with flexible for controlling described first First button portion of buckle;The first side wall at first carry end is equipped with what confession first telescopic buckle was passed through or retracted First card hole;
The second telescopic buckle is also respectively provided on the opposite both ends of the second shell, the other both ends of the surface of the second shell are set There is the second button portion for controlling second telescopic buckle;The second sidewall at second carry end is equipped with for described the The second card hole that two telescopic buckles are passed through or retracted.
6. unmanned plane gondola mounting structure as claimed in claim 4, which is characterized in that first carry end includes the first electricity Source output module and the first communication output module, the first airborne end include being set to intracorporal first communication of the first shell Input module and the first Power Entry Module, the first communication output module communicate input module with first and dock, and described the One power supply output module is docked with first Power Entry Module;
Second carry end includes second source output module and the second communication output module, and the second airborne end includes setting Be placed in the intracorporal second communication input module and second source input module of the second shell, the second communication output module with Second communication input module docking, the second source output module are docked with the second source input module.
7. such as unmanned plane gondola mounting structure described in any one of claims 1 to 6, which is characterized in that first Quick Release Device is identical as the structure of second device for quickly disassembling.
8. the unmanned plane gondola mounting structure as described in any one of claim 3 to 6, which is characterized in that the carrying board group Part includes the upper plate for being installed on the lower end at first carry end, the lower plate connecting with second device for quickly disassembling and is connected to Side plate between the upper plate and lower plate limits a cavity between the upper plate, lower plate and side plate.
9. unmanned plane gondola mounting structure as claimed in claim 8, which is characterized in that the upper plate is equipped with upper through-hole, described Lower plate is equipped with the first lower through-hole and multiple second lower through-holes, is equipped with connection and power supply line in the cavity, the connection and Through-hole is stretched out in one end of power supply line, and the other end of the connection stretches out first lower through-hole, the power supply line it is another Second lower through-hole is stretched out in one end.
10. a kind of unmanned machine equipment, which is characterized in that including the described in any item unmanned plane gondola installation knots of claim 1 to 9 Structure.
CN201821292278.0U 2018-08-10 2018-08-10 Unmanned plane gondola mounting structure and unmanned machine equipment Active CN209008869U (en)

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Application Number Priority Date Filing Date Title
CN201821292278.0U CN209008869U (en) 2018-08-10 2018-08-10 Unmanned plane gondola mounting structure and unmanned machine equipment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201821292278.0U CN209008869U (en) 2018-08-10 2018-08-10 Unmanned plane gondola mounting structure and unmanned machine equipment

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Publication Number Publication Date
CN209008869U true CN209008869U (en) 2019-06-21

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114572409A (en) * 2022-05-07 2022-06-03 北京卓翼智能科技有限公司 A installation device and unmanned aerial vehicle for unmanned aerial vehicle load

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114572409A (en) * 2022-05-07 2022-06-03 北京卓翼智能科技有限公司 A installation device and unmanned aerial vehicle for unmanned aerial vehicle load
CN114572409B (en) * 2022-05-07 2022-07-29 北京卓翼智能科技有限公司 A installation device and unmanned aerial vehicle for unmanned aerial vehicle load

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