CN211702606U - Airborne control box and unmanned aerial vehicle - Google Patents

Airborne control box and unmanned aerial vehicle Download PDF

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Publication number
CN211702606U
CN211702606U CN202020613614.8U CN202020613614U CN211702606U CN 211702606 U CN211702606 U CN 211702606U CN 202020613614 U CN202020613614 U CN 202020613614U CN 211702606 U CN211702606 U CN 211702606U
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China
Prior art keywords
bottom plate
control box
box body
unmanned aerial
aerial vehicle
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CN202020613614.8U
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Chinese (zh)
Inventor
曹海滨
王金元
涂玥
薛华武
孟德义
樊亮
张宇川
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.)
Hangjin Banner Huasheng Photovoltaic Energy Co Ltd
Siziwangqi Wind Power Heating Co Ltd
State Power Investment Group Damaoqi New Energy Power Generation Co Ltd
State Power Investment Group Dengkou Photovoltaic Power Generation Co Ltd
State Power Investment Group Wulat Zhongqi New Energy Power Generation Co Ltd
Spic Inner Mongolia New Energy Co ltd
Original Assignee
Hangjin Banner Huasheng Photovoltaic Energy Co Ltd
Siziwangqi Wind Power Heating Co Ltd
State Power Investment Group Damaoqi New Energy Power Generation Co Ltd
State Power Investment Group Dengkou Photovoltaic Power Generation Co Ltd
State Power Investment Group Wulat Zhongqi New Energy Power Generation Co Ltd
Spic Inner Mongolia New Energy Co ltd
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Application filed by Hangjin Banner Huasheng Photovoltaic Energy Co Ltd, Siziwangqi Wind Power Heating Co Ltd, State Power Investment Group Damaoqi New Energy Power Generation Co Ltd, State Power Investment Group Dengkou Photovoltaic Power Generation Co Ltd, State Power Investment Group Wulat Zhongqi New Energy Power Generation Co Ltd, Spic Inner Mongolia New Energy Co ltd filed Critical Hangjin Banner Huasheng Photovoltaic Energy Co Ltd
Priority to CN202020613614.8U priority Critical patent/CN211702606U/en
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Publication of CN211702606U publication Critical patent/CN211702606U/en
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Abstract

The utility model relates to the technical field of unmanned aerial vehicles, in particular to an airborne control box and an unmanned aerial vehicle, the airborne control box comprises a box body and a base, a holding cavity with an open end is arranged in the box body, and the holding cavity is used for holding a control assembly; the base includes the bottom plate and sets up a plurality of flaky and elastic engaging lugs that are all around the bottom plate, and the bottom plate can be dismantled with the box body and be connected and will uncovered the closure, and the engaging lug is connected with the bottom plate, and the engaging lug is used for being connected with unmanned aerial vehicle's organism, and the engaging lug can be with the unsettled support of bottom plate in the organism. This machine carries control box, after the engaging lug is connected with unmanned aerial vehicle's organism, bottom plate and box body can be unsettled with unmanned aerial vehicle's organism, because the engaging lug has elasticity to when organism acceleration and deceleration or emergence vibration, the stability of box body internal control subassembly can be guaranteed to bottom plate and box body damping to the accessible engaging lug. This unmanned aerial vehicle includes above-mentioned airborne control box.

Description

Airborne control box and unmanned aerial vehicle
Technical Field
The utility model relates to an unmanned air vehicle technique field especially relates to an airborne control box and unmanned aerial vehicle.
Background
Currently, an image processor (such as an invida TX2 image processor) is integrated on the unmanned aerial vehicle, and the image processor can assist the unmanned aerial vehicle to realize functions of target identification, accurate landing and the like.
In the related art, the image processor is usually accommodated in an onboard control box, and the onboard control box is connected and fixed with the unmanned aerial vehicle. Disclose an unmanned aerial vehicle management and control platform's machine carries control box as in the earlier stage patent of application number CN201810812378.X, including casing and apron, it is fixed with unmanned aerial vehicle's organism through the casing, specifically, can refer to its attached 1, it has the curb plate to extend to both sides on the casing diapire, and the curb plate is on a parallel with the diapire to be equipped with the mounting hole on the curb plate, can realize fixing between casing and the unmanned aerial vehicle through mounting hole and cooperation bolt. However, there is no necessary vibration damping measure between the housing and the unmanned aerial vehicle, and when the unmanned aerial vehicle flies, the stability of the housing is poor, and the stability of the control components inside the housing is easily affected.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a: the utility model provides an airborne control box and unmanned aerial vehicle to lack necessary damping measure among the solution correlation technique between airborne control box and the unmanned aerial vehicle, airborne control box poor stability's problem.
In one aspect, the utility model provides an airborne control box, this airborne control box includes:
the box body is internally provided with an accommodating cavity with one open end, and the accommodating cavity is used for accommodating the control assembly;
the base, including the bottom plate with set up in a plurality of bottom plate all around are the slice and have elastic engaging lug, the bottom plate with the box body can be dismantled to be connected and will uncovered closed, the engaging lug with the bottom plate is connected, the engaging lug is used for being connected with unmanned aerial vehicle's organism, just the engaging lug can with the unsettled support of bottom plate in the organism.
As an optimal technical scheme of the airborne control box, the connection lug comprises a support sheet and an installation sheet, one end of the support sheet is connected with the bottom plate, the support sheet is obliquely arranged relative to the bottom plate, the installation sheet is connected with the other end of the support sheet, the installation sheet is used for being connected with the body, and the installation sheet is arranged parallel to the bottom plate.
As the preferable technical scheme of the airborne control box, the end face of the supporting sheet is provided with a through hole.
As the preferred technical scheme of the airborne control box, the box body comprises a box top plate and side walls arranged around the box top plate, and the side walls are provided with vent holes.
As a preferred technical solution of the onboard control box, the onboard control box further includes a film, the film is attached to the side wall, and the film closes the vent hole, and the film is configured to allow gas to pass through and can prevent water from passing through.
As the preferable technical scheme of the airborne control box, the box body is positioned above the base, the vent hole is provided with a first hole end communicated with the accommodating cavity and a second hole end communicated with the outside, and the first hole end is positioned above the second hole end.
As the preferred technical scheme of the airborne control box, the surface of the bottom plate, which is positioned on one side of the containing cavity, is provided with an annular positioning boss, the positioning boss is enclosed into a positioning groove, and a plurality of clamping hooks are arranged on the positioning groove at intervals.
As the preferred technical scheme of machine carries control box, machine carries control box is the cuboid form, be equipped with four engaging lugs on the bottom plate, the bottom plate includes two first sides on the width direction and two second sides on the length direction, each all be equipped with two on the first side the engaging lug, just two on the first side the engaging lug is located respectively first side length direction's both ends.
As the preferred technical scheme of machine carries the control box, machine carries the control box and still includes a plurality of screws, be equipped with a plurality of screw holes on the box body, be equipped with a plurality of unthreaded holes on the bottom plate, it is a plurality of unthreaded hole and a plurality of screw hole one-to-one sets up and with a plurality of the screw one-to-one sets up, the screw passes the correspondence unthreaded hole and with the correspondence screw hole threaded connection.
On the other hand, the utility model provides an unmanned aerial vehicle, the machine that includes in the above-mentioned arbitrary scheme carries control box.
The utility model has the advantages that:
the utility model provides a machine carries control box and unmanned aerial vehicle, this machine carries control box includes box body and base. Wherein, an accommodating cavity with one open end is arranged in the box body and is used for accommodating the control component; the base includes the bottom plate and sets up a plurality of flaky and elastic engaging lugs that are all around the bottom plate, and the bottom plate can be dismantled with the box body and be connected and will uncovered the closure, and the engaging lug is connected with the bottom plate, and the engaging lug is used for being connected with unmanned aerial vehicle's organism, and the engaging lug can be with the unsettled support of bottom plate in the organism. This machine carries control box, after the engaging lug is connected with unmanned aerial vehicle's organism, bottom plate and box body can be unsettled with unmanned aerial vehicle's organism, because the engaging lug has elasticity to when organism acceleration and deceleration or emergence vibration, the stability of box body internal control subassembly can be guaranteed to bottom plate and box body damping to the accessible engaging lug.
Drawings
Fig. 1 is a first schematic structural diagram of an onboard control box in an embodiment of the present invention;
fig. 2 is a schematic structural diagram ii of an onboard control box in an embodiment of the present invention;
FIG. 3 is a schematic structural diagram of a box body according to an embodiment of the present invention;
FIG. 4 is a cross-sectional view of the case according to an embodiment of the present invention;
fig. 5 is a schematic structural diagram of the base in the embodiment of the present invention.
In the figure:
1. a box body; 11. a cassette top plate; 12. side walls; 121. a vent hole; 1211. a first bore end; 1212. a second bore end; 123. a threaded hole; 13. an accommodating cavity;
2. a base; 21. connecting lugs; 211. mounting a sheet; 212. a support sheet; 2122. a through hole; 22. a base plate; 221. a light hole; 222. positioning the boss; 223. positioning a groove; 224. a hook;
3. and (4) screws.
Detailed Description
The technical solution of the present invention will be described clearly and completely with reference to the accompanying drawings, and obviously, the described embodiments are some, but not all embodiments of the present invention. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first," "second," and the like are used for descriptive purposes only and are not to be construed as indicating or implying relative importance. Where the terms "first position" and "second position" are two different positions, and where a first feature is "over", "above" and "on" a second feature, it is intended that the first feature is directly over and obliquely above the second feature, or simply means that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature includes the first feature being directly under and obliquely below the second feature, or simply meaning that the first feature is at a lesser elevation than the second feature.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are exemplary only for the purpose of explaining the present invention, and should not be construed as limiting the present invention.
As shown in fig. 1 to 5, the present embodiment provides an onboard control box, which includes a box body 1 and a base 2. Wherein, an accommodating cavity 13 with one open end is arranged in the box body 1, and the accommodating cavity 13 is used for accommodating the control assembly; base 2 includes bottom plate 22 and sets up a plurality of flaky and elastic engaging lug 21 that are all around in bottom plate 22, and bottom plate 22 can dismantle with box body 1 and be connected and with uncovered seal, and engaging lug 21 is connected with bottom plate 22, and engaging lug 21 is used for being connected with unmanned aerial vehicle's organism, and engaging lug 21 can be with bottom plate 22 unsettled support in the organism. The airborne control box that this embodiment provided, after engaging lug 21 is connected with unmanned aerial vehicle's organism, bottom plate 22 and box body 1 can be unsettled with unmanned aerial vehicle's organism, because engaging lug 21 has elasticity to when organism acceleration and deceleration or emergence vibration, accessible engaging lug 21 can guarantee the stability of 1 internal control of box body subassembly to bottom plate 22 and 1 damping of box body. Wherein, the control component can be a TX2 image processor and the like.
Optionally, referring to fig. 1, fig. 2 and fig. 5, the connecting lug 21 includes a supporting piece 212 and a mounting piece 211, one end of the supporting piece 212 is connected to the bottom plate 22, the supporting piece 212 is disposed obliquely with respect to the bottom plate 22, the mounting piece 211 is connected to the other end of the supporting piece 212, the mounting piece 211 is used for being connected to the body, and the mounting piece 211 is disposed parallel to the bottom plate 22. By having the support sheet 212 disposed obliquely to the base plate 22, the elastic properties of the support sheet 212 are optimized. As shown in fig. 5, in the present embodiment, the included angle between the supporting piece 212 and the bottom plate 22 is α, and α is preferably 120 °. Of course, in other embodiments, the angle between the support sheet 212 and the base plate 22 may be set as desired.
In this embodiment, the engaging lug 21 and the bottom plate 22 are made of metal, and specifically, the engaging lug 21 and the bottom plate 22 are made of aluminum alloy. It will be appreciated that the tab-like engaging lug 21, not only has a supporting function, but also has a certain elasticity. Preferably, the support piece 212 and the mounting piece 211 of the engaging lug 21 are integrally formed, and the engaging lug 21 and the bottom plate 22 are integrally formed.
Optionally, the supporting piece 212 is provided with a through hole 2122 on an end surface thereof, and by providing the through hole 2122, the supporting piece 212 will have a stronger elastic deformation capability to enhance the vibration damping effect on the base plate 22 and the case 1.
Referring to fig. 2 and 3, the airborne control box further includes a plurality of screws 3, a plurality of threaded holes 123 are disposed on the box body 1, a plurality of unthreaded holes 221 are disposed on the bottom plate 22, the unthreaded holes 221 and the threaded holes 123 are disposed in a one-to-one correspondence and are disposed in a one-to-one correspondence with the screws 3, and the screws 3 pass through the corresponding unthreaded holes 221 and are in threaded connection with the corresponding threaded holes 123.
Optionally, the box body 1 includes a box top plate 11 and a side wall 12 surrounding the box top plate 11, and the side wall 12 is provided with a vent hole 121. The control components in the accommodating cavity 13 can be dissipated through the vent holes 121. Preferably, the onboard control box further comprises a membrane (not shown in the drawings) attached to the side walls 12 and closing the vent holes 121, the membrane being configured to allow the passage of gas and to prevent the passage of water. In this embodiment, the membrane is a waterproof and breathable membrane, and is specifically made of e-PTFE material. So set up, can prevent that water, dust etc. from getting into in the box body 1, and do not influence ventilation cooling. In this embodiment, the screw hole 123 is provided on the end surface of the side wall 12.
Referring to fig. 4, in the present embodiment, the box body 1 is located above the base 2, the vent hole 121 has a first hole end 1211 communicated with the accommodating cavity 13 and a second hole end 1212 communicated with the outside, and the first hole end 1211 is located above the second hole end 1212. That is, the vent hole 121 is disposed obliquely with respect to the side wall 12 and obliquely downward in the inside-out direction of the accommodating chamber 13. With such an arrangement, water, dust and the like can be further prevented from entering the accommodating cavity 13, so as to protect the internal control assembly.
Optionally, referring to fig. 5, a ring-shaped positioning boss 222 is disposed on a surface of the bottom plate 22 on one side of the accommodating cavity 13, and a positioning groove 223 is defined by the positioning boss 222. The positioning slot 223 is used to position the control assembly. Preferably, the positioning groove 223 is provided with a plurality of hooks 224 at intervals. The hooks 224 are engaged with the slots disposed on the control module to further enhance the fixing effect of the control module.
In this embodiment, the airborne control box is the cuboid form, is equipped with four engaging lugs 21 on the bottom plate 22, and bottom plate 22 includes two first sides on the width direction and two second sides on the length direction, all is equipped with two engaging lugs 21 on each first side, and two engaging lugs 21 on the first side are located first side length direction's both ends respectively. It should be noted that the present embodiment is not limited to the specific number of the engaging lugs 21, and is not limited to the installation position thereof.
This embodiment still provides an unmanned aerial vehicle, includes the airborne control box in the above-mentioned scheme.
It is obvious that the above embodiments of the present invention are only examples for clearly illustrating the present invention, and are not intended to limit the embodiments of the present invention. Other variations and modifications will be apparent to persons skilled in the art in light of the above description. And are neither required nor exhaustive of all embodiments. Any modification, equivalent replacement, and improvement made within the spirit and principle of the present invention should be included in the protection scope of the claims of the present invention.

Claims (10)

1. An onboard control pod, comprising:
the box comprises a box body (1), wherein an accommodating cavity (13) with one open end is formed in the box body (1), and the accommodating cavity (13) is used for accommodating a control assembly;
base (2), including bottom plate (22) and set up in bottom plate (22) a plurality of all around are the slice and have elastic engaging lug (21), bottom plate (22) with box body (1) can be dismantled to be connected and will uncovered is sealed, engaging lug (21) with bottom plate (22) are connected, engaging lug (21) are used for being connected with unmanned aerial vehicle's organism, just engaging lug (21) can with bottom plate (22) unsettled support in the organism.
2. The onboard control box according to claim 1, wherein the connection lug (21) comprises a support piece (212) and a mounting piece (211), one end of the support piece (212) is connected with the bottom plate (22) and the support piece (212) is arranged obliquely relative to the bottom plate (22), the mounting piece (211) is connected with the other end of the support piece (212), the mounting piece (211) is used for being connected with the machine body, and the mounting piece (211) is arranged in parallel with the bottom plate (22).
3. The onboard control box according to claim 2, wherein the support piece (212) is provided with a through hole (2122) on an end surface thereof.
4. The onboard control box according to claim 1, wherein the box body (1) comprises a box top plate (11) and a side wall (12) surrounding the box top plate (11), and the side wall (12) is provided with a vent hole (121).
5. The onboard control box according to claim 4, further comprising a membrane attached to the side wall (12) and closing the vent (121), the membrane being configured to allow the passage of gas and to block the passage of water.
6. The onboard control box according to claim 4, characterized in that said box body (1) is located above said base (2), said vent hole (121) having a first hole end (1211) communicating with said housing chamber (13) and a second hole end (1212) communicating with the outside, said first hole end (1211) being located above said second hole end (1212).
7. The onboard control box according to claim 1, wherein the surface of the bottom plate (22) on one side of the accommodating cavity (13) is provided with an annular positioning boss (222), the positioning boss (222) is enclosed into a positioning groove (223), and the positioning groove (223) is provided with a plurality of hooks (224) at intervals.
8. The onboard control box according to any one of claims 1 to 7, wherein the onboard control box is rectangular, four engaging lugs (21) are provided on the bottom plate (22), the bottom plate (22) includes two first sides in a width direction and two second sides in a length direction, two engaging lugs (21) are provided on each first side, and the two engaging lugs (21) on the first side are respectively located at two ends of the first side in the length direction.
9. The onboard control box according to any one of claims 1 to 7, further comprising a plurality of screws (3), wherein a plurality of threaded holes (123) are formed in the box body (1), a plurality of unthreaded holes (221) are formed in the bottom plate (22), the plurality of unthreaded holes (221) and the plurality of threaded holes (123) are arranged in a one-to-one correspondence manner and the plurality of screws (3) are arranged in a one-to-one correspondence manner, and the screws (3) penetrate through the corresponding unthreaded holes (221) and are in threaded connection with the corresponding threaded holes (123).
10. An unmanned aerial vehicle comprising the onboard control box of any one of claims 1-9.
CN202020613614.8U 2020-04-22 2020-04-22 Airborne control box and unmanned aerial vehicle Active CN211702606U (en)

Priority Applications (1)

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CN202020613614.8U CN211702606U (en) 2020-04-22 2020-04-22 Airborne control box and unmanned aerial vehicle

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Application Number Priority Date Filing Date Title
CN202020613614.8U CN211702606U (en) 2020-04-22 2020-04-22 Airborne control box and unmanned aerial vehicle

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11788871B1 (en) * 2021-01-25 2023-10-17 Windrock, Inc. Heat resistant device base

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11788871B1 (en) * 2021-01-25 2023-10-17 Windrock, Inc. Heat resistant device base

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