CN207320294U - Unmanned vehicle aerial mounting structure - Google Patents
Unmanned vehicle aerial mounting structure Download PDFInfo
- Publication number
- CN207320294U CN207320294U CN201720917389.5U CN201720917389U CN207320294U CN 207320294 U CN207320294 U CN 207320294U CN 201720917389 U CN201720917389 U CN 201720917389U CN 207320294 U CN207320294 U CN 207320294U
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- Prior art keywords
- perforation
- casing
- unmanned vehicle
- switching interface
- vehicle aerial
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Abstract
The utility model proposes a kind of unmanned vehicle aerial mounting structure, including：Including：Casing, and external antenna structure；The casing is equipped with least partly covers the perforation with the perforation that can wear out structure, the structure of wearing out；The external antenna structure is worn out under structure is removed state described, and installation on the housing, and is connected with inside antenna connection structure.The unmanned vehicle aerial mounting structure of the utility model, can meet different demands.
Description
Technical field
It the utility model is related to unmanned vehicle technical field, more particularly to a kind of unmanned vehicle antenna installation knot
Structure.
Background technology
The application scenario of unmanned vehicle is very wide.In some scenarios, it is necessary to will after being taken photo by plane by unmanned vehicle
Image transmitting goes back to ground remote control end, in this case it is desirable to scheme to pass antenna etc. to realize that image is passed back；And in other occasions
In, user simultaneously need not scheme the function of passing, thus in this case, just need not scheme to pass antenna etc. on aircraft.User is according to need
Can select the unmanned vehicle of corresponding style, but at present, unmanned vehicle or be designed as equipped with figure pass antenna or
It is designed as not filling figure biography antenna, can not installs external antenna again in the casing for being designed as not installation diagram biography antenna, can not meet
Different demands.
Utility model content
Technical problem to be solved in the utility model is to provide a kind of unmanned vehicle aerial mounting structure, can meet
Different demands.
To solve the above problems, the utility model proposes a kind of unmanned vehicle aerial mounting structure, including：Casing, and
External antenna structure；The casing is equipped with least partly covers institute with the perforation that can wear out structure, the structure of wearing out
State perforation；The external antenna structure is worn out under structure is removed state described, installation on the housing, and with inside
Antenna attachment structure connects.
One embodiment according to the present utility model, the structure of wearing out is half disconnected structure or thin-wall construction.
One embodiment according to the present utility model, described half disconnected structure include a size be less than the perforation mounting and
The thin muscle of at least one connection mounting and perforated edge.
One embodiment according to the present utility model, the thin-wall construction including one be thinner than enclosure wall and with the perforation phase
Matched mounting.
One embodiment according to the present utility model, further includes adapter assembly, including the first switching interface and the second switching
Interface；First switching interface is connected with the inside antenna connection structure, and is arranged on the machine with corresponding to the perforation
The inner side of shell；Second switching interface is connected with the external antenna structure, and is arranged on the machine with corresponding to the perforation
The outside of shell；Second switching interface is docked at perforation with first switching interface and fixed on the housing.
One embodiment according to the present utility model, location structure, the corresponding perforation are provided with the inside of the casing
Set, to position first switching interface.
One embodiment according to the present utility model, first switching interface are the antennal interface connection with horn shape swivel nut
Device；The location structure includes at least setting the block reinforcement of the both sides of the perforation, and the angle of the first switching interface is set between block reinforcement
Shape swivel nut is rotated with limiting.
One embodiment according to the present utility model, the location structure further include the supporting rib of the corresponding block reinforcement of support, institute
It is vertical or connect the block reinforcement with being tilted a certain angle to state the relatively described block reinforcement of supporting rib.
One embodiment according to the present utility model, the casing include chassis body and upper cover；On the chassis body
The perforation is provided with, is further opened with being open on the chassis body；The upper cover is detachably connected on the chassis body
Opening.
One embodiment according to the present utility model, further includes a positioning antenna structure, is arranged in the casing.
One embodiment according to the present utility model, the unlimited shielding box in upside is additionally provided with the casing, to hold
Put the positioning antenna structure.
One embodiment according to the present utility model, the figure that the external antenna structure is passed for figure in antenna, with casing pass
Circuit board is electrically connected.
After adopting the above technical scheme, the utility model has the advantages that compared with prior art：
By opening up perforation on casing, the preformed hole position as the alternative installation of external antenna structure so that same
The unmanned vehicle of style can load onto external antenna structure when user needs antenna and can not install when not needed outer
Antenna structure is put, can meet different demands；And structure can be worn out by being set in the perforation of casing, then need not can install
Ensure the appearance consistency of casing during external antenna structure, and worn out when needing and installing external antenna structure and peace can be achieved
Dress；
When external antenna structure is installed, by the corresponding adapter assembly of outside setting in casing, external day had both been realized
The electric connection of cable architecture and inside antenna connection structure, and realize the fixation of external antenna structure；Pass through the of interior outside
One switching interface is docked with the second switching interface so that external antenna structure is installed on the site of perforation of casing, without in casing
Inside sets extra antenna installation position；
Set block reinforcement to block the horn shape stud of the first switching interface in perforation both sides, can prevent the first switching interface from existing
Rotate when the second switching interface connects, ensure to be connected firmly；Supporting rib vertically or tiltedly connects block reinforcement, can keep off
Muscle is played a supporting role on length direction, avoid block reinforcement the first switching interface rotatory force effect under be softened and
Laterally collapse.
Brief description of the drawings
Fig. 1 is that half disconnected structure of the unmanned vehicle aerial mounting structure of one embodiment of the utility model is not the worse for wear state
Under structure diagram；
Fig. 2 is the A partial enlargement structural representations of Fig. 1；
Fig. 3 is the structural representation of the installment state of the unmanned vehicle aerial mounting structure of one embodiment of the utility model
Figure；
Fig. 4 is that the detonation configuration of the installment state of the unmanned vehicle aerial mounting structure of one embodiment of the utility model shows
It is intended to；
Fig. 5 is the B partial enlargement structural representations of Fig. 4.
Description of symbols in figure：
1- casings, 11- perforation, 12- block reinforcements, 13- supporting ribs, half disconnected structures of 2-, 21- mountings, the thin muscle of 22-, the external days of 3-
Cable architecture, the first switching interfaces of 41-, the second switching interfaces of 42-, 43- nuts.
Embodiment
To enable the above-mentioned purpose of the utility model, feature and advantage more obvious understandable, below in conjunction with the accompanying drawings to this
The embodiment of utility model is described in detail.
Many details are elaborated in the following description in order to fully understand the utility model.But this practicality is new
Type can be much to implement different from other manner described here, and those skilled in the art can be new without prejudice to this practicality
Similar popularization is done in the case of type intension, therefore the utility model is from the limitation of following public specific implementation.
In one embodiment, can include referring to Fig. 1-5, unmanned vehicle aerial mounting structure：Casing 1, and it is external
Antenna structure.Certainly miscellaneous part or device can also be included on unmanned vehicle, can be set as needed.Casing is equipped with
Perforation, it is described；The external antenna structure is worn out under structure is removed state described, installation on the housing, and
It is connected with inside antenna connection structure.
Casing 1 is equipped with the perforation 11 that can wear out structure, and the size and size of the perforation 11 can pacify as needed
Depending on the connection structure for filling antenna structure.Structure can be worn out and at least partly cover perforation, perforation can also all be sealed.Scheming
In, perforate 11 shape it is rounded, size can allow connection structure to pass through.The position of perforation 11 is unlimited, as long as not influencing nobody
The work of aircraft miscellaneous part or device, such as shown in figure, perforation 11 is arranged on the afterbody position of casing 1.
By opening up perforation 11 on casing 1, the preformed hole position as the alternative installation of external antenna structure 3 so that
The unmanned vehicle of same style can load onto external antenna structure 3 when user needs antenna and when not needed can not
External antenna structure 3 is installed, can meet different demands；, then can be and structure can be worn out by being set in the perforation 11 of casing 1
Ensure the appearance consistency of casing 11 when external antenna structure 3 need not be installed, and worn when needing and installing external antenna structure 3
It is broken that installation can be achieved.
Structure can be worn out due to that can be removed, under the use state of installation external antenna structure 3, knot can be worn out
Structure is being destroyed or being completely taken off.Structure, which can be worn out, to be integrally formed manufacture in perforation 11 when casing 1 manufactures
At position, appearance consistency is kept with 1 outerplanar of casing.In figure, it illustrate only and a perforation 11 is set on casing 1, but not
Limited to this, when being likely to require installation two and above external antenna structure 3, can also be correspondingly arranged wearing for respective numbers
Hole 11, can set and can wear out structure in each perforation 11.
External antenna structure 3 by being installed on casing 1 the perforation 11 that structure is removed under state can be worn out, and with it is interior
Portion's antenna attachment structure connection.In other words, external antenna structure 3 can selectively be installed or do not resided on casing 1,
Install external antenna structure 3 when, can wear out structure be in be removed state.The connection structure of external antenna structure 3 can connect
11 position of perforation of casing 1 is fixed on, or can be goed deep into pass through perforation 11 to casing 1, is fastened on inside casing 1
In structure.
Inside antenna connection structure can be circuit, the circuit etc. for being electrically connected with external antenna structure 3, such as can
To be that the figure being directly electrically connected with the connection structure of external antenna structure 3 passes plate, or external antenna can be for connection to
The connection structure and figure of structure 3 pass the line construction of plate.
Certainly, inside antenna connection structure can be arranged in casing 1 always, regardless of whether installation external antenna structure 3,
And when needing installation, as long as the electric connection of inside antenna connection structure and external antenna structure 3 being realized, figure passes work(
Energy；Inside antenna connection structure can also be only arranged in casing 1 when needing and installing external antenna structure 3.
Optionally, structure can be worn out as half disconnected structure or thin-wall construction.Referring to Fig. 1 and Fig. 2, half disconnected structure 2, Ke Yili
Solution, is the structure being not exclusively connected in perforation 11, can be removed under external force, after half disconnected structure 2 removes, external day
The connection structure of cable architecture 3 can pass through perforation 11, realize the installation of external antenna structure 3.Thin-wall construction is due to its thin-walled
Property, it can equally be the worse for wear under external force, after thin-wall construction is worn out, the connection structure of external antenna structure can pass through
The installation of external antenna structure is realized in perforation.
In one embodiment, with continued reference to Fig. 1 and Fig. 2, half disconnected structure 2 can include a mounting 21 and at least one thin
Muscle 22.21 size of mounting is less than perforation 11, among perforation 11, can cover up the major part of perforation 11, but mounting
Also there are certain gap between 21 and 11 edges of perforation.Thin muscle 22 is connected between 11 edges of mounting 21 and perforation, by mounting
21 connect with 11 edges of perforation so that mounting 21 can be fixed in perforation 11, while sets thin muscle 22 can be with gap
Mounting 21 is enabled to easily fall off perforation.
Preferably, the quantity of thin muscle 22 be two, naturally it is also possible to be three or four etc., be disposed on mounting 21 with
Perforate between 11 edges, more preferably each thin muscle 22 is symmetrical arranged with respect to mounting 21.The thickness of thin muscle 22 can be thinner than mounting
21 or the thickness of 1 wall of casing.
Alternatively, thin-wall construction can include a mounting, which is thinner than enclosure wall and matches with perforation, will can perforate
Seal completely, but due to being thinner than enclosure wall, thus can be worn out easily.
In one embodiment, adapter assembly can also be included referring to Fig. 3-5, unmanned vehicle aerial mounting structure.Turn
Connected components include the first switching interface 41 and the second switching interface 42.First switching interface 41 connects with inside antenna connection structure
Connect, and 11 ground of corresponding perforation are arranged on the inner side of casing 1.Second switching interface 42 is connected with external antenna structure 3, and correspondence is worn
11 ground of hole is arranged on the outside of casing 1.Second switching interface 42 is docked with the first switching interface 41 and is fixed at perforation 11
On casing 1, both when the second switching interface 42 is docked with the first switching interface 41 while electrically conduct.
When external antenna structure 3 is installed, by the corresponding adapter assembly of outside setting in casing 1, both realized external
Antenna structure 3 and the electric connection of inside antenna connection structure, and realize the fixation of external antenna structure 3；Pass through interior outside
The first switching interface 41 docked with the second switching interface 42 so that external antenna structure 3 be installed on casing 1 perforation 11
Position, without setting extra antenna installation position inside casing 1.
Preferably, the inner side of casing 1 is provided with location structure, and corresponding perforation 11 is set, to position the first switching interface
41.Location structure is arranged near perforation 11, e.g. the both sides of perforation 110, can be used for positioning the first switching interface 41,
Prevent mobile etc. after movement or connection of first switching interface 41 in connection procedure.
Specifically, referring to Fig. 4 and Fig. 5, the first switching interface 41 can be the antenna interface connectors with horn shape swivel nut, when
So, the second switching interface 42 can be corresponding antenna interface connectors.Antenna interface connectors can be SMA (Sub-
Miniature-A, radio antenna interface) connector.Such as depicted, the first switching interface 41 and the second switching interface
42 be a pair of antenna interface connectors with hexagonal swivel nut, one of them is male connector, and one is female.It is of course also possible to it is band
There are the antenna interface connectors of corner swivel nut or hexagonal swivel nut etc..Location structure can include the both sides at least setting perforation 11
Block reinforcement 12, the horn shape swivel nut of the first switching interface 41 is set between block reinforcement 12, and horn shape swivel nut is blocked and can not rotated by block reinforcement 12, with
Limit the rotation of the first switching interface 41.
Preferably, two block reinforcements 12 can be symmetricly set on the both sides of perforation 11, and 12 shape of block reinforcement can be kept off according to it
Can be straight line muscle or horn shape muscle from the point of view of cross section depending on the shape at 41 position of the first switching interface.Block reinforcement 12 and first turn
41 corresponding position of connection interface fits closely, and avoids horn shape swivel nut from having the space of rotation.
Further, the supporting rib 13 of the corresponding block reinforcement 12 of support can also be included with continued reference to Fig. 4 and Fig. 5, location structure,
Supporting rib 13 is vertical with respect to block reinforcement 12 or connects block reinforcement 12 with being tilted a certain angle.Supporting rib 13 preferably connects 12 length side of block reinforcement
To close centre position or centre position.11 side of remote perforation of every block reinforcement 12 is all connected with a supporting rib 13.
Perforating, 11 both sides set block reinforcement 12 to block the horn shape stud of the first switching interface 41, can prevent the first switching
Interface 41 is to rotate during the connection of the second switching interface 42, ensures to be connected firmly；Supporting rib 13 vertically or tiltedly connects
Block reinforcement 12, can playing a supporting role on length direction in block reinforcement 12, avoid block reinforcement 12 in the first switching interface 41
Rotatory force effect under be softened and laterally collapse.
In figs. 3-5, there is external thread part, hexagonal swivel nut is located at below external thread part, this is outer on the first switching interface 41
Threaded portion stretches out in perforation 11, and hexagonal swivel nut is pushed against 11 positions of perforation and is limited by block reinforcement 12, and the second switching interface 42 has
Internal thread part, correspondence are connected on the external thread part of the first switching interface 41.Optionally, in the first switching interface 41 and second turn
One nut 43 can also be set between connection interface 42.Be spirally connected the external thread part of the first switching interface 41 by nut 43, first by
The residue that one switching interface 41 was fixed at perforation 11 and then was screwed to the second switching interface 42 first switching interface 41 is outer
Threaded portion.
In one embodiment, casing 1 can include chassis body and upper cover.Perforation 11 is set on chassis body, casing
It is further opened with being open in main body, perforation 11 can be arranged on chassis body on the position of opening.Can be so as to by the opening
In the connection of the first switching interface 41 and the second switching interface 42, repair and replacement of 1 internal part of casing etc. are also allowed for certainly.On
Lid is detachably connected on the opening of chassis body, ensures the integrality of casing 1, and opening upper cover can be by the first switching interface 41
Stretch out perforation 11 and position, then realize connection.
In one embodiment, positioning antenna structure is additionally provided with casing 1.It is, for example, GPS to position antenna structure
(Global Positioning System, global positioning system) antenna structure.
Further, the unlimited shielding box (not shown) in upside is additionally provided with casing 1, to accommodating positioning antenna
Structure, can be arranged on the tip position of casing 1.Positioning antenna structure is arranged in the unlimited shielding box in upside, unlimited upside
It can be used for the signal radiation for positioning antenna structure, and shielding box can prevent the signal of positioning antenna structure for external antenna
The interference of structure 3, plays the role of interference and insulation.
In one embodiment, external antenna structure 3 can be that the figure biography circuit board that figure is passed in antenna, with casing electrically connects
Connect.It can be 5.8GH omnidirectional antennas that figure, which passes antenna, and as shown in Figures 3 and 4, it is a mushroom antenna which, which passes antenna, mushroom antenna
Body portion can be twisted with stress, so as to adjust antenna direction.
Although the utility model is disclosed as above with preferred embodiment, it is not for limiting claim, Ren Heben
Field technology personnel without departing from the spirit and scope of the utility model, can make possible variation and modification, therefore
The scope of protection of the utility model should be subject to the scope that the utility model claims are defined.
Claims (12)
- A kind of 1. unmanned vehicle aerial mounting structure, it is characterised in that including：Casing, and external antenna structure；The casing It is equipped with and at least partly covers the perforation with the perforation that can wear out structure, the structure of wearing out；The external antenna knot Structure is worn out under structure is removed state described, and installation on the housing, and is connected with inside antenna connection structure.
- 2. unmanned vehicle aerial mounting structure as claimed in claim 1, it is characterised in that the structure of wearing out is broken for half Structure or thin-wall construction.
- 3. unmanned vehicle aerial mounting structure as claimed in claim 2, it is characterised in that the half disconnected structure includes a ruler The very little thin muscle that the mounting and perforated edge are connected less than the mounting of the perforation and at least one.
- 4. unmanned vehicle aerial mounting structure as claimed in claim 2, it is characterised in that it is thin that the thin-wall construction includes one In enclosure wall and with the mounting that matches of perforating.
- 5. unmanned vehicle aerial mounting structure as claimed in claim 1, it is characterised in that adapter assembly is further included, including First switching interface and the second switching interface；First switching interface is connected with the inside antenna connection structure, and corresponding The perforation it is arranged on the inner side of the casing；Second switching interface is connected with the external antenna structure, and corresponding The perforation it is arranged on the outside of the casing；Second switching interface is docked with first switching interface at perforation And fix on the housing.
- 6. unmanned vehicle aerial mounting structure as claimed in claim 5, it is characterised in that be provided with the inside of the casing Location structure, the corresponding perforation is set, to position first switching interface.
- 7. unmanned vehicle aerial mounting structure as claimed in claim 6, it is characterised in that first switching interface is band The antenna interface connectors of horn shape swivel nut；The location structure include at least set the perforation both sides block reinforcement, block reinforcement it Between the horn shape swivel nut of the first switching interface be set rotated with limiting.
- 8. unmanned vehicle aerial mounting structure as claimed in claim 7, it is characterised in that the location structure further includes branch The supporting rib of the corresponding block reinforcement of support, the relatively described block reinforcement of the supporting rib is vertical or connects the block reinforcement with being tilted a certain angle.
- 9. unmanned vehicle aerial mounting structure as claimed in claim 1, it is characterised in that the casing includes chassis body And upper cover；The perforation is provided with the chassis body, is further opened with being open on the chassis body；The upper cover is detachable It is connected to the opening of the chassis body.
- 10. unmanned vehicle aerial mounting structure as claimed in claim 1, it is characterised in that further include a positioning antenna knot Structure, is arranged in the casing.
- 11. unmanned vehicle aerial mounting structure as claimed in claim 10, it is characterised in that be additionally provided with the casing The shielding box that upside is opened wide, to house the positioning antenna structure.
- 12. unmanned vehicle aerial mounting structure as claimed in claim 1, it is characterised in that the external antenna structure is The figure that figure is passed in antenna, with casing passes circuit board and is electrically connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720917389.5U CN207320294U (en) | 2017-07-26 | 2017-07-26 | Unmanned vehicle aerial mounting structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720917389.5U CN207320294U (en) | 2017-07-26 | 2017-07-26 | Unmanned vehicle aerial mounting structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207320294U true CN207320294U (en) | 2018-05-04 |
Family
ID=62433897
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720917389.5U Active CN207320294U (en) | 2017-07-26 | 2017-07-26 | Unmanned vehicle aerial mounting structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207320294U (en) |
-
2017
- 2017-07-26 CN CN201720917389.5U patent/CN207320294U/en active Active
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