CN205998129U - For the aerial device thrown in - Google Patents
For the aerial device thrown in Download PDFInfo
- Publication number
- CN205998129U CN205998129U CN201621022901.1U CN201621022901U CN205998129U CN 205998129 U CN205998129 U CN 205998129U CN 201621022901 U CN201621022901 U CN 201621022901U CN 205998129 U CN205998129 U CN 205998129U
- Authority
- CN
- China
- Prior art keywords
- housing
- thrown
- fixed
- cover body
- thing
- 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.)
- Expired - Fee Related
Links
Landscapes
- Pivots And Pivotal Connections (AREA)
Abstract
The utility model discloses a kind of be applied to unmanned plane for the aerial device thrown in, the described device for aerial input includes：Body, described body is fixed on described unmanned plane, and described body includes：Memory area；First housing；Second housing, described first housing and described second housing are flexibly connected, and the two can relatively rotate, and the clearance space between described first housing and described second housing constitutes described memory area；Actuator, described actuator is flexibly connected with described second housing；Wherein, described second housing, by being rotated with respect to described first housing, makes described second shell body phase open for described first housing or close, and is thrown in or storage with will be stored in thing to be thrown described in described memory area.This utility model achieve can not be affected by adverse circumstances or aerial barrage thing institute and cause damage, have the characteristics that structure is simple, security performance is high and applicable performance is wide.
Description
Technical field
This utility model belongs to technical field of aerospace, particularly to a kind of for the aerial device thrown in.
Background technology
In prior art, generally pass through unmanned plane and needs are thrown in certain ad-hoc location (as marine site, mountain area, forest etc.)
The goods and materials put are thrown in, and then play emergencing action.
However, due to the characteristic of unmanned plane itself, being all often directly to be fixed on no thing to be thrown loading when throwing thing
Thing to be thrown directly is carried out throwing in when running aerial by man-machine bottom.But this kind of mode makes thing to be thrown completely exposed
In the air, cause to damage so that running in the presence of a harsh environment or in the air and easily treating throwing thing during barrier.
Utility model content
Technical problem to be solved in the utility model is how to guarantee that thing to be thrown is not subject to adverse circumstances during transporting
Or aerial barrage thing is affected and causes to damage.
For solving above-mentioned technical problem, this utility model provides a kind of device for aerial input, is applied to unmanned
Machine, the described device for aerial input includes：Body, described body is fixed on described unmanned plane, and described body includes：
Memory area, for storing thing to be thrown；First housing；Second housing, described first housing and described second housing are flexibly connected,
And the two can relatively rotate, the clearance space between described first housing and described second housing constitutes described memory area；Drive
Moving part, described actuator is flexibly connected with described second housing, drives described second shell body phase for institute to obtain control signal
State the first housing to be rotated；Wherein, described second housing, by being rotated with respect to described first housing, makes described second
Housing is opened with respect to described first housing or is closed, with will be stored in thing to be thrown described in described memory area throw in or
Storage.
Optionally, the quantity of described body is n, and the n parallel bottom being fixed on described unmanned plane of described body；
The quantity of described actuator is corresponding with the quantity of described body, and each described actuator accordingly with a described body
In described second housing be flexibly connected；Wherein, described n is more than or equal to 2, and each described actuator obtains independently respectively
Control signal, accordingly controls the described second shell body phase in a described body to enter for accordingly described first housing
Row rotation.
Optionally, also include：Positioning element, described positioning element is fixed on described first housing, to wait to throw to described
The placement position of thing is positioned.
Optionally, also include：Camera head, described camera head is fixed on described first housing, to wait to throw to described
The placement position of thing carries out real-time photography.
Optionally, described positioning element is laser designator；And/or, described camera head is video camera.
Optionally, also include：Connecting seat, described connecting seat is fixed on the bottom of described unmanned plane；2 described bodies are parallel
Be fixed on described connecting seat.
Optionally, also include：Positioning element, described positioning element is fixed on described connecting seat, with to described thing to be thrown
Placement position positioned.
Optionally, also include：Camera head, described camera head is fixed on described connecting seat, with to described thing to be thrown
Placement position carry out real-time photography.
Optionally, described positioning element is laser designator；And/or, described camera head is video camera.
Optionally, described second housing includes：Drive end and synchronous end, described drive end and described synchronous end are symmetrically divided
It is distributed in the two ends of described second housing；Described body also includes：Bearing assembly；First cover body, described first cover body is fixed on institute
State on drive end, and described actuator is fixed in described first cover body；Second cover body, described second cover body is fixed on described same
On step end, and described bearing assembly is fixed in described second cover body；Wherein, described actuator is in described first cover body and institute
State drive end to be flexibly connected, described bearing assembly is flexibly connected with described synchronous end in described second cover body, and described bearing
Assembly is in described second cover body and the synchronous axial system of described synchronous end.
Beneficial effect：
This utility model provides a kind of device for aerial input, is applied to unmanned plane, by being fixed on body
On unmanned plane, and at this, the first housing that can first rotate against and the second housing are set in vivo, by the first housing and second shell
Clearance space between body constitutes a memory area, for storing thing to be thrown.Pass through second shell body phase for the first housing simultaneously
Rotated so that second shell body phase may be at opening or closing two states for the first housing, that is, when open, treated
Throw thing to be launched, upon closing, then thing to be thrown is stored in this memory area.So allow for thing to be thrown to exist by unmanned plane
Aerial transport during, because thing to be thrown is disposed between in memory area, in acting on of the first housing and the second housing
Be isolated with free surrounding space, with this ensure that thing to be thrown transport during be not subject to extraneous adverse circumstances (as thunderstorm weather) or
Aerial barrage thing is affected and causes to damage, and has the characteristics that structure is simple, security performance is high.
Brief description
In order to be illustrated more clearly that this utility model embodiment or technical scheme of the prior art, below will be to embodiment
In required use accompanying drawing be briefly described it should be apparent that, drawings in the following description are only of the present utility model
Some embodiments, for those of ordinary skill in the art, on the premise of not paying creative work, can also be according to this
A little accompanying drawings obtain other accompanying drawings.
The overall structure diagram for the aerial device thrown in that Fig. 1 provides for this utility model embodiment；
The upward view for the aerial device thrown in that Fig. 2 provides for this utility model embodiment；
The top view for the aerial device thrown in that Fig. 3 provides for this utility model embodiment；
The side view for the aerial device thrown in that Fig. 4 provides for this utility model embodiment；
The overall structure exploded perspective view one for the aerial device thrown in that Fig. 5 provides for this utility model embodiment；
The overall structure exploded perspective view two for the aerial device thrown in that Fig. 6 provides for this utility model embodiment.
Specific embodiment
This utility model provides a kind of device for aerial input, is applied to unmanned plane, by being fixed on body
On unmanned plane, and at this, the first housing that can first rotate against and the second housing are set in vivo, by the first housing and second shell
Clearance space between body constitutes a memory area, for storing thing to be thrown.Pass through second shell body phase for the first housing simultaneously
Rotated so that second shell body phase may be at opening or closing two states for the first housing, that is, when open, treated
Throw thing to be launched, upon closing, then thing to be thrown is stored in this memory area.So allow for thing to be thrown to exist by unmanned plane
Aerial transport during, because thing to be thrown is disposed between in memory area, in acting on of the first housing and the second housing
Be isolated with free surrounding space, with this ensure that thing to be thrown transport during be not subject to extraneous adverse circumstances (as thunderstorm weather) or
Aerial barrage thing is affected and causes to damage, and has the characteristics that structure is simple, security performance is high.
Below in conjunction with the accompanying drawing in this utility model embodiment, the technical scheme in this utility model embodiment is carried out
Clearly and completely description is it is clear that described embodiment is only a part of embodiment of this utility model rather than whole
Embodiment.Based on the embodiment in this utility model, the every other embodiment that those of ordinary skill in the art are obtained, all belong to
Scope in this utility model protection；Wherein involved in this enforcement "and/or" key word, represent and or two kinds of situations, change
Sentence is talked about, A and/or B mentioned by this utility model embodiment illustrates A and B, two kinds of situations of A or B, describe A and B and deposited
Three kinds of states, such as A and/or B, represent：Only include A and do not include B；Only include B and do not include A；Including A and B.
Meanwhile, in this utility model embodiment, when assembly is referred to as " being fixed on " another assembly, it can be directly another
On one assembly or can also there is assembly placed in the middle.When an assembly is considered as " connection " another assembly, it can be
It is directly connected to another assembly or may be simultaneously present assembly placed in the middle.When assembly be considered as " being arranged at " another
Assembly, it can be to be set directly on another assembly or may be simultaneously present assembly placed in the middle.This utility model embodiment
Used in term " vertical ", " level ", "left", "right" and similar statement be merely for purposes of illustration, not
It is intended to limit this utility model.
Refer to Fig. 1-4, a kind of device for aerial input that this utility model embodiment provides, it is applied to unmanned
Machine, the described device for aerial input at least can include：Body 1, actuator 14, positioning element 3 and camera head 4.
Wherein, described body 1 includes：For storing the memory area 13 of thing to be thrown, the first housing 11, the second housing 12.
Described first housing 11 is fixed on the bottom of described unmanned plane, and described first housing 11 and described second housing 12 activity are even
Connect, and the two can relatively rotate, the clearance space between described first housing 11 and described second housing 12 constitutes described storage
Region 13.Described actuator 14 is flexibly connected with described second housing 12, drives described second housing 12 to obtain control signal
Rotated with respect to described first housing 11.
It will be understood by those skilled in the art that the loading body of described body 1 thing as to be thrown, it is installed in the machine of unmanned plane
Body bottom.Certainly, how body 1 is arranged on the fuselage of unmanned plane, this utility model does not limit to, can be by one
Fixing device is fixed on the fuselage of unmanned plane or by the detachable machine being fixed on unmanned plane of a Quick-dismantle component
With, directly can also pass through screw or bolt it is fixed on the fuselage of unmanned plane threadably, then all
It is applied to this utility model.Likewise, for body 1 installation position on the fuselage of unmanned plane, this utility model is not yet
Limitation, can be fixed on the fuselage of unmanned plane according to the spatial distribution position of practical function demand unmanned aerial vehicle body bottom
Bottom middle part, the latter's sidepiece, or anterior, or rear portion etc., may also apply to this utility model.
Further, described second housing 12 in this utility model embodiment passes through to enter with respect to described first housing 11
Row rotation, makes described second housing 12 open with respect to described first housing 11 or close, will be stored in described memory block
Thing to be thrown described in domain 13 is thrown in or is stored.
Specifically, the first housing 12 in described body 1, can be a shell structure in semi-circular cylindrical, permissible
It is not understood as a hollow cylindrical tube Yan Qi center vertical pivot being switched to two halves, wherein half is the first described housing 11, another
Half is described second housing 12.Certainly, unlike this utility model embodiment, the inside radius of described first housing 11 is more than
The inside radius of described second housing 12, thus so that the lateral surface of described second housing 12 can closely be fitted in institute
The medial surface stating the first housing 11 is rotated.To realize described second housing 12 with this to open with respect to described first housing 11
Or close.That is, when described second housing 12 is opened with respect to described first housing 11, then now described second housing 12
The medial surface of lateral surface and described first housing 11 is (can be understood as overlapping) bonded to each other, memory area 13
It is opened, thing to be thrown is launched.When described second housing 12 is closed with respect to described first housing 11, then now described second
The medial surface of the lateral surface of housing 12 and described first housing 11 is (can be understood as misaligned) being separated from each other, now
Described memory area 13 is constituted by the clearance space between described second housing 12 and described first housing 11, that is, thing quilt to be thrown
It is stored in described memory area 13.
Thus it is effectively guaranteed, when unmanned plane flight in the air, by described second housing 12 and described first shell
Body 11 constitutes a protective cover, is stored in memory area 13 by temporary for thing to be thrown, so that described thing to be thrown and free surrounding space phase
Isolation, so prevent the external world adverse circumstances such as thunderstorm weather or aerial barrage thing treat throwing thing because contact or collide and
Cause to damage.
It should be noted that the first above-mentioned housing 11, the definition of the second housing 12, it is not to the first housing 11, second
The essence of the number order of housing 12 limits, and in this utility model embodiment, the first housing 11, the second housing 12 are only to shell
Body makes a distinction used.In other words, when the second housing 12 is fixed on unmanned plane, and the inside radius of the second housing 12 is more than the
The inside radius of one housing 11, makes the second housing 12 be rotated with respect to the first housing 11, to realize described first shell then
Body 11 is opened with respect to described second housing 12 or is closed, and is also applied for this utility model.
Below, this utility model embodiment will continue to be more than the inside radius of the second housing 12 with the inside radius of the first housing 11
As a example, this utility model is expanded on further.
In this utility model embodiment, in order to, in launch process, standard be carried out in default position to missile
True input, what this utility model embodiment was provided also includes a positioning element 2, described positioning for the aerial device thrown in
Part 2 can be fixed on described first housing 11, is positioned with the placement position to described thing to be thrown.And positioning element 2
There is the laser designator of instruction positioning function.Certainly, in order to observe impression information to be put in real time, and collection is thrown
Put the geographical location information on ground, this utility model embodiment is additionally provided with camera head 3, described camera head 3 is fixed on institute
State on the first housing 11, real-time photography is carried out with the placement position to described thing to be thrown.
It is noted that involved actuator 14 in this utility model embodiment, positioning element 2 and camera head 3,
All can be connected with the flight control system within unmanned plane or earth station or remote terminal and carry out information transmission, with by flying
Row control system or earth station or remote terminal send driving instruction to described actuator 14, then pass through described actuator
14 described second housings 12 of driving are rotated with respect to described first housing 11.
Further, Fig. 5-6 are referred to, for described second housing 12, described second housing 12 can include：
Drive end 121 and synchronous end 122.Described drive end 121 and described synchronous end 122 are symmetrically distributed in described second housing 12
Two ends.It is also understood that described drive end 121 and described synchronous end 122 are the two ends of described second housing 12.Institute simultaneously
State body 1 also to include：Bearing assembly 15, the first cover body 16 and the second cover body 17.Wherein, described in described first cover body 16 is fixed on
On drive end 121, and described actuator 14 is fixed in described first cover body 16.Described second cover body 17 is fixed on described synchronization
On end 122, and described bearing assembly 15 is fixed in described second cover body 17.
Specifically, described actuator 14 is flexibly connected with described drive end 121 in described first cover body 16, to receive
Drive signal drives described drive end 122 to be rotated, and simultaneously drives end 121 to make second shell as one end of the second housing 12
Body 12 is overall to synchronize rotation therewith.Described bearing assembly 15 is movable with described synchronous end 122 in described second cover body 17
Connect, and described bearing assembly 15 described second cover body 17 in described synchronous end 122 synchronous axial system.
Further, described first cover body 16 is in hemispherical configuration so that the circular open and first of the first cover body 16
The semicircle opening of housing 11 and the second housing 12 matches.Described first cover body 16 includes one first circular open ends 161, and
It is fixed on described drive end 121 by described first circular open ends 161.Here, the first cover body 16 is in hemispherical configuration, can
To be interpreted as the first cover body 16 by its tail end, internal diameter is gradually reduced with drive end 121 connecting portion, that is, described first is circular
Opening 161 is a maximum circular port of diameter in described hemispherical configuration.Likewise, described second cover body 17 is in hemisphere
Shape structure is so that the circular open of the second cover body 17 is also matched with the semicircle opening of the first housing 11 and the second housing 12.
Described second cover body 17 includes one second circular open ends 171, and is fixed on described same by described second circular open ends 171
On step end 122.Here, the second cover body 17 be in hemispherical configuration it can be understood as the second cover body 17 by with synchronous end 122 connecting portion
It is gradually reduced to its tail end, internal diameter at position, that is, described second circular open ends 171 are that in described hemispherical configuration, diameter is maximum
One circular port.
Need exist for especially it is emphasized that why described first cover body 16 and described second cover body 17 are designed to hemisphere
Shape structure, so that the lateral surface of described first cover body 16 and described second cover body 17 (can be understood as unmanned plane during flying process
In for the aerial device thrown in windward side) as windward side when, the resistance of wind is along described first cover body 16 and/or described
The spherical surface of the second cover body 17 is slowed down, so maximized reduce that this utility model embodiment provides throw for aerial
The resistance that the device put is received in running in the air.It is also possible to make to work as run into bad weather circumstances such as thunderstorm
During weather, the rainwater that lands on described first cover body 16 and/or described second cover body 17, can be along described first cover body 16
And/or the spherical surface of described second cover body 17 is dirty, it is to avoid hydrops.
For actuator 15, described in this utility model embodiment, actuator 15 can include：Steering wheel 141 and rudder
Machine disk 142.Wherein, described steering wheel 141 is fixed in described first cover body 16.Described steering wheel disk 142 is fixed on described drive end
On 121, and it is flexibly connected with described steering wheel 141, so that control instruction is obtained by described steering wheel 141, drive described steering wheel disk 142
Described drive end 121 is driven to be rotated.Carried out therewith with the second housing 12 entirety that rotarily drives that this to realize drive end 121
Rotation, realizes described second housing 12 and opens with respect to described first housing 11 or close.That is, control when steering wheel 141 obtains
Instruction, drives described steering wheel disk 142 to drive described drive end 121 (the second housing 12) to open with respect to described first housing 11
When, then now the medial surface of the lateral surface of described second housing 12 and described first housing 11 is bonded to each other (being appreciated that
It is to overlap), memory area 13 is opened, and thing to be thrown is launched.When steering wheel 141 obtains control instruction, drive described
When steering wheel disk 142 drives described drive end 121 (the second housing 12) to close with respect to described first housing 11, then now described
The medial surface of the lateral surface of two housings 12 and described first housing 11 is (can be understood as misaligned) being separated from each other, this
When described memory area 13 is constituted by the clearance space between described second housing 12 and described first housing 11, that is, thing to be thrown
It is stored in described memory area 13.
In addition, in this utility model embodiment, further referring to Fig. 5-6, described actuator 14 can also include：The
One terminal pad 143 and the second terminal pad 18.Wherein, described first terminal pad 143 and described first circular open ends 161 are mutually blocked
Connect, and described drive end 121 is fixed in described first terminal pad 143, one end of described first housing 11 is with described first even
Flange 143 phase clamping.
Specifically, by described first terminal pad 143 and the phase clamping of described first circular open ends 161, and described drive
Moved end 121 is fixed in described first terminal pad 143, and this allows for when steering wheel 141 drives steering wheel disk 142 to be rotated, rotation
Steering wheel disk 142 in turning drives described drive end 121 to synchronize rotation, and due to drive end 121 and described first terminal pad
It is fixedly connected between 143, and then make described first terminal pad 143 also synchronous axial system.By described first terminal pad 143 and institute
State the first circular open ends 161, one end phase clamping of described first housing 11, therefore described first terminal pad 143 was rotating
Cheng Zhong, you can realize described first circular open ends 161 (the first cover body 16) and described first housing 11 with respect in rotation
First terminal pad remains static.
For the snap fit between described first terminal pad 143 and described first circular open ends 161, described first company
Snap fit between one end of flange 143 and described first housing 11, can be in described first circular open ends 161
Side opens up the annulus chute of a depression, opens up the boss of a projection in the edge of described first terminal pad 143, and by being somebody's turn to do
Boss is connected in the annulus chute of the first circular open ends 161 inner side, with this be implemented in described first terminal pad 143 with described
Clamping between first circular open ends 161, and make described first terminal pad 143 can be with respect to described first circular open ends
161 are rotated.Likewise, for the snap fit between one end of described first terminal pad 143 and described first housing 11,
Can also be to open up an annulus chute at the edge side surface of the first terminal pad 143, now can be by described first terminal pad 143
On the boss that opens up be interpreted as in described first terminal pad 143 diametric(al), the annulus that described first terminal pad 143 opens up
In the card of described first terminal pad 143, the plane that the two is located is mutually perpendicular to chute.The one of described first housing 11 simultaneously
End offers the boss of a projection, and is connected at the edge side surface of described first terminal pad 143 by this boss and is opened up
In annulus chute, the clamping between described first terminal pad 143 and described first housing 11 is realized with this, and makes described first
Terminal pad 143 can be rotated with respect to described first housing.
Certainly, for described first terminal pad 143 can with respect to described first housing 11, described first cover body 16 can relatively
Rotate, that is, during the first terminal pad 143 rotation, described first housing 11, described first cover body 16 transfixion.Also deposit
In other designs, above-mentioned described first terminal pad 143 of this utility model embodiment and described first circular open ends
Phase clamping between 161, one end phase clamping of described first terminal pad 143 and described first housing 11 are only one kind of wherein realization
Mode, not limits to.
For example, it is also possible to be respectively with described first by one end of described first terminal pad 143 and described first housing 11
The first circular open ends 161 phase clamping of cover body 16, that is, in the edge of described first circular open ends 161, near side
The medial surface of edge position, opens up the annulus chute of depression respectively, starts a coupling in the edge of the first terminal pad 143 simultaneously
Boss, also open up the boss of a coupling in the edge of one end of the first housing 11, and then respectively by the first terminal pad 143
Edge boss be connected to the first circular open ends 161 in the annulus chute of edge medial surface, and by
The boss of one end of one housing 11 is connected in the annulus chute of the first circular open ends 161 edge, also be can achieve with this
Described first terminal pad 143 can be able to relatively rotate with respect to described first housing 11, described first cover body 16, that is, in the first connection
During disk 143 rotation, described first housing 11, described first cover body 16 transfixion, may also apply to this utility model.
You need to add is that, described first terminal pad 143 is located between described steering wheel disk 142 and described drive end 121, institute
State steering wheel disk 142 to be fixedly connected with described first terminal pad 143, to drive described steering wheel disk successively by described steering wheel 141
142nd, described first terminal pad 143 drives described drive end 121 to be rotated.Described steering wheel disk 142 and described first terminal pad
Being fixedly connected between 143 can be mode connects for screw or bolt connection, and this utility model does not limit, as long as can
So that being fixedly connected of synchronous axial system can occur therebetween, then all within protection domain of the present utility model.
Corresponding with the first terminal pad 143, what this utility model embodiment provided also includes for the aerial device thrown in：
Second terminal pad 18, described second terminal pad 18 and the phase clamping of described second circular open ends 171, and described synchronous end 122 is solid
In described second terminal pad 18, the other end of described second housing 12 and the phase clamping of described second terminal pad 18；Described axle
Bearing assembly 15 is flexibly connected with described synchronous end 122 by described second terminal pad 18 in described second cover body 17.
Identical, described second terminal pad 18 and the phase clamping of described second circular open ends 171, and described synchronous end 121
It is fixed in described second terminal pad 18, this allows for when steering wheel 141 drives steering wheel disk 142 to be rotated, the rudder in rotation
Machine disk 142 drives described drive end 121 (the second housing 12) to synchronize rotation, and due to synchronous end 122 with described second even
It is fixedly connected between flange 18, and then make described second terminal pad 18 also synchronous axial system.Due to described second terminal pad 18 with
Described second circular open ends 171, the other end phase clamping of described first housing 11, therefore described second terminal pad 18 is rotating
During, you can realize described second circular open ends 171 (the second cover body 17) and described first housing 11 with respect in rotation
The second terminal pad 18 remain static.
For the snap fit between described second terminal pad 18 and described second circular open ends 171, described second company
Snap fit between the other end of flange 18 and described first housing 11, can be in described second circular open ends 171
Inner side opens up the annulus chute of a depression, opens up the boss of a projection in the edge of described second terminal pad 18, and passes through
This boss is connected in the annulus chute of the second circular open ends 171 inner side, is implemented in described second terminal pad 18 and institute with this
State the clamping between the second circular open ends 171, and make described second terminal pad 18 can be with respect to described second circular open
End 171 is rotated.Likewise, for the clamping side between the other end of described second terminal pad 18 and described first housing 11
Formula or open up an annulus chute at the edge side surface of the second terminal pad 18, now can be by described second terminal pad
The boss opening up on 18 is interpreted as in described second terminal pad 18 diametric(al), the annulus that described second terminal pad 18 opens up
In the card of described second terminal pad 18, the plane that the two is located is mutually perpendicular to chute.Described first housing 11 is another simultaneously
One end also offers the boss of a projection, and is connected at the edge side surface of described second terminal pad 18 by this boss and is opened
If in annulus chute, the clamping between described second terminal pad 18 and described first housing 11 is realized with this, and make described
Two terminal pads 18 can be rotated with respect to described first housing 11.
Certainly, for described second terminal pad 18 can with respect to described first housing 11, described second cover body 17 can relatively
Rotate, that is, during the second terminal pad 18 rotation, described first housing 11, described first cover body 17 transfixion.Also deposit
In other designs, above-mentioned described second terminal pad 18 of this utility model embodiment and described second circular open ends
Between 171, phase clamping, described second terminal pad 18 and the other end phase clamping of described first housing 11 are only the one of wherein realization
The mode of kind, not limits to.
For example, it is also possible to be respectively with described second by the other end of described second terminal pad 18 and described first housing 11
The second circular open ends 171 phase clamping of cover body 17, that is, in the edge of described second circular open ends 171, near side
The medial surface of edge position, opens up the annulus chute of depression respectively, starts a coupling in the edge of the second terminal pad 18 simultaneously
Boss, also open up the boss of a coupling in the edge of the other end of the first housing 11, and then respectively by the second terminal pad
18 edge boss is connected to the second circular open ends 171 in the annulus chute of edge medial surface, and will
The boss of the other end of the first housing 11 is connected in the annulus chute of the second circular open ends 171 edge, also may be used with this
Realize described second terminal pad 18 can to relatively rotate with respect to described first housing 11, described second cover body 17, that is, second
During terminal pad 18 rotation, described first housing 11, described second cover body 17 transfixion, may also apply to this practicality new
Type.
By above-mentioned first terminal pad 143 and the second terminal pad 18 it is achieved that described second housing 12 and described first shell
The connected mode rotating against between body 11, that is, achieve described second housing 12 and can be at respect to described first housing 11
The state opened or close.Certainly, in order to mitigate main screw lift, because the first terminal pad 143 will be with the card of steering wheel disk 142
It is flexibly connected, therefore solid structure is used for the first terminal pad 143, and for the second terminal pad 18, due to
It does not need to be connected with the card of steering wheel disk 142, therefore the structure of " hollow body " can be adopted to set for the second terminal pad 18 as far as possible
Meter, to mitigate automatically, such as：Second terminal pad includes：Cross type frame 181, support disk 182 are framework 183.Cross type frame
181 are used for connecting described support disk 182 and described framework 183 as support frame so that described support disk 182 is fixed
In described framework 183, replace the solid structure of the first terminal pad 143 with this by the structure of cross type frame 181, reach
Mitigate the technique effect of deadweight.Bearing assembly 15 is fixed on described support disk 182, and as this utility model embodiment
A kind of embodiment, described bearing assembly 15 can include a bearing 151 and a ring flange 152.Wherein, described bearing 151 He
Described ring flange 152 bearing at described support disk 182 connects.For described bearing 151, described ring flange 152 and described
The bearing supporting disk 182 connects, and to realize the relatively rotating to be prior art of the second terminal pad 18, here is omitted.
It is noted that arranging described bearing assembly 15 in this utility model embodiment, be so that described bearing assembly 15 with
Described actuator 14 constitutes the balance fulcrum of a pair of rotation at the two ends of described second housing 12, only exists actuator to avoid working as
During 14 this pivot point, the second housing 12 is caused to rotate jiggly technological deficiency.
Finally it is emphasized that a kind of embodiment of this utility model embodiment described above, the nothing each meaning
Man-machine fuselage bottom secures a body 1, but the quantity this utility model for body 1 does not limit.Namely at this
In utility model, the quantity of described body 1 is can be with n, and n described body 1 can be parallel is fixed on described unmanned plane
Bottom.Meanwhile, the quantity of described actuator 14 is corresponding with the quantity of described body 1, and each described actuator 14 is right
Should be flexibly connected with described second housing 12 in a described body 1 on ground；Wherein, described n is more than or equal to 2, and each institute
State actuator 14 and obtain independently controlled signal respectively, accordingly control described second housing 12 phase in a described body 1
Accordingly described first housing 11 is rotated.
For example, with continued reference to of the present utility model a kind of embodiment during Fig. 1-4, as n=2, now for the ease of
Connect 2 or multiple body 1 (being illustrated below), this utility model can also include a connecting seat 4 taking n=2 as a example.
And 2 parallel being fixed on described connecting seat 4 of described body 1.
Specifically, described connecting seat can include：Pedestal 41, the first lid 42 and the second lid 43.
Wherein, described pedestal 41 includes：First side, second side, the 3rd side and the 4th side；And described first side
Face, described second side, described 3rd side and described 4th side are surrounded and are formed an internal described pedestal in hollow-core construction
41；Described first side and described second side are two opposites, and described 3rd side and described 4th side are right for two
Facade；2 described bodies 1 are symmetrically fixed on described 3rd side and described 4th side.Described first lid 42 covers
In described first side, and described connecting seat 4 is fixedly connected with the bottom of described unmanned plane by described first lid 42；Institute
State the second lid 43 to cover in described second side, and the first projection window 431 and are offered on described second lid 43
Two projection windows 432.Described positioning element 2 is fixed at described first projection window 431, and described camera head 3 is fixed on institute
State at the second projection window 432.Identical, described positioning element 2 can be laser designator；Described camera head 3 can be
Video camera.
It should be noted last that, above specific embodiment is only in order to illustrate the technical solution of the utility model rather than limit
System, although being described in detail to this utility model with reference to example, it will be understood by those within the art that, can be right
The technical solution of the utility model is modified or equivalent, the spirit without deviating from technical solutions of the utility model and model
Enclose, it all should be covered in the middle of right of the present utility model.
Claims (10)
1. a kind of for the aerial device thrown in, be applied to unmanned plane it is characterised in that described for the aerial device bag thrown in
Include：
Body, described body is fixed on described unmanned plane, and described body includes：
Memory area, for storing thing to be thrown；
First housing；
Second housing, described first housing and described second housing are flexibly connected, and the two can relatively rotate, described first housing
Clearance space and described second housing between constitutes described memory area；
Actuator, described actuator is flexibly connected with described second housing, drives described second shell body phase to obtain control signal
Described first housing is rotated；
Wherein, described second housing, by being rotated with respect to described first housing, makes described second shell body phase for described
First housing is opened or is closed, and is thrown in or storage with will be stored in thing to be thrown described in described memory area.
2. as claimed in claim 1 be used for the aerial device thrown in it is characterised in that：
The quantity of described body is n, and the n parallel bottom being fixed on described unmanned plane of described body；
The quantity of described actuator is corresponding with the quantity of described body, and each described actuator accordingly with described in one
Described second housing in body is flexibly connected；
Wherein, described n is more than or equal to 2, and each described actuator obtains independently controlled signal respectively, accordingly controls one
Described second shell body phase in individual described body rotates for accordingly described first housing.
3. the device being used for aerial input as claimed in claim 1 is it is characterised in that also include：
Positioning element, described positioning element is fixed on described first housing, and it is fixed to be carried out with the placement position to described thing to be thrown
Position.
4. the device being used for aerial input as claimed in claim 3 is it is characterised in that also include：
Camera head, described camera head is fixed on described first housing, carries out reality with the placement position to described thing to be thrown
When shooting.
5. as claimed in claim 4 be used for the aerial device thrown in it is characterised in that：
Described positioning element is laser designator；
And/or,
Described camera head is video camera.
6. the device being used for aerial input as claimed in claim 2 is it is characterised in that also include：
Connecting seat, described connecting seat is fixed on the bottom of described unmanned plane；
2 parallel being fixed on described connecting seat of described body.
7. the device being used for aerial input as claimed in claim 6 is it is characterised in that also include：
Positioning element, described positioning element is fixed on described connecting seat, is positioned with the placement position to described thing to be thrown.
8. the device being used for aerial input as claimed in claim 7 is it is characterised in that also include：
Camera head, described camera head is fixed on described connecting seat, is carried out in real time with the placement position to described thing to be thrown
Shooting.
9. as claimed in claim 8 be used for the aerial device thrown in it is characterised in that：
Described positioning element is laser designator；
And/or,
Described camera head is video camera.
10. as described in any one of claim 3-9 for the aerial device thrown in it is characterised in that：
Described second housing includes：Drive end and synchronous end, described drive end and described synchronous end are symmetrically distributed in described the
The two ends of two housings；
Described body also includes：
Bearing assembly；
First cover body, described first cover body is fixed on described drive end, and described actuator is fixed in described first cover body；
Second cover body, described second cover body is fixed on described synchronous end, and described bearing assembly is fixed on described second cover body
Interior；
Wherein, described actuator is flexibly connected with described drive end in described first cover body, and described bearing assembly is described
It is flexibly connected with described synchronous end in two cover bodies, and described bearing assembly synchronously turns with described synchronous end in described second cover body
Dynamic.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621022901.1U CN205998129U (en) | 2016-08-31 | 2016-08-31 | For the aerial device thrown in |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621022901.1U CN205998129U (en) | 2016-08-31 | 2016-08-31 | For the aerial device thrown in |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205998129U true CN205998129U (en) | 2017-03-08 |
Family
ID=58192853
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621022901.1U Expired - Fee Related CN205998129U (en) | 2016-08-31 | 2016-08-31 | For the aerial device thrown in |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205998129U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106672237A (en) * | 2016-08-31 | 2017-05-17 | 易瓦特科技股份公司 | Device used for airdrop |
-
2016
- 2016-08-31 CN CN201621022901.1U patent/CN205998129U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106672237A (en) * | 2016-08-31 | 2017-05-17 | 易瓦特科技股份公司 | Device used for airdrop |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US9561849B2 (en) | Vehicle configuration with motors that rotate between a lifting position and a thrusting position | |
| CN206050090U (en) | Based Intelligent Control photoelectric nacelle | |
| CN105966599B (en) | A kind of aircraft | |
| CN210391577U (en) | Small-size two optical nacelle of triaxial | |
| CN205998131U (en) | There is the unmanned plane of many bodies Aerial Delivery Equipment | |
| CN108216593A (en) | Undercarriage and the unmanned vehicle with this undercarriage | |
| CN205998129U (en) | For the aerial device thrown in | |
| CN205998130U (en) | The aerial delivery device of double bodies | |
| CN106143938B (en) | A kind of thunderstorm weather electric power Drones for surveillance's bus stop | |
| CN106394904B (en) | Unmanned plane for launching in the air | |
| RU180861U1 (en) | Land vehicle equipped with a module for storing and automatically launching a UAV | |
| CN107933896A (en) | Assemble efficiently aircraft landing gear easy to carry | |
| CN204418461U (en) | Nested type astronomical ball top, three-in-one many skylights curtain | |
| CN102829783B (en) | Frame shafting support system for three-shaft inertially stabilized platform | |
| CN106240818B (en) | Unmanned plane grabs object device | |
| CN105508829A (en) | Two-shaft four-frame photoelectric platform inner frame mechanism | |
| CN205931259U (en) | Unmanned aerial vehicle grabs thing device | |
| CN106347665A (en) | Aerial multi-body putting device | |
| CN106672238B (en) | The aerial delivery device of double ontologies | |
| CN106275437B (en) | More ontology delivery devices applied to unmanned plane | |
| CN106672237A (en) | Device used for airdrop | |
| CN106275438A (en) | There is the unmanned plane of many bodies Aerial Delivery Equipment | |
| CN105035324B (en) | Coaxial two wheels robot is jettisoninged cabin | |
| CN207985218U (en) | A kind of plant protection drone motor mount | |
| CN205998158U (en) | It is applied to the arrangement for deflecting of photoelectric nacelle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170308 Termination date: 20210831 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |