CN106394916A - Device for rotating collection - Google Patents
Device for rotating collection Download PDFInfo
- Publication number
- CN106394916A CN106394916A CN201610789275.7A CN201610789275A CN106394916A CN 106394916 A CN106394916 A CN 106394916A CN 201610789275 A CN201610789275 A CN 201610789275A CN 106394916 A CN106394916 A CN 106394916A
- Authority
- CN
- China
- Prior art keywords
- lateral part
- cover body
- fixed
- medial
- inner housing
- 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.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- G—PHYSICS
- G03—PHOTOGRAPHY; CINEMATOGRAPHY; ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ELECTROGRAPHY; HOLOGRAPHY
- G03B—APPARATUS OR ARRANGEMENTS FOR TAKING PHOTOGRAPHS OR FOR PROJECTING OR VIEWING THEM; APPARATUS OR ARRANGEMENTS EMPLOYING ANALOGOUS TECHNIQUES USING WAVES OTHER THAN OPTICAL WAVES; ACCESSORIES THEREFOR
- G03B17/00—Details of cameras or camera bodies; Accessories therefor
- G03B17/56—Accessories
- G03B17/561—Support related camera accessories
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
Abstract
The invention discloses a device for rotating collection, and belongs to the technical field of unmanned aerial vehicles. The device for rotating collection comprises a rotating body, a first drive piece, a first deflection assembly and a first magnetic induction encoder. The rotating body is rotationally fixed to outside loading equipment, and a photographic device is fixed in the rotating body. The first drive piece is fixed to the rotating body and movably connected with the photographic device. The first deflection assembly is rotationally fixed between the loading equipment and the rotating body. The first magnetic induction encoder is fixed to the first drive piece and connected with an outside flight control system so as to detect the rotating angle of the first drive piece. The device for rotating collection is assembled on the outside loading equipment (such as an aircraft), multi-angle collection of image and video information in the horizontal direction and the vertical direction is achieved on the premise of not influencing the flight state and the flight efficiency of the aircraft, and the device has the beneficial effects of being simple in structure and wide in applicability.
Description
Technical field
The invention belongs to technical field of aerospace, particularly to a kind of device for carrying out rotating acquisition.
Background technology
In prior art, charging appliance is varied, and such as the airborne vehicle for flight is one of charging appliance, boat
Pocket (English:Aircraft), refer to that the relative motion by fuselage and air (is not anti-work ground being occurred by air
With) and obtain the machine of air force lift-off flight.Including dirigible, aircraft, aerodone, gyroplane, helicopter, flapping-wing aircraft, incline
Switch rotor machine etc..
Airborne vehicle in flight course, because job requirements generally require to carry out Real-time Collection to the relevant information in way,
As image on the way, video information etc..Therefore generally it is fixed with a head in its fuselage bottom, however, head itself is usually
" static " operation, can only be directed at a direction and carry out information gathering, and often lead to when needing and other angles being acquired
The flight attitude crossing adjustment airborne vehicle completes information gathering action, and this kind of acquisition mode with airborne vehicle as regulating object is excessively numerous
Trivial, and the flight attitude of airborne vehicle is carried out with real-time adjustment also easily the impact state of flight of airborne vehicle and flight efficiency.
Content of the invention
The technical problem to be solved is how to provide and realize the rotatable dress for carrying out rotating acquisition
Put, be automatically performed the multi-angle collection of image, video information on the premise of the operational efficiency not affecting charging appliance.
For solving above-mentioned technical problem, the invention provides a kind of device for carrying out rotating acquisition, described be used for into
The device of row rotating acquisition includes：Rotating mass, described rotating mass are rotationally fixed on extraneous charging appliance, and described rotation
Turn and be fixed with one in main body for carrying out the camera head of information gathering, by described rotating mass with respect to described charging appliance
Rotated in the horizontal direction, to drive described camera head to carry out Real-time Collection to the visual information in horizontal direction；The
One actuator, described first actuator is fixed in described rotating mass, and is flexibly connected with described camera head, and described
One actuator obtains control signal and drives described camera head to carry out turning vertical direction relative to described rotating mass first
Dynamic, so that Real-time Collection is carried out to the visual information on the first vertical direction；Wherein, described rotating mass set with respect to described loading
Standby rotation in the horizontal direction, and described camera head with respect to described rotating mass the rotation phase on the first vertical direction
Mutually independent.
Optionally, the described device for carrying out rotating acquisition also includes：First yoke assembly, described first yoke assembly
It is rotationally fixed between described charging appliance and described rotating mass, and described rotating mass pass through described first yoke assembly
Rotated in the horizontal direction with respect to described charging appliance.
Optionally, described rotating mass include：Shell body, described shell body is fixed on institute by described first yoke assembly
State on charging appliance；Inner housing, described inner housing is set in the inside of described shell body, and is flexibly connected with described shell body,
And described inner housing is rotatable with respect to described shell body, described camera head is fixed on described inner housing；First combination cover
Body, described first combination cover body envelope is in the outside of described shell body, and is fixedly connected with described shell body, and described first drive
Moving part is fixed in described first combination cover body；Second combination cover body, described second combination cover body envelope is in described inner housing
Outside, and be fixedly connected with described inner housing.
Optionally, described shell body is in chondritic, and inside is in hollow-core construction, to place described inner housing；And it is described
Shell body includes：First lateral part；Second lateral part, described second lateral part and described first lateral part opposition are distributed in described
The both sides of shell body；3rd lateral part；4th lateral part, described 4th lateral part and described 3rd lateral part opposition are distributed in institute
State the both sides of shell body；5th lateral part；6th lateral part, described 6th lateral part and described 5th lateral part opposition are distributed in
The both sides of described shell body；Wherein, described first lateral part, described second lateral part, described 3rd lateral part, outside the described 4th
Sidepiece, described 5th lateral part and described 6th lateral part surround and form the internal described shell body in hollow-core construction, and described
3rd outside left between described first lateral part and described second lateral part, and respectively with described first lateral part and described
Second lateral part is adjacent；Described shell body is rotationally fixed on described first yoke assembly by described 3rd lateral part；Institute
State the 4th lateral part, described 5th lateral part and described 6th lateral part all in hatch frame, and the inside of described shell body is empty
Between communicated with the external world by described 4th lateral part, described 5th lateral part and/or described 6th lateral part；Described first combination
Cover body is individually fixed on described first lateral part and described second lateral part.
Optionally, described inner housing is in chondritic, and inside is in hollow-core construction, to place described camera head；And institute
State inner housing to include：First medial part；Second medial part, described second medial part and described first medial part opposition are distributed in institute
State the both sides of inner housing；3rd medial part；4th medial part, described 4th medial part and described 3rd medial part opposition are distributed in
The both sides of described inner housing；5th medial part；6th medial part, described 6th medial part and described 5th medial part opposition distribution
Both sides in described inner housing；Wherein, described first medial part, described second medial part, described 3rd medial part, the described 4th
Medial part, described 5th medial part and described 6th medial part surround and form the internal described inner housing in hollow-core construction, and institute
State the 3rd inside line between described first medial part and described second medial part, and respectively with described first medial part and institute
State the second medial part adjacent；Described inner housing passes through described first medial part and described second medial part and described shell body activity
Connect, and described first medial part and described first lateral part fit, described second medial part and described second lateral part phase
Laminating, described 3rd medial part and described 3rd lateral part fit, and described 4th inside line is in described 4th lateral part
Hatch frame position；Described 5th medial part and described 6th medial part are all in hatch frame, and described second combination cover body
Correspondence is fixed on described 5th medial part and described 6th medial part.
Optionally, described first combination cover body includes：First cover body, described first cover body is fixed on described first lateral part
On, and described first actuator is fixed in described first cover body, and described first actuator pass through described first lateral part with
Described first medial part is flexibly connected；Second cover body, described second cover body is fixed on described second lateral part；And bearing group
Part, described bearing assembly is fixed in described second cover body, and described bearing assembly passes through described second lateral part and described the
Two private sides are fixedly connected, so that described second private side can relatively rotate with respect to described second lateral part.
Optionally, state the second combination cover body to include：3rd cover body, described 3rd cover body is fixed on described 5th medial surface
On, and one first projection window is offered on described 3rd cover body, so that described camera head passes through described first projection window
Mouth is communicated with the extraneous visual field；4th cover body, described 4th cover body is fixed on described 6th medial surface.
Optionally, described second lateral part includes：Support frame；Support disk, described support frame is symmetrically fixed on
At the peripheral edge position of described support disk, and described bearing assembly is fixed on described support disk.
Optionally, also include：Limiting component, described limiting component is fixed on described bearing assembly, and with described bearing
Component synchronization rotates；And be provided with position stop piece on described support frame, described limiting component contact with described position stop piece or point
From being carried out spacing with the rotation to described bearing assembly.
Optionally, described position stop piece is screw, and described screw is fixed on described support frame；Described limiting component is
One swingle, described swingle includes positioning end and turning end, and described positioning end is fixed on described bearing assembly, described rotation
End is rotated with respect to described positioning end, to be contacted with described screw or to separate.
Optionally, described 3rd cover body includes one the 3rd opening, and is fixed on described by described 3rd opening
On five medial surface, and described 3rd opening is provided with the groove of a ring-type, and the edge of described 5th medial part is provided with
In the projection of one ring-type, and the described groove of described raised insertion.
Beneficial effect：
The invention provides a kind of device for carrying out rotating acquisition, and by the device being used for carrying out rotating acquisition
Rotating mass are rotationally fixed on extraneous charging appliance, and are fixed with one in rotating mass for carrying out information gathering simultaneously
Camera head, so allows for being rotated in the horizontal direction with respect to described charging appliance by rotating mass, to drive
Camera head carries out Real-time Collection to the visual information in horizontal direction；On the other hand rotation master is fixed on by the first actuator
On body, and it is flexibly connected with this camera head, drive camera head perpendicular first to obtain control signal by the first actuator
Nogata is rotated with respect to rotating mass upwards, to carry out Real-time Collection to the visual information on the first vertical direction.Finally
Regulating object is used as by the device for carrying out rotating acquisition, on the premise of the operational efficiency not affecting charging appliance automatically
Complete the multi-angle collection of image, video information, have the characteristics that structure is simple, the suitability is wide.
Brief description
In order to be illustrated more clearly that the embodiment of the present invention or technical scheme of the prior art, below will be to institute in embodiment
Need use accompanying drawing be briefly described it should be apparent that, drawings in the following description be only the present invention some enforcement
Example, for those of ordinary skill in the art, on the premise of not paying creative work, can also obtain according to these accompanying drawings
Obtain other accompanying drawings.
Fig. 1 is the overall structure diagram one of the device for carrying out rotating acquisition provided in an embodiment of the present invention；
Fig. 2 is the side view of Fig. 1；
Fig. 3 is the overall structure diagram two of the device for carrying out rotating acquisition provided in an embodiment of the present invention；
Fig. 4 is the overall structure diagram three of the device for carrying out rotating acquisition provided in an embodiment of the present invention；
Fig. 5 is the side view of Fig. 4；
Fig. 6 is the explosive view of Fig. 1；
Fig. 7 is the explosive view of Fig. 3；
Fig. 8 is the explosive view of Fig. 4；
Fig. 9 is the structural representation of shell body；
Figure 10 is the structural representation of inner housing；
Figure 11 is annexation schematic diagram in the device for carrying out rotating acquisition for the limiting component；
Figure 12 is the annexation schematic diagram of the first lateral surface and the first opening.
Specific embodiment
The invention provides a kind of device for carrying out rotating acquisition, and by the device being used for carrying out rotating acquisition
Rotating mass are rotationally fixed on extraneous charging appliance, and are fixed with one in rotating mass for carrying out information gathering simultaneously
Camera head, so allows for being rotated in the horizontal direction with respect to described charging appliance by rotating mass, to drive
Camera head carries out Real-time Collection to the visual information in horizontal direction；On the other hand rotation master is fixed on by the first actuator
On body, and it is flexibly connected with this camera head, drive camera head perpendicular first to obtain control signal by the first actuator
Nogata is rotated with respect to rotating mass upwards, to carry out Real-time Collection to the visual information on the first vertical direction.Finally
Regulating object is used as by the device for carrying out rotating acquisition, on the premise of the operational efficiency not affecting charging appliance automatically
Complete the multi-angle collection of image, video information, have the characteristics that structure is simple, the suitability is wide.
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Site preparation description is it is clear that described embodiment is only a part of embodiment of the present invention, rather than whole embodiments.It is based on
Embodiment in the present invention, the every other embodiment that those of ordinary skill in the art are obtained, broadly fall into present invention protection
Scope；Wherein involved in this enforcement "and/or" key word, represent and or two kinds of situations, in other words, the present invention implement
A and/or B mentioned by example, illustrates A and B, two kinds of situations of A or B, describes A and three kinds of states existing for B, such as A and/or
B, represents：Only include A and do not include B；Only include B and do not include A；Including A and B.
Meanwhile, in the embodiment of the present invention, when assembly is referred to as " being fixed on " another assembly, it can be directly at another
On assembly or can also there is assembly placed in the middle.When an assembly is considered as " connection " another assembly, it can be direct
It is connected to another assembly or may be simultaneously present assembly placed in the middle.When an assembly is considered as " being arranged at " another group
Part, it can be to be set directly on another assembly or may be simultaneously present assembly placed in the middle.Made in the embodiment of the present invention
Term " vertical ", " level ", "left", "right" and similar statement are merely for purposes of illustration, and are not intended to
Limit the present invention.
The device for carrying out rotating acquisition in order to provide to invention elaborates, to be solved to support to invent
Technical problem, below, in the embodiment that the present invention provides, first the loading of the device being mounted with for carrying out rotating acquisition is set
The overall structure of standby () elaborates taking airborne vehicle as a example, then during narration charging appliance (airborne vehicle), enters one
Step targetedly draws the device provided by the present invention for carrying out rotating acquisition, to reach mesh that is complete, clear, understanding
's.
Refer to Fig. 1-5, embodiments provide a kind of airborne vehicle, including：Fuselage, for carrying out rotating acquisition
Device.
Wherein, the described device for carrying out rotating acquisition is rotationally fixed to described fuselage.To be used for by adjustment
Carry out rotating acquisition device deflection angle come to realize for carry out rotating acquisition device in flight course water on the way
Square upwards with vertical direction on image/video information.
For the device for carrying out rotating acquisition, the described device for carrying out rotating acquisition can include：Rotation
Turn main body 1 and the first actuator 2.And described rotating mass 1 are rotationally fixed on described fuselage, and described rotating mass
It is fixed with one for carrying out the camera head 3 of information gathering, by described rotating mass 1 with respect to described fuselage in level in 1
Rotated on direction, to drive described camera head 3 to carry out Real-time Collection to the visual information in horizontal direction.Meanwhile, institute
State the first actuator 2 to be fixed in described rotating mass 1, and be flexibly connected with described camera head 3, and described first actuator
2 acquisition control signals drive described camera head 3 to be rotated vertical direction relative to described rotating mass 1 first, with
Real-time Collection is carried out to the visual information on the first vertical direction.
Wherein, described first actuator 2 can be the first motor including stator and rotor, and by rotor and shooting dress
Put 3 rotations to connect, the first motor is connected the control letter that acquisition control system is exported with the flight control system of aircraft interior
Number, rotated with the rotor driving described first motor, and then the rotor in rotation is driven camera head 3 in the first vertical side
Rotated upwards, realized the camera angle of adjustment camera head 3.Here the first vertical direction is appreciated that with respect to water
The vertical direction (that is, perpendicular to the direction of level ground) of plane earth.It is noted that described rotating mass 1 are with respect to institute
State fuselage rotation in the horizontal direction, and described camera head 4 with respect to described rotating mass 1 on the first vertical direction
Rotate separate, i.e. rotation therebetween is independent of each other so that camera head 4 to the information gathering in horizontal direction and
Mutually contradictory to the information gathering on the first vertical direction.
Further, the described device for carrying out rotating acquisition also includes：First yoke assembly 5.Described first deflection
Assembly 5 is rotationally fixed between described fuselage and described rotating mass 1, and described rotating mass 1 deflect by described first
Assembly 5 is rotated in the horizontal direction with respect to described fuselage.Here the first yoke assembly 5 can be understood as right
Described rotating mass 1 enter the drive component of horizontal deflection in the horizontal direction, and it is fixed on fuselage, by this first yoke assembly
5, drive described rotating mass 1 to enter horizontal deflection in the horizontal direction, regarded with the image obtaining any deflection angle in horizontal direction
Frequency information.How first yoke assembly 5 is fixed on fuselage, the embodiment of the present invention is not limited to, can be directly to pass through
Screw is threadedly connected on fuselage, also can be fixed in the bottom of fuselage by a fixing device, as long as being capable of
First yoke assembly 5 is relatively fixed with fuselage, then be all applied to the present invention.
For rotating mass 1, described rotating mass 1 can include：Shell body 12, inner housing 11, first combination cover
Body 13 and the second combination cover body 14.Wherein, described shell body 12 is fixed on described fuselage by described first yoke assembly 5；
Described inner housing 11 is set in the inside of described shell body 12, and is flexibly connected with described shell body 12, and described inner housing 11
Rotatable with respect to described shell body 12, described camera head 3 is fixed on described inner housing 11.Described first combination cover body 13
Envelope is in the outside of described shell body 12, and is fixedly connected with described shell body 12, and described first actuator 2 be fixed on described
In first combination cover body 13.Described second combination cover body 14 envelope in the outside of described inner housing 11, and with described inner housing 11
It is fixedly connected.
It should be noted that " interior ", " outward " in shell body 12 in the embodiment of the present invention, inner housing 11, and first group
Close " first ", " second " in cover body 13 and the second combination cover body 14, and involved elsewhere in the embodiment of the present invention
" first ", " second ", is only to discriminate between used, not feature is substantially limited, be first explained here.
In embodiments of the present invention, please continue to refer to Fig. 6-7, described shell body 12 can be in chondritic, and inside is in
Hollow-core construction, to place described inner housing 11.Described inner housing 11 is also in chondritic, and inside is in hollow-core construction, to place
Described camera head 3.Certainly, chondritic here is relative, is not necessarily referring to completely whole spheroid, described shell body 12 He
Described inner housing 11 is the part spherical structure cutting from whole spheroid.But by described shell body 12, described inner housing 11, institute
State the first combination cover body 13 and the overall rotating mass 1 being constituted of described second combination cover body 14, be then a whole sphere structure.
Specifically, described shell body 12 includes：First lateral part 121, the second lateral part 122, the 3rd lateral part 123,
4th lateral part 124, the 5th lateral part 125, the 6th lateral part 126.
Wherein, as shown in figs. 9-10, the first lateral part 121 can be understood as the left side of described shell body 12, outside second
Sidepiece 122 is appreciated that the right side of described shell body 12, and the 3rd lateral part 123 is appreciated that the upper of described shell body 12
Side, the 4th lateral part 124 is appreciated that the downside of described shell body 12, and the 5th lateral part 125 is appreciated that described shell
The front side of body 12, the 6th lateral part 126 is appreciated that the rear side of described shell body 12.And described second lateral part 122 and institute
State the both sides that the first lateral part 121 opposition is distributed in described shell body 12；Described 4th lateral part 124 and described 3rd lateral part
123 opposition are distributed in the both sides of described shell body 12.Described 6th lateral part 126 and the opposition distribution of described 5th lateral part 125
Both sides in described shell body 12.
With this pass through described first lateral part 121, described second lateral part 122, described 3rd lateral part 123, described the
It is internal described in hollow-core construction that four lateral parts 124, described 5th lateral part 125 and described 6th lateral part 126 surround formation
Shell body 12, and described 3rd lateral part 123 is located between described first lateral part 121 and described second lateral part 122, and point
Not adjacent with described first lateral part 121 and described second lateral part 122；Described shell body 12 passes through described 3rd lateral part
123 are rotationally fixed on described first yoke assembly 5；Described 4th lateral part 124, described 5th lateral part 125 and described
6th lateral part 126 is all in hatch frame, and described 4th lateral part 124, described is passed through in the inner space of described shell body 12
5th lateral part 125 and/or described 6th lateral part 126 are communicated with the external world；Described first combination cover body 12 is individually fixed in institute
State on the first lateral part 121 and described second lateral part 122.
Likewise, described inner housing 11 may include：First medial part 111, the second medial part 112, the 3rd medial part 113,
4th medial part 114, the 5th medial part 115, the 6th medial part 116.
Wherein, the first medial part 111 can be understood as the left side of described inner housing 11, and the second medial part 112 can be managed
Solution is the right side of described inner housing 11, and the 3rd medial part 113 is appreciated that the upside of described inner housing 11, the 4th medial part
114 downsides being appreciated that described inner housing 11, the 5th medial part 115 is appreciated that the front side of described inner housing 11, the
Six medial parts 116 are appreciated that the rear side of described inner housing 11.And described second medial part 112 and described first medial part
111 opposition are distributed in the both sides of described inner housing 11；Described 4th medial part 114 and the opposition distribution of described 3rd medial part 113
Both sides in described inner housing 12.Described 6th medial part 116 and described 5th medial part 115 opposition are distributed in described inner housing
11 both sides.And described second medial part 112 and described first medial part 111 opposition are distributed in the both sides of described inner housing 11.
Described 4th medial part 114 and described 3rd medial part 113 oppose and are distributed in the both sides of described inner housing 11.Inside described 6th
Portion 116 and described 5th medial part 115 oppose and are distributed in the both sides of described inner housing 11.
With this pass through described first medial part 111, described second medial part 112, described 3rd medial part 113, described the
It is internal described in hollow-core construction that four medial parts 114, described 5th medial part 115 and described 6th medial part 116 surround formation
Inner housing 11, and described 3rd medial part 113 is located between described first medial part 111 and described second medial part 112, and point
Not adjacent with described first medial part 111 and described second medial part 112.Described inner housing 11 passes through described first medial part
111 and described second medial part 112 be flexibly connected with described shell body 12, and outside described first medial part 111 and described first
Sidepiece 121 fits, and described second medial part 112 and described second lateral part 121 fit, described 3rd medial part 113 He
Described 3rd lateral part 123 fits, and described 4th medial part 114 is located at the hatch frame position of described 4th lateral part 124
Place；Described 5th medial part 115 and described 6th medial part 116 are all in hatch frame, and described second combination cover body 14 is corresponding
It is fixed on described 5th medial part 115 and described 6th medial part 116.
For the described first combination cover body 13, include for described first combination cover body 13：First cover body 131,
Two cover bodies 132 and bearing assembly 133.
Wherein, described first cover body 13 is fixed on the first lateral part 121 of described shell body 12, and described first driving
Part 2 is fixed in described first cover body 13, so that described first actuator 2 passes through described first lateral part 121 interior with described
First medial part 111 of housing 11 is flexibly connected.Described second cover body 14 is fixed on the second lateral part 121 of described shell body 12
On.Described bearing assembly 133 is fixed in described second cover body 14, and described bearing assembly 133 passes through described shell body 12
Second lateral part 121 is fixedly connected with described second private side 112 of described inner housing 11, so that described second private side 112
Can relatively rotate with respect to the second lateral part 122 of described shell body 12.
It should be noted that the first actuator 2 is fixed on an airtight sky by the first cover body 13 by the embodiment of the present invention
Interior, it is damaged with preventing the first actuator 2 to be exposed in external environment (as rainwash, entrance of dust etc.),
Lead to the first actuator 2 cannot normal work.Meanwhile, be provided with bearing assembly 133 at the second lateral part 122 here so as to
Equalizing feature as the first actuator 2 driving force is it can be understood as work as the first actuator 2 in the first lateral part 121 drives
When housing 11 drives camera head 3 to be rotated, if now do not had with the second lateral part 122 of the first lateral part 121 opposition
There is the rotary part balancing each other therewith, then easily go out in rotary course because whole inner housing 11 only exists a pivot point
Now rock, unsteady technological deficiency, therefore the embodiment of the present invention pass through arrange bearing assembly 133 for the first actuator 2
Another corresponding pivot point is supported to the rotation of inner housing 11, allows it to smoothly drive camera head to enter
Row rotation.
Here described bearing assembly 133 can include：Bearing 1331 and ring flange 1332.Wherein, described ring flange
1332 are fixed on described second lateral part 122, and described bearing 1331 and described ring flange 1332 bearing connect.Need explanation
, described bearing 1331 and described ring flange 1332 bearing are connected to constitute an axle that can carry out referring now to rotation
How bearing assembly 133, to be prior art, carries out bearing connection and how to carry out rotating no longer repeating herein for it, and
For bearing assembly 133 being applied to the present invention so as to constitute, with the first actuator 2, two rotations that described inner housing 11 opposes
Fulcrum, to reach the technique effect that described inner housing 11 smoothly drives described camera head 3 to be rotated, is that the present invention is implemented
The innovation of example is located, and first offers some clarification herein.
For the described second combination cover body 14, described second combination cover body 14 can include：3rd cover body 141 and
Four cover bodies 142.
Wherein, described 3rd cover body 141 is fixed on described 5th medial surface 115, and opens up on described 3rd cover body 141
There is one first projection window 1411, so that described camera head 3 is by the described first projection window 1411 and extraneous visual field phase
Logical.Described 4th cover body 142 is fixed on described 6th medial surface 116.
In embodiments of the present invention, suffered during flying in the air in order to maximized reduction airborne vehicle
Air drag, as a kind of embodiment of the embodiment of the present invention, described first cover body 131, described second cover body 132, described
3rd cover body 141 and described 4th cover body 142 are all in hemispherical configuration.
And for the first cover body 131,
Described first cover body 131 includes one first opening 1311, and is fixed on institute by described first opening 1311
State on the first lateral part 121；Described first opening 1311 is a maximum opening of diameter in described hemispherical configuration.Can
To be interpreted as the first cover body 131 by its tail end, internal diameter is gradually reduced, i.e. described first opening with the first opening 1311
1311 is a maximum circular port of diameter in described hemispherical configuration.
And for the second cover body 132,
Described second cover body 132 also includes one second opening 1322, and is fixed on by described second opening 1322
On described second lateral part 122；Described second opening 1322 is a maximum opening of diameter in described hemispherical configuration.
Can be understood as the second cover body 132 by its tail end, internal diameter is gradually reduced, i.e. described second opening with the second opening 1322
1322 is a maximum circular port of diameter in described hemispherical configuration.
And for the 3rd cover body 141 and the 4th cover body 142, described 3rd cover body 141 includes one the 3rd opening
1411, and be fixed on described 5th medial surface by described 3rd opening 1411, described 4th cover body 142 includes one the 4th
Opening 1421, and be fixed on described 6th medial surface 116 by described 4th opening 1421, and described 4th opening
At 1421 end portion being arranged on described 4th cover body 142.Meanwhile, described 3rd cover body 141 and described 4th cover body 142
The all spherical shape in lateral wall.
It is noted that because camera head 3 is fixed in described inner housing 11, and camera head 3 produces as electronics
Product, its work all can be generated heat for a period of time, so that camera head 3 can radiate in inner housing 11 in time, to ensure to take the photograph
As device 3 safe and stable operation, the embodiment of the present invention, on the outer wall of described 4th cover body 142, is additionally provided with several air drafts
Mouth 1422, so that the inner space of described 4th cover body 142 is communicated with external air flow by several exhaust outlets 1422 described.But
It is the quantity for exhaust outlet 1422, discharge regulation, and the opening shape embodiment of the present invention do not limit to, words sentence is talked about, row
The quantity in air port 1422 can be 2,3,4 or multiple, and exhaust outlet 1422 can be and column distribution or random
Distribution, exhaust outlet 1422 can be pyramid type or cylinder type, as long as being finally capable of described 4th cover body 142
Inner space is communicated with external air flow by several exhaust outlets 1422 described, camera head 3 is cooled down, is then all applied to
The present invention.
Need exist for especially it is emphasized that why described first cover body 131 and described second cover body 132 are designed to half
Chondritic, and all spherical shape in lateral wall of described 3rd cover body 141 and described 4th cover body 142, described shell simultaneously
Body 12 and described inner housing 11 are the part spherical structure cutting from whole spheroid.Be so that last by described shell body
12nd, described inner housing 11, described first cover body 131, described second cover body 132, described 3rd cover body 141 and described 4th cover body
The 142 overall rotating mass 1 being constituted, are whole sphere structures.So that described shell body 12, described inner housing 11, institute
State the first cover body 131, the lateral surface of described second cover body 132, described 3rd cover body 141 and described 4th cover body 142 (can be managed
Solve as being used for during aircraft carrying out the windward side of the device of rotating acquisition) as windward side when, the resistance of wind along
Described shell body 12, described inner housing 11, described first cover body 131, described second cover body 132, described 3rd cover body 141 and/
Or the spherical surface of described 4th cover body 142 is slowed down, and then maximized reduction airborne vehicle provided in an embodiment of the present invention
The resistance being received in running in the air.It is also possible to make when running into bad weather circumstances such as thunderstorm weather, fall
Fall within described shell body 12, described inner housing 11, described first cover body 131, described second cover body 132, described 3rd cover body 141
And/or the rainwater of described 4th cover body 142, can along described shell body 12, described inner housing 11, described first cover body 131,
The spherical surface of described second cover body 132, described 3rd cover body 141 and/or described 4th cover body 142 is dirty, it is to avoid hydrops.
Certainly, for the 4th cover body 142, because its lateral wall offers several exhaust outlets 1422 in order to avoid rain
Water is poured in down a chimney in entrance inner housing 11 by several exhaust outlets 1422, and then damages camera head, as one kind enforcement of the present invention
Mode, the opening direction of several exhaust outlets 1422 down, that is, horizontal by an angle, is splashed down in the 4th cover body with reaching
The technique effect that rainwater on 142 lateral walls is directly flowed down due to self gravitation effect, at several exhaust outlets 1422.
Further, in embodiments of the present invention, the first opening 1311 for the first cover body 131 and the first lateral part
Connected mode between 121, the connected mode between the second opening 1321 of the second cover body 132 and the second lateral part 122, the
Connected mode between 3rd opening 1413 of three cover bodies 141 and the 3rd lateral part 123, the 4th opening of the 4th cover body 142
Connected mode between end 1421 and the 4th lateral part 124, can be described in detail below：
Refer to the groove that Figure 12 is provided with a ring-type on described first opening 1311 of described first cover body 131
1311a, is provided with the raised 1211a of a ring-type in the edge of described first lateral part 121, and described projection 1211a inserts
Enter in described groove 1311a.Likewise, the groove of a ring-type is provided with described second opening 1321, outside described second
The edge of sidepiece 122 is provided with the projection of a ring-type, and in the described groove of described raised insertion.In described 3rd opening
It is also equipped with the groove of a ring-type on 1413, be provided with the projection of a ring-type in the edge of described 5th medial part 115, and
In the described groove of described raised insertion.The groove of one ring-type is also equipped with described 4th opening 1421, in the described 6th
The edge of sidepiece is provided with the projection of a ring-type, and in the described groove of described raised insertion.
Due to the connected mode between the first opening 1311 of the first cover body 131 and the first lateral part 121, with the second cover
Connected mode between second opening 1321 of body 132 and the second lateral part 122, the 3rd opening of the 3rd cover body 141
1413 and the 3rd connected mode, the 4th opening 1421 of the 4th cover body 142 and the 4th lateral parts 124 between lateral part 123
Between connected mode all same, therefore, below with the first opening 1311 of the first cover body 131 and the first lateral part 121 it
Between connected mode as a example being described in detail, the second opening 1321 for the second cover body 132 and the second lateral part 122
Between connected mode, the connected mode between the 3rd opening 1413 of the 3rd cover body 141 and the 3rd lateral part 123, the 4th
The non-detailed portion of connected mode between 4th opening 1421 of cover body 142 and the 4th lateral part 124, refers to the first cover body
Connected mode between 131 the first opening 1311 and the first lateral part 121 describes.
Specifically, the groove of a ring-type is arranged on described first opening 1311 of described first cover body 131
1311a, arranges the raised 1211a of a ring-type in the edge of described first lateral part 121, and by described projection 1211a
Insert in described groove 1311a it is possible to understand that on vertical direction as shown in figure 12, when running into bad weather circumstances such as thunderstorm
During weather, rainwater falls into described first opening 1311 of described first cover body 131 and the connecting portion of described first lateral part 121
During the place of position, the nonlinear type type because its connection gap is bending type, the inflow flowing in gap that therefore slow down rainwater is fast
Degree, the more spherical expression of the first cover body 131 of arranging in pairs or groups is so that fall into the rainwater of the first cover body 131 soon in the work of self gravitation
Flowed down with lower, on the contrary, if described first opening 1311 of described first cover body 131, straight with described first lateral part 121
Connect laminating, and do not open up the 1211a or groove 1311a of any projection, be i.e. described first opening of described first cover body 131
End 1311, the connection gap with described first lateral part 121 is linear type, then when rainwater falls into gap, due to be one vertically
Downward gap, rainwater easily flows in inner housing 11 in the presence of self gravitation, and camera head 3 is caused damage.
Certainly, in order to further strengthen waterproof and dustproof effect, in described first opening of described first cover body 131
On 1311, can also open up a plurality of similar to described groove 1311a, that is, some described groove 1311a are in described first opening
The distribution from the top down arranged side by side at end 1311, on the simultaneously matched edge of described first lateral part 121, setting
There is the raised 1211a with described groove 1311a quantity identical ring-type, the corresponding insertion of each raised 1211a one is described recessed
In groove 1311a, material is thus formed some " bending type " gaps, with to the effect playing multilayer flashing.
Additionally need supplementary in embodiments of the present invention, in inner housing in addition to camera head 3 is installed, also can pacify simultaneously
Fill other devices, for example can be fixed with again in described inner housing 11 one for illumination infrared facility 4 so that infrared facility 4
Use with camera head collocation and carry out realizing night camera.Now one second projection window can be opened up on described 3rd cover body 141
Mouth 1412, so that described infrared facility 4 is communicated with the extraneous visual field by the described second projection window 1412.Meanwhile, described interior
The middle part of housing 11 is provided with a mounting groove 117, and is provided with a dividing plate 118 on described mounting groove 117, will be described red
Outer device 4 and described camera head 3 are arranged on the both sides up and down of described dividing plate 118.As one embodiment of the present invention, institute
Stating camera head 3 can be video camera；Described infrared facility 4 can be radar stealthy materials.
Certainly, for the distribution mode of the first projection window 1411 and the second projection window 1412, can be varied
, the present invention does not limit to.For example, the first projection window 1411 and the second projection window 1412 can be in the pass being distributed up and down
System is distributed on described 3rd cover body 141 or in left and right, the relation of distribution is distributed on described 3rd cover body 141, also
Can be that mode in clinodiagonal is distributed on described 3rd cover body 141, throw as long as being capable of camera head 3 and passing through first
Penetrate window 1411 to communicate with the extraneous visual field, infrared facility 4 is communicated with the extraneous visual field by the second projection window 1412, then all applicable
In the present invention.
In order to mitigate the device main screw lift for carrying out rotating acquisition, because the first actuator 2 will be with the first lateral part
121 card is flexibly connected, and therefore uses solid structure for the first lateral part 121, and for the second lateral part 122
For, the structure design of " hollow body " can be adopted, to mitigate automatically, such as far as possible：Second lateral part 122 can include cross
The support frame 1221 of type structure and support disk 1222.Wherein, described support frame 1221 is symmetrically fixed on described support
At the peripheral edge position of disk 1222, and described bearing assembly 133 is fixed on described support disk 1222.Support frame
1221 are used for connecting described support disk 1222 and bearing assembly 133 as support frame, with this by cross type frame structure Lai
Replace the solid structure of the first lateral part 121, reach the technique effect mitigating deadweight.
Further, refer to Figure 11 to be driven in rotary course by the first actuator 2 in inner housing 11, in order to avoid
Inner housing 11 rotates excessively, namely the anglec of rotation is excessive and affects normal photographing, preferably, described be used for carrying out rotating acquisition
Device also include：Limiting component 6.Described limiting component 6 is fixed on described bearing assembly 133, and with described bearing assembly
133 synchronous axial system；And offer a gear hole 1221a on described support frame 1221, described gear hole 1221a is provided with one
Position stop piece, described limiting component 6 is contacted with described position stop piece or separates, and is limited with the rotation to described bearing assembly 133
Position.
Specifically, described position stop piece can be a screw, and described gear hole 1221a can be and described screw phase
The screwed hole joined, described limiting component 6 is a swingle.And described swingle includes positioning end 61 and turning end 62, described fixed
Position end 61 be fixed on described ring flange, described turning end 62 is rotated with respect to described positioning end 61, with described screw
Contact or separation.Rotated in certain angle herein for the described swingle of control, and then controlled inner housing certain
Rotated in angle, two gear hole 1221as can be fixedly installed in support frame 1221, and fix two screws so that by
Two screws constitute a subtended angle on supporting disk 1222, and then when swingle rotates to a certain angle with bearing assembly 133,
Stopped by screw and limit rotation.And in order to enable swingle to better contact with turning end 62, as the present invention
A kind of implementation,.One shift slot 63 is further opened with turning end 62.The notch internal diameter of described shift slot 63 be more than or
Equal to the external diameter of described screw, contacted with screw by this shift slot 63 with this turning end 62.
Further, in order to inner housing 11, the anglec of rotation on the first vertical direction carries out real-time detection, this
The described device for carrying out rotating acquisition that inventive embodiments are provided also includes：First magnetic induction encoder 7.Described first
Magnetic induction encoder 7 is fixed on described first motor, and is connected with extraneous flight control system, with to described first motor
The anglec of rotation carries out Real-time Collection, and then the deflection angle of inner housing described in real-time detection.It should be noted that magnetic induction coding
The operation principle that device is detected to angle yaw displacement by changes of magnetic field has been prior art, and here is omitted, and
By magnetic induction encoder applies in the present invention, match with the first actuator 2 and inner housing 11 with the shooting angle to camera head 3
Degree is controlled, and is that the innovative point of the present invention is located, first offers some clarification herein.
In embodiments of the present invention, described first yoke assembly 5 can include：Second actuator 51 and suspension housing 52.
Wherein, described suspension housing 52 is in hollow cylindrical structure, is fixed on described rotating mass 1 by its end portion
On, it is fixed on described fuselage by its upper part.Likewise, how to be fixed on fuselage for suspender 52, the present invention
Embodiment is not limited to, and can be directly to be threadedly connected on fuselage by screw, also can by a fixing device by its
Being fixed on the bottom of fuselage, as long as be capable of the first yoke assembly 5 being relatively fixed with fuselage, being then all applied to the present invention.
Wherein, described second actuator 51 can be the second motor, be fixed in described suspension housing 52 in, and with described
Rotating mass 1 are flexibly connected, and described second actuator 51 obtains control signal and drives described rotating mass in the horizontal direction
Rotated with respect to described fuselage, so that Real-time Collection is carried out to the visual information in horizontal direction.
Identical, in order to the anglec of rotation in the horizontal direction of inner housing 11 is carried out with real-time detection, the present invention is implemented
Described first yoke assembly that example is provided also includes：Second magnetic induction encoder 53.Described second magnetic induction encoder 53 is solid
On described second motor, and it is connected with extraneous flight control system, reality is carried out with the anglec of rotation to described second motor
When collection, and then inner housing 11 deflection angle in the horizontal direction described in real-time detection.It should be noted that magnetic induction coding
The operation principle that device is detected to angle yaw displacement by changes of magnetic field has been prior art, and here is omitted, and
By magnetic induction encoder applies in the present invention, match with the second actuator 51 and inner housing 11 with the shooting to camera head 3
Angle is controlled, and is that the innovative point of the present invention is located, first offers some clarification herein.
Further, timely in order to realize image/video information captured by camera head 3 in embodiments of the present invention
Output, the embodiment of the present invention is additionally provided with first external interface being used for external external device in described suspension on housing 52
521, such as USB transmission interface, same is provided with one second external interface 1423 on described 4th cover body 142, such as USB transmission
Interface.
Above-mentioned airborne vehicle provided in an embodiment of the present invention, on the one hand passes through to be used for carrying out the rotation in the device of rotating acquisition
It is fixed on turning body rotation on the described fuselage of airborne vehicle, and fixes one simultaneously in rotating mass and be used for carrying out information gathering
Camera head, so allow for being rotated in the horizontal direction with respect to fuselage by rotating mass, with drive shooting dress
Put and Real-time Collection is carried out to the visual information in horizontal direction；On the other hand it is fixed in rotating mass by the first actuator,
And be flexibly connected with this camera head, drive camera head in the first vertical direction so that control signal is obtained by the first actuator
On rotated with respect to rotating mass, so that Real-time Collection is carried out to the visual information on the first vertical direction.Eventually through with
In carrying out the device of rotating acquisition as regulating object, realize not affecting the state of flight of airborne vehicle and the premise of flight efficiency
Under, complete the multi-angle collection of image in horizontal direction and vertical direction, video information, have that structure is simple, the suitability is wide
Feature.
Certainly, in order to realize carrying out image/video letter for the device carrying out rotating acquisition in wider array of field-of-view angle
The collection of breath, is such as revolved with (both direction) on the first vertical direction with respect in the horizontal direction of level ground except above-mentioned
Turn, the another embodiment that the present invention provides also can achieve for the device carrying out rotating acquisition in the level with respect to level ground
Rotated on (three directions) on direction, on the first vertical direction and on the second vertical direction, wherein, described first vertical side
To with described second vertical direction be orthogonal two vertical directions.
In this embodiment, refer to Fig. 8, the described device for carrying out rotating acquisition can also include：Second deflection
Assembly 8 (replaces first yoke assembly 5 of above-described embodiment), described second yoke assembly 8 be rotationally fixed to described fuselage and
Between described rotating mass 1, and described rotating mass 1 by described second yoke assembly 8 with respect to described fuselage in level side
Upwards, rotated on described first vertical direction and on the second vertical direction；And described first vertical direction and described second
Vertical direction is mutually perpendicular to.
Specifically, described second yoke assembly 8 includes：Second actuator 51, the 3rd actuator 81, suspension housing 52 and
Support housing 82.Wherein, described second actuator 51 is fixed in described suspension housing 52；Described 3rd actuator 81 is fixed on
In described support housing 82；And described suspension housing 52 be fixed on described fuselage, and pass through described second actuator 51 and institute
State support housing 82 to be flexibly connected；Described support housing 82 is by described 3rd actuator 81 with the activity of described rotating mass 1 even
Connect.
In this embodiment, described second actuator 51, the 3rd actuator 81 are the second motor and the 3rd motor respectively, and
Same in order to the anglec of rotation in the anglec of rotation in the horizontal direction of inner housing 11 and the second vertical direction, this is real
Described second yoke assembly 8 that applying example is provided also includes：Second magnetic induction encoder 53 and the 3rd magnetic inductor.Described second
Magnetic induction encoder 53 is fixed on described second motor, and is connected with extraneous flight control system, with to described second motor
The anglec of rotation carry out Real-time Collection, and then inner housing 11 deflection angle in the horizontal direction described in real-time detection.Described
Three magnetic induction encoders are fixed on described 3rd motor, and are connected with extraneous flight control system, with to described 3rd motor
The anglec of rotation carry out Real-time Collection, and then deflection angle on the second vertical direction for the inner housing 11 described in real-time detection.With
Sample is it should be noted that magnetic induction encoder by changes of magnetic field come the operation principle that angle yaw displacement is detected is
Prior art, here is omitted, and by magnetic induction encoder applies in the present invention, with the second actuator 51, the 3rd actuator
81 and inner housing 11 match and be controlled with the shooting angle to camera head 3, be that the innovative point of the present invention is located, herein first
Offer some clarification.
Further, described support housing 82 is in that the moon is curved, and described support housing 82 includes the first round end 821 and the
Two round ends 822.Described support housing 82 is rotationally fixed on described suspension housing 52 by described first round end 821,
And be rotationally fixed in described rotating mass 1 by described second round end 822.Finally realize the second actuator 51 and drive institute
State support housing 82 to be rotated in the horizontal direction, to drive described rotating mass 1 to be rotated in the horizontal direction.
It is significant to note that, in this embodiment, because the second actuator 51 and support housing 82 are joined directly together
Carry the gravity supporting housing 82 and rotating mass 1, to this in order to mitigate the second actuator 51 with respect to support housing 82
Bearing pressure, the described device for carrying out rotating acquisition also includes：Stress assembly 84.Described stress assembly 84 is fixed on institute
State at the first round end 821, to connect described suspension housing 52 and described support housing 82, and described stress assembly 84 envelope institute
State the second actuator 52.
Can be understood as stress assembly 84 is over-stressed part, and it will hang housing 52 and described support housing 82 phase
Even, and by including described second actuator 52, the second actuator 52 and the first round end 821 supporting housing 82 are alleviated with this
The gravity supporting housing 82 and rotating mass 1 being carried in connection procedure, serves protective action to the second actuator 52.
Further, described stress assembly 84 can include：First stressed plate 841, the second stressed plate 842 and support column
843.Wherein, described first stressed plate 841 is fixed on described suspension housing 52, and described second stressed plate 841 is fixed on described
On first round end 821, described first stressed plate 841 is fixedly connected by described support column 843 with described second stressed plate 842,
And described second actuator 51 is fixed between described first stressed plate 841 and described second stressed plate 842.Need explanation
It is, the first stressed plate 841 described herein and the described fixation hung between housing 52, described second stressed plate 841 and described the
Fixation between one round end 821, and in the application the position described by remaining place fix but the two phase can occur
Whether, to " fixation " of rotating, the relative position being only worth therebetween is fixed, and will not be subjected to displacement, when can occur to it
Relatively rotate, do not limit, be explained herein.
It should be noted last that, above specific embodiment only in order to technical scheme to be described and unrestricted,
Although being described in detail to the present invention with reference to example, it will be understood by those within the art that, can be to the present invention
Technical scheme modify or equivalent, without deviating from the spirit and scope of technical solution of the present invention, it all should be covered
In the middle of scope of the presently claimed invention.
Claims (10)
1. a kind of device for carrying out rotating acquisition is it is characterised in that the described device for carrying out rotating acquisition includes：
Rotating mass, described rotating mass are rotationally fixed on extraneous charging appliance, and are fixed with one in described rotating mass
For carrying out the camera head of information gathering, carried out in the horizontal direction with respect to described charging appliance by described rotating mass
Rotate, to drive described camera head to carry out Real-time Collection to the visual information in horizontal direction；
First actuator, described first actuator is fixed in described rotating mass, and is flexibly connected with described camera head, and
Described first actuator obtains control signal and drives described camera head first vertical direction relative to described rotating mass
Rotated, so that Real-time Collection is carried out to the visual information on the first vertical direction；
First yoke assembly, described first yoke assembly is rotationally fixed between described charging appliance and described rotating mass,
And described rotating mass are rotated with respect to described charging appliance in the horizontal direction by described first yoke assembly；
First magnetic induction encoder；Described first magnetic induction encoder is fixed on described first actuator, and flies with extraneous
Control system connects, and carries out real-time detection with the anglec of rotation to described first actuator.
2. it is used for as claimed in claim 1 carrying out the device of rotating acquisition it is characterised in that described rotating mass include：
Shell body, described shell body is fixed on described charging appliance by described first yoke assembly；
Inner housing, described inner housing is set in the inside of described shell body, and is flexibly connected with described shell body, and described inner shell
Body phase is rotatable for described shell body, and described camera head is fixed on described inner housing；
First combination cover body, described first combination cover body envelope is in the outside of described shell body, and fixes even with described shell body
Connect, and described first actuator is fixed in described first combination cover body；
Second combination cover body, described second combination cover body envelope is in the outside of described inner housing, and fixes even with described inner housing
Connect.
3. the as claimed in claim 2 device being used for carrying out rotating acquisition it is characterised in that：
Described shell body is in chondritic, and inside is in hollow-core construction, to place described inner housing；And described shell body includes：
First lateral part；
Second lateral part, described second lateral part and described first lateral part opposition are distributed in the both sides of described shell body；
3rd lateral part；
4th lateral part, described 4th lateral part and described 3rd lateral part opposition are distributed in the both sides of described shell body；
5th lateral part；
6th lateral part, described 6th lateral part and described 5th lateral part opposition are distributed in the both sides of described shell body；
Wherein, described first lateral part, described second lateral part, described 3rd lateral part, described 4th lateral part, the described 5th
Lateral part and described 6th lateral part surround and form the internal described shell body in hollow-core construction, and described 3rd outside left in
Between described first lateral part and described second lateral part, and respectively with described first lateral part and described second lateral part phase
Adjacent；Described shell body is rotationally fixed on described first yoke assembly by described 3rd lateral part；Described 4th lateral part,
Described 5th lateral part and described 6th lateral part are all in hatch frame, and the inner space of described shell body passes through the described 4th
Lateral part, described 5th lateral part and/or described 6th lateral part are communicated with the external world；Described first combination cover body is individually fixed in
On described first lateral part and described second lateral part.
4. the as claimed in claim 3 device being used for carrying out rotating acquisition it is characterised in that：
Described inner housing is in chondritic, and inside is in hollow-core construction, to place described camera head；And described inner housing bag
Include：
First medial part；
Second medial part, described second medial part and described first medial part opposition are distributed in the both sides of described inner housing；
3rd medial part；
4th medial part, described 4th medial part and described 3rd medial part opposition are distributed in the both sides of described inner housing；
5th medial part；
6th medial part, described 6th medial part and described 5th medial part opposition are distributed in the both sides of described inner housing；
Wherein, described first medial part, described second medial part, described 3rd medial part, described 4th medial part, the described 5th
Medial part and described 6th medial part surround and form the internal described inner housing in hollow-core construction, and described 3rd inside line in
Between described first medial part and described second medial part, and respectively with described first medial part and described second medial part phase
Adjacent；Described inner housing is passed through described first medial part and described second medial part and is flexibly connected with described shell body, and described the
One medial part and described first lateral part fit, and described second medial part and described second lateral part fit, and the described 3rd
Medial part and described 3rd lateral part fit, and described 4th inside line is in the hatch frame position of described 4th lateral part
Place；Described 5th medial part and described 6th medial part are all in hatch frame, and described second combination cover body correspondence is fixed on institute
State on the 5th medial part and described 6th medial part.
5. the device being used for carrying out rotating acquisition as claimed in claim 4 is it is characterised in that described first combines cover body bag
Include：
First cover body, described first cover body is fixed on described first lateral part, and described first actuator is fixed on described
In one cover body, and described first actuator is flexibly connected through described first lateral part with described first medial part；
Second cover body, described second cover body is fixed on described second lateral part；With
Bearing assembly, described bearing assembly is fixed in described second cover body, and described bearing assembly passes through outside described second
Portion is fixedly connected with described second private side, so that described second private side can relatively rotate with respect to described second lateral part.
6. the device being used for carrying out rotating acquisition as claimed in claim 5 is it is characterised in that described second combines cover body bag
Include：
3rd cover body, described 3rd cover body is fixed on described 5th medial surface, and offers one first on described 3rd cover body
Projection window, so that described camera head is communicated with the extraneous visual field by the described first projection window；
4th cover body, described 4th cover body is fixed on described 6th medial surface.
7. it is used for as claimed in claim 6 carrying out the device of rotating acquisition it is characterised in that described second lateral part includes：
Support frame；
Support disk, described support frame is symmetrically fixed at the peripheral edge position of described support disk, and described bearing
Assembly is fixed on described support disk.
8. it is used for as claimed in claim 7 carrying out the device of rotating acquisition it is characterised in that also including：
Limiting component, described limiting component is fixed on described bearing assembly, and with described bearing assembly synchronous axial system；And
It is provided with position stop piece, described limiting component is contacted with described position stop piece or separates, with to described on described support frame
The rotation of bearing assembly carries out spacing.
9. the as claimed in claim 8 device being used for carrying out rotating acquisition it is characterised in that
Described position stop piece is screw, and described screw is fixed on described support frame；
Described limiting component is a swingle, and described swingle includes positioning end and turning end, and described positioning end is fixed on described
On bearing assembly, described turning end is rotated with respect to described positioning end, to contact with described screw or to separate.
10. the as claimed in claim 6 device being used for carrying out rotating acquisition it is characterised in that：
Described 3rd cover body includes one the 3rd opening, and is fixed on described 5th medial surface by described 3rd opening,
And described 3rd opening is provided with the groove of a ring-type, the edge of described 5th medial part is provided with the convex of a ring-type
Rise, and in the described groove of described raised insertion.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610789275.7A CN106394916A (en) | 2016-08-31 | 2016-08-31 | Device for rotating collection |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610789275.7A CN106394916A (en) | 2016-08-31 | 2016-08-31 | Device for rotating collection |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106394916A true CN106394916A (en) | 2017-02-15 |
Family
ID=58000592
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610789275.7A Pending CN106394916A (en) | 2016-08-31 | 2016-08-31 | Device for rotating collection |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106394916A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201235938Y (en) * | 2008-07-04 | 2009-05-13 | 中国船舶重工集团公司第七一七研究所 | Machine-carried visible light image apparatus |
| US20130048792A1 (en) * | 2011-08-29 | 2013-02-28 | Aerovironment, Inc. | Tilt-Ball Turret With Gimbal Lock Avoidance |
| CN104668712A (en) * | 2013-11-27 | 2015-06-03 | 大连渤海起重机器股份有限公司 | Sliding rail locking structure of semiautomatic flame cutting machine |
| CN204836322U (en) * | 2015-06-30 | 2015-12-02 | 桂林飞宇电子科技有限公司 | Take moving camera of camera lens stabilization function |
| CN205418138U (en) * | 2016-03-18 | 2016-08-03 | 江苏数字鹰科技发展有限公司 | Triaxial optoelectronic pod |
-
2016
- 2016-08-31 CN CN201610789275.7A patent/CN106394916A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201235938Y (en) * | 2008-07-04 | 2009-05-13 | 中国船舶重工集团公司第七一七研究所 | Machine-carried visible light image apparatus |
| US20130048792A1 (en) * | 2011-08-29 | 2013-02-28 | Aerovironment, Inc. | Tilt-Ball Turret With Gimbal Lock Avoidance |
| CN104668712A (en) * | 2013-11-27 | 2015-06-03 | 大连渤海起重机器股份有限公司 | Sliding rail locking structure of semiautomatic flame cutting machine |
| CN204836322U (en) * | 2015-06-30 | 2015-12-02 | 桂林飞宇电子科技有限公司 | Take moving camera of camera lens stabilization function |
| CN205418138U (en) * | 2016-03-18 | 2016-08-03 | 江苏数字鹰科技发展有限公司 | Triaxial optoelectronic pod |
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Application publication date: 20170215 |
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