CN206273683U - A kind of unmanned plane - Google Patents
A kind of unmanned plane Download PDFInfo
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- CN206273683U CN206273683U CN201621325952.1U CN201621325952U CN206273683U CN 206273683 U CN206273683 U CN 206273683U CN 201621325952 U CN201621325952 U CN 201621325952U CN 206273683 U CN206273683 U CN 206273683U
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- connecting rod
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Abstract
The utility model embodiment discloses a kind of unmanned plane, including：Fuselage；Undercarriage, is arranged at the bottom of the fuselage, and the undercarriage has connection end and the ground terminal of the bottom away from the fuselage of the bottom of the connection fuselage；Fold mechanism, is arranged at the bottom of the fuselage；And, image mechanism is installed on the one end of the fold mechanism away from the fuselage；The fold mechanism is in when under contraction state, and the image mechanism is less than the distance of the ground terminal and the bottom of the fuselage with the distance of the bottom of the fuselage；The fold mechanism is in when under deployed condition, and the image mechanism is more than the distance of the ground terminal and the bottom of the fuselage with the distance of the bottom of the fuselage.Through the above way, the utility model embodiment can realize glitch-free panoramic shooting, meanwhile, Project Realization principle is simple, workable.
Description
Technical field
The utility model embodiment is related to unmanned air vehicle technique field, undercarriage can be avoided when more particularly to one kind is imaged and is done
The unmanned plane disturbed.
Background technology
Current augmented reality (Augmented Reality, AR) and virtual reality (Virtual Reality, VR) technology
Development is swift and violent, the demand that it is shot for panoramic video also more and more higher, is taken photo by plane using unmanned plane, is to obtain true field
A kind of important way of the panoramic picture of scape.And in order to the accurate image for obtaining multiple angles, carried out when using unmanned plane
During panoramic shooting, the camera that unmanned plane is carried needs to avoid blocking for undercarriage.It is existing to realize unmanned plane panoramic shooting
Technical scheme be：Camera is down stretched out by expansion link, camera is located at the lower section of undercarriage.However, general
Unmanned plane undercarriage is highly about 15cm or so, to make the lower section of the fully extended undercarriage of camera, it is necessary to make camera and cloud
Platform moves distance very long, and this requires expansion link long enough, in addition, it is general by expansion link be arranged at unmanned plane body just under
Side, expansion link is hidden in body, it is necessary in about one passage of about 15cm of whole body center outflow, and general machine
Internal center is mainly used in placing battery, motherboard etc., therefore, this scheme actually implements difficult with very big engineering
Degree.
Utility model content
The utility model embodiment provides a kind of unmanned plane, can solve the problem that when panoramic shooting is carried out, will by expansion link
Camera is placed in below undercarriage that blocking for undercarriage is evaded and realized the big problem of engineering difficulty.
In order to solve the above technical problems, the technical scheme that the utility model is used is：A kind of unmanned plane is provided, the nothing
It is man-machine including：Fuselage；
Undercarriage, is arranged at the bottom of the fuselage, and the undercarriage has the connection end of the bottom of the connection fuselage
With the ground terminal of the bottom away from the fuselage；
Fold mechanism, is arranged at the bottom of the fuselage；And,
Image mechanism, is installed on the one end of the fold mechanism away from the fuselage；
The fold mechanism is in when under contraction state, and the image mechanism is less than institute with the distance of the bottom of the fuselage
State the distance of ground terminal and the bottom of the fuselage；The fold mechanism is in when under deployed condition, the image mechanism and institute
The distance for stating the bottom of fuselage is more than the distance of the ground terminal and the bottom of the fuselage.
Wherein, the fold mechanism includes：First connecting rod and second connecting rod, the first connecting rod include the first connection end and
Second connection end, the second connecting rod includes the 3rd connection end and the 4th connection end；First connection end connects with the fuselage
Connect, second connection end and the 3rd connection end chain connection, the 4th connection end is connected with the image mechanism.
Wherein, second connection end is provided with the drive device for driving the second connecting rod to rotate.
Wherein, the drive device includes rotating shaft and first gear, and the first gear is fixedly connected with the rotating shaft；Institute
State the 3rd connection end and be provided with second gear；The first gear is engaged with the second gear；Rotating shaft connection described the
Two connection ends and the 3rd connection end, when the axis of rotation, drive the second gear to rotate by the first gear, with
The second connecting rod is set to be rotated relative to the first connecting rod.
Wherein, the first cable is provided with the first connecting rod, first cable includes the first termination and the second termination；
First termination is electrically connected with the electric supply installation in the fuselage, and second termination is connected with the drive device；Institute
State and be provided with second connecting rod the second cable, second cable includes the 3rd termination and the 4th termination；Second connection end
3rd connection end is provided with relative sets of vias, the 3rd termination is electrical with the second termination through the sets of vias
Connection, the 4th termination is connected with the image mechanism.
Wherein, the bottom of the fuselage is provided with the first draw-in groove, and first connection end is provided with the first clamp, described
One clamp is detachably connected with first draw-in groove.
Wherein, the side that first draw-in groove and first clamp are abutted against is provided with the first metal clips group, described
First metal clips group is electrically connected with the first termination of first cable.
Wherein, the 4th connection end is provided with the second draw-in groove, and the image mechanism is connected with the 4th connection end
One end is provided with the second clamp, and second clamp is detachably connected with second draw-in groove.
Wherein, the side that second draw-in groove and second clamp are abutted against is provided with the second metal clips group, described
Second metal clips group is electrically connected with the 4th termination of second cable.
Wherein, the fold mechanism also includes：Third connecting rod, the third connecting rod includes the 5th connection end and the 6th connection
End, the 5th connection end and second connection end chain connection, the 6th connection end and the 3rd connection end hinge
Connection；The first connecting rod drives the third connecting rod to rotate, and the third connecting rod drives the second connecting rod to rotate.
Wherein, the image mechanism includes：Head and video capturing device, one end of the head and the fold mechanism
Connection, the other end of the head is connected with the video capturing device.
Wherein, the head includes damping device, and one end of the damping device is connected with the fold mechanism, described to subtract
The other end for shaking device is connected with the video capturing device.
Wherein, the fold mechanism is arranged at the middle position of the bottom of the fuselage.
The beneficial effect of the utility model embodiment is：The situation of prior art is different from, the utility model embodiment is carried
The unmanned plane of confession controls packing up and discharging for image mechanism using fold mechanism, can effectively avoid the interference of undercarriage, real
Existing glitch-free panoramic shooting, meanwhile, Project Realization principle is simple, workable.
Brief description of the drawings
In order to illustrate more clearly of the technical scheme of the utility model embodiment, below will be in the utility model embodiment
The required accompanying drawing for using is briefly described.It should be evident that drawings described below is only of the present utility model one
A little embodiments, for those of ordinary skill in the art, on the premise of not paying creative work, can also be according to these
Accompanying drawing obtains other accompanying drawings.
Fig. 1 is the positive view that a kind of unmanned plane that the utility model embodiment is provided is under state of flight；
Fig. 2 is the positive view (a) and top view (b) that the unmanned plane in Fig. 1 is under landing state；
Fig. 3 is a kind of structural representation of fold mechanism that the utility model embodiment is provided；
Fig. 4 is the structural representation of another fold mechanism that the utility model embodiment is provided；
Fig. 5 is the exploded view of the fuselage bottom, fold mechanism and image mechanism in Fig. 1；
Fig. 6 is the structural representation of first gear and second gear in Fig. 5；
Fig. 7 is the positive view that another unmanned plane that the utility model embodiment is provided is under landing state；And,
Fig. 8 is the structural representation of the fold mechanism in Fig. 7.
Specific embodiment
For the ease of understanding the utility model, below in conjunction with the accompanying drawings and specific embodiment, the utility model is carried out more detailed
Thin explanation.It should be noted that when element is expressed " being fixed on " another element, it can directly in another element
Above or therebetween there may be one or more elements placed in the middle.When an element is expressed " connection " another element, it can
To be directly to another element or there may be one or more elements placed in the middle therebetween.This specification is used
The instruction such as term " vertical ", " level ", "left", "right", " " center ", " on ", D score, " interior ", " outward " orientation or position
The relation of putting is, based on orientation shown in the drawings or position relationship, to be for only for ease of description the utility model and simplify description, and
Be not indicate or imply meaning device or element must have specific orientation, with specific azimuth configuration and operation, therefore
It is not intended that to limitation of the present utility model.Additionally, term " first ", " second ", " the 3rd " etc. are only used for describing purpose, and
It is not intended that indicating or implying relative importance.
Unless otherwise defined, this specification is used all of technology and scientific terminology with belong to skill of the present utility model
The implication that the technical staff in art field is generally understood that is identical.In art used in the description of the present utility model in this specification
Language is intended merely to describe the purpose of specific embodiment, is not intended to limit the utility model.Additionally, this reality disclosed below
As long as not constituting conflict each other with technical characteristic involved in new each implementation method can just be mutually combined.This
The term "and/or" that specification is used includes the arbitrary and all of combination of one or more related Listed Items.
Fig. 1 is the sectional view that a kind of unmanned plane that the utility model embodiment is provided is under state of flight；Fig. 2 is Fig. 1
In unmanned plane be in landing state under sectional view (a) and top view (b).Fig. 1 and Fig. 2 is referred to, the unmanned plane 100 is wrapped
Include：Fuselage 1, undercarriage 2, fold mechanism 3 and image mechanism 4.Undercarriage 2 and fold mechanism 3 may be contained within the bottom of fuselage 1,
Image mechanism 4 is installed on the one end of fold mechanism 3 away from the fuselage 1, wherein, undercarriage 2 has the bottom of connection fuselage 1
Connection end 21 and the ground terminal 22 of the bottom away from fuselage 1.When 100 flight of unmanned plane, fold mechanism 3 is in deployed condition,
As shown in figure 1, the distance of the bottom of image mechanism 4 and fuselage 1 more than undercarriage 2 ground terminal 22 and the bottom of fuselage 1 away from
From；When unmanned plane 100 lands, fold mechanism 3 is in contraction state, as shown in Fig. 2 image mechanism 4 and the bottom of fuselage 1
Distance is less than the ground terminal 22 of undercarriage 2 and the distance of the bottom of fuselage 1.
In the present embodiment, the quantity of undercarriage 2 is unrestricted, can be two, four etc., and it is act as in unmanned plane
It can be made smoothly to be parked in ground or a plane during 100 landing, played a supporting role.Fold mechanism 3 is to refer to adjustment to take the photograph
The mechanism of the height of camera structure 4, when unmanned plane 100 drop to certain altitude, the fold mechanism 3 shrinks, while driving shooting
Mechanism 4 shrinks upwards, to cause that image mechanism 4 is packed up in the space surrounded in undercarriage 2, can effectively prevent unmanned plane
100 in landing image mechanism 4 collide ground and cause the damage of image mechanism 4.When unmanned plane 100 takes off to certain altitude
Afterwards, fold mechanism 3 launches, while drive image mechanism 4 to move down, to cause that image mechanism 4 is stretched out outside undercarriage 2, from
And blocking for undercarriage 2 can be avoided, realize panoramic shooting.The fold mechanism 3 can be arranged at any one of the bottom of fuselage 1
Individual position, such as：Front side, left side, right side or rear side.
In certain embodiments, in order to keep the balance of fuselage 1, fold mechanism 3 can be arranged at the bottom of fuselage 1
Middle position.
Additionally, the form of expression of the fold mechanism 3 can be diversified, for example：Can be as shown in Figure 3 by two
The stretching structure that root or many connecting rods are nested, can control bottom by the control unit being arranged in fuselage 1 or connecting rod
The raising and lowering of the connecting rod in portion realizes the expansion and contraction of the fold mechanism, wherein, Fig. 3 (a) is the exhibition of the fold mechanism
Open state, Fig. 3 (b) is the contraction state of the fold mechanism.Or, the fold mechanism can also be as shown in Figure 4 by many
Connecting rod constitute folding structure, the fold mechanism can be pulled by control unit realize the fold mechanism expansion and
Shrink, wherein, Fig. 4 (a) is the deployed condition of the fold mechanism, and Fig. 4 (b) is the contraction state of the fold mechanism.
Preferably, in the present embodiment, as shown in figure 5, fold mechanism 3 includes：First connecting rod 31 and second connecting rod 32, the
One connecting rod 31 includes the first connection end 311 and the second connection end 312, and second connecting rod 32 includes that the 3rd connection end 322 and the 4th connects
Connect end 321；Wherein, the first connection end 311 is fuselage connection end, the bottom for fold mechanism 3 to be arranged at fuselage 1；Second
The connection end 322 of connection end 312 and the 3rd is respectively the connecting rod connection end of first connecting rod 31 and second connecting rod 32, for connecting first
Connecting rod 31 and second connecting rod 32；4th connection end 321 is image mechanism connection end, for connecting fold mechanism 3 and image mechanism
4.In the present embodiment, the first connection end 311 is connected with the bottom of fuselage 1；Cut with scissors with the 3rd connection end 322 the second connection end 312
Chain is connected；4th connection end 321 is connected with image mechanism 4.
In the present embodiment, after unmanned plane 100 takes off to certain altitude, first connecting rod 31 and second connecting rod 32 are expansion
State, first connecting rod 31 is more long than undercarriage 2 plus the vertical length of second connecting rod 32, so that image mechanism 4 is placed in and rises and falls
Outside frame 2.When unmanned plane 100 drop to certain altitude, second connecting rod 32 is rotated up certain angle around first connecting rod 31, this
When fold mechanism 3 vertical length it is shorter than undercarriage 2, meanwhile, image mechanism 4 is packed up under the drive of second connecting rod 32 in rising and falling
In the space that frame 2 is surrounded.In the present embodiment, fold mechanism is constituted with hinged first connecting rod 31 and second connecting rod 32
3, the position of image mechanism 4 can be effectively adjusted, meanwhile, simple structure is easy to use.
Wherein, can be lived by any one hinged mode between the second connection end 312 and the 3rd connection end 322
Dynamic connection.In certain embodiments, for the ease of the contraction and expansion of control fold mechanism 3, the second connection end 312 can be set
There is the drive device 3121 for driving second connecting rod 32 to rotate, when drive device 3121 starts, second connecting rod 32 is with second
Connection end 312 and the 3rd upwardly or downwardly rotates default angle centered on connection end 322, to realize that the fold mechanism 3 is received
Contracting and the switching of deployed condition.Wherein, drive device 3121 can be motor or motor.
In another embodiment, in order to more precisely control the rotational angle of second connecting rod 32, drive device
3121 specifically include the rotating shaft 3121a and first gear 3121b being fixedly connected with rotating shaft 3121a；3rd connection end 322 is provided with
Second gear 3221；First gear 3121b and second gear 3221 are engaged (refer to Fig. 6), and rotating shaft 3121a connections second are connected
The connection end 322 of end 312 and the 3rd, when rotating shaft 3121a is rotated, drives second gear 3221 to rotate by first gear 3121b,
So that second connecting rod 32 is rotated relative to first connecting rod 31.Optionally, first gear 3121b and second gear 3221 can be by outer
The tooth of side intermeshes to realize that one drives another to rotate；One gear can also be set to convex gear, a gear
Spill gear is set to, convex gear is embedded in realize engagement in spill gear, and then one drives another to rotate.
Further, when fold mechanism 3 needs switching contraction or deployed condition, can be connected by wireless signal
Mode carrys out driver 3121, or, in the present embodiment, in order to reduce cost of implementation, it is also possible to by folding machine
Cable is set in structure 3 and carrys out transmitting telecommunication number.Specifically, the first cable 331 is provided with first connecting rod 31, first cable 331
Including the first termination 331a and the second termination 331b, wherein, the first termination 331a is electrically connected with the electric supply installation in fuselage 1,
Second termination 331b is connected with drive device 3121.Meanwhile, it is provided with the second cable 332, the second cable 332 in second connecting rod 32
Including the 3rd termination 332a and the 4th termination 332b, the second connection end 312 and the 3rd connection end 322 are provided with relative sets of vias
34, then the 3rd termination 332a be electrically connected with the second termination 331b after the sets of vias 34, the 4th termination 332b and video camera
Structure 4 is connected.Can be that drive device 3121 and image mechanism 4 are powered by the first cable 331 and the second cable 332.
Wherein, fuselage 1 can be with the connected mode of image mechanism 4 with the first connection end 311 and the 4th connection end 321
Single connected mode, for example：Integral type connection, welding, bolt connection, threaded connection, riveting etc., it is also possible to any two kinds or
The combination of various connected modes.Wherein, the connected mode and the 4th connection end 321 and video camera of the connection end 311 of fuselage 1 and first
The connected mode of structure 4 can be that identical can also be different.In order to the difficulty and cost and lifting that reduce engineering are replaced
Convenience, in the present embodiment, fuselage 1 is used with the first connection end 311 and the 4th connection end 321 with image mechanism 4
Dismountable connected mode for snapping connection.
Specifically, in the present embodiment, the bottom of fuselage 1 is provided with the first draw-in groove 11, the first connection end 311 be provided with
The first clamp 3111 that first draw-in groove 11 is detachably connected, when the first clamp 3111 snaps in the first draw-in groove 11, fold mechanism 3 is consolidated
Surely it is arranged at the bottom of fuselage 1.Similarly, the 4th connection end 321 is provided with the second draw-in groove 3211, and image mechanism 4 is provided with and
The second clamp 41 that two draw-in groove 3211 is detachably connected, when the second clamp 41 snaps in the second draw-in groove 3211, image mechanism 4 is fixed
It is arranged at the one end of fold mechanism 3 away from fuselage 1.
Further, when the fold mechanism 3 by cable come transmitting telecommunication when, for the ease of the transmission of electric signal,
The side that one draw-in groove 11 and the first clamp 3111 are abutted against is provided with the first metal clips group 51, the first metal clips group 51 with
First termination 331a of the first cable 331 is electrically connected with, for transmitting the electric signal between fuselage 1 and fold mechanism 3.Its
In, the first metal clips group 51 can by be fixedly installed on respectively the first draw-in groove 11 inner side and the first clamp 3111 it is upper
Side, and one-to-one a pair or multipair metal clips composition, in Fig. 5 by taking 4 pairs of metal clips as an example, but are not used in restriction
The utility model embodiment.It is understood that the logarithm of metal clips can determine according to the quantity of cable in fold mechanism 3
It is fixed, such as one cable a pair of metal clips of correspondence.Metal clips can be made of copper sheet or other conductive metals.Similarly,
The side that second draw-in groove 3211 and the second clamp 41 are abutted against is provided with the second metal clips group 52, the second metal clips group 52
The 4th termination 332b with the second cable 332 is electrically connected with, for transmitting the electric signal between fold mechanism 3 and image mechanism 4.
Additionally, in certain embodiments, as shown in Figure 7 and Figure 8, fold mechanism 3 also includes third connecting rod 35, third connecting rod
35 include the 5th connection end 351 and the 6th connection end 352, and the 5th connection end 351 and the 6th connection end 352 are connecting rod connection
End, is respectively used to connection first connecting rod 31 and third connecting rod 35 and connection third connecting rod 35 and second connecting rod 32, wherein, the 5th
The chain connection of 351 and second connection end of connection end 312, the 6th connection end 352 and the chain connection of the 3rd connection end 322, then, and first
Connecting rod 31 drives third connecting rod 35 to rotate, and third connecting rod 35 drives second connecting rod 32 to rotate.Additionally, its specific chain connection side
Formula can refer to the chain connection mode of the second connection end 312 and the 3rd connection end 322 shown in Fig. 5, just no longer describe in detail herein.
In the present embodiment, by adding third connecting rod 35 between first connecting rod 31 and second connecting rod 32, the 3rd can simultaneously be rotated
, to shorten time of contraction (or expansion) fold mechanism 3, (or decentralization) shooting is packed up in lifting for connecting rod 35 and second connecting rod 32
The speed of mechanism 4.The rotation of third connecting rod 35 and second connecting rod 32 can be linkage, it is also possible to be non-linkage, this implementation
Example is not construed as limiting.When first connecting rod 31 drives third connecting rod 35 to rotate, third connecting rod 35 can also drive second connecting rod 32 to rotate,
No matter to cause fold mechanism 3 be in contraction state or deployed condition, image mechanism 4 remains vertical.
In the present embodiment, image mechanism 4 refers to the image mechanism that can arbitrarily realize pan-shot, can be single
Full-view camera, or by can 360 ° of heads of rotation carry the panoramic shooting mechanism that unidirectional camera is constituted.In this reality
Apply in example, image mechanism 4 includes：Head 43 and video capturing device 44, one end of head 43 are connected with fold mechanism 3, wherein,
In the present embodiment, one end of head 43 is provided with the second clamp 41, is snapped connection by the second clamp 41 and fold mechanism 3；
And the other end of head 43 is equipped with video capturing device 44, i.e., it is connected with video capturing device 44.In the present embodiment, image
Acquisition device 44 is used to gather image or video during unmanned plane during flying.Head 43 is used for the profit during unmanned plane during flying
When being imaged with video capturing device 44, prevent video capturing device 44 from shaking, to maintain the carrying out of its balance and stability
Work.Preferably, in order in time efficiently obtain all angles photographed scene, the video capturing device 44 can be complete
Scape camera, the full-view camera is both provided with sub- camera 441 in a plurality of directions, and all directions are obtained by being not required to rotate
Photographed scene.It is understood that the video capturing device 44 can also be the video capturing device of other forms, such as take a picture
Machine, video camera etc., the present embodiment is not construed as limiting.
In the present embodiment, head 43 can include a damping device 42, and one end and the fold mechanism 3 of damping device 42 connect
Connect, the other end of damping device 42 is connected with video capturing device 44.The shape of damping device 42 can be square or circle.Subtract
Shake device 42 can include at least two vibration damper plates and at least three shock-absorbing balls, and one is connected to by shock-absorbing ball between vibration damper plate
Rise.When being directly connected to due to shock-absorbing ball and vibration damper plate, lifting surface area is smaller, therefore can be set between shock-absorbing ball and vibration damper plate
Shock structure, connects vibration damper plate and shock-absorbing ball respectively.Shock-absorbing ball and shock structure can be made up of silica gel or rubber.By providing
Damping device 42, further increases the stability of head, can reduce head because the next frequently adjustment of shattering zone, it is ensured that
Shooting effect.
It is understood that damping device 42 can also such as increase shock insulation plate using the damping device of other forms, will
Damping device makes circular, ellipse etc. into, equally applicable in the present embodiment, repeats no more herein.
Additionally, in the case of unmanned plane is metastable, damping device 42 can be set, so as to further reduction
The weight of unmanned plane, can equally realize shooting purpose.
In certain embodiments, in order to be protected to video capturing device, can also be outside video capturing device
Transparent protective shield is set.
According to the above-mentioned technical solution, the beneficial effect of the utility model embodiment is：By using fold mechanism
To control packing up and discharging for image mechanism, the interference of undercarriage can be effectively avoided, realize glitch-free panoramic shooting, together
When, the Project Realization principle of fold mechanism is simple, workable.
It should be noted that given in specification of the present utility model and its accompanying drawing of the present utility model preferably implementing
Example, but, the utility model can be realized by many different forms, however it is not limited to the implementation described by this specification
Example, these embodiments are not as the extra limitation to the utility model content, there is provided the purpose of these embodiments is made to this reality
Understanding with new disclosure is more thorough comprehensive.Also, above-mentioned each technical characteristic continues to be mutually combined, formed not upper
The various embodiments that face is enumerated, are accordingly to be regarded as the scope of the utility model specification record；Further, to ordinary skill
For personnel, can according to the above description be improved or be converted, and all these modifications and variations should all belong to this practicality newly
The protection domain of type appended claims.
Claims (13)
1. a kind of unmanned plane, it is characterised in that including：
Fuselage (1)；
Undercarriage (2), is arranged at the bottom of the fuselage (1), and the undercarriage (2) is with the bottom for connecting the fuselage (1)
Connection end (21) and the bottom away from the fuselage (1) ground terminal (22)；
Fold mechanism (3), is arranged at the bottom of the fuselage (1)；And,
Image mechanism (4), is installed on the one end of the fold mechanism (3) away from the fuselage (1)；
When the fold mechanism (3) is under contraction state, the distance of the image mechanism (4) and the bottom of the fuselage (1)
Less than the distance of the ground terminal (22) and the bottom of the fuselage (1)；When the fold mechanism (3) is under deployed condition,
The image mechanism (4) is more than the bottom of the ground terminal (22) and the fuselage (1) with the distance of the bottom of the fuselage (1)
Distance.
2. unmanned plane according to claim 1, it is characterised in that the fold mechanism (3) includes：First connecting rod (31) and
Second connecting rod (32), the first connecting rod (31) includes the first connection end and the second connection end, and the second connecting rod (32) includes
3rd connection end and the 4th connection end；First connection end is connected with the fuselage (1), second connection end and described
Three connection end chain connections, the 4th connection end is connected with the image mechanism (4).
3. unmanned plane according to claim 2, it is characterised in that second connection end is provided with for driving described
The drive device (3121) that two connecting rods (32) are rotated.
4. unmanned plane according to claim 3, it is characterised in that
The drive device (3121) includes rotating shaft (3121a) and first gear (3121b), the first gear (3121b) with
The rotating shaft (3121a) is fixedly connected；
3rd connection end is provided with second gear (3221)；
The first gear (3121b) is engaged with the second gear (3221)；
The rotating shaft (3121a) connects second connection end and the 3rd connection end, when the rotating shaft (3121a) is rotated, leads to
Crossing the first gear (3121b) drives the second gear (3221) to rotate, so that the second connecting rod (32) is relatively described
First connecting rod (31) is rotated.
5. unmanned plane according to claim 3, it is characterised in that
The first cable (331) is provided with the first connecting rod (31), first cable (331) includes the first termination and second
Termination；Electric supply installation in first termination and the fuselage (1) is electrically connected with, second termination and the drive device
(3121) connect；
The second cable (332) is provided with the second connecting rod (32), second cable (332) includes the 3rd termination and the 4th
Termination；
Second connection end and the 3rd connection end are provided with relative sets of vias (34), and the 3rd termination is through described
Sets of vias (34) is electrically connected with second termination, and the 4th termination is connected with the image mechanism (4).
6. unmanned plane according to claim 5, it is characterised in that the bottom of the fuselage (1) is provided with the first draw-in groove
(11), first connection end is provided with the first clamp (3111), first clamp (3111) and first draw-in groove (11)
It is detachably connected.
7. unmanned plane according to claim 6, it is characterised in that first draw-in groove (11) and first clamp
(3111) side for abutting against is provided with the first metal clips group (51), the first metal clips group (51) and the described first electricity
First termination of cable (331) is electrically connected with.
8. unmanned plane according to claim 5, it is characterised in that the 4th connection end is provided with the second draw-in groove
(3211) one end that, the image mechanism (4) is connected with the 4th connection end is provided with the second clamp (41), second card
Plate (41) is detachably connected with second draw-in groove (3211).
9. unmanned plane according to claim 8, it is characterised in that second draw-in groove (3211) and second clamp
(41) side for abutting against is provided with the second metal clips group (52), the second metal clips group (52) and second cable
(332) the 4th termination is electrically connected with.
10. the unmanned plane according to claim any one of 2-9, it is characterised in that the fold mechanism also includes：3rd connects
Bar (35), the third connecting rod (35) includes the 5th connection end and the 6th connection end, and the 5th connection end connects with described second
Connect end chain connection, the 6th connection end and the 3rd connection end chain connection；The first connecting rod (31) drives described
Third connecting rod (35) is rotated, and the third connecting rod (35) drives the second connecting rod (32) to rotate.
11. unmanned plane according to claim any one of 1-9, it is characterised in that the image mechanism (4) includes：Head
(43) and video capturing device (44), one end of the head (43) is connected with the fold mechanism (3), the head (43)
The other end is connected with the video capturing device (44).
12. unmanned planes according to claim 11, it is characterised in that the head (43) includes damping device (42), institute
The one end for stating damping device (42) is connected with the fold mechanism (3), the other end and the image of the damping device (42)
Acquisition device (44) is connected.
13. unmanned plane according to claim any one of 1-9, it is characterised in that the fold mechanism (3) is arranged at described
The middle position of the bottom of fuselage (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621325952.1U CN206273683U (en) | 2016-12-05 | 2016-12-05 | A kind of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621325952.1U CN206273683U (en) | 2016-12-05 | 2016-12-05 | A kind of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206273683U true CN206273683U (en) | 2017-06-23 |
Family
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| CN201621325952.1U Active CN206273683U (en) | 2016-12-05 | 2016-12-05 | A kind of unmanned plane |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107226214A (en) * | 2017-06-26 | 2017-10-03 | 中国电建集团成都勘测设计研究院有限公司 | Panorama camera mounting structure on a kind of unmanned plane |
| CN109969420A (en) * | 2017-12-28 | 2019-07-05 | 昆山优尼电能运动科技有限公司 | A kind of folding holder of servo driving |
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2016
- 2016-12-05 CN CN201621325952.1U patent/CN206273683U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107226214A (en) * | 2017-06-26 | 2017-10-03 | 中国电建集团成都勘测设计研究院有限公司 | Panorama camera mounting structure on a kind of unmanned plane |
| CN109969420A (en) * | 2017-12-28 | 2019-07-05 | 昆山优尼电能运动科技有限公司 | A kind of folding holder of servo driving |
| CN109969420B (en) * | 2017-12-28 | 2024-02-09 | 昆山合朗航空科技有限公司 | Steering engine driven folding cradle head |
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Address after: 518055 Guangdong city of Shenzhen province Nanshan District Xili Street Xueyuan Road No. 1001 Chi Yuen Building 9 layer B1 Patentee after: Shenzhen daotong intelligent Aviation Technology Co.,Ltd. Address before: 518055 Guangdong city of Shenzhen province Nanshan District Xili Street Xueyuan Road No. 1001 Chi Yuen Building 9 layer B1 Patentee before: AUTEL ROBOTICS Co.,Ltd. |