CN206694765U - A kind of unmanned plane of the load component and carry load component - Google Patents
A kind of unmanned plane of the load component and carry load component Download PDFInfo
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- CN206694765U CN206694765U CN201621047561.8U CN201621047561U CN206694765U CN 206694765 U CN206694765 U CN 206694765U CN 201621047561 U CN201621047561 U CN 201621047561U CN 206694765 U CN206694765 U CN 206694765U
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- unmanned plane
- foot stool
- load
- main body
- support arm
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Abstract
The utility model discloses the unmanned plane of a kind of load component and the carry load component, the load component includes：Head and foot stool, the head include the second installation portion and head main body, and second installation portion is used to coordinate with the carry main body of load component described in carry, realizes the connection between the head and the carry main body；The head main body is used for dead load, and the unmanned plane foot stool is fixed on the load component, and outside the loaded work piece angle.By the above-mentioned means, during loaded work piece, foot stool will not block load all the time, and then realize 360 ° of unobstructed work, and foot rest structure is simple, it is not necessary to which extra power driving is packed up, so as to reduce the weight of unmanned plane.
Description
Technical field
Unmanned plane field is the utility model is related to, more particularly to the nothing of a kind of load component and the carry load component
It is man-machine.
Background technology
Unmanned plane is usually constructed with undercarriage at present, and unmanned plane can be supported at ground, and nobody can be protected in landing
Machine is not hit.
The undercarriage of usual unmanned plane is located at the lower section of unmanned aerial vehicle body, is fixed on unmanned aerial vehicle body, and use extendible
Structure, it can be packed up when winged unmanned plane is in state of flight, get out of the way the space and visual angle below fuselage, turn head camera
It will not be blocked when dynamic, realize the operation of taking photo by plane of wide-angle.The undercarriage of this extendible needs to use a series of mechanism
(such as linkage, rack-and-pinion, linear electric motors etc.), structure is complex, and weight is larger, and needs to provide extra power
Folding and unfolding can be realized, influences the performance of unmanned plane.
Utility model content
The utility model is mainly solving the technical problems that provide a kind of nothing of load component and carry load component
It is man-machine, unmanned plane is can solve the problem that to avoid undercarriage from influenceing the problem of having to increase somewhat complex design of taking photo by plane.
In order to solve the above problems, the technical scheme that the application uses is：A kind of unmanned plane is provided, including：Nobody
Owner's body, head and multiple unmanned plane foot stools；The unmanned plane bottom part body is provided with the first installation portion, and the head includes the
Two installation portions and head main body, second installation portion of the head are matched somebody with somebody with first installation portion of the unmanned plane main body
Close, realize the connection between the head and the unmanned plane main body；The head main body is used for dead load, the unmanned plane
Foot stool is fixed on the head main body, and outside the operating angle of the load.
Wherein, the head includes course bracing strut, roll bracing strut and the pitching bracing strut being rotatably connected successively,
The load is connected to the pitching bracing strut；The unmanned plane foot stool is connected to the course bracing strut.
Wherein, the course bracing strut includes the first vertical arm and the switching arm extended from first vertical arm, described
Roll bracing strut is rotatably coupled with the switching arm, and the multiple unmanned plane foot stool is all connected to first vertical arm.
Wherein, the unmanned plane foot stool quantity be at least three, each unmanned plane foot stool include first support arm and
First vertical arm or second transverse arm, the first support arm other end are fixed in second support arm, described first support arm one end
It is relatively fixed with described second support arm one end.
Wherein, the unmanned plane foot stool quantity is four.
Wherein, the unmanned plane foot stool includes the buffering foot pad for being arranged at the second support arm other end, the buffering pin
Pad for buffering the impulse force between the unmanned plane and level point.
Wherein, the unmanned plane foot stool includes adaptor, and the first support arm and the second support arm pass through the switching
Part is end-to-end to be relatively fixed.
Wherein, the adaptor is bending member, and the end face at the bending member both ends is equipped with jointing holes, the first support arm
Insert the jointing holes at the bending member both ends in a manner of detachable respectively with each one end of the second support arm.
Wherein, the load is picture pick-up device, and the unmanned plane foot stool is located at the maximum shooting angle of the picture pick-up device
Outside, and follow the picture pick-up device to rotate and rotate.
In order to solve the above problems, another technical scheme that the application uses is：A kind of load component is provided, its feature
It is, including：Head and foot stool, the head include head main body and the second installation portion, and second installation portion is used for
Coordinate with the carry main body of load component described in carry, realize the connection between the head and the carry main body；The cloud
Platform main body is used for dead load, and the foot stool is fixed on the head main body, and positioned at the load factor operating angle it
Outside.
Wherein, the head main body includes course bracing strut, roll bracing strut and the pitch axis being rotatably connected successively
Support, the load are connected to the pitching bracing strut；The foot stool is connected to the course bracing strut.
Wherein, the course bracing strut includes the first vertical arm, the first transverse arm and the second vertical arm；Second installation position
In the first vertical arm upper end, the first vertical arm lower end is connected with described first transverse arm one end, the first transverse arm other end
It is connected with the second vertical arm upper end, the second vertical arm lower end and the roll bracing strut；All foot stools are both secured to
First vertical arm.
Wherein, the unmanned plane foot stool quantity is at least three, and each foot stool includes first support arm and second
First vertical arm or second transverse arm are fixed in arm, described first support arm one end, the first support arm other end with it is described
Second support arm one end is relatively fixed.
Wherein, the foot stool quantity is four.
Wherein, the foot stool includes the buffering foot pad for being arranged at the second support arm other end.
Wherein, the unmanned plane foot stool includes adaptor, and the first support arm and the second support arm pass through the switching
Part is end-to-end to be relatively fixed.
Wherein, the adaptor is bending member, and the end face at the bending member both ends is equipped with jointing holes, the first support arm
Insert the jointing holes at the bending member both ends in a manner of detachable respectively with each one end of the second support arm.
Wherein, the load is picture pick-up device, and the foot stool is located at outside the maximum shooting angle of the picture pick-up device, and
The picture pick-up device is followed to rotate and rotate.
The beneficial effect of the application is：The situation of prior art is different from, the application is by the way that unmanned plane foot stool is fixed on
The head main body of unmanned plane, and foot stool is positioned at being fixed on outside the operating angle of the load in head main body, so that pin
Frame can will not block load with head body rotation, and then can realize 360 ° of unobstructed work.
Further, unmanned plane foot stool can be designed as to non-extendible structure, it is not necessary to which extra power drives, so as to reduce nothing
Man-machine weight.
Brief description of the drawings
Fig. 1 is the structural representation of the utility model load component first embodiment；
Fig. 2 is the structural representation of the utility model load component second embodiment；
Fig. 3 is the structural representation of the embodiment of the utility model load component the 3rd；
Fig. 4 is the structural representation of the embodiment of the utility model unmanned plane one.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out
Clearly and completely describing, it is clear that described embodiment is only part of the embodiment of the present utility model, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment obtained, belong to the scope of the utility model protection.
Referring to Fig. 1, Fig. 1 is the structural representation of the first embodiment of the application load component.As shown in figure 1, this
The load component of application includes：Head and foot stool 13, the head includes the installation portion 11 of head main body 12 and second, described
Second installation portion 11 is used to coordinate with the carry main body of load component described in carry, realize the head and the carry main body it
Between connection, the head main body is used for dead load, and the foot stool 13 is fixed on the head main body 12, and positioned at described negative
Outside the operating angle for loading with load.In the present embodiment, the load component can carry on unmanned plane.
Specifically, head is located at the lower section of unmanned plane main body, and the second installation portion 11 of head is fixed on head main body 12, can
So that the other modes such as bolt thread, pivot joint and unmanned owner are installed or used with unmanned plane main body using snap
Body is installed, and is not specifically limited herein.Head after installation can rotate relative to unmanned plane main body, such as around unmanned plane main body Z
Axle and relative to unmanned plane main body rotate.
Head main body 12 is used for dead load, and unmanned plane foot stool 13 is fixed on head main body 12, and is located at loaded work piece angle
Outside degree.
Wherein, load can be the capture apparatus such as video camera, mobile phone or launch the detecting devices of infrared light even
The lighting apparatus such as torch.In the presence of a maximum functional angle about light, electric transmitting/reception during loaded work piece, different loads
Maximum functional angle may be different, and the position of unmanned plane foot stool 13 is set with specific reference to the load that head main body is fixed, herein not
It is specifically limited.
In an application examples, load is picture pick-up device, and unmanned plane foot stool 13 is located at the maximum shooting angle of picture pick-up device
Outside, and following picture pick-up device to rotate and rotate so that the camera lens of picture pick-up device is not at least during operation always by unmanned plane
Foot stool 13 blocks, so as to realize 360 ° of unobstructed shootings.
Fig. 1 is further regarded to, head main body 12 includes course bracing strut 121, the roll bracing strut being rotatably connected successively
122 and pitching bracing strut 123, load is connected to pitching bracing strut 123；Unmanned plane foot stool 13 is connected to course bracing strut 121.
Wherein, the vertical arm 1211 of course bracing strut 121 first, the first transverse arm 1212 and the roll bracing strut of the second vertical arm 1213
122；Second installation portion 11 is located at the upper end of the first vertical arm 1211, and the lower end of the first vertical arm 1211 is connected with the one end of the first transverse arm 1212,
The other end of first transverse arm 1212 is connected with the upper end of the second vertical arm 1213, and the lower end of the second vertical arm 1213 is connected with roll bracing strut 122；
All unmanned plane foot stools 13 are both secured to the first vertical arm 1211.
Specifically, the first vertical arm 1211 can rotate according to the control of user or unmanned plane main body around course axle, drive solid
Unmanned plane foot stool 13 due to the first vertical arm 1211 rotates, while can drive the first transverse arm for being connected to the first vertical arm 1211
1212, then the second vertical arm 1213 for being connected to the first transverse arm 1212 is driven, and then drive the roll for being connected to the second vertical arm 1213
Bracing strut 122, then drives the pitching bracing strut 123 for being connected to roll bracing strut 122, and final drive is fixed on pitching bracing strut
123 load so that load and unmanned plane foot stool 13 rotate together, and because load and unmanned plane foot stool 13 are all by first
Vertical arm 1211 drives rotation, and angle, direction and the speed of rotation are all identical with the first vertical arm 1211, therefore unmanned plane foot stool 13 1
It is straight to be located at outside the maximum functional angle of load, do not interfere with the normal work of load.
Similarly, roll bracing strut 122 can also rotate according to the control of user or unmanned plane main body around X-axis, final band
The dynamic load rotation for being fixed on pitching bracing strut 123；Pitching bracing strut 123 can also be according to the control of user or unmanned plane main body
Rotated around Y-axis, and then cause the load rotation for being fixed on pitching bracing strut 123；Likewise, due to the position always of unmanned plane foot stool 13
Outside the maximum functional angle of load, therefore load the normal work that unmanned plane foot stool 13 when rotating does not interfere with load.
As shown in figure 1, in present embodiment, the first vertical arm 1211 can by the way of screw bolt with the first transverse arm
1212 are relatively fixed, or using other modes such as welding.And in other embodiments, the first vertical arm 1211 and the first transverse arm
1212 connections, and can be slided on the first transverse arm 1212.
In an application examples, the second vertical arm 1213 connects the first transverse arm 1212, two relative sides of the first transverse arm 1212
Face is provided with two tracks, and the upper end of the second vertical arm 1213 is provided with a through hole, be provided with the inside of through hole with the side of the first transverse arm 1212
Orbit Matching guide so that the second vertical arm 1213 can sliding axially along the first transverse arm 1212.Certainly, should at other
In use-case, the upper end of the second vertical arm 1213 can be provided with the miscellaneous parts such as the annulus that inner side matches with the radial section of the first transverse arm 1212
Realization be relatively fixed with the first transverse arm 1212 and can sliding axially along the first transverse arm 1212, or the second vertical arm 1213 can also
First transverse arm 1212 is fixed on using modes such as welding.
In above-mentioned application examples, the second vertical arm 1213 is provided with a battery case, and inside can install battery, available for for cloud
The running of platform provides power supply, and charge port is provided with the second vertical arm 1213, can be that battery charges.In other application example, the
Two vertical arm 1213 may not be battery case, can also not have charge port.
In the present embodiment, roll bracing strut 122 is the U-shaped arm of a connection and the second vertical arm 1213, pitching bracing strut
123 include rotating shaft 1231 and base 1232.Wherein, the U-shaped opening both ends of U-shaped arm connect two of pitching bracing strut 123 respectively
Rotating shaft 1231, base 1232 are connected between two rotating shafts 1231, for placement and dead load, and load is located at U-shaped arm
U type slot in.
In other embodiments, course bracing strut 121 can not include the first transverse arm 1212, now, the second installation portion
11 are located at the upper end of the first vertical arm 1211, and the lower end of the first vertical arm 1211 is connected with the one end of the second vertical arm 1213, and the second vertical arm 1213 is another
One end is connected with roll bracing strut 122；Or load can directly be suspended to the lower end of the first vertical arm 1211.
Specifically, the one end of the second vertical arm 1213 can be relatively fixed using welding manner with the lower end of the first vertical arm 1211, the
The one end of two vertical arm 1213 can also be provided with screwed hole in inner side, be installed with the bolt that the lower end of the first vertical arm 1211 is provided with, so as to real
Now it is relatively fixed, certain one end of second vertical arm 1213 can also be relatively fixed using other modes with the lower end of the first vertical arm 1211,
It is not specifically limited herein.
As shown in figure 1, in present embodiment, the quantity of unmanned plane foot stool 13 is three, and each unmanned plane foot stool 13 wraps
First support arm 131 and second support arm 132 are included, the first vertical arm 121, the other end of first support arm 131 are fixed in the one end of first support arm 131
It is relatively fixed with the one end of second support arm 132.
Specifically, first support arm 131 can be fixed on the first vertical arm 1211 or first by the way of welding
The one end of arm 131 is provided with screw thread, and rotation is installed in the screwed hole in the outside of the first vertical arm 1211, can also be other fixed forms,
It is not specifically limited herein.The other end of first support arm 131 can also use similar method and the one end of second support arm 132 relative solid
It is fixed.
In present embodiment, positioned at load rear a unmanned plane foot stool 13 second support arm 132 directly with head master
One end of the first transverse arm 122 of body 12 is relatively fixed.In other embodiments, the unmanned plane foot stool 13 positioned at load rear also may be used
The first vertical arm 1211, the other end of first support arm 131 and second support arm 132 1 are fixed on or using the one end of first support arm 131
Hold relatively-stationary mode.
Wherein, first support arm 131 and second support arm 132 can use carbon fiber pipe, can also use other are in light weight,
The high material of intensity and toughness, is not specifically limited herein.
Fig. 1 is further regarded to, unmanned plane foot stool 13 further comprises the buffering foot pad for being arranged at the other end of second support arm 132
133, buffering foot pad 133 is used to buffer the impulse force between unmanned plane and level point.
Wherein, buffering foot pad 133 can use the soft wear-resistant material such as plug or wear-resisting foam, and can periodically more
Change, effectively buffer the impulse force between unmanned plane and level point, play a part of protecting unmanned plane.
In above-mentioned embodiment, unmanned plane foot stool is fixed on unmanned machine head, and outside the operating angle of load,
Load can be followed to rotate and rotate so that unmanned plane foot stool will not block loaded work piece, and then realize 360 ° it is unobstructed
Work, and unmanned plane foot rest structure is simple, it is not necessary to which extra power driving is packed up, and can use that in light weight, intensity and toughness is high
Material, so as to reduce the weight of unmanned plane.
Referring to Fig. 2, Fig. 2 is the structural representation of the head second embodiment of the application unmanned plane.Fig. 2 and Fig. 1 knots
Structure is similar, and here is omitted, and difference is that unmanned plane foot stool 23 further comprises adaptor 234, the He of first support arm 231
Second support arm 232 is relatively fixed by the way that adaptor 234 is end-to-end.
Specifically, adaptor 234 is bending member, and the end face at bending member both ends is equipped with jointing holes, first support arm 231 and
The jointing holes at bending member both ends are inserted in two support arms, 232 each one end in a manner of detachable respectively.Wherein, adaptor 234 can be adopted
With plastic cement material or the material of other lighter in weight, dismantle, install and change so that unmanned plane foot stool 23 can facilitate.
In above-mentioned embodiment, the quantity of unmanned plane foot stool is three, and in other embodiments, unmanned plane foot stool
Quantity can be four or more.
Referring particularly to Fig. 3, Fig. 3 is the structural representation of the embodiment of head the 3rd of the application unmanned plane.Fig. 3 and Fig. 2
Structure is similar, and here is omitted, and difference is that the quantity of unmanned plane foot stool 33 is four.
Wherein, the number of unmanned plane foot stool 33 is four, and workspace in front of fixed load in head main body 32
Outside domain, i.e., the angle between two unmanned plane foot stools 33 of load front both sides is more than the operating angle of load.For example, load
It is video camera, a maximum shooting angle be present in video camera, therefore, two unmanned plane foot stools 33 positioned at both sides in front of video camera
Between angle be more than the maximum shooting angle of video camera, the normal photographing of video camera could not be blocked.
Course bracing strut (figure do not mark) include the first vertical arm and and the switching arm extended from first vertical arm, it is described
Roll bracing strut is rotatably coupled with the switching arm.In the present embodiment, the battery is installed in switching arm, when load is pacified
During loaded in the head main body 32, the switching arm is located at the rear of the load.Four unmanned plane foot stools 33 are located at two-by-two
The both sides of the load.In the present embodiment, symmetrical shaft position of the switching arm positioned at the unmanned plane foot stool 33 two-by-two.
The unmanned plane foot stool 33 is provided separately with the Change-over frame, so as to ensure that the unmanned plane foot stool 33 is installed and more
The convenience changed, and suffered vibrations when the foot stool contacts to earth will not be directly delivered to Change-over frame, ensure that and held on Change-over frame
The element of load, such as battery, stability, and then avoid accident power-off, ensure that the stable operation of unmanned plane.
In addition, the unmanned plane foot stool 33 and the Change-over frame are provided separately, the vertical arm of Change-over frame will not be hindered along transverse arm
Slip or position adjustment, unmanned plane foot stool 33 and Change-over frame activity will not be caused to cause to interfere.
In addition, the unmanned plane foot stool 33 is distributed in load both sides, symmetrical structure further ensures stability, reduced
Load the vibrations being subject to.And the support strength and stability of multiple unmanned machine supports 33 are further enhanced.
In present embodiment, the quantity of unmanned plane foot stool is four, and in other embodiments, the number of unmanned plane foot stool
Amount can be five, six, seven, etc. it is even more more, as long as making the no unmanned plane foot stool in load front block its normal work
Work.And the switching arm with the course bracing strut is provided separately.
Referring to Fig. 4, Fig. 4 is the structural representation of the embodiment of the application unmanned plane one.As shown in figure 4, the application without
It is man-machine including：Unmanned plane main body 41, head 42 and unmanned plane foot stool 43；Wherein, the bottom of unmanned plane main body 41 is provided with the first peace
Dress portion 411, head 42 include the second installation portion 421 and head main body 422, the second installation portion 421 of head 42 and unmanned owner
First installation portion 411 of body 41 coordinates, and realizes the connection between head 42 and unmanned plane main body 41；Head main body 422 is used for solid
Fixed load, unmanned plane foot stool 43 are fixed on head main body 422, and outside loaded work piece angle.
Specifically, unmanned plane main body 41 is multiaxis airframe structure, i.e., multiple axles, each axle at least one are provided with fuselage
Individual propeller, the bottom of unmanned plane main body 41 are provided with the first installation portion 411, installed with the second installation portion 421 of head 42, realize
Connection between head 42 and unmanned plane main body 41.Head after installation can rotate relative to unmanned plane main body, such as around nobody
Owner's body Z axis and relative to unmanned plane main body rotate.
Wherein, the first installation portion 411 can be installed with the second installation portion 421 by the way of buckle, can also be adopted
Installed, be not specifically limited herein in other ways.
As shown in figure 4, in present embodiment, unmanned machine head 42 and unmanned plane foot stool 43 use the cloud of the application unmanned plane
The structure of the embodiment of platform the 3rd, is not repeated herein.Certainly, in other embodiments, unmanned machine head 42 and unmanned plane
Foot stool 43 can be not repeated herein using one kind in the head first or second embodiment of the application unmanned plane.
Course bracing strut (figure do not mark) include the first vertical arm and and the switching arm extended from first vertical arm, it is described
Roll bracing strut is rotatably coupled with the switching arm.In the present embodiment, the battery is installed in switching arm, when load is pacified
During loaded in the head main body 422, the switching arm is located at the rear of the load.Four unmanned plane foot stools 43 are located at two-by-two
The both sides of the load.In the present embodiment, symmetrical shaft position of the switching arm positioned at the unmanned plane foot stool 43 two-by-two.Its
Described in the direction that loads it is consistent with the direction of the head of the unmanned plane, first vertical arm is located at the tail side of the aircraft
To.
The unmanned plane foot stool 43 is provided separately with the Change-over frame, so as to ensure that the unmanned plane foot stool 43 is installed and more
The convenience changed, and the vibrations suffered when unmanned plane lands of the foot stool 43 will not be directly delivered to Change-over frame, ensure that
The element carried on Change-over frame, such as battery, stability, and then avoid accident power-off, ensure that the stable operation of unmanned plane.
In addition, the unmanned plane foot stool 43 and the Change-over frame are provided separately, the vertical arm of Change-over frame will not be hindered along transverse arm
Slip or position adjustment, unmanned plane foot stool 43 and Change-over frame activity will not be caused to cause to interfere.
In addition, the unmanned plane foot stool 43 is distributed in load both sides, symmetrical structure further ensures stability, reduced
Load the vibrations being subject to.And the support strength and stability of multiple unmanned machine supports 43 are further enhanced.
The unmanned plane of the application is located at by the way that unmanned plane foot stool is fixed on into head main body and is fixed on the negative of head main body
Outside the maximum functional angle of load, and the rotation of load can be followed and rotated, so that during loaded work piece, unmanned plane
Foot stool will not block load all the time, and then realize 360 ° of unobstructed work, and unmanned plane foot rest structure is simple, it is not necessary to extra
Power drive is packed up, and can use material in light weight, intensity and toughness is high, so as to reduce the weight of unmanned plane.
Presently filed embodiment is the foregoing is only, not thereby limits the scope of the claims of the present utility model, every profit
The equivalent structure or equivalent flow conversion made with present specification and accompanying drawing content, or directly or indirectly it is used in other phases
The technical field of pass, is similarly included in the scope of patent protection of the application.
Embodiment of the present utility model is the foregoing is only, not thereby limits the scope of the claims of the present utility model, it is all
It is the equivalent structure or equivalent flow conversion made using the utility model specification and accompanying drawing content, or directly or indirectly uses
In other related technical areas, similarly it is included in scope of patent protection of the present utility model.
Claims (18)
- A kind of 1. unmanned plane, it is characterised in that including：Unmanned plane main body, head and multiple unmanned plane foot stools；The unmanned plane bottom part body is provided with the first installation portion, and the head includes the second installation portion and head main body, the cloud Second installation portion of platform and first installation portion of the unmanned plane main body coordinate, realize the head with it is described nobody The connection of owner's body；The head main body is used for dead load, and the unmanned plane foot stool is fixed on the head main body, and is located at the load Operating angle outside.
- 2. unmanned plane according to claim 1, it is characterised in thatThe head includes course bracing strut, roll bracing strut and the pitching bracing strut being rotatably connected successively, the load It is connected to the pitching bracing strut；The unmanned plane foot stool is connected to the course bracing strut.
- 3. unmanned plane according to claim 2, it is characterised in thatThe course bracing strut includes the first vertical arm and the switching arm extended from first vertical arm, the roll bracing strut It is rotatably coupled with the switching arm, the multiple unmanned plane foot stool is all connected to first vertical arm.
- 4. unmanned plane according to claim 3, it is characterised in thatThe unmanned plane foot stool quantity is at least three, and each unmanned plane foot stool includes first support arm and second support arm, The course bracing strut is fixed in described first support arm one end, and the first support arm other end connects with described second support arm one end Connect.
- 5. unmanned plane according to claim 4, it is characterised in thatThe unmanned plane foot stool quantity is four.
- 6. unmanned plane according to claim 4, it is characterised in thatThe unmanned plane foot stool includes the buffering foot pad for being arranged at the second support arm other end, and the buffering foot pad is used to buffer Impulse force between the unmanned plane and level point.
- 7. unmanned plane according to claim 4, it is characterised in thatThe unmanned plane foot stool includes adaptor, the first support arm and the second support arm and passes through the end-to-end phase of the adaptor To fixation.
- 8. unmanned plane according to claim 7, it is characterised in thatThe adaptor is bending member, and the end face at the bending member both ends is equipped with jointing holes, the first support arm and described The jointing holes at the bending member both ends are inserted in each one end of two support arms in a manner of detachable respectively.
- 9. according to the unmanned plane described in claims 1 to 3,5 to 8 any one, it is characterised in thatThe load is picture pick-up device, and the unmanned plane foot stool is located at outside the maximum shooting angle of the picture pick-up device, and with Rotate and rotate with the picture pick-up device.
- A kind of 10. load component, it is characterised in that including：Head and foot stool, the head include head main body and the second installation portion, and second installation portion is used for and carry The carry main body of the load component coordinates, and realizes the connection between the head and the carry main body；The head main body is used for dead load, and the foot stool is fixed on the head main body, and positioned at the work of the load Outside angle.
- 11. load component according to claim 10, it is characterised in thatThe head main body includes course bracing strut, roll bracing strut and the pitching bracing strut being rotatably connected successively, described Load is connected to the pitching bracing strut；The foot stool is connected to the course bracing strut.
- 12. load component according to claim 11, it is characterised in that the course bracing strut include the first vertical arm and The switching arm extended from first vertical arm, the roll bracing strut are rotatably coupled with the switching arm, all described Foot stool is all connected to first vertical arm.
- 13. load component according to claim 12, it is characterised in thatThe foot stool quantity is at least three, and each foot stool includes first support arm and second support arm, the first support arm First vertical arm is fixed in one end, and the first support arm other end is relatively fixed with described second support arm one end.
- 14. load component according to claim 13, it is characterised in thatThe foot stool quantity is four.
- 15. load component according to claim 13, it is characterised in thatThe foot stool includes the buffering foot pad for being arranged at the second support arm other end.
- 16. load component according to claim 13, it is characterised in thatIt is end-to-end relatively solid by the adaptor that the foot stool includes adaptor, the first support arm and the second support arm It is fixed.
- 17. load component according to claim 16, it is characterised in thatThe adaptor is bending member, and the end face at the bending member both ends is equipped with jointing holes, the first support arm and described The jointing holes at the bending member both ends are inserted in each one end of two support arms in a manner of detachable respectively.
- 18. according to the load component described in claim 10 to 12,14 to 17 any one, it is characterised in thatThe load is picture pick-up device, and the foot stool is located at outside the maximum shooting angle of the picture pick-up device, and is followed described Picture pick-up device rotates and rotated.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621047561.8U CN206694765U (en) | 2016-09-09 | 2016-09-09 | A kind of unmanned plane of the load component and carry load component |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621047561.8U CN206694765U (en) | 2016-09-09 | 2016-09-09 | A kind of unmanned plane of the load component and carry load component |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206694765U true CN206694765U (en) | 2017-12-01 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621047561.8U Expired - Fee Related CN206694765U (en) | 2016-09-09 | 2016-09-09 | A kind of unmanned plane of the load component and carry load component |
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Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106687376A (en) * | 2016-09-09 | 2017-05-17 | 深圳市大疆创新科技有限公司 | Load component and UAV equipped with load component |
| CN108528738A (en) * | 2018-03-09 | 2018-09-14 | 深圳臻迪信息技术有限公司 | Multifunctional hanging carrying platform |
| WO2019173990A1 (en) * | 2018-03-14 | 2019-09-19 | 深圳市大疆创新科技有限公司 | Mounting mechanism, landing gear, rack and unmanned aerial vehicle |
| CN110667867A (en) * | 2019-08-30 | 2020-01-10 | 南京精微迅智能科技有限公司 | Agricultural unmanned aerial vehicle mounting device |
| CN110892352A (en) * | 2018-07-27 | 2020-03-17 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle control method and device and unmanned aerial vehicle |
| CN111824440A (en) * | 2020-07-24 | 2020-10-27 | 浙江点辰航空科技有限公司 | Novel unmanned aerial vehicle |
| CN111824439A (en) * | 2020-07-24 | 2020-10-27 | 浙江点辰航空科技有限公司 | Unmanned aerial vehicle support |
| TWI721390B (en) * | 2019-01-28 | 2021-03-11 | 中光電智能機器人股份有限公司 | Monitoring system, base station and control method thereof |
| CN113060298A (en) * | 2021-03-19 | 2021-07-02 | 广州中科云图智能科技有限公司 | Unmanned aerial vehicle starlight level carries and unmanned aerial vehicle of making a video recording |
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2016
- 2016-09-09 CN CN201621047561.8U patent/CN206694765U/en not_active Expired - Fee Related
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
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| US11155344B2 (en) | 2016-09-09 | 2021-10-26 | SZ DJI Technology Co., Ltd. | Load assembly and unmanned aerial vehicle |
| CN106687376B (en) * | 2016-09-09 | 2020-03-20 | 深圳市大疆创新科技有限公司 | Load assembly and unmanned aerial vehicle mounted with same |
| CN106687376A (en) * | 2016-09-09 | 2017-05-17 | 深圳市大疆创新科技有限公司 | Load component and UAV equipped with load component |
| CN108528738A (en) * | 2018-03-09 | 2018-09-14 | 深圳臻迪信息技术有限公司 | Multifunctional hanging carrying platform |
| WO2019173990A1 (en) * | 2018-03-14 | 2019-09-19 | 深圳市大疆创新科技有限公司 | Mounting mechanism, landing gear, rack and unmanned aerial vehicle |
| CN110892352A (en) * | 2018-07-27 | 2020-03-17 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle control method and device and unmanned aerial vehicle |
| US11814191B2 (en) | 2019-01-28 | 2023-11-14 | Coretronic Intelligent Robotics Corporation | Monitoring system, base station and control method thereof |
| TWI721390B (en) * | 2019-01-28 | 2021-03-11 | 中光電智能機器人股份有限公司 | Monitoring system, base station and control method thereof |
| CN110667867A (en) * | 2019-08-30 | 2020-01-10 | 南京精微迅智能科技有限公司 | Agricultural unmanned aerial vehicle mounting device |
| CN111824440A (en) * | 2020-07-24 | 2020-10-27 | 浙江点辰航空科技有限公司 | Novel unmanned aerial vehicle |
| CN111824440B (en) * | 2020-07-24 | 2023-07-28 | 广州力泰能源技术有限公司 | Novel unmanned aerial vehicle |
| CN111824439A (en) * | 2020-07-24 | 2020-10-27 | 浙江点辰航空科技有限公司 | Unmanned aerial vehicle support |
| CN113060298A (en) * | 2021-03-19 | 2021-07-02 | 广州中科云图智能科技有限公司 | Unmanned aerial vehicle starlight level carries and unmanned aerial vehicle of making a video recording |
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