CN206202668U - Aircraft and its foot rest structure - Google Patents
Aircraft and its foot rest structure Download PDFInfo
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- CN206202668U CN206202668U CN201621273108.9U CN201621273108U CN206202668U CN 206202668 U CN206202668 U CN 206202668U CN 201621273108 U CN201621273108 U CN 201621273108U CN 206202668 U CN206202668 U CN 206202668U
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- aircraft
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- rest structure
- foot stool
- foot rest
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Abstract
The disclosure is directed to a kind of aircraft and its foot rest structure, the foot rest structure can include：Some foot stools, some foot stools are respectively arranged at the default rigging position of aircraft body bottom；Wherein, at least one foot stool is provided with the image collection assembly of the aircraft.By the technical scheme of the disclosure, the foot rest structure of aircraft and the space layout of aircraft body can be optimized, additionally it is possible to optimize the view data that image collection assembly is collected.
Description
Technical field
This disclosure relates to vehicle technology field, more particularly to a kind of aircraft and its foot rest structure.
Background technology
Such as many isostructural unmanned vehicles of rotor, multiple necks such as be widely used in taking photo by plane, explored, rescue
Domain.In the related art, the first-class image collection assembly of shooting is hung by the bottom of aircraft body, allows it in flight
Realize that IMAQ is operated in the flight course of device.
But, when image collection assembly to be hung on the bottom of aircraft body, still suffer from some problem demanding prompt solutions.
Such as, because the bottom of aircraft body needs to set foot rest structure, it is easy to cause to block the camera lens of image collection assembly,
The image frame that influence is collected.
Utility model content
The disclosure provides a kind of aircraft and its foot rest structure, to solve the deficiency in correlation technique.
According to the first aspect of the embodiment of the present disclosure, there is provided a kind of foot rest structure of aircraft, including：Some foot stools, institute
State the default rigging position that some foot stools are respectively arranged at aircraft body bottom；Wherein, at least one foot stool is provided with described
The image collection assembly of aircraft.
Optionally, the camera lens of described image acquisition component is directed away from the outside of the aircraft.
Optionally, the camera lens of described image acquisition component adopts described image towards being in predetermined angle with corresponding foot stool
The camera lens picture for collecting component does not include the aircraft body and the foot rest structure.
Optionally, when the foot stool of image collection assembly is provided with the presence of multiple, the camera lens direction of multiple images acquisition component
Between match, be panoramic image data to cause the corresponding view data for collecting sliceable.
Optionally, the foot rest structure includes four foot stools, and four foot stools are arranged at aircraft body with being centrosymmetric
Bottom；Wherein, an image collection assembly is respectively equipped with each foot stool, the camera lens of the image collection assembly is directed away from described flying
The outside of row device, and the camera lens visual angle of the image collection assembly is not less than 90 °.
Optionally, at least one foot stool is provided with avoidance sensor.
Optionally, the avoidance sensor is on the foot stool comprising described image acquisition component, and the avoidance is sensed
Device is located near described image acquisition component.
Optionally, the avoidance sensor includes：Distance measuring sensor or vision sensor.
Optionally,
Described image acquisition component is fixedly installed on the foot stool, and the foot stool is fixedly attached to aircraft body bottom
Portion；
Or, described image acquisition component is fixedly installed on the foot stool, and the foot stool is rotatably connected to fly
Row device bottom part body；
Or, described image acquisition component is installed on the active segment on the foot stool, wherein the active segment can be relative to
Remaining canned paragraph realizes the rotation of predetermined angle on the foot stool, and the canned paragraph is fixedly attached to aircraft body bottom
Portion.
Optionally, also include：
Data transmission link, is arranged in the pre-set path inside the foot stool inside and aircraft body, and the number
The circuit module in described image acquisition component and aircraft body is respectively connecting to according to transmission line, described image is gathered
The view data that component is collected is transmitted to the circuit module.
According to the second aspect of the embodiment of the present disclosure, there is provided a kind of aircraft, including：
Aircraft body；
Foot rest structure as described in any in above-mentioned embodiment.
Optionally, battery connecting piece is provided with the bottom centre of the aircraft body, the battery connecting piece can be to standby
Fixation is attached with battery modules, the reserve battery module is fixed at the bottom centre of the aircraft body.
Optionally, also include：
It is connected with the image collection assembly on the foot rest structure, and the image that all image collection assemblies can be collected
Data carry out the image processing modules of splicing；Wherein, described image processing assembly is located in the aircraft body.
Optionally, also include：
For the diagram data transmission that the splicing of collect described image acquisition component or described image processing assembly is obtained
To the communication part of pre-set user equipment, the communication part is located in the aircraft body.
The technical scheme provided by this disclosed embodiment can include the following benefits：
From above-described embodiment, the disclosure is arranged on foot stool by by image collection assembly, can be by image
The reasonable Arrangement of acquisition component, makes it avoid photographing foot stool or aircraft body.Meanwhile, set by by image collection assembly
In on foot stool, the space utilization to foot stool on the one hand can be realized, the aircraft body bottom that on the other hand can amortize originally should
Region for hanging the image collection assembly, allows it to be applied to set the other functions component such as reserve battery module
Put, to lift performance of the aircraft in related fields such as continuations of the journey.
It should be appreciated that the general description of the above and detailed description hereinafter are only exemplary and explanatory, not
The disclosure can be limited.
Brief description of the drawings
Accompanying drawing herein is merged in specification and constitutes the part of this specification, shows the implementation for meeting the disclosure
Example, and it is used to explain the principle of the disclosure together with specification.
Fig. 1 is a kind of dimensional structure diagram of the aircraft in correlation technique.
Fig. 2 is a kind of dimensional structure diagram of the aircraft according to an exemplary embodiment.
Fig. 3 is the schematic diagram of the horizontal shooting angle scope of the aircraft shown in Fig. 2.
Fig. 4 is the schematic diagram of the horizontal shooting angle scope of the aircraft in correlation technique.
Fig. 5 is the dimensional structure diagram under another angle of the aircraft shown in Fig. 2.
Fig. 6 is a kind of schematic diagram that flight control is carried out to aircraft according to an exemplary embodiment.
Fig. 7 is the dimensional structure diagram of another aircraft according to an exemplary embodiment.
Specific embodiment
Here exemplary embodiment will be illustrated in detail, its example is illustrated in the accompanying drawings.Following description is related to
During accompanying drawing, unless otherwise indicated, the same numbers in different accompanying drawings represent same or analogous key element.Following exemplary embodiment
Described in implementation method do not represent all implementation methods consistent with the disclosure.Conversely, they be only with it is such as appended
The example of the consistent apparatus and method of some aspects described in detail in claims, the disclosure.
Fig. 1 is a kind of dimensional structure diagram of the aircraft in correlation technique.As shown in figure 1, being with four-axle aircraft
Example, the bottom of the aircraft body 1 ' in correlation technique is respectively arranged with foot stool 2 ' and image collection assembly 3 ', wherein foot stool 2 '
For carrying out lifting support to aircraft, and image collection assembly 3 ' is for the image collecting function such as realize taking pictures, image.
But, the image collection assembly 3 ' assembled on aircraft is generally in by the state of multiple foot stools 2 ' " encirclement ", is made
Image collection assembly 3 ' is obtained during IMAQ is performed, it is easy to foot stool 2 ' is shot into mirror, shooting picture is destroyed.
Therefore, the disclosure can solve the above-mentioned technical problem in correlation technique by improving the foot rest structure of aircraft.
It is described in detail with reference to embodiment：
Fig. 2 is a kind of dimensional structure diagram of the aircraft according to an exemplary embodiment.As shown in Fig. 2 with
As a example by four-axle aircraft, aircraft of this disclosure and its foot rest structure are described, but the technical scheme of the disclosure is not limited
In four-axle aircraft, multi-rotor aerocraft is also not restricted to.In the embodiment shown in Figure 2, the foot rest structure of aircraft includes
Some foot stools 2, some foot stools 2 are respectively arranged at the default rigging position of the bottom of aircraft body 1；Such as in fig. 2, this is pre-
If respectively positioned at four ends of spiral arm of aircraft body 1, certain disclosure is limited rigging position not to this.
Wherein, at least one foot stool 2 is provided with the image collection assembly 31 of the aircraft.Set by image collection assembly 31
It is placed in when on foot stool 2, because foot stool 2 is not by other structures " encirclement ", thus bigger horizontal shooting angle model can be obtained
Enclose.For example after carrying out abstract to the position of each foot stool 2 and image collection assembly 31 in Fig. 3, when the image collection assembly 3
Camera lens is directed away from the outside of the aircraft (such as the foot stool 2 being located in Fig. 3 at the lower section spiral arm of aircraft body 1, the pin
Frame 2 corresponding " away from the outside of aircraft " be able to can be fixed for the lower section in Fig. 3, thus the camera lens of image collection assembly 31
Towards the lower section in Fig. 3) when, the horizontal shooting angle scope being correspondingly formed even can reach about 270 °.And relatively, Fig. 4
After abstract being carried out to each foot stool 2 in correlation technique and the position of image collection assembly 31, it is seen that：Due to each foot stool 2
" encirclement " structure caused to image collection assembly 31 so that image collection assembly 31 formed horizontal shooting angle be only for about
90 °, much smaller than 270 ° of horizontal shooting angle shown in Fig. 3.
In one embodiment, based on above-mentioned bigger horizontal shooting angle scope, image collection assembly 31 can be using wide
Angle mirror head (such as beyond 90 °, even up to above-mentioned 270 ° of shooting angle) need not be carried on a shoulder pole with obtaining broader shooting picture
Heart foot stool 2 or aircraft body 1 enter mirror.
In another embodiment, image collection assembly 31 can realize the rotating operation around vertical axis, such that it is able to logical
The rotation to the image collection assembly 31 is crossed, above-mentioned bigger horizontal shooting angle scope is made full use of.For example, working as IMAQ
When the camera lens visual angle of component 31 is 90 °, it is allowed to which the image collection assembly 31 is rotated towards both sides in the horizontal direction, and per side
Rotational angle can reach 90 °, so as to make full use of above-mentioned 270 ° of horizontal shooting angle scope.Wherein it is possible to be based on following
Structure, makes image collection assembly 31 realize above-mentioned rotating operation：
A kind of structure can be：Image collection assembly 31 is fixedly installed on the foot stool 2, the foot stool 2 it is rotatable (for example around
Vertical axis rotate) be connected to the bottom of aircraft body 1.So, by controlling the unitary rotation of foot stool 2, you can band motion video
Acquisition component 31 rotates therewith.
Another structure can be：Image collection assembly 31 is fixedly installed in the active segment on the foot stool 2, and the active segment can
Relative to the rotation (such as being rotated around vertical axis) that remaining canned paragraph on the foot stool 2 realizes predetermined angle, and the canned paragraph
It is fixedly attached to the bottom of aircraft body 1.So, rotated by controlling active segment, you can drive image collection assembly 31
Rotate therewith.
Certainly, image collection assembly 31 can also be rotated, such as image collection assembly 31 is fixedly installed in foot stool 2
Upper, foot stool 2 is fixedly attached to the bottom of aircraft body 1.So, when image collection assembly 31 cannot rotate, Ke Yitong
Cross and cause that the camera lens of image collection assembly 31, in predetermined angle, makes the mirror of the image collection assembly 31 towards with corresponding foot stool 2
Head picture does not include aircraft body 1 and corresponding foot rest structure.
Further, as shown in Fig. 2 in the foot rest structure of the disclosure, avoidance biography can be provided with least one foot stool 2
Sensor 32.In one embodiment, the avoidance sensor 32 on the foot stool 2 comprising the image collection assembly 31, and can be somebody's turn to do
Avoidance sensor 32 may be located near the image collection assembly 31.Wherein, avoidance sensor 32 can use distance measuring sensor
(such as ultrasonic distance-measuring sensor, infrared distance sensor, laser range sensor) or vision sensor (or, light spreads
Sensor).
For example, in the embodiment shown in Figure 2, image collection assembly 31 can be integrated into one with avoidance sensor 32 and combined
Module 3, and the composite module 3 is arranged on foot stool 2.It is located near image collection assembly 31 by by avoidance sensor 32
(being such as disposed adjacent) so that the ambient condition information that avoidance sensor 32 is detected, such as around barrier etc., you can by with
As the ambient condition information of the image collection assembly 31, then aircraft after the ambient condition information is received, Neng Gougeng
Adequately perform intelligent barrier avoiding function；Especially, when user is regarded according to the view data that image collection assembly 31 is returned
During the flight of field, it can be ensured that the passback image that user sees keeps one with the ambient condition information that avoidance sensor 32 is detected
Cause, so as to help to lift the winged control precision of user, reduce winged control difficulty.
In the technical scheme of the disclosure, the foot rest structure of aircraft can include that multiple is provided with image collection assembly 31
Foot stool, such as shown in Fig. 5：Foot rest structure can be including foot stool 2A, foot stool 2B, foot stool 2C and four foot stools etc. foot stool 2D, and four
Individual foot stool is arranged at the bottom of aircraft body 1 in which can be centrosymmetric.With image collection assembly 31 and avoidance sensor 32
It is integrated into as a example by composite module 3, as shown in Figure 5, it is assumed that be respectively arranged with foot stool 2A, foot stool 2B, foot stool 2C and foot stool 2D
Composite module 3A, composite module 3B, composite module 3C and composite module 3D, show to be equipped with corresponding image on this four foot stools
Acquisition component 31；It is possible to by making to be included in composite module 3A, composite module 3B, composite module 3C and composite module 3D
The camera lens of image collection assembly 31 match between, such as cause the camera lens of each image collection assembly 31 towards remote
From aircraft outside (camera lens of the image collection assembly 31 that the composite module 3A in such as upper left corner is included towards (Fig. 5's, under
The camera lens of the image collection assembly 31 that the upper left corner, the composite module 3B in the lower left corner are included is towards the lower left corner, the combination in the lower right corner together)
The IMAQ group that the camera lens of the image collection assembly 31 that module 3C is included is included towards the composite module 3D in the lower right corner, the upper right corner
The camera lens of part 31 is towards the upper right corner), then in the case where the camera lens visual angle of each image collection assembly 31 is not less than 90 °,
The view data that these image collection assemblies 31 are collected can be spliced into panoramic image data.
Wherein, data transmission link can be included in foot rest structure.When any foot stool 2 is provided with image collection assembly 31,
Data transmission link can be provided with the foot stool, the data transmission link is arranged inside the inside of foot stool 2 and aircraft body 1
Pre-set path in, and the data transmission link be respectively connecting on the foot stool 2 set image collection assembly 31 and aircraft
Circuit module in main body 1, the view data that the image collection assembly 31 is collected is transmitted to the circuit module, and by this
Circuit module is processed.And circuit module can include image processing modules, the image processing modules can be with foot rest structure
On image collection assembly 31 be connected, and the view data that can be collected to all image collection assemblies 31 carries out splicing,
Such as splicing obtains above-mentioned panoramic image data.
Further, circuit module can also include communication part, and such as communication part can include bluetooth module, from
And under the scene shown in Fig. 6, communication part can set up bluetooth connection with the grade pre-set user equipment of mobile phone 4, and by the indigo plant
The diagram data that image processing modules splicing that tooth connection collects image collection assembly 31 or above-mentioned is obtained is transmitted to mobile phone
4；Meanwhile, when mobile phone 4 is assemblied in virtual reality glasses 5, and the mobile phone 5 is when being configured as virtual reality display pattern, user
Can by wearing the virtual reality glasses 5, using aircraft obtain panoramic image data as virtual reality display content, and
When user carries out flight control to aircraft by remote control 6, the virtual reality display content can be with the control operation of user
Real-time change, so that user obtains flight impression on the spot in person.
In embodiment of the disclosure, it is arranged on the foot stool 2 of aircraft by by image collection assembly 31, can be amortized
The bottom of aircraft body 1 is applied to hang the region of the image collection assembly 31 originally, it is applied to other work(
The setting of energy component.For example shown in Fig. 7, by setting battery connecting piece at the bottom centre of aircraft body 1, the battery connects
Fitting can be attached fixation to reserve battery module 4 so that the reserve battery module 4 is fixed in the aircraft body 1
At bottom centre such that it is able to lift performance of the aircraft in related fields such as continuations of the journey.
Those skilled in the art will readily occur to its of the disclosure after considering specification and putting into practice disclosure disclosed herein
Its embodiment.The application is intended to any modification, purposes or the adaptations of the disclosure, these modifications, purposes or
Person's adaptations follow the general principle of the disclosure and including the undocumented common knowledge in the art of the disclosure
Or conventional techniques.Description and embodiments are considered only as exemplary, and the true scope of the disclosure and spirit are by following
Claim is pointed out.
It should be appreciated that the disclosure is not limited to the precision architecture for being described above and being shown in the drawings, and
And can without departing from the scope carry out various modifications and changes.The scope of the present disclosure is only limited by appended claim.
Claims (14)
1. a kind of foot rest structure of aircraft, it is characterised in that including：Some foot stools, some foot stools are respectively arranged at winged
The default rigging position of row device bottom part body；Wherein, at least one foot stool is provided with the image collection assembly of the aircraft.
2. foot rest structure according to claim 1, it is characterised in that the camera lens of described image acquisition component is directed away from institute
State the outside of aircraft.
3. foot rest structure according to claim 2, it is characterised in that the camera lens of described image acquisition component towards with it is corresponding
Foot stool be in predetermined angle, make described image acquisition component camera lens picture do not include the aircraft body and the foot stool knot
Structure.
4. foot rest structure according to claim 1, it is characterised in that when the foot stools that image collection assembly is provided with the presence of multiple
When, the camera lens of multiple images acquisition component matches between, to cause the corresponding view data for collecting sliceable for complete
Scape view data.
5. foot rest structure according to claim 4, it is characterised in that the foot rest structure includes four foot stools, four pin
Frame is arranged at aircraft body bottom with being centrosymmetric；Wherein, an image collection assembly is respectively equipped with each foot stool, the figure
The outside of the aircraft is directed away from as the camera lens of acquisition component, and the camera lens visual angle of the image collection assembly is not less than 90 °.
6. foot rest structure according to claim 1, it is characterised in that at least one foot stool is provided with avoidance sensor.
7. foot rest structure according to claim 6, it is characterised in that the avoidance sensor comprising described image located at adopting
Collect on the foot stool of component, and the avoidance sensor is located near described image acquisition component.
8. foot rest structure according to claim 6, it is characterised in that the avoidance sensor includes：Distance measuring sensor or
Vision sensor.
9. foot rest structure according to claim 1, it is characterised in that
Described image acquisition component is fixedly installed on the foot stool, and the foot stool is fixedly attached to aircraft body bottom；
Or, described image acquisition component is fixedly installed on the foot stool, and the foot stool is rotatably connected to aircraft
Bottom part body；
Or, described image acquisition component is installed on the active segment on the foot stool, wherein the active segment can be relative to described
Remaining canned paragraph realizes the rotation of predetermined angle on foot stool, and the canned paragraph is fixedly attached to aircraft body bottom.
10. foot rest structure according to claim 1, it is characterised in that also include：
Data transmission link, is arranged in the pre-set path inside the foot stool inside and aircraft body, and the data are passed
Defeated circuit is respectively connecting to the circuit module in described image acquisition component and aircraft body, by described image acquisition component
The view data for collecting is transmitted to the circuit module.
A kind of 11. aircraft, it is characterised in that including：
Aircraft body；
Foot rest structure as any one of claim 1-10.
12. aircraft according to claim 11, it is characterised in that be provided with electricity at the bottom centre of the aircraft body
Pond connector, the battery connecting piece can be attached fixation to reserve battery module, and the reserve battery module is fixed
At the bottom centre of the aircraft body.
13. aircraft according to claim 11, it is characterised in that also include：
It is connected with the image collection assembly on the foot rest structure, and the view data that all image collection assemblies can be collected
Carry out the image processing modules of splicing；Wherein, described image processing assembly is located in the aircraft body.
14. aircraft according to claim 13, it is characterised in that also include：
The diagram data obtained for the splicing of collecting described image acquisition component or described image processing assembly is transmitted to pre-
If the communication part of user equipment, the communication part is located in the aircraft body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621273108.9U CN206202668U (en) | 2016-11-23 | 2016-11-23 | Aircraft and its foot rest structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621273108.9U CN206202668U (en) | 2016-11-23 | 2016-11-23 | Aircraft and its foot rest structure |
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| Publication Number | Publication Date |
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| CN206202668U true CN206202668U (en) | 2017-05-31 |
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| CN201621273108.9U Active CN206202668U (en) | 2016-11-23 | 2016-11-23 | Aircraft and its foot rest structure |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106477028A (en) * | 2016-11-23 | 2017-03-08 | 北京小米移动软件有限公司 | Aircraft and its foot rest structure |
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- 2016-11-23 CN CN201621273108.9U patent/CN206202668U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106477028A (en) * | 2016-11-23 | 2017-03-08 | 北京小米移动软件有限公司 | Aircraft and its foot rest structure |
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