CN103419942A - Unmanned aerial vehicle - Google Patents
Unmanned aerial vehicle Download PDFInfo
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- CN103419942A CN103419942A CN2013104104715A CN201310410471A CN103419942A CN 103419942 A CN103419942 A CN 103419942A CN 2013104104715 A CN2013104104715 A CN 2013104104715A CN 201310410471 A CN201310410471 A CN 201310410471A CN 103419942 A CN103419942 A CN 103419942A
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- 230000000712 assembly Effects 0.000 claims description 18
- 238000000429 assembly Methods 0.000 claims description 18
- 230000001681 protective effect Effects 0.000 claims description 8
- 108010066057 cabin-1 Proteins 0.000 description 8
- 230000000007 visual effect Effects 0.000 description 5
- 238000012423 maintenance Methods 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 230000000903 blocking effect Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
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Abstract
The invention discloses an unmanned aerial vehicle which comprises a cabin and a cloud deck which is arranged at the front end of the cabin. A first rotating shaft which extends forwards and backwards is arranged at the rear end of the cloud deck, and the cloud deck is connected with the cabin through the first rotating shaft in a rotating mode. According to the unmanned aerial vehicle, the cloud deck is placed right ahead of the cabin and is placed in the same horizontal plane with the aerial vehicle, and an all-angle all-directional camera shooting demand is met. The cloud deck can rotate by 360 degrees around the first rotating shaft relative to an aerial vehicle body, and a fixing plate for supporting camera shooting equipment rotates by 360 degrees around a second rotating shaft relative to the cloud deck. The structure is used, no matter how the unmanned aerial vehicle rotates, tilts and overturns, the cloud deck can guarantee to be horizontally stable, and the quality of shot films is high.
Description
Technical field
The aircraft field that the present invention relates to take photo by plane, relate in particular to a kind of unmanned vehicle.
Background technology
In aerial photography, if can obtain rapidly the ground image and arrange rapidly picture mosaic, just can be more rapidly, in time, fully understand the reality of target area, for managerial decision provides strong information support.The technology of taking photo by plane can be widely used in the fields such as the condition of a disaster assessment, rescue and relief work, on-the-spot scouting, military exercise, and quick obtaining ground image information becomes the key of above-mentioned technology.The advantages such as at present, the carrier of holder for aerial photographing has a lot, and fixed wing aircraft, helicopter, unmanned vehicle, dynamic-delta-wing etc. are arranged, and wherein unmanned vehicle is high with cost performance, landing is flexible, environmental conditions is wide, obtain extensive concern.
In prior art, the pick up camera carried due to The Cloud Terrace is placed under aircraft, can't absorb image directly over aircraft, causes the Aerial Images angle sufficiently complete.
Summary of the invention
The object of the present invention is to provide all unmanned vehicles of 360 ° of rotations unrestrictedly of a kind of The Cloud Terrace and picture pick-up device, to address the above problem.
In order to achieve the above object, technical scheme of the present invention is achieved in that
A kind of unmanned vehicle, comprise cabin and the The Cloud Terrace of being located at this cabin front end, first rotating shaft of extending before and after the rear end of described The Cloud Terrace is provided with, and described The Cloud Terrace is rotationally connected by this first rotating shaft and described cabin.
Compared with prior art, the advantage of the embodiment of the present invention is:
A kind of unmanned vehicle provided by the invention, the structure of analyzing above-mentioned unmanned vehicle is known: The Cloud Terrace is positioned at the dead ahead in cabin, itself and aircraft self are positioned on same level, The Cloud Terrace shooting visual angle can become very large like this, and it vertically no longer includes blocking of cabin in top, and The Cloud Terrace can be around the first rotating shaft with respect to 360 ° of rotations of aircraft body, owing to having carried picture pick-up device on The Cloud Terrace, utilize like this said structure, picture pick-up device can obtain larger shooting visual angle, has ensured the shooting requirement.
The accompanying drawing explanation
The structural representation of the unmanned vehicle that Fig. 1 provides for the embodiment of the present invention one;
The STRUCTURE DECOMPOSITION figure of the unmanned vehicle that Fig. 2 provides for the embodiment of the present invention one;
Fig. 3 is The Cloud Terrace and birds-eye view after cabin is connected in the embodiment of the present invention one;
Fig. 4 is The Cloud Terrace and structural representation after adapter plate is connected in the embodiment of the present invention one;
The The Cloud Terrace that Fig. 5 is the embodiment of the present invention one and partial schematic diagram after cabin is connected;
The The Cloud Terrace that Fig. 6 is the embodiment of the present invention one and structural representation after cabin is connected;
Structural representation after the The Cloud Terrace that Fig. 7 is the embodiment of the present invention one in Fig. 6 rotates to an angle with respect to cabin;
The The Cloud Terrace that Fig. 8 is the embodiment of the present invention one and lateral plan after cabin is connected;
The structural representation that Fig. 9 is The Cloud Terrace in the embodiment of the present invention one;
Structural representation after the rotor assemblies that Figure 10 is the embodiment of the present invention one is folding with respect to cabin;
The partial enlarged drawing that Figure 11 is A place in Figure 10;
The structural representation that Figure 12 is rotor protective case in the embodiment of the present invention one.
The specific embodiment
Below by specific embodiment, also by reference to the accompanying drawings the present invention is described in further detail.
Embodiment mono-
Referring to Fig. 1 and Fig. 2, a kind of unmanned vehicle that the embodiment of the present invention one provides, the adapter plate 3 that comprises cabin 1 and the The Cloud Terrace 2 of being located at this cabin front end and supporting picture pick-up device, described The Cloud Terrace 2 utilizations are located at its rear end the first rotating shaft 20 that also extend front and back and are rotationally connected with described cabin 1.
In the embodiment of the present invention one, the structure of analyzing above-mentioned unmanned vehicle is known: The Cloud Terrace is positioned at the dead ahead in cabin, itself and aircraft self are positioned on same level, The Cloud Terrace shooting visual angle can become very large like this, and it vertically no longer includes blocking of cabin in top, and The Cloud Terrace can be around the first rotating shaft with respect to 360 ° of rotations of aircraft body, owing to having carried picture pick-up device on The Cloud Terrace, utilize like this said structure, picture pick-up device can obtain larger shooting visual angle, has ensured the shooting requirement.
Further, as a kind of embodiment, above-mentioned unmanned vehicle also comprises the adapter plate 3 for supporting picture pick-up device, be connected with on described adapter plate 3 that left and right is extended and with the second rotating shaft 30 of described the first rotating shaft 20 spatial vertical, described adapter plate 3 is rotationally connected with described The Cloud Terrace 2 by the second rotating shaft 30.
It should be noted that, the unmanned vehicle that the embodiment of the present invention one relates to, The Cloud Terrace not only can be around the first rotating shaft with respect to 360 ° of rotations of aircraft body, also can be around the second rotating shaft with respect to 360 ° of rotations of The Cloud Terrace for the adapter plate that supports picture pick-up device, to further increase the shooting visual angle of the equipment of taking photo by plane (being picture pick-up device) like this, utilize said structure, unmanned vehicle can meet full angle, omnibearing shooting requirement.
Obviously, above-mentioned unmanned vehicle can carry The Cloud Terrace, and the picture pick-up device on the lift-launch The Cloud Terrace to carry out that the shooting angle such as pitching and roll change (but be picture pick-up device self the 360 degree rotations that The Cloud Terrace carries, The Cloud Terrace itself is 360 degree rotations simultaneously also), in addition when carrying out some special angle shootings, without carrying out tumbling action, by the regulating action of above-mentioned the first rotating shaft and the second rotating shaft, regulate the camera lens head for target of picture pick-up device, directly taken.
In addition, analysis can be learnt: according to this practical flight needs, possible unmanned vehicle will be carried out the operations such as upset, inclination, but no matter how aircraft rotates, tilts, overturns, The Cloud Terrace can be by the driving effect (being that the multiaxis driving realizes the multi-angle adjusting) of the first rotating shaft and the second rotating shaft, drive picture pick-up device and remain horizontal stable, take the photograph like this to such an extent that video quality is higher, more can meet the practical flight needs.
Preferably, described cabin 1 comprises upper-deck cabin body 10 and the lower cabin body 11 connected up and down, in described lower cabin body 11, is provided with for driving the first rotating shaft drive motor of described the first rotating shaft rotation.
Preferably, the rear in described cabin 1 is provided with battery flat 4, and it is that upper cover 40 and the battery flat cabin body 41 connected forms that this battery flat 4 comprises separable, and battery flat cabin body 41 is fixedly connected with lower cabin body 11, as shown in Fig. 2, Fig. 3 and Fig. 8.
Preferably, as shown in Fig. 4～Fig. 6, described The Cloud Terrace 2 comprises front latter linked U-shaped frame 21 and the first rotating shaft 20, and described adapter plate 3 is located between two side arms of described U-shaped frame 21.
The both sides of described adapter plate 3 are respectively established 30, two described the second rotating shafts 30 of described second rotating shaft and are rotationally connected with two described side arms accordingly.
Be provided with the second rotating shaft drive motor that drives described the second rotating shaft to rotate in one of them described side arm.
Preferably, position corresponding to described the second rotating shaft drive motor on one of them side arm 210 of described U-shaped frame 21 offers the second rotating shaft drive motor mounting hole 211(as Fig. 7), the second rotating shaft drive motor is installed in side arm 210 and (on the second rotating shaft drive motor mounting hole, is covered with the second rotating shaft drive motor adapter plate) through this second rotating shaft drive motor mounting hole 211, then fix with the second rotating shaft drive motor adapter plate 212, offer the knock hole 213 of described the second rotating shaft 30 on described the second rotating shaft drive motor adapter plate 212.
It should be noted that, wherein, described the first rotating shaft 20 hollows, which is provided with The Cloud Terrace mounting hole 201 and cable hole 200, and as shown in Figure 9, the cable of picture pick-up device and the second rotating shaft drive motor is interspersed in the centre hole of the first rotating shaft 20 through this cable hole 200.
The first rotating shaft drive motor and the second rotating shaft drive motor in the present embodiment are all selected servomotor.It should be noted that, the The Cloud Terrace that the embodiment of the present invention relates to (from steady The Cloud Terrace) can be controlled by the servomechanism type direction and the angular adjustment that are arranged on the aircraft central inner self.
Preferably, as shown in figure 10, the both sides in described cabin 1 respectively are provided with a rotor assemblies 5, and each described rotor assemblies 5 comprises two screw propeller bracing frames and screw propeller, the bottom of each described rotor assemblies and described cabin are hinged, and the top of described rotor assemblies and the clamping of described cabin.The center of each described screw propeller bracing frame is provided with the screw propeller mounting hole and screw propeller drive motor mounting hole 500(separately is shown in Figure 12), described screw propeller is fixed on the screw propeller mounting hole of described screw propeller bracing frame.
The unmanned vehicle that the embodiment of the present invention relates to is from designing as accordion structure; every two blades (containing the integrated protective cover) are a folded formation structure, and this structure has greatly been simplified aircraft self installation, safeguards; maintenance work, make its globality more obviously outstanding.
Preferably, the outer gusset of each described screw propeller bracing frame also is provided with a rotor protective case 50, and two described rotor protective cases 50 of homonymy are one-body molded, which is provided with mounting hole 502 and the motor radiating hole 503 of antenna mounting hole 501, arc alighting gear, as Figure 12.
The unmanned vehicle that the embodiment of the present invention relates to (being quadrotor) overall appearance is succinct, and four screw propellers are supported by the screw propeller bracing frame, by peripheral rotor protective case around protection.Wherein the screw propeller bracing frame can be one-body molded with the rotor protective case, and the embodiment of the present invention is not specifically limited this.
Above-mentioned rotor protective case 50 is made by special composite material, insulation fully, and intensity is high, very light weight.
As shown in figure 11, the bottom of each described rotor assemblies 5 is hinged by rotating shaft 6 and described cabin 1, simultaneously, the top of each described rotor assemblies 5 is provided with block tongue 51, the top in described cabin 1 is provided with the upper latch notch (not shown), and the top of described rotor assemblies 5 utilizes described upper block tongue 51 and described upper latch notch clamping; The bottom of each described rotor assemblies 5 is provided with lower block tongue 52, and the bottom in described cabin 1 is provided with lower bayonet socket (not shown), and the bottom of described rotor assemblies 5 utilizes described lower block tongue 52 and described lower bayonet socket clamping.By said structure, unmanned vehicle is accordion structure, has greatly simplified installation, maintenance and the maintenance work of aircraft, makes its globality more outstanding.
In sum, in the embodiment of the present invention one, the monnolithic case of unmanned vehicle structure is succinct, and the cradle head structure brand-new design is also preposition, and the aircraft overall performance is greatly improved.The Cloud Terrace is positioned at the dead ahead in cabin, and itself and aircraft self are positioned on same level, meets full angle, omnibearing shooting requirement.The Cloud Terrace can be around the first rotating shaft with respect to 360 ° of rotations of aircraft body, the supporting picture pick-up device adapter plate around the second rotating shaft with respect to 360 ° of rotations of The Cloud Terrace, utilize said structure, unmanned vehicle can meet full angle, omnibearing shooting requirement, no matter how aircraft rotates, tilts, overturns simultaneously, The Cloud Terrace all can keep horizontal stable, takes the photograph to such an extent that video quality is high.
The unmanned vehicle that the embodiment of the present invention relates to, the cradle head structure from profile to succinct internal structure and brand-new design all is improved, and promotes function and the framework of existing aircraft fully from many aspects.
The foregoing is only the preferred embodiments of the present invention, be not limited to the present invention, for a person skilled in the art, the present invention can have various modifications and variations.Within the spirit and principles in the present invention all, any modification of doing, be equal to replacement, improvement etc., within all should being included in protection scope of the present invention.
Claims (9)
1. a unmanned vehicle, is characterized in that, comprises cabin and the The Cloud Terrace of being located at this cabin front end;
First rotating shaft of extending before and after the rear end of described The Cloud Terrace is provided with, described The Cloud Terrace is rotationally connected by this first rotating shaft and described cabin.
2. unmanned vehicle as claimed in claim 1, is characterized in that,
Also comprise for supporting the adapter plate of picture pick-up device, be connected with on this adapter plate that left and right is extended and with the second rotating shaft of described the first rotating shaft spatial vertical, described adapter plate is connected with described cloud platform rotation by the second rotating shaft.
3. unmanned vehicle as claimed in claim 2, is characterized in that,
Described The Cloud Terrace comprises front latter linked U-shaped frame and described the first rotating shaft, and described adapter plate is located between two side arms of described U-shaped frame;
Described second rotating shaft is respectively established in the both sides of described adapter plate, and two described the second rotating shafts are rotationally connected with two described side arms accordingly;
Be provided with the second rotating shaft drive motor that drives described the second rotating shaft to rotate in one of them described side arm.
4. unmanned vehicle as claimed in claim 1, is characterized in that,
The both sides in described cabin respectively are provided with a rotor assemblies;
Each described rotor assemblies comprises two screw propeller bracing frames and screw propeller, and the bottom of each described rotor assemblies and described cabin are hinged, and the top of described rotor assemblies and the clamping of described cabin.
5. unmanned vehicle as claimed in claim 4, is characterized in that,
The outer gusset of each described screw propeller bracing frame also is provided with a rotor protective case.
6. unmanned vehicle as claimed in claim 4, is characterized in that,
The center of each described screw propeller bracing frame also is provided with the screw propeller mounting hole, and described screw propeller is fixed on the screw propeller mounting hole of described screw propeller bracing frame.
7. unmanned vehicle as claimed in claim 1, is characterized in that,
Described cabin comprises upper-deck cabin body and lower cabin body, in the body of described lower cabin, is provided with for driving the first rotating shaft drive motor of described the first rotating shaft rotation.
8. unmanned vehicle as claimed in claim 3, is characterized in that,
Position corresponding to described the second rotating shaft drive motor on the side arm of described U-shaped frame offers the second rotating shaft drive motor mounting hole;
Be covered with the second rotating shaft drive motor adapter plate on described the second rotating shaft drive motor mounting hole, offer the knock hole of described the second rotating shaft on this second rotating shaft drive motor adapter plate.
9. unmanned vehicle as claimed in claim 4, is characterized in that,
The top of each described rotor assemblies is provided with block tongue, and the top in described cabin is provided with upper latch notch, and the top of described rotor assemblies utilizes described upper block tongue and described upper latch notch clamping;
The bottom of each described rotor assemblies is provided with lower block tongue, and the bottom in described cabin is provided with lower bayonet socket, and the bottom of described rotor assemblies utilizes described lower block tongue and described lower bayonet socket clamping.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
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| CN201310410471.5A CN103419942B (en) | 2013-09-10 | 2013-09-10 | A kind of unmanned vehicle |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201310410471.5A CN103419942B (en) | 2013-09-10 | 2013-09-10 | A kind of unmanned vehicle |
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| CN103419942A true CN103419942A (en) | 2013-12-04 |
| CN103419942B CN103419942B (en) | 2015-08-05 |
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| AT520144A1 (en) * | 2017-06-22 | 2019-01-15 | Werner Dipl Ing Holzer | SWIVELING PROPELLER PROTECTION FRAME WITH INTEGRATED ELECTRICALLY DRIVEN PROPELLERS |
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| CN107972858A (en) * | 2017-12-06 | 2018-05-01 | 佛山市神风航空科技有限公司 | A kind of special aircraft |
| CN107933904A (en) * | 2017-12-06 | 2018-04-20 | 佛山市神风航空科技有限公司 | A kind of flexible aircraft |
| CN108674646A (en) * | 2018-05-31 | 2018-10-19 | 江苏常探机器人有限公司 | With without the rear single ducted fan formula composite wing cargo aircraft for pushing away the compound auxiliary wing |
| CN108622401A (en) * | 2018-05-31 | 2018-10-09 | 江苏常探机器人有限公司 | A kind of compound rotor aircraft of folding of the compound auxiliary wing of twin screw thrust |
| CN108791883A (en) * | 2018-07-26 | 2018-11-13 | 广州点优广告传媒有限公司 | A kind of party array unmanned plane and its control system |
| WO2020019553A1 (en) * | 2018-07-27 | 2020-01-30 | 深圳市大疆创新科技有限公司 | Gimbal connecting device and unmanned aerial vehicle |
| WO2024124569A1 (en) * | 2022-12-16 | 2024-06-20 | 深圳市闪至科技有限公司 | Unmanned aerial vehicle |
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