CN203461140U - Unmanned aerial vehicle - Google Patents
Unmanned aerial vehicle Download PDFInfo
- Publication number
- CN203461140U CN203461140U CN201320560996.2U CN201320560996U CN203461140U CN 203461140 U CN203461140 U CN 203461140U CN 201320560996 U CN201320560996 U CN 201320560996U CN 203461140 U CN203461140 U CN 203461140U
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- rotating shaft
- cabin
- unmanned vehicle
- drive motor
- screw propeller
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Abstract
The utility model discloses an unmanned aerial vehicle. The unmanned aerial vehicle comprises a cabin and a holder, wherein the holder is arranged at the front end of the cabin; a first rotating shaft extending in a front-back direction is arranged at the rear end of the holder; and the holder is rotationally connected with the cabin through the first rotating shaft. According to the unmanned aerial vehicle, the holder is located in front of the cabin and on the same horizontal plane with the aerial vehicle, so that all-angle omnibearing camera shooting requirements are met. The holder can rotate by 360 degrees around the first rotating shaft relative to an aerial vehicle body, a fixed plate supporting camera shooting equipment can rotate by 360 degrees around a second rotating shaft relative to the holder, with the adoption of the structure, however the aerial vehicle rotates, tilts and overturns, the holder can remain horizontal and stable, and the obtained film quality is high.
Description
Technical field
The utility model relates to the aircraft field of taking photo by plane, and relates in particular to a kind of unmanned vehicle.
Background technology
In aerial photography, if can obtain rapidly 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, has fixed wing aircraft, helicopter, unmanned vehicle, dynamic-delta-wing etc., 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 carrying due to The Cloud Terrace is placed under aircraft, cannot absorb image directly over aircraft, causes Aerial Images angle sufficiently complete.
Utility model content
The purpose of this utility model 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, the technical solution of the utility model is achieved in that
A unmanned vehicle, 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, and described The Cloud Terrace is rotationally connected by this first rotating shaft and described cabin.
Compared with prior art, the advantage of the utility model embodiment is:
A kind of unmanned vehicle that the utility model provides, 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 in 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 shooting requirement.
Accompanying drawing explanation
The structural representation of the unmanned vehicle that Fig. 1 provides for the utility model embodiment mono-;
The STRUCTURE DECOMPOSITION figure of the unmanned vehicle that Fig. 2 provides for the utility model embodiment mono-;
Fig. 3 is the birds-eye view of The Cloud Terrace after being connected with cabin in the utility model embodiment mono-;
Fig. 4 is the structural representation of The Cloud Terrace after being connected with adapter plate in the utility model embodiment mono-;
Fig. 5 is the partial schematic diagram after the The Cloud Terrace of the utility model embodiment mono-is connected with cabin;
Fig. 6 is the structural representation after the The Cloud Terrace of the utility model embodiment mono-is connected with cabin;
Fig. 7 is the structural representation after the The Cloud Terrace of the utility model embodiment mono-in Fig. 6 rotates to an angle with respect to cabin;
Fig. 8 is the lateral plan after the The Cloud Terrace of the utility model embodiment mono-is connected with cabin;
Fig. 9 is the structural representation of The Cloud Terrace in the utility model embodiment mono-;
Figure 10 is the structural representation of the rotor assemblies of the utility model embodiment mono-after folding with respect to cabin;
Figure 11 is the partial enlarged drawing at A place in Figure 10;
Figure 12 is the structural representation of rotor protective case in the utility model embodiment mono-.
The specific embodiment
Below by specific embodiment, also by reference to the accompanying drawings the utility model is described in further detail.
Embodiment mono-
Referring to Fig. 1 and Fig. 2, a kind of unmanned vehicle that the utility model embodiment mono-provides, comprise cabin 1 and be located at the The Cloud Terrace 2 of this cabin front end and the adapter plate 3 of 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 utility model embodiment mono-, 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 in 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 shooting requirement.
Further, as a kind of embodiment, above-mentioned unmanned vehicle also comprises for supporting the adapter plate 3 of picture pick-up device, on described adapter plate 3, be connected with 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 utility model embodiment mono-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 supporting the adapter plate of 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 carrying picture pick-up device on 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 take.
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 multiaxis driving realizes multi-angle adjusting) of the first rotating shaft and the second rotating shaft, drive picture pick-up device to remain horizontal stable, take the photograph like this to such an extent that video quality is higher, more can meet practical flight needs.
Preferably, described cabin 1 comprises upper-deck cabin body 10 and the lower cabin body 11 connecting up and down, is provided with for driving the first rotating shaft drive motor of described the first rotating shaft rotation in described lower cabin body 11.
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 connecting 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.
Described in one of them, in side arm, be provided with the second rotating shaft drive motor that drives described the second rotating shaft to rotate.
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 with the second rotating shaft drive motor adapter plate 212, fix, on described the second rotating shaft drive motor adapter plate 212, offer the knock hole 213 of described the second rotating shaft 30.
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 utility model embodiment relates to (from steady The Cloud Terrace) can be controlled by being arranged on servomechanism type direction and the angular adjustment of aircraft central interior self.
Preferably, as shown in figure 10, the both sides in described cabin 1 are respectively provided with a rotor assemblies 5, and described in each, rotor assemblies 5 comprises two screw propeller bracing frames and screw propeller, described in each, the bottom of rotor assemblies and described cabin are hinged, and the top of described rotor assemblies and the clamping of described cabin.Described in each, the center of screw propeller bracing frame is provided with screw propeller mounting hole and screw propeller drive motor mounting hole 500(is separately 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 utility model embodiment relates to is from designing as accordion structure; every two blades (containing integrated protective cover) are a folded formation structure, and this structure has greatly been simplified aircraft self installation, safeguards; maintenance work, makes its globality more obviously outstanding.
Preferably, described in each, the outer gusset of screw propeller bracing frame is also 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 utility model embodiment relates to (being quadrotor) overall appearance is succinct, and four screw propellers are supported by screw propeller bracing frame, by peripheral rotor protective case around protection.Wherein screw propeller bracing frame can be one-body molded with rotor protective case, and the utility model embodiment is not specifically limited this.
Above-mentioned rotor protective case 50 is made by special composite material, insulation completely, and intensity is high, very light weight.
As shown in figure 11, described in each, the bottom of rotor assemblies 5 is hinged by rotating shaft 6 and described cabin 1, simultaneously, described in each, the top of rotor assemblies 5 is provided with block tongue 51, the top in described cabin 1 is provided with 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; Described in each, the bottom of 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 utility model embodiment mono-, the monnolithic case of unmanned vehicle structure is succinct, and cradle head structure brand-new design is also preposition, and aircraft overall performance is greatly improved.The Cloud Terrace is positioned at the dead ahead in cabin, and itself and aircraft self are positioned in 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, 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 utility model embodiment relates to, the cradle head structure from profile to succinct internal structure and brand-new design is all improved, and from many aspects, promotes function and the framework of existing aircraft completely.
The foregoing is only preferred embodiment of the present utility model, be not limited to the utility model, for a person skilled in the art, the utility model can have various modifications and variations.All within spirit of the present utility model and principle, any modification of doing, be equal to replacement, improvement etc., within all should being included in protection domain of the present utility model.
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, on this adapter plate, be connected with 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;
Described in one of them, in side arm, be provided with the second rotating shaft drive motor that drives described the second rotating shaft to rotate.
4. unmanned vehicle as claimed in claim 1, is characterized in that,
The both sides in described cabin are respectively provided with a rotor assemblies;
Described in each, rotor assemblies comprises two screw propeller bracing frames and screw propeller, and described in each, the bottom of 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,
Described in each, the outer gusset of screw propeller bracing frame is also provided with a rotor protective case.
6. unmanned vehicle as claimed in claim 4, is characterized in that,
Described in each, the center of screw propeller bracing frame is also provided with 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, is provided with for driving the first rotating shaft drive motor of described the first rotating shaft rotation in the body of described lower cabin.
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;
On described the second rotating shaft drive motor mounting hole, be covered with the second rotating shaft drive motor adapter plate, on this second rotating shaft drive motor adapter plate, offer the knock hole of described the second rotating shaft.
9. unmanned vehicle as claimed in claim 4, is characterized in that,
Described in each, the top of 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;
Described in each, the bottom of 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 |
|---|---|---|---|
| CN201320560996.2U CN203461140U (en) | 2013-09-10 | 2013-09-10 | Unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320560996.2U CN203461140U (en) | 2013-09-10 | 2013-09-10 | Unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203461140U true CN203461140U (en) | 2014-03-05 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320560996.2U Expired - Lifetime CN203461140U (en) | 2013-09-10 | 2013-09-10 | Unmanned aerial vehicle |
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| CN (1) | CN203461140U (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103419942B (en) * | 2013-09-10 | 2015-08-05 | 北京臻迪科技有限公司 | A kind of unmanned vehicle |
| CN105620778A (en) * | 2016-04-07 | 2016-06-01 | 天津航天中为数据***科技有限公司 | Mounting platform of unmanned aerial vehicle |
| CN106715268A (en) * | 2016-09-21 | 2017-05-24 | 深圳市大疆创新科技有限公司 | Holder fixing support and UAV including the same |
| CN107128502A (en) * | 2017-05-30 | 2017-09-05 | 佛山市神风航空科技有限公司 | A kind of scalable 360 ° of photography and vedio recording unmanned planes of taking photo by plane |
| US10118697B2 (en) | 2015-06-25 | 2018-11-06 | Riderless Technologies Inc. | Unmanned aerial vehicle |
| JPWO2018029739A1 (en) * | 2016-08-08 | 2019-06-27 | エスゼット ディージェイアイ テクノロジー カンパニー リミテッドＳｚ Ｄｊｉ Ｔｅｃｈｎｏｌｏｇｙ Ｃｏ．，Ｌｔｄ | Mobile body and method of manufacturing imaging device |
| CN113581464A (en) * | 2015-09-11 | 2021-11-02 | 深圳市大疆灵眸科技有限公司 | Carrier for unmanned aerial vehicle |
-
2013
- 2013-09-10 CN CN201320560996.2U patent/CN203461140U/en not_active Expired - Lifetime
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103419942B (en) * | 2013-09-10 | 2015-08-05 | 北京臻迪科技有限公司 | A kind of unmanned vehicle |
| US10118697B2 (en) | 2015-06-25 | 2018-11-06 | Riderless Technologies Inc. | Unmanned aerial vehicle |
| CN113581464A (en) * | 2015-09-11 | 2021-11-02 | 深圳市大疆灵眸科技有限公司 | Carrier for unmanned aerial vehicle |
| CN105620778A (en) * | 2016-04-07 | 2016-06-01 | 天津航天中为数据***科技有限公司 | Mounting platform of unmanned aerial vehicle |
| JPWO2018029739A1 (en) * | 2016-08-08 | 2019-06-27 | エスゼット ディージェイアイ テクノロジー カンパニー リミテッドＳｚ Ｄｊｉ Ｔｅｃｈｎｏｌｏｇｙ Ｃｏ．，Ｌｔｄ | Mobile body and method of manufacturing imaging device |
| JP7009696B2 (en) | 2016-08-08 | 2022-01-26 | エスゼット ディージェイアイ テクノロジー カンパニー リミテッド | Mobile |
| CN106715268A (en) * | 2016-09-21 | 2017-05-24 | 深圳市大疆创新科技有限公司 | Holder fixing support and UAV including the same |
| WO2018053697A1 (en) * | 2016-09-21 | 2018-03-29 | 深圳市大疆灵眸科技有限公司 | Head fixing mount and unmanned aerial vehicle having same |
| CN106715268B (en) * | 2016-09-21 | 2019-04-23 | 深圳市大疆灵眸科技有限公司 | Holder fixed frame and unmanned plane with the holder fixed frame |
| CN107128502A (en) * | 2017-05-30 | 2017-09-05 | 佛山市神风航空科技有限公司 | A kind of scalable 360 ° of photography and vedio recording unmanned planes of taking photo by plane |
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| GR01 | Patent grant | ||
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| C56 | Change in the name or address of the patentee | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 100107 Beijing city Chaoyang District Road No. 9 Fu A unit 301 Patentee after: POWERVISION TECH Inc. Address before: 100107 Beijing city Chaoyang District Road No. 9 Fu A unit 301 Patentee before: Beijing Zhendi Technology Co.,Ltd. |
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| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: Inertia measuring module of unmanned aircraft Effective date of registration: 20160621 Granted publication date: 20140305 Pledgee: Zhongguancun Beijing technology financing Company limited by guarantee Pledgor: POWERVISION TECH Inc. Registration number: 2016990000519 |
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Granted publication date: 20140305 |
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| CX01 | Expiry of patent term |