CN203127141U - Multi-rotor wing unmanned aerial vehicle - Google Patents
Multi-rotor wing unmanned aerial vehicle Download PDFInfo
- Publication number
- CN203127141U CN203127141U CN2012206867312U CN201220686731U CN203127141U CN 203127141 U CN203127141 U CN 203127141U CN 2012206867312 U CN2012206867312 U CN 2012206867312U CN 201220686731 U CN201220686731 U CN 201220686731U CN 203127141 U CN203127141 U CN 203127141U
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- unmanned vehicle
- housing
- many rotors
- shell
- rotors unmanned
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Abstract
The utility model discloses a multi-rotor wing unmanned aerial vehicle. The multi-rotor wing unmanned aerial vehicle comprises a hollow housing and a circuit board which is contained in the housing, wherein the housing comprises a main body part and a housing inner cavity which is formed by the enclosing of the main body part; the circuit module is contained in the housing inner cavity; the multi-rotor ring unmanned aerial vehicle further comprises a sensor which is arranged on the housing and far from the housing inner cavity. The sensor is far from the housing inner cavity, namely far from the circuit module, so that the interferences on the sensor caused by the circuit module are avoided, and the flight reliability is ensured.
Description
Technical field
The utility model belongs to the unmanned vehicle field, relates in particular to a kind of many rotors unmanned vehicle.
Background technology
Many rotors unmanned vehicle of correlation technique comprises housing, the horn that links to each other with housing, is located at the control system that is used for driving the power system of described many rotors unmanned vehicle flight on the horn and is used for the described many rotors unmanned vehicle flight of control.Described control system comprises circuit module and respectively to the sensor of circuit module Data transmission.Described sensor comprises magnetic sensors and GPS locating module.Described magnetic sensors is used for distinguishing the orientation of described many rotors unmanned vehicle, and it can select compass; Described GPS locating module is used for judging the locus of described many rotors unmanned vehicle.Described circuit module sends control signal according to the data that obtain from sensor to power system.
Yet the sensor of many rotors unmanned vehicle of correlation technique is subjected to electromagnetic interference easily, causes described many rotors unmanned vehicle flight reliability poor, even can not normal flight.Described electromagnetic interference comes from circuit module to the interference of sensor.
Therefore, be necessary to provide a kind of improved many rotors unmanned vehicle in fact.
The utility model content
The purpose of this utility model has been to provide a kind of many rotors unmanned vehicle of anti-electromagnetic interference.
The utility model is achieved in that a kind of many rotors unmanned vehicle, it comprises the shell of hollow and is contained in the interior circuit module of shell, described shell comprises main part and the shell inner cavity that is enclosed by main part, described circuit module is contained in the shell inner cavity, and described many rotors unmanned vehicle also comprises and placing on the shell and away from the sensor of shell inner cavity.
Preferably, described sensor is magnetic sensors.
Preferably, described magnetic sensors is compass.
Preferably, described sensor is the GPS locating module.
Preferably, the shell of described many rotors unmanned vehicle also comprises the foot rest that links to each other with main part, and described sensor is positioned on the foot rest.
Preferably, described foot rest comprises a pair of support portion in a certain distance apart from one another and the connecting portion that is connected two support portions that links to each other with main part, and described sensor is located on the support portion.
Preferably, described main part comprise housing and with the integrated wing of housing.
Many rotors unmanned vehicle provided by the utility model, described sensor namely away from circuit module, have been avoided the interference of circuit module to sensor away from shell inner cavity, have guaranteed the reliability of flight.
Description of drawings
Fig. 1 is the three-dimensional assembly drowing after many rotors unmanned vehicle of providing of the utility model embodiment is removed rotor;
Fig. 2 is the three-dimensional assembly drowing after many rotors unmanned vehicle of providing of the utility model embodiment is removed upper shell;
Fig. 3 is the three-dimensional assembly drowing that many rotors unmanned vehicle shown in Figure 2 is removed another visual angle behind the upper shell;
Fig. 4 is the block diagram of the foot rest of many rotors unmanned vehicle of the present utility model.
The specific embodiment
In order to make the purpose of this utility model, technical scheme and advantage clearer, below in conjunction with drawings and Examples, the utility model is further elaborated.Should be appreciated that specific embodiment described herein only in order to explaining the utility model, and be not used in restriction the utility model.
A kind of many rotors unmanned vehicle that the utility model embodiment provides, it cooperates with remote controller and is used for taking photo by plane, ground mapping, the condition of a disaster investigation and rescue, monitoring and polling transmission line etc. in the air.During work, described many rotors unmanned vehicle carries The Cloud Terrace and pick up camera and receives the remote signal of remote controller, thereby realizes above-mentioned functions.
As shown in Figures 1 to 4, above-mentioned many rotors unmanned vehicle (not label) comprise hollow shell (not label), be contained in circuit module 3 in the shell, place engine installation 2 on the shell, be contained in the electric mode transfer piece 34 that is electrically connected with circuit module 3 in the shell, be located on the shell for many rotors unmanned vehicle provide energy power supply (not shown), place shell outward sensor 7 and respectively with the connecting device (not shown) of sensor 7, circuit module 3, power supply, electric mode transfer piece 34 and engine installation 2 electrical connections.
Described shell comprises the main part 10 of hollow, the foot rest 4 that links to each other with main part 10 and the shell inner cavity 13 that is enclosed by main part 10.Described circuit module 3 is contained in the described shell inner cavity 13.The main part 10 of described shell comprises housing 11 and the horn 12 that links to each other with housing 11.Described foot rest 4 links to each other with the housing 11 of main part 10, is used for supportive body portion 10 and protection pick up camera 6, and it comprises first foot rest 41 and second foot rest 42 identical and separated by a distance with first foot rest, 41 structures.First foot rest 41 comprises a pair of support portion 411 in a certain distance apart from one another and the connecting portion 412 that is connected two support portions 411 that links to each other with the housing 11 of main part 10.
Described sensor 7 is located on the support portion 411 of first foot rest 41, thereby guarantees that sensor 7 is away from shell inner cavity 13, namely away from circuit module 3.Described sensor 7 can be magnetic sensors (not label) or GPS locating module (not label).Described magnetic sensors can be compass or magnetic heading pin.
Housing 11 comprises upper shell 111, the housing inner chambers 113 that form jointly with the involutory lower house 112 of upper shell 111, by upper shell 111 and lower house 112.Horn 12 is the arm shape of hollow, it comprise horn housing 121, with the involutory following horn housing 122 of last horn housing 121 and the horn inner chamber 123 that is enclosed jointly by last horn housing 121 and following horn housing 122.Described horn inner chamber 123 and housing inner chamber 113 communicate and form shell inner cavity 13 jointly, to make things convenient for connecting device in the layout of 12 of housing 11 and horns.The last horn housing 121 of described horn 12 is provided with the installation position 120 for the rotor actuating device 22 that engine installation 2 is installed.Horn 12 is 4 in the present embodiment; Correspondingly, horn 12 is provided with an engine installation 2 arbitrarily, and namely engine installation 2 also is 4.4 horns 12 are arranged with " X " shape or " ten " font and are connected in housing 11.In the present embodiment, horn 12 is the center of circle with the center shaft of housing 11, circumferentially be distributed in housing 11 around.The number of described horn can be adjusted as required, and its quantity can equate with the quantity of engine installation.Certainly, the quantity of horn and engine installation also can arrange according to actual conditions.As mentioned above, for guaranteeing the smooth flight of many rotors unmanned vehicle, the quantity of horn, rotating driving device and engine installation is no less than 3.In selectable embodiment, described horn also is provided with indicator lamp (not shown).In concrete the application, can offer light inlet window (not shown) in the lower end of horn, light inlet window place captive joint is useful on the transmission element of capping light inlet window, and indicator lamp is arranged at the light inlet window place.Indicator lamp can be LED, and its brightness height, power consumption are little, long and convenient flight of life-span.In other selectable embodiments, described indicator lamp, transmission element and light inlet window can be located on the housing.
In the present embodiment, last horn housing 121 and upper shell 111 one-body molded formation upper body 15, following horn housing 122 and lower house 112 one-body molded formation lower body 16.Described main part 10 is also formed jointly by upper body 15 and lower body 16.Horn housing 121 and upper shell 111 on the described one-body molded finger, and horn housing 122 adopts the integrally manufactured moulding of suitable method such as injection moulding with lower house 112 distributions down.During assembling, described upper body 15 can be captiveed joint by fastener with lower body 16, so that the maintenance of aircraft.When needs are safeguarded, only need upper body 15 is removed from lower body 16, just can intuitively all devices in the main part 10 be observed and safeguard.Described locking piece can be screw or buckle etc.In other selectable embodiments, upper shell, lower house, last horn housing and following horn housing are captiveed joint by modes such as locking piece locking or welding respectively.Perhaps, also can flexibly connect between horn and the housing.In concrete the application, but the horn unitary rotation be connected on the housing, horn housing relatively folds.When not using, can horn is folding, so that deposit and carry.In use, horn can be launched and fixes.
Described circuit module 3 is as the critical component of many rotors unmanned vehicle, can realize function that each associated components is controlled, and it comprises IMU(Inertial Measuring Unit, Inertial Measurement Unit) module (not label) and main control module 33 etc.
Described connecting device is selected electric wire.Described part electric wire end is provided with adaptor union.Described power supply is battery.
Described electric mode transfer piece 34 is located at the following horn housing 122 under the described rotor actuating device 22 and is contained in horn inner chamber 123, and it can be electrically connected with rotor actuating device 22 and circuit module 3 respectively by connecting device.The control signal of described electric mode transfer piece 34 is provided by main control module 33, is used for the described rotor actuating device 22 of control.Described electric mode transfer piece 34 is contained in horn inner chamber 123, is convenient to electric mode transfer piece 34 and is electrically connected with rotor actuating device 22.Certainly, in selectable embodiment, electric mode transfer piece can be arranged at the housing inner chamber.
Many rotors unmanned vehicle of the present utility model, each parts directly are positioned on housing or the horn, and the user need not to assemble voluntarily and debug aircraft, can reach the effect of " in one's hands namely use ".Convenient for users to use, greatly reduce the requirement to user specialty degree, avoid user installation wrong situation to occur, thereby avoided situation such as aircraft bombing.And but connecting device need not all to adopt the adaptor union of plug to connect, and the mode of part connecting device by welding can be connected as one.And, even but the adaptor union of plug connecting device is connected, when in factory, assembling, the specialty the skilled worker adaptor union can be in place, thereby reduced the risk that adaptor union gets loose, further improved the reliability of many rotors unmanned vehicle.
Described many rotors unmanned vehicle also comprises the radio receiver 31 that is used for receiving remote signal of being located at housing inner chamber 113.Also be provided with on the described radio receiver 31 to sign indicating number button 311 and with to sign indicating number button 311 separated by a distance to sign indicating number indicator lamp 312, so that described many rotors unmanned vehicle is connected with remote controller.
In other optional embodiments, described many rotors unmanned vehicle can not arrange foot rest, directly utilizes the lower body of shell to be supported on the ground.Described lift-launch The Cloud Terrace and pick up camera directly place on the lower body side away from shell inner cavity.Correspondingly, sensor also can place on the shell and away from shell inner cavity.
Many rotors unmanned vehicle of the present utility model, its sensor namely away from circuit module, have been avoided the interference of circuit module to sensor away from shell inner cavity, have guaranteed the reliability of flight.
Need to prove that the front end in the present embodiment, position term such as upper and lower are that conventional operation attitude with aircraft is reference, and do not will be understood that it is restrictive.
Below only be preferred embodiment of the present utility model, not in order to limiting the utility model, all any modifications of within spirit of the present utility model and principle, doing, be equal to and replace or improvement etc., all should be included within the protection domain of the present utility model.
Claims (7)
1. rotor unmanned vehicle more than a kind, it comprises the shell of hollow and is contained in the interior circuit module of shell, described shell comprises main part and the shell inner cavity that is enclosed by main part, described circuit module is contained in the shell inner cavity, it is characterized in that described many rotors unmanned vehicle also comprises and placing on the shell and away from the sensor of shell inner cavity.
2. many rotors unmanned vehicle according to claim 1 is characterized in that, described sensor is magnetic sensors.
3. many rotors unmanned vehicle according to claim 2 is characterized in that, described magnetic sensors is compass.
4. many rotors unmanned vehicle according to claim 1 is characterized in that, described sensor is the GPS locating module.
5. many rotors unmanned vehicle according to claim 1 is characterized in that the shell of described many rotors unmanned vehicle also comprises the foot rest that links to each other with main part, and described sensor is positioned on the foot rest.
6. many rotors unmanned vehicle according to claim 5 is characterized in that, described foot rest comprises a pair of support portion in a certain distance apart from one another and the connecting portion that is connected two support portions that links to each other with main part, and described sensor is located on the support portion.
7. many rotors unmanned vehicle according to claim 1 is characterized in that, described main part comprise housing and with the integrated wing of housing.
Priority Applications (24)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2012206867312U CN203127141U (en) | 2012-12-13 | 2012-12-13 | Multi-rotor wing unmanned aerial vehicle |
DE202013012546.2U DE202013012546U1 (en) | 2012-11-15 | 2013-11-13 | Unmanned aerial vehicle with multiple rotors |
EP13795150.5A EP2763896B1 (en) | 2012-11-15 | 2013-11-13 | A multi-rotor unmanned aerial vehicle |
DE202013012543.8U DE202013012543U1 (en) | 2012-11-15 | 2013-11-13 | Unmanned aerial vehicle with multiple rotors |
DE202013012544.6U DE202013012544U1 (en) | 2012-11-15 | 2013-11-13 | Unmanned aerial vehicle with multiple rotors |
DE202013012547.0U DE202013012547U1 (en) | 2012-11-15 | 2013-11-13 | Unmanned aerial vehicle with multiple rotors |
DE202013012545.4U DE202013012545U1 (en) | 2012-11-15 | 2013-11-13 | Unmanned aerial vehicle with multiple rotors |
JP2015542149A JP2016505435A (en) | 2012-11-15 | 2013-11-13 | Multi-rotor unmanned aerial vehicle |
PCT/CN2013/087053 WO2014075609A1 (en) | 2012-11-15 | 2013-11-13 | A multi-rotor unmanned aerial vehicle |
DE202013012541.1U DE202013012541U1 (en) | 2012-11-15 | 2013-11-13 | Unmanned aerial vehicle with multiple rotors |
US14/092,653 US9016617B2 (en) | 2012-11-15 | 2013-11-27 | Unmanned aerial vehicle and operations thereof |
US14/515,357 US9221536B2 (en) | 2012-11-15 | 2014-10-15 | Unmanned aerial vehicle and operations thereof |
US14/534,127 US9221537B2 (en) | 2012-11-15 | 2014-11-05 | Unmanned aerial vehicle and operations thereof |
US14/836,344 US9233754B1 (en) | 2012-11-15 | 2015-08-26 | Unmanned aerial vehicle and operations thereof |
US14/947,923 US9321530B2 (en) | 2012-11-15 | 2015-11-20 | Unmanned aerial vehicle and operations thereof |
US14/954,427 US9284049B1 (en) | 2012-11-15 | 2015-11-30 | Unmanned aerial vehicle and operations thereof |
US15/012,006 US9394048B2 (en) | 2012-11-15 | 2016-02-01 | Unmanned aerial vehicle and operations thereof |
US15/175,473 US10155584B2 (en) | 2012-11-15 | 2016-06-07 | Unmanned aerial vehicle and operations thereof |
US15/947,650 US10189562B2 (en) | 2012-11-15 | 2018-04-06 | Unmanned aerial vehicle and operations thereof |
US16/005,309 US10196137B2 (en) | 2012-11-15 | 2018-06-11 | Unmanned aerial vehicle and operations thereof |
US16/027,178 US10272994B2 (en) | 2012-11-15 | 2018-07-03 | Unmanned aerial vehicle and operations thereof |
US16/353,999 US10472056B2 (en) | 2012-11-15 | 2019-03-14 | Unmanned aerial vehicle and operations thereof |
US16/679,984 US11338912B2 (en) | 2012-11-15 | 2019-11-11 | Unmanned aerial vehicle and operations thereof |
US17/664,629 US20220281592A1 (en) | 2012-11-15 | 2022-05-23 | Unmanned aerial vehicle and operations thereof |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2012206867312U CN203127141U (en) | 2012-12-13 | 2012-12-13 | Multi-rotor wing unmanned aerial vehicle |
Publications (1)
Publication Number | Publication Date |
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CN203127141U true CN203127141U (en) | 2013-08-14 |
Family
ID=48935144
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2012206867312U Ceased CN203127141U (en) | 2012-11-15 | 2012-12-13 | Multi-rotor wing unmanned aerial vehicle |
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Country | Link |
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CN (1) | CN203127141U (en) |
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WO2014075609A1 (en) * | 2012-11-15 | 2014-05-22 | SZ DJI Technology Co., Ltd | A multi-rotor unmanned aerial vehicle |
CN104386249A (en) * | 2014-11-17 | 2015-03-04 | 马鞍山市靓马航空科技有限公司 | Multi-rotor unmanned aerial vehicle for fast surveying and surveying method of multi-rotor unmanned aerial vehicle |
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2012
- 2012-12-13 CN CN2012206867312U patent/CN203127141U/en not_active Ceased
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