Patent Application
20170297445
This docking mechanism is designed especially for A SPLICED DOUBLE UNMANNED AERIAL VEHICLE SYSTEM WITH IMPROVED ENDURANCE ABILITY as well as UAV charge stations.
This disclosure refers to the technical field of aerial vehicle, in particular, but not limited to a spliced double unmanned system with improved endurance ability. It also can serve as UAV ground charging stations.
Unmanned aerial vehicle (UAV) is also known as multi-rotor type aerial vehicle with characteristics, such as, convenience, lightweight, stable flight and low noise. Unmanned aerial vehicle (UAV) with imaging equipment and monitoring equipment provides an effective means for undercover investigation, especially in an area people cannot easily approach. Unmanned aerial vehicle can provide first-hand video materials.
It is reported that a research group from Texas University found a new unmanned aerial vehicle (UAV) application, which is emergency communication. The group develops an unmanned aerial vehicle communication system, which is able to provide WiFi for the disaster area. The cover area can reach 5 km. It is understood that, the cover area of ordinary WiFi antenna is limited to 100 m radius. However, the antenna used by the group is a directive antenna, which is able to detect the target automatically and provide accurate and stable signal for the target. The directive antenna also shows extraordinary performance in anti-interference.
Currently, the war of unmanned aerial vehicle network service between Google and Facebook is realized quietly in the army. A team of unmanned aerial vehicle served in Iraq is assigned to a new task: providing WiFi at remote battlefields. Unmanned aerial vehicle RQ-7 shadow plays a role of reconnaissance, surveillance, target acquisition and battle damage assessment. But now, they have become the best wireless router in the world. In remote battlefield, communication is a big problem. Poor communication may mean defeat by enemies. Unmanned aerial vehicle used as a WiFi main center is configured to be a supplement for the limitation of wireless signal and to increase data transmission channels.
However, the biggest problem of unmanned aerial vehicle is the consumer market is the cruising ability. The cruising duration of the civil unmanned aerial vehicle system is about 20 minutes; the cruising duration of the unmanned aerial vehicle system used in some industries is only up to 1-2 hours. Furthermore, there is no technology about long cruising duration or infinite cruising duration on the market. Especially in military unmanned aerial vehicles with WiFi technology, if the unmanned aerial vehicles need to be charged after being used for 20 minutes, the Wifi signal or internet signal will be broken off.
Currently, there is a patented technology about endurance of UAV, when a first UAV's power is running low, a second UAV is started to perform the same task. At the same time, the first UAV returns to the starting place or a specific charging place to be charged. When the charging is finished, the first UAV takes off and the second UAV returns to be charged. Circulating like this, the purpose of extending the endurance time is achieved. Of course, when the first UAV is being charged, manual recharging can be used. A machine vision technology can also be used to enable the UAV find the charging preparation place and return to be charged automatically. Contact charging or non-contact wireless charging can be used.
However, regardless of the methods stated above, when performing critical tasks, problems like breaking off and discontinuity always exist, because the first UAV and the second UAV do not connect with each other. The position where the first UAV's power urns out is not the exact position the second UAV arrives at. Therefore, this technology has the defect of inaccuracy in cruising position.
At the same time, this technology also has defect of task separation. For example, when the first UAV is shooting key videos or images, unfortunately, the first UAV's power runs out, the first UAV can only return to launch site for charging along with the camera. The second UAV with another camera takes off to continue performing the task. The details in the video are interrupted and the video materials shot by two independent cameras must be united and processed. Uniting videos is also very tedious and it is easy to lose key information.
Furthermore, two separate UAVs with the same load are unable to increase the cruising duration. Two separate UAVs with the same cruising duration are unable to achieve a heavier load. Therefore, existing UAV's cruising duration and load are unable to change flexibly.
For UAV automatic charging station, no matter it is contact or contactless charging station, often that the interconnection between a UAV and charging station is not precise and as a result, the contactless charging station may not provide enough charge power due to misalignment between charge pad and a UAV. For contact charging station, it needs to have multiple large expansive pieces of metal contacts designed to the landing pads. These exposed metal contacts will have fire risk due to metal debris could fall on the charging pads and cause short circuit. By using our cone shaped docking and releasing charge mechanism it provides precise connection and therefore it will eliminate this risk since the contacts are relatively small, inexpensive and vertically installed. Also, the charge station can be designed to be accessed from below which will eliminate the risk completely.
The present invention is a cone shaped docking and releasing mechanism which provides rigid connection between a parent UAV and a sub UAV to form a spliced double unmanned aerial vehicle system with improved cruising duration ability by providing sub UAV battery power module with charging function in the system. By using this cone shaped docking and releasing mechanism, parent UAV and sub UAV joint together reliably and they can fly together like a single UAV. But also, both UAV can be separated with ease. This cone shaped docking and releasing mechanism can also be implemented as part of ground charging docking pads for UAV. It solves the existing UAVs' problems of cruising duration, task interruption and inaccuracy of position when using two independent UAVs to execute tasks under long endurance and the problem that existing UAV's endurance time and load are unable to change flexibly.
In order to solve the problems as described in the background technology, the present invention uses technical solution as below: it comprises a parent UAV, a sub UAV and a cone shaped docking mechanism, the parent UAV and the sub UAV are connected with each other through the cone shaped docking mechanism to form a double UAV system.
The docking mechanism comprises an inner cone shaped docking control mechanism which is fixed to the lower part of the parent UAV and an outer cone shaped docking plug which is fixed to the upper part of the sub UAV (or the other way, an outer cone shaped docking control mechanism is fixed to the lower part of the parent UAV and an inner cone shaped docking plug is fixed to the upper part of the sub UAV); the outer cone shaped docking plug is matted with an inner cone surface of the docking mechanism in a plug-in way; the docking control mechanism comprises a imaging system, e.g. a near field Intel realsense 3D camera module and a far field Intel realsense 3D camera module, a docking/releasing mechanism and a sensor component configured to detect whether the docking plug is in place; the docking/releasing mechanism and the sensor component are electrically connected with a parent UAV internal control system; the docking/releasing, mechanism is droved by a gear reduction servo motors. The docking control mechanism system also comprises charging ports assembly designed to engage with the charging input ports on the sub UAV to provide the sub UAV battery charging power. A charging circuit electrically is independently connected between the sub UAV battery and charging input ports.
The parent UAV system comprises a parent UAV CPU mainboard, a parent UAV battery power source, a parent voltage-current sensor module, a parent UAV GPS receiver and compass combo module, a docking/releasing linear actuator motor control module, a parent UAV telemetering radio transceiver module, a parent UAV radio control receiver module and the two Intel Realsense Camera Modules (one is near field and other is far field). All the parent UAV modules are electrically connected with the parent UAV CPU mainboard; the telemetering radio transceiver module and the radio control receiver module are separately connected with an antenna; a docking success sensor module is electrically connected with the docking/releasing motor control module; each parent UAV rotor wing motor is electrically connected with their corresponding electronic speed control (ESC) module, the ESCs are electrically connected with the parent UAV CPU mainboard and the parent UAV battery power source E1.
The sub UAV system comprises of a sub UAV CPU mainboard, a sub UAV battery power module, a sub UAV voltage and current sensor module, a sub UAV GPS receiver and compass combo module, an Intel realsense camera module, a sub UAV telemetering radio transceiver module and a sub UAV radio control receiver module. All the sub UAV modules are electrically connected with the sub UAV CPU mainboard; the sub UAV telemetering radio transceiver module and sub UAV radio control receiver module are separately connected with an antenna, a task executing device installed on a lower end of the sub UAV is electrically connected with the sub UAV CPU mainboard and the sub UAV battery power module; each sub UAV rotor wing motor is electrically connected with their corresponding electronic motor speed control (ESC) modules; the ESCs are electrically connected with the sub UAV CPU mainboard and its own battery power supply.
As a further improvement for the present invention, the parent UAV is a bigger aircraft, the sub UAV is either a smaller aircraft or as big as the parent UAV.
The working process of the present invention comprises:
First, a docking process of the parent UAV and the sub UAV comprises:
Second, a separation process of the parent UAV and the sub UAV comprises:
Third, when the parent UAV malfunctions in the process of executing task, the sub UAV can carry the parent UAV back to the ground, which increases the stability of the system;
Fourth, repeating the docking process and the separating process achieve the purpose of long cruising duration and aerial charging of the double UAV system.
Beneficial Effects of the Invention:
1. The present invention solves the endurance problem of existing UAV system, besides, aerial charging is realized. No matter which kind of UAV is being used, the cruising duration can be improved when executing tasks with this invention.
2. The present invention overcomes the defects of task interruption and location inaccuracy in long-endurance mission of existing technology by using two separate UAVs.
3. The present invention overcomes the defects of endurance time and load is unable to change flexibly.
In order to clarify the intention, technical solution and advantages of the invention, a detailed description of the present invention is presented in conjunction with the drawings and the specific embodiment. It should be understood that, the specific embodiment is only used to describe rather than limit the present invention.
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Limit switch position sensor switches S1 and S2 are separately located at an initial end and terminal end of slide rail 3.
Optical docking success sensor module comprises a LED light source and an IR sensor diode 13.
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The principle of the embodiment is described as below: parent UAV 1 and sub UAV 2 fly to a position after docking successfully. At this time, the propellers of parent UAV 1 rotate and propellers of sub UAV 2 located under the parent UAV is not started. After flying to the working place, when battery level of parent UAV 1 is low; propellers of sub UAV 2 start, parent UAV 1 releases sub UAV 2 located under the parent UAV. Sub UAV 2 works independently. Parent UAV 1 returns to ground for changing the battery. After parent UAV gets new battery, parent UAV 1 flies up above sub UAV 2 again, then docks with sub UAV 2. After docking successfully, propellers of sub UAV 2 stop rotating for saving power, then parent UAV 1 charges the battery of sub UAV 2 for recovering the energy loss. The whole docking process will spend no more than 5 minutes; electric energy loss of sub UAV 2 is minimum. The battery capacity of sub UAV 2 just needs to support for about 5 minutes, then a successful docking process will be guaranteed. Parent UAV 1 charges sub UAV 2 for about 10 minutes, the electric energy loss during the docking process will be compensated. In this process, propellers of sub UAV 2 are kept stationary. After sub UAV 2 is fully charged, until battery level of parent UAV 1 is at low level, parent UAV 1 returns to ground for changing battery. Repeating all these steps, the cycle repeats to achieve a long cruising duration.
Referring to
The aerial charging spliced double UAV system stated by the above specific embodiments can solve the endurance problem of existing UAV system, no matter which kind of UAV it is, the endurance time can be improved during executing tasks. In particular, the present invention can be used to provide a WiFi base station for a long time or provide a mobile operator base station to provide an internet system; defects like task dissociation and location inaccuracy can be overcome. The defect of inability to change endurance time and load flexibly can also be overcome.
The above description is preferred embodiments of the present invention. The present invention is not limited to the description stated above. Equal modifications or replacements according to the technical solutions of the present invention are also within the scope of this application, especially for the other use of the cone shaped docking and releasing mechanism.
