Mobile robot
US-9440355-B2 · Sep 13, 2016 · US
US2016236346A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016236346-A1 |
| Application number | US-201514923442-A |
| Country | US |
| Kind code | A1 |
| Filing date | Oct 27, 2015 |
| Priority date | Feb 17, 2015 |
| Publication date | Aug 18, 2016 |
| Grant date | — |
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Official abstract text for this publication.
A multi-link type working apparatus moved by a thrust generating device is provided. The multi-link type working apparatus performs a work by moving a link apparatus, in which a plurality of links are connected by at least one joint, by using the thrust generating device. The multi-link type working apparatus moved by a thrust generating device may variously expand lengths of links, the number of links, and the freedom of movement by using the thrust generating device as an actuator for moving the links, compared to a general multi-link type working apparatus that uses a motor or a hydraulic cylinder as an actuator.
Opening claim text (preview).
What is claimed is: 1 . A multi-link type working apparatus moved by a thrust generating device, the multi-link type working apparatus comprising: a link apparatus that comprises a plurality of links and at least one joint connecting two neighboring links between each of the plurality of links; a plurality of thrust generating devices that comprise a control module enabling communication between an external device and a rotor generating thrust to control operations of the rotor, and are respectively combined to the plurality of links of the link apparatus to move the plurality of links; and a control device that comprises a controller in which a control process for controlling the plurality of thrust generating devices is stored, and a communicator transmitting a control signal to the plurality of thrust generating device according to the control process. 2 . The multi-link type working apparatus of claim 1 , further comprising at least one end effector that has a working function and is combined to the link apparatus. 3 . The multi-link type working apparatus of claim 1 , further comprising a plurality of link connecting apparatuses that detachably connect the plurality of links of the link apparatus and the plurality of thrust generating devices between the plurality of links and the plurality of thrust generating devices. 4 . The multi-link type working apparatus of claim 3 , wherein the plurality of link connecting apparatuses comprise a joint structure that adjusts an angle of the plurality of thrust generating devices with respect to the plurality of links of the link apparatus. 5 . The multi-link type working apparatus of claim 1 , wherein the plurality of thrust generating devices are respectively electrically connected to the plurality of links of the link apparatus. 6 . The multi-link type working apparatus of claim 1 , wherein each of the plurality of thrust generating devices comprises a multi-rotor type unmanned aerial vehicle (UAV) comprising a plurality of the rotors. 7 . The multi-link type working apparatus of claim 1 , further comprising a base that supports the link apparatus as any one of the plurality of links of the link apparatus is connected to the base. 8 . The multi-link type working apparatus of claim 7 , further comprising a power supply apparatus that supplies power to the plurality of thrust generating device through the plurality of links of the link apparatus. 9 . The multi-link type working apparatus of claim 1 , further comprising a moving apparatus that supports the link apparatus as any one of the plurality of links of the link apparatus is connected to the moving apparatus, and is movable by comprising a moving mechanism.
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