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公开(公告)号:TW201622790A
公开(公告)日:2016-07-01
申请号:TW103143929
申请日:2014-12-16
Applicant: 和碩聯合科技股份有限公司 , PEGATRON CORPORATION
Inventor: 陳昱璋 , CHEN, YU CHANG , 張皓詠 , CHANG, HAO YUNG , 鄭道華 , CHENG, TAO HUA
CPC classification number: B64D47/08 , B64C27/08 , B64C27/20 , B64C39/024 , B64C2201/141 , G05D1/0016
Abstract: 本發明之飛行裝置包含本體、第一距離感測器及第二距離感測器。第一距離感測器與第二距離感測器係分別設置於本體之底面及頂面。此外,本體內具有處理模組,其可接收自第一距離感測器或第二距離感測器所輸出之感測訊號,並根據第一感測訊號的內容以輸出位移訊號。當第一距離感測器與被感測物的相對距離小於預設接收距離時,則第一距離感測器輸出第一感測訊號。當第二距離感測器與被感測物的相對距離小於預設接收距離時,則第二距離感測器輸出第三感測訊號。本體內另具有飛行驅動模組係接收並根據位移訊號以升高或降低飛行裝置。
Abstract in simplified Chinese: 本发明之飞行设备包含本体、第一距离传感器及第二距离传感器。第一距离传感器与第二距离传感器系分别设置于本体之底面及顶面。此外,本体内具有处理模块,其可接收自第一距离传感器或第二距离传感器所输出之传感信号,并根据第一传感信号的内容以输出位移信号。当第一距离传感器与被传感物的相对距离小于默认接收距离时,则第一距离传感器输出第一传感信号。当第二距离传感器与被传感物的相对距离小于默认接收距离时,则第二距离传感器输出第三传感信号。本体内另具有飞行驱动模块系接收并根据位移信号以升高或降低飞行设备。
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公开(公告)号:TWI528989B
公开(公告)日:2016-04-11
申请号:TW104111617
申请日:2015-04-10
Applicant: 蕭文昌
Inventor: 蕭文昌
IPC: A63H27/133 , F24J2/38
CPC classification number: B64C39/024 , B64C27/06 , B64C27/08 , B64C2201/024 , B64C2201/027 , B64C2201/108 , B64C2201/12 , B64C2201/141 , B64C2201/145 , G05D1/102 , Y02E10/47
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283.
公开(公告)号:EP3045393B1
公开(公告)日:2018-12-12
申请号:EP13875320.7
申请日:2013-12-13
Applicant: Korea Aerospace Research Institute
Inventor: LEE, Sang Cherl , REW, Dong Young , SIM, Eun Sup , CHOI, Gi Hyuk , CHO, Dong Hyun , KIM, Hae Dong , KIM, Jeong Hoon , KIM, In Kyu , MOON, Sang Man , HAN, Sang Hyuck , MOON, Sung Tae , SUK, Jin Young , KIM, Jin-Won , NO, Tae Soo , GONG, Hyeon Cheol , KIM, Min Ki , KIM, Jong Chul
CPC classification number: B64F1/222 , B64C39/024 , B64C2201/042 , B64C2201/141 , B64C2201/145 , B64C2201/208 , B64F1/007 , B64F1/362 , E04H6/44 , G05D1/042 , G08G5/0013 , G08G5/0069 , G08G5/025
Abstract: An apparatus and method of charging and housing of an unmanned vertical take-off and landing (VTOL) aircraft is disclosed. The apparatus includes an accommodator to accommodate an aircraft, a landing platform on which the aircraft lands, a housing portion to monitor state data by housing or charging the aircraft, and a sensor to assist in landing of the aircraft by allowing the aircraft to communicate with the apparatus. The apparatus enhances operational efficiency by reducing a travel time of the aircraft.
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公开(公告)号:EP3147210B1
公开(公告)日:2018-11-14
申请号:EP16190742.3
申请日:2016-09-27
Applicant: Ewatt Technology Co., Ltd.
Inventor: ZHAO, Guocheng , LUO, Wei , QI, Pengcheng
CPC classification number: B64D33/02 , B64C27/82 , B64C39/024 , B64C2201/024 , B64C2201/044 , B64C2201/141 , B64C2201/146 , B64D27/08 , B64D33/06 , B64D33/08 , B64D2033/0246 , B64D2033/028
Abstract: The present invention discloses an unmanned helicopter, and belongs to the technical field of unmanned aerial vehicles. The unmanned helicopter includes an air inlet system, an exhaust system, a cooling system and a dynamic balance system. The air inlet system is fixed on a second side; the exhaust system is fixed on a third side; and the cooling system is fixed on a first side, and the dynamic balance system is fixed on a tail. The airflow at the outside of the unmanned helicopter flows into the air inlet system smoothly, quickly and efficiently under the action of its own flow velocity relative to the unmanned helicopter, therefore the technical problem in the prior art that the air entering the fuselage with a unit volume is burnt insufficiently, which generates adverse effects on the normal flight of the unmanned helicopter, is solved.
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公开(公告)号:EP3387398A2
公开(公告)日:2018-10-17
申请号:EP16865280.8
申请日:2016-12-09
Applicant: Flir Systems, Inc.
Inventor: FRANK, Jeffrey D. , HOELTER, Theodore R. , HÖGASTEN, Nicholas , RICHARDS, Austin A. , KENT, Michael , MOREIRA, Julie R. , BOULANGER, Pierre , VALDES, Raymond , LI, Jonathan
CPC classification number: G01J5/00 , B64C39/024 , B64C2201/123 , B64C2201/127 , B64C2201/141 , B64C2201/146 , G01J5/007 , G01J5/0265 , G01J5/06 , G01J5/061 , G01J2005/0048 , G01J2005/0055 , G01J2005/0077 , G01J2005/068 , G03B15/006 , G06K9/0063 , G08G5/0091 , H02J4/00 , H02S50/00 , H02S50/15 , H04N5/2351 , H04N5/243 , H04N5/33 , H04N7/185 , H04W4/046 , H04W84/18
Abstract: Flight based infrared imaging systems and related techniques, and in particular UAS based thermal imaging systems, are provided to improve the monitoring capabilities of such systems over conventional infrared monitoring systems. An infrared imaging system is configured to compensate for various environmental effects (e.g., position and/or strength of the sun, atmospheric effects) to provide high resolution and accuracy radiometric measurements of targets imaged by the infrared imaging system. An infrared imaging system is alternatively configured to monitor and determine environmental conditions, modify data received from infrared imaging systems and other systems, modify flight paths and other commands, and/or create a representation of the environment.
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公开(公告)号:EP3371048A1
公开(公告)日:2018-09-12
申请号:EP16908458.9
申请日:2016-07-14
Applicant: SZ DJI Technology Co., Ltd.
Inventor: LIU, Wanqi , LAN, Qiu , ZHOU, Changxing
CPC classification number: B64C13/04 , B64C27/12 , B64C27/56 , B64C2201/042 , B64C2201/141 , B64D31/06 , H02P6/182 , H02P21/0025 , H02P23/0031 , H02P27/08
Abstract: A method for operating a motor controller includes obtaining an electrical signal via a port on the motor controller and selecting a motor control parameter from a plurality of different motor control parameters based on the electrical signal. The port is configured to be electrically connected to a motor. The motor controller is configured to control the motor based on the selected motor control parameter.
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287.
公开(公告)号:EP3367315A1
公开(公告)日:2018-08-29
申请号:EP17158275.2
申请日:2017-02-28
Applicant: TRUMPF Werkzeugmaschinen GmbH + Co. KG
Inventor: BAUER, Klaus , WAHL, Eberhard , SCHLEGEL, Rainer , HOEFERT, Christian , OECHSLE, Stephan , ROEDER, Dr. Holger , WETZEL, Matthias
CPC classification number: G05B19/41895 , B41M5/0047 , B41M5/262 , B60P1/64 , B64C39/02 , B64C39/024 , B64C2201/108 , B64C2201/12 , B64C2201/128 , B64C2201/141 , G05B2219/40171 , G05B2219/40282 , G05B2219/45134 , G05B2219/45186 , G05D1/102 , G06Q10/08 , G06Q50/04 , G06Q50/28 , Y02P90/30
Abstract: Ein Produktionssystem (1) mit mindestens einer Werkzeugmaschine (3, 6a, 6b) zum Bearbeiten von Werkstücken (4) weist erfindungsgemäß mindestens ein die Werkzeugmaschine (3, 6a, 6b) anfliegendes Fluggerät (10, 10'), welches eine Werkstück-Applikationseinheit (13, 14) aufweist, wobei Applikationsdaten für den Einsatz der Applikationseinheit (13, 14) an einem Werkstück (4) Logistikdaten für das bearbeitete oder noch zu bearbeitende Werkstück (4) umfassen.
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288.
公开(公告)号:EP3120597B1
公开(公告)日:2018-08-22
申请号:EP14711237.9
申请日:2014-03-18
Applicant: Telefonaktiebolaget LM Ericsson (publ)
Inventor: POTENTAS, Wojciech , DJORDJEVIC, Branko , DUDDA, Torsten
CPC classification number: H04W16/26 , B64C39/024 , B64C2201/122 , B64C2201/141 , G08G1/202 , G08G5/0043 , G08G5/0069 , H04B7/18504 , H04W16/32 , H04W24/02 , H04W88/08
Abstract: A plurality of mobile robots provide a radio coverage area of a wireless communication network. Each mobile robot comprises a radio base station of the wireless communication network. A mobile robot of the plurality of mobile robots moves to a geographical position to deploy as part of a daisy chain loop of the mobile robots upon receiving instruction from a maintenance base. Upon receiving further instruction from the maintenance base, the mobile robot moves to a further geographical position as part of a circular shift operation performed by the mobile robots deployed to the daisy chain loop to maintain the radio coverage area and send a further mobile robot of the mobile robots deployed to the daisy chain loop to the maintenance base.
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公开(公告)号:EP3299925A3
公开(公告)日:2018-08-01
申请号:EP17192401.2
申请日:2017-09-21
Applicant: Beijing Xiaomi Mobile Software Co., Ltd.
Inventor: CHENG, Yue , XIE, Yan , CHU, Yueyue
IPC: G05D1/10
CPC classification number: G05D1/101 , B64C39/024 , B64C2201/127 , B64C2201/141 , B64C2201/146 , G05D1/0011 , G05D1/102
Abstract: The present invention relates to a method, apparatus and system for controlling an unmanned aerial vehicle, belonging to the field of aircraft technology. The method includes: receiving (201) a flight area control parameter transmitted by a control device; determining (202,404) a flight area based on the flight area control parameter; and cruising (203) within the flight area. invention
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公开(公告)号:EP3344545A1
公开(公告)日:2018-07-11
申请号:EP16760141.8
申请日:2016-08-26
Applicant: BAE SYSTEMS plc
Inventor: WOODHOUSE, Gordon, Charles , BOSTON, Luke, Michael
CPC classification number: B64D31/06 , B64C39/024 , B64C2201/141 , B64D41/00 , B64D45/04 , B64D2041/005 , B64D2045/0085 , G05D1/0088 , G05D1/105 , G07C5/0808 , Y02T50/54
Abstract: A vehicle (100) comprising: an engine (102); a system for starting the engine (102); a fault detection module (120); an electrical power source (110); and a controller (116, 122). The controller (116, 122) is configured to, responsive to the fault detection module (120) detecting a fault occurring with the engine (102): determine a window in which to attempt to start the engine (102); control the electrical power source (110) to provide electrical power to the system for starting the engine (102); and control the system for starting the engine (102) to attempt to start the engine (102) using the supplied electrical power only during the determined window.
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