PH12012000274A1 - Unmanned aerial vehicle system with cable connection equipment - Google Patents

Unmanned aerial vehicle system with cable connection equipment

Info

Publication number
PH12012000274A1
PH12012000274A1 PH1/2012/000274A PH12012000274A PH12012000274A1 PH 12012000274 A1 PH12012000274 A1 PH 12012000274A1 PH 12012000274 A PH12012000274 A PH 12012000274A PH 12012000274 A1 PH12012000274 A1 PH 12012000274A1
Authority
PH
Philippines
Prior art keywords
aerial vehicle
unmanned aerial
ground
stay
air
Prior art date
Application number
PH1/2012/000274A
Inventor
Han Kim Sang
Original Assignee
Ucon System Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Ucon System Co Ltd filed Critical Ucon System Co Ltd
Publication of PH12012000274A1 publication Critical patent/PH12012000274A1/en

Links

Classifications

    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
    • H02G11/00—Arrangements of electric cables or lines between relatively-movable parts
    • H02G11/02—Arrangements of electric cables or lines between relatively-movable parts using take-up reel or drum
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F3/00—Ground installations specially adapted for captive aircraft
    • B64F3/02—Ground installations specially adapted for captive aircraft with means for supplying electricity to aircraft during flight
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/60—Tethered aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20—Rotors; Rotor supports
    • B64U30/26—Ducted or shrouded rotors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/13—Propulsion using external fans or propellers
    • B64U50/14—Propulsion using external fans or propellers ducted or shrouded
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/30—Supply or distribution of electrical power
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/30—Supply or distribution of electrical power
    • B64U50/34—In-flight charging
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00—UAVs specially adapted for particular uses or applications
    • B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
    • B64U2101/31—UAVs specially adapted for particular uses or applications for imaging, photography or videography for surveillance
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2201/00—UAVs characterised by their flight controls
    • B64U2201/20—Remote controls
    • B64U2201/202—Remote controls using tethers for connecting to ground station

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Electric Cable Installation (AREA)
  • Forklifts And Lifting Vehicles (AREA)

Abstract

The present invention relates to a wired unmanned aerial vehicle system which is configured to be supplied with electric power from the ground to stay in the air for a long time to conduct a mission, and to stably stay in the air at a position according to a command from the ground with autonomous flying through the control of posture and position of the unmanned aerial vehicle, in which the electric power is required for operating a thrust motor of the unmanned aerial vehicle and electronic equipments loaded in the aerial vehicle. The wired unmanned aerial vehicle system includes: a rotary wing type unmanned aerial vehicle (100) equipped with a communication system and an observation system, and configured to stay in the air by operating one or more rotors (150); a ground control equipment (200) configured to communicate with the unmanned aerial vehicle (100) to control a long-duration flight of the unmanned aerial vehicle and to receive observation information, wherein the unmanned aerial vehicle (100) and the ground control equipment (200) are electrically interconnected through a tether cable 310 that comprises a power line (312), and the ground control equipment supplies electric power required by the unmanned aerial vehicle (100) through the power line (312).
PH1/2012/000274A 2012-04-24 2012-09-24 Unmanned aerial vehicle system with cable connection equipment PH12012000274A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
KR1020120042580A KR101350291B1 (en) 2012-04-24 2012-04-24 Unmanned aerial vehicle system with cable connection equipment

Publications (1)

Publication Number Publication Date
PH12012000274A1 true PH12012000274A1 (en) 2017-10-04

Family

ID=49483395

Family Applications (1)

Application Number Title Priority Date Filing Date
PH1/2012/000274A PH12012000274A1 (en) 2012-04-24 2012-09-24 Unmanned aerial vehicle system with cable connection equipment

Country Status (3)

Country Link
KR (1) KR101350291B1 (en)
PH (1) PH12012000274A1 (en)
WO (1) WO2013162128A1 (en)

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Also Published As

Publication number Publication date
WO2013162128A1 (en) 2013-10-31
KR101350291B1 (en) 2014-01-10
KR20130119633A (en) 2013-11-01

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