MX382001B - Aeronave multirotor. - Google Patents

Aeronave multirotor.

Info

Publication number
MX382001B
MX382001B MX2018007640A MX2018007640A MX382001B MX 382001 B MX382001 B MX 382001B MX 2018007640 A MX2018007640 A MX 2018007640A MX 2018007640 A MX2018007640 A MX 2018007640A MX 382001 B MX382001 B MX 382001B
Authority
MX
Mexico
Prior art keywords
aircraft
rotor
motors
failure
operating structure
Prior art date
Application number
MX2018007640A
Other languages
English (en)
Other versions
MX2018007640A (es
Inventor
Christoph Geyer
Manfred Bernhard
Marius Bebesel
Michael Geiss
Sebastian Mores
Stefan Haisch
Original Assignee
Airbus Helicopters Deutschland GmbH
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 Airbus Helicopters Deutschland GmbH filed Critical Airbus Helicopters Deutschland GmbH
Publication of MX2018007640A publication Critical patent/MX2018007640A/es
Publication of MX382001B publication Critical patent/MX382001B/es

Links

Classifications

    • 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
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L50/00—Electric propulsion with power supplied within the vehicle
    • B60L50/50—Electric propulsion with power supplied within the vehicle using propulsion power supplied by batteries or fuel cells
    • B60L50/60—Electric propulsion with power supplied within the vehicle using propulsion power supplied by batteries or fuel cells using power supplied by batteries
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/10—Rotorcrafts
    • B64U10/13—Flying platforms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L2200/00—Type of vehicles
    • B60L2200/10—Air crafts
    • 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
    • B64D2221/00—Electric power distribution systems onboard aircraft
    • 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
    • B64U2101/60—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons
    • B64U2101/61—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons for transporting passengers
    • 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
    • B64U30/24—Coaxial rotors
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/60—Other road transportation technologies with climate change mitigation effect
    • Y02T10/70—Energy storage systems for electromobility, e.g. batteries

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Remote Sensing (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Power Engineering (AREA)
  • Transportation (AREA)
  • Transmission Devices (AREA)
  • Retarders (AREA)
  • Control Of Multiple Motors (AREA)
  • Safety Devices In Control Systems (AREA)

Abstract

La invención se refiere a una aeronave multirotor (1) con al menos dos unidades de producción de empuje (3a, 3x, 3b, 3c, 3y, 3d), la aeronave multirotor (1) estando adaptada para el transporte de pasajeros y comprendiendo una estructura de operación de aeronave (7a, 7b, 7c, 7d) para operación en modo de operación libre de fallos, y una arquitectura de seguridad redundante (8a, 8b, 8c, 8d) para operación en caso de una falla de la estructura de operación de aeronave (7a, 7b, 7c, 7d) en operación. Al menos dos planos de rotor/hélice (21, 22) pueden estar posicionados uno encima del otro. Motores eléctricos (14a, 14b) pueden estar segregados, los motores estando conectados a múltiples fuentes de un sistema de suministro de energía (24) para formar un diseño redundante cruzado frontal/posterior, superior/inferior e izquierdo/derecho aumentando la seguridad de la aeronave multirotor (1) en caso de falla de los motores designados.
MX2018007640A 2015-12-21 2016-12-16 Aeronave multirotor. MX382001B (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP15400058.2A EP3184425B1 (en) 2015-12-21 2015-12-21 Multirotor aircraft
PCT/EP2016/081574 WO2017108634A1 (en) 2015-12-21 2016-12-16 Multirotor aircraft

Publications (2)

Publication Number Publication Date
MX2018007640A MX2018007640A (es) 2018-09-21
MX382001B true MX382001B (es) 2025-03-13

Family

ID=55300341

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2018007640A MX382001B (es) 2015-12-21 2016-12-16 Aeronave multirotor.

Country Status (6)

Country Link
US (1) US11052998B2 (es)
EP (2) EP3184425B1 (es)
JP (1) JP6663011B2 (es)
CN (1) CN108602558B (es)
MX (1) MX382001B (es)
WO (1) WO2017108634A1 (es)

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Also Published As

Publication number Publication date
MX2018007640A (es) 2018-09-21
EP3393904B1 (en) 2019-10-23
JP6663011B2 (ja) 2020-03-11
CN108602558B (zh) 2022-04-15
CN108602558A (zh) 2018-09-28
JP2018537348A (ja) 2018-12-20
US20200283134A1 (en) 2020-09-10
WO2017108634A1 (en) 2017-06-29
EP3393904A1 (en) 2018-10-31
EP3184425B1 (en) 2018-09-12
US11052998B2 (en) 2021-07-06
EP3184425A1 (en) 2017-06-28

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