PT2440984E - Sistema eletrónico de controlo de voo para um avião capaz de voo estacionário - Google Patents

Sistema eletrónico de controlo de voo para um avião capaz de voo estacionário Download PDF

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Publication number
PT2440984E
PT2440984E PT107456766T PT10745676T PT2440984E PT 2440984 E PT2440984 E PT 2440984E PT 107456766 T PT107456766 T PT 107456766T PT 10745676 T PT10745676 T PT 10745676T PT 2440984 E PT2440984 E PT 2440984E
Authority
PT
Portugal
Prior art keywords
hovering
control system
flight control
electronic flight
aircraft capable
Prior art date
Application number
PT107456766T
Other languages
English (en)
Inventor
Fabio Nannoni
Pierre Abdel Nour
Marco Cicale
Original Assignee
Agustawestland Spa
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 Agustawestland Spa filed Critical Agustawestland Spa
Publication of PT2440984E publication Critical patent/PT2440984E/pt

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Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D13/00—Control of linear speed; Control of angular speed; Control of acceleration or deceleration, e.g. of a prime mover
    • G05D13/62—Control of linear speed; Control of angular speed; Control of acceleration or deceleration, e.g. of a prime mover characterised by the use of electric means, e.g. use of a tachometric dynamo, use of a transducer converting an electric value into a displacement
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0858—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted for vertical take-off of aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
    • B64C27/56—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement characterised by the control initiating means, e.g. manually actuated
    • B64C27/57—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement characterised by the control initiating means, e.g. manually actuated automatic or condition responsive, e.g. responsive to rotor speed, torque or thrust

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Physics & Mathematics (AREA)
  • Remote Sensing (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Mechanical Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Toys (AREA)
  • Measuring Fluid Pressure (AREA)
  • Control Of Multiple Motors (AREA)
  • Control Of Electric Motors In General (AREA)
PT107456766T 2009-06-10 2010-06-10 Sistema eletrónico de controlo de voo para um avião capaz de voo estacionário PT2440984E (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT000079U ITTO20090079U1 (it) 2009-06-10 2009-06-10 Sistema per la gestione ed il controllo della velocita' di uno o piu' rotori di un aeromobile atto a volare a punto fisso

Publications (1)

Publication Number Publication Date
PT2440984E true PT2440984E (pt) 2014-07-28

Family

ID=43309288

Family Applications (1)

Application Number Title Priority Date Filing Date
PT107456766T PT2440984E (pt) 2009-06-10 2010-06-10 Sistema eletrónico de controlo de voo para um avião capaz de voo estacionário

Country Status (10)

Country Link
US (1) US8989921B2 (pt)
EP (1) EP2440984B1 (pt)
JP (1) JP5543585B2 (pt)
KR (1) KR101652315B1 (pt)
CN (1) CN102483630B (pt)
IT (1) ITTO20090079U1 (pt)
PL (1) PL2440984T3 (pt)
PT (1) PT2440984E (pt)
RU (1) RU2529573C2 (pt)
WO (1) WO2010143051A2 (pt)

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Also Published As

Publication number Publication date
KR20120037460A (ko) 2012-04-19
JP5543585B2 (ja) 2014-07-09
WO2010143051A3 (en) 2012-01-05
PL2440984T3 (pl) 2014-12-31
US8989921B2 (en) 2015-03-24
ITTO20090079U1 (it) 2010-12-11
EP2440984B1 (en) 2014-05-21
CN102483630B (zh) 2014-03-05
JP2012529401A (ja) 2012-11-22
EP2440984A2 (en) 2012-04-18
KR101652315B1 (ko) 2016-08-30
RU2529573C2 (ru) 2014-09-27
CN102483630A (zh) 2012-05-30
RU2011154187A (ru) 2013-07-20
WO2010143051A2 (en) 2010-12-16
US20120153074A1 (en) 2012-06-21

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