BRPI0403104A - Sistema de flaps na asa de sustentação de um avião com asas rìgidas - Google Patents

Sistema de flaps na asa de sustentação de um avião com asas rìgidas

Info

Publication number
BRPI0403104A
BRPI0403104A BR0403104-0A BRPI0403104A BRPI0403104A BR PI0403104 A BRPI0403104 A BR PI0403104A BR PI0403104 A BRPI0403104 A BR PI0403104A BR PI0403104 A BRPI0403104 A BR PI0403104A
Authority
BR
Brazil
Prior art keywords
flap system
rigid
wing
support
aircraft
Prior art date
Application number
BR0403104-0A
Other languages
English (en)
Inventor
Martin Recksiek
Harald Rechter
Wolfgang Besing
Original Assignee
Airbus 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 Gmbh filed Critical Airbus Gmbh
Publication of BRPI0403104A publication Critical patent/BRPI0403104A/pt

Links

Classifications

    • 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
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/0005—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification
    • B64C13/50—Transmitting means with power amplification using electrical energy
    • B64C13/505—Transmitting means with power amplification using electrical energy having duplication or stand-by provisions
    • 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
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/0005—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear
    • B64D2045/001—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear for indicating symmetry of flaps deflection

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Toys (AREA)
  • Transmission Devices (AREA)
  • Blinds (AREA)
  • Executing Machine-Instructions (AREA)
  • Radio Relay Systems (AREA)
  • Traffic Control Systems (AREA)
  • Seats For Vehicles (AREA)

Abstract

"SISTEMA DE FLAPS NA ASA DE SUSTENTAçãO DE UM AVIãO COM ASAS RìGIDAS". A presente invenção refere-se a um sistema de flaps na asa de sustentação de um avião com asas rígidas, conforme o preâmbulo da reivindicação 1. Com ela obtém-se um aumento da disponibilidade das funções de flap, que é acompanhada de uma maior flexibilidade funcional do sistema de flaps. O sistema de flaps é monitorado centralizadamente por um dispositivo de controle de vóo interno ao avião, o qual, durante o vóo, é alimentado com dados de vóo atualizados e, em função desses dados, deduz informações de ajuste correspondentes à alteração de flaps de borda anterior e de borda posterior dispostos na asa de sustentação. O dispositivo de controle de vóo está ligado condutivelmente com pelo menos uma unidade central de controle de flaps. Todos os flaps de borda anterior e de borda posterior estão acoplados mecanicamente com acionamentos integrados à asa, os quais estão instalados com mobilidade na borda anterior de asa e na borda posterior de asa da asa de sustentação. Os acionamentos estão ligados condutivelmente com a unidade de controle de flaps e podem ser controlados individualmente por esta.
BR0403104-0A 2003-03-27 2004-03-26 Sistema de flaps na asa de sustentação de um avião com asas rìgidas BRPI0403104A (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE10313728A DE10313728B4 (de) 2003-03-27 2003-03-27 Klappensystem am Tragflügel eines Starrflügel-Flugzeuges

Publications (1)

Publication Number Publication Date
BRPI0403104A true BRPI0403104A (pt) 2005-01-04

Family

ID=32798122

Family Applications (1)

Application Number Title Priority Date Filing Date
BR0403104-0A BRPI0403104A (pt) 2003-03-27 2004-03-26 Sistema de flaps na asa de sustentação de um avião com asas rìgidas

Country Status (9)

Country Link
US (1) US7048234B2 (pt)
EP (1) EP1462361B1 (pt)
JP (1) JP4418698B2 (pt)
AT (1) ATE331660T1 (pt)
BR (1) BRPI0403104A (pt)
CA (1) CA2462217C (pt)
DE (2) DE10313728B4 (pt)
ES (1) ES2266933T3 (pt)
RU (1) RU2346851C2 (pt)

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Also Published As

Publication number Publication date
RU2004109127A (ru) 2005-09-20
EP1462361B1 (de) 2006-06-28
DE10313728A1 (de) 2004-10-28
ES2266933T3 (es) 2007-03-01
EP1462361A1 (de) 2004-09-29
CA2462217C (en) 2011-01-11
DE10313728B4 (de) 2011-07-21
DE502004000856D1 (de) 2006-08-10
JP2004291957A (ja) 2004-10-21
US7048234B2 (en) 2006-05-23
CA2462217A1 (en) 2004-09-27
ATE331660T1 (de) 2006-07-15
US20050151027A1 (en) 2005-07-14
RU2346851C2 (ru) 2009-02-20
JP4418698B2 (ja) 2010-02-17

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