BRPI0512472A - processo de melhoramento da manobrabilidade de uma aeronave, dispositivo de melhoramento da manobrabilidade de uma aeronave e aeronave - Google Patents

processo de melhoramento da manobrabilidade de uma aeronave, dispositivo de melhoramento da manobrabilidade de uma aeronave e aeronave

Info

Publication number
BRPI0512472A
BRPI0512472A BRPI0512472-7A BRPI0512472A BRPI0512472A BR PI0512472 A BRPI0512472 A BR PI0512472A BR PI0512472 A BRPI0512472 A BR PI0512472A BR PI0512472 A BRPI0512472 A BR PI0512472A
Authority
BR
Brazil
Prior art keywords
aircraft
maneuverability
rounding
during
improvement process
Prior art date
Application number
BRPI0512472-7A
Other languages
English (en)
Inventor
Stephane Boissenin
Jacques Rosay
Original Assignee
Airbus France
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
Priority claimed from FR0407952A external-priority patent/FR2873094B1/fr
Application filed by Airbus France filed Critical Airbus France
Publication of BRPI0512472A publication Critical patent/BRPI0512472A/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/32—Air braking surfaces
    • 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
    • B64C13/02—Initiating means
    • B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C19/00—Aircraft control not otherwise provided for
    • B64C19/02—Conjoint controls
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • B64C9/20—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by multiple flaps
    • 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
    • G05D1/04—Control of altitude or depth
    • G05D1/06—Rate of change of altitude or depth
    • G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
    • G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
    • G05D1/0676—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing
    • 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
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/30—Wing lift efficiency

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Traffic Control Systems (AREA)
  • Braking Arrangements (AREA)
  • Mobile Radio Communication Systems (AREA)

Abstract

PROCESSO DE MELHORAMENTO DA MANOBRABILIDADE DE UMA AERONAVE, DISPOSITIVO DE MELHORAMENTO DA MANOBRABILIDADE DE UMA AERONAVE E AERONAVE O processo melhora a manobrabilidade de uma aeronave durante a fase de aproximação antes da aterrissagem, seguida da de arredondamento, estando a aeronave equipada com aerofreios. De acordo com o processo, os aerofreios são colocados numa primeira posição estendida curva CFAA durante a fase de aproximação antes da aterrissagem e, em função de um parâmetro representativo de uma altitude dada e em caso de aproximação sob declive acentuado, comanda-se a sua passagem para uma segunda posição mais retraída do que a primeira posição curva (CFSA), de maneira a obter um arredondamento que permita conservar sensivelmente a mesma incidência, correspondente, em caso de aproximação sob declive acentuado, à obtenção de um arredondamento com referências externas de pilotagem habituais durante a fase de arredondamento.
BRPI0512472-7A 2004-07-16 2005-07-13 processo de melhoramento da manobrabilidade de uma aeronave, dispositivo de melhoramento da manobrabilidade de uma aeronave e aeronave BRPI0512472A (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0407952A FR2873094B1 (fr) 2004-07-16 2004-07-16 Procede et dispositif d'amelioration de la manoeuvrabilite d'un aeronef lors des phases d'approche avant l'atterrissage puis d'arrondi
US61439404P 2004-09-30 2004-09-30
PCT/FR2005/001815 WO2006016070A1 (fr) 2004-07-16 2005-07-13 Procede et dispositif d'amelioration de la manoeuvrabilite d'un aeronef lors des phases d'approche avant l'atterrissage puis d'arrondi

Publications (1)

Publication Number Publication Date
BRPI0512472A true BRPI0512472A (pt) 2008-03-11

Family

ID=37776565

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0512472-7A BRPI0512472A (pt) 2004-07-16 2005-07-13 processo de melhoramento da manobrabilidade de uma aeronave, dispositivo de melhoramento da manobrabilidade de uma aeronave e aeronave

Country Status (6)

Country Link
US (2) US7614587B2 (pt)
EP (1) EP1768899B1 (pt)
JP (1) JP5184884B2 (pt)
BR (1) BRPI0512472A (pt)
CA (1) CA2568848C (pt)
WO (1) WO2006016070A1 (pt)

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US7367530B2 (en) * 2005-06-21 2008-05-06 The Boeing Company Aerospace vehicle yaw generating systems and associated methods
GB2444742B (en) 2006-12-11 2011-06-08 Embraer Aeronautica Sa Flight Control System
FR2911689B1 (fr) * 2007-01-19 2009-04-03 Airbus Sas Procede et dispositif de controle de la vitesse d'un aeronef
DE102007045547A1 (de) * 2007-09-24 2009-04-16 Airbus Deutschland Gmbh Automatische Steuerung eines Hochauftriebssystems eines Flugzeugs
US9671788B2 (en) * 2007-11-27 2017-06-06 The Boeing Company Vertical path control augmentation using lateral control surfaces
DE102009013758A1 (de) * 2009-03-17 2010-09-23 Airbus Deutschland Gmbh Flugzeug mit einer Vorrichtung zur Beeinflussung der Richtungsstabilität des Flugzeugs sowie Verfahren zur Beeinflussung der Richtungsstabilität des Flugzeugs
FR2953627B1 (fr) * 2009-12-04 2012-07-13 Thales Sa Procede d'aide a la rejointe d'une trajectoire verticale de descente et dispositif associe
ES2485294T3 (es) * 2010-08-24 2014-08-13 The Boeing Company Guiado en cuatro dimensiones de una aeronave
US8781653B2 (en) * 2012-01-11 2014-07-15 The Boeing Company Quiet landing attitude modifier for airplane
DE102012001268A1 (de) 2012-01-23 2013-07-25 Airbus Operations Gmbh Verfahren zur Planung eines Landeanflugs eines Flugzeugs, Computerprogrammprodukt, Medium mit einem darauf gespeicherten Landeanflugplan sowie Vorrichtung zur Planung eines Landeanflugs
US9153139B2 (en) 2012-12-21 2015-10-06 Embraer S.A. Steep approach performance improvements and optimization
US9327827B2 (en) * 2013-09-24 2016-05-03 The Boeing Company Leading and trailing edge device deflections during descent of an aircraft
FR3026177B1 (fr) * 2014-09-22 2019-11-01 Thales Procede d'adaptation d'un segment de trajectoire d'aeronef a pente sol constante selon au moins un critere de performance
US11327508B2 (en) * 2015-09-29 2022-05-10 University Of Malta Fast flight trajectory optimisation for in-flight computation and flight management systems
US11987368B2 (en) 2017-06-29 2024-05-21 Bombarder Inc. Aircraft operation during steep approach
US10889369B2 (en) * 2018-08-29 2021-01-12 Textron Innovations Inc. Passive gust alleviation systems for aircraft devices
US20210253268A1 (en) * 2020-01-20 2021-08-19 Honeywell International Inc. Systems and methods that optimize speed brake operations
US12020583B2 (en) 2020-03-10 2024-06-25 Honeywell International Inc. Systems and methods providing assist-to-land and emergency land functions
US12112649B2 (en) 2021-06-22 2024-10-08 Honeywell International Inc. Automatic autoland activation methods and systems
US12344372B2 (en) * 2021-08-19 2025-07-01 Boom Technology, Inc. Variable noise reduction systems for supersonic aircraft, and associated methods

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US2421870A (en) * 1938-01-29 1947-06-10 Dornier Claude Air brake for aircraft
US2369152A (en) * 1943-06-07 1945-02-13 Arthur L Lowell Means for operation of bellowstype wing flaps and the like
US2384997A (en) * 1944-08-03 1945-09-18 Hansson Arthur David Braking device for airplanes
US2462459A (en) * 1945-11-10 1949-02-22 Charles A Bigelow Air resistant brake flap
US2612329A (en) * 1948-11-13 1952-09-30 Northrop Aircraft Inc Aileron, flap, and dive brake
US2791385A (en) * 1952-03-10 1957-05-07 Lockheed Aircraft Corp Landing drag flap and lift spoiler
US3589648A (en) * 1969-01-02 1971-06-29 Lockheed Aircraft Corp Means for controlling the vertical path of an aircraft
US3738594A (en) * 1971-08-16 1973-06-12 Mc Donnell Douglas Corp Lift control mechanism
IT1042517B (it) * 1974-09-17 1980-01-30 Messerschmitt Boelkow Blohm Dispositivo di comando del flap di frenatura di un aered
US4042197A (en) * 1975-09-29 1977-08-16 The Boeing Company Automatic controls for airplane take-off and landing modes
US4087065A (en) * 1977-02-04 1978-05-02 The Boeing Company Electrical control system for actuating inboard spoilers on aircraft
US4093159A (en) * 1977-03-07 1978-06-06 The Ohio State University Research Foundation Semi-automatic aircraft control system
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US4956780A (en) * 1988-12-08 1990-09-11 The Boeing Company Flight path angle command flight control system for landing flare
FR2661149B1 (fr) * 1990-04-24 1992-08-14 Aerospatiale Systeme pour le pilotage d'un avion en tangage.
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Also Published As

Publication number Publication date
JP2008506577A (ja) 2008-03-06
US7614587B2 (en) 2009-11-10
US20070057114A1 (en) 2007-03-15
US20090314897A1 (en) 2009-12-24
JP5184884B2 (ja) 2013-04-17
CA2568848A1 (en) 2006-02-16
EP1768899A1 (fr) 2007-04-04
EP1768899B1 (fr) 2013-12-11
WO2006016070A1 (fr) 2006-02-16
US7896293B2 (en) 2011-03-01
WO2006016070A8 (fr) 2007-03-08
CA2568848C (en) 2013-06-25

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Legal Events

Date Code Title Description
B25A Requested transfer of rights approved

Owner name: AIRBUS OPERATIONS SAS (FR)

Free format text: TRANSFERIDO POR INCORPORACAO DE: AIRBUS FRANCE

B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]
B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2470 DE 08-05-2018 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.