BRPI0516920A - método para intensificar a eficiência de frenagem de uma aeronave taxiando no solo e dispositivo para implementar método - Google Patents

método para intensificar a eficiência de frenagem de uma aeronave taxiando no solo e dispositivo para implementar método

Info

Publication number
BRPI0516920A
BRPI0516920A BRPI0516920-8A BRPI0516920A BRPI0516920A BR PI0516920 A BRPI0516920 A BR PI0516920A BR PI0516920 A BRPI0516920 A BR PI0516920A BR PI0516920 A BRPI0516920 A BR PI0516920A
Authority
BR
Brazil
Prior art keywords
ground
enhancing
braking efficiency
aircraft taxiing
implementing
Prior art date
Application number
BRPI0516920-8A
Other languages
English (en)
Inventor
Gerard Mathieu
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
Application filed by Airbus France filed Critical Airbus France
Publication of BRPI0516920A publication Critical patent/BRPI0516920A/pt
Publication of BRPI0516920B1 publication Critical patent/BRPI0516920B1/pt

Links

Classifications

    • 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
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/42—Arrangement or adaptation of brakes

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Mechanical Engineering (AREA)
  • Braking Arrangements (AREA)
  • Vehicle Body Suspensions (AREA)
  • Elevator Control (AREA)
  • Hydraulic Control Valves For Brake Systems (AREA)
  • Consolidation Of Soil By Introduction Of Solidifying Substances Into Soil (AREA)
  • Testing Of Balance (AREA)

Abstract

MéTODO PARA INTENSIFICAR A EFICIêNCIA DE FRENAGEM DE UNA AERONAVE TAXIANDO NO SOLO E DISPOSITIVO PARA IMPLEMENTAR MéTODO. De acordo com a invenção, os profundores (8) e/ou o estabilizador horizontal ajustável (6) são operados de tal modo que uma sustentação negativa (DP2) seja gerada e um momento de nariz para cima (CDP) seja assim criado para compensar o movimento de nariz para baixo (CB) resultante de frenagem. O valor da sustentação negativa (DP2) combina com a força vertical exercida pelo solo no trem de aterrisagem dianteiro (12) , cuja força está sujeita a um valor de referência (Fav3).
BRPI0516920-8A 2004-11-02 2005-10-18 Método para intensificar a eficiência de frenagem de uma aeronave taxiando no solo e dispositivo para implementar método BRPI0516920B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0411634A FR2877312B1 (fr) 2004-11-02 2004-11-02 Procede et dispositif pour ameliorer l'efficacite de freinage d'un aeronef roulant sur le sol
FR0411634 2004-11-02
PCT/FR2005/002574 WO2006048519A1 (fr) 2004-11-02 2005-10-18 Procede et dispositif pour ameliorer l'efficacite de freinage d'un aeronef roulant sur le sol

Publications (2)

Publication Number Publication Date
BRPI0516920A true BRPI0516920A (pt) 2008-09-23
BRPI0516920B1 BRPI0516920B1 (pt) 2018-01-16

Family

ID=34950931

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0516920-8A BRPI0516920B1 (pt) 2004-11-02 2005-10-18 Método para intensificar a eficiência de frenagem de uma aeronave taxiando no solo e dispositivo para implementar método

Country Status (11)

Country Link
US (1) US7708223B2 (pt)
EP (1) EP1807304B1 (pt)
JP (1) JP4714221B2 (pt)
CN (1) CN100509557C (pt)
AT (1) ATE389582T1 (pt)
BR (1) BRPI0516920B1 (pt)
CA (1) CA2581436C (pt)
DE (1) DE602005005513T2 (pt)
FR (1) FR2877312B1 (pt)
RU (1) RU2341409C1 (pt)
WO (1) WO2006048519A1 (pt)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2893909B1 (fr) * 2005-11-29 2007-12-21 Airbus France Sas Procede pour assurer la securite d'un aeronef volant horizontalement a faible vitesse.
US8548652B2 (en) * 2006-01-31 2013-10-01 Hydro-Aire, Inc., Subsidiary Of Crane Co. System for reducing carbon brake wear
FR2918638B1 (fr) * 2007-07-09 2010-02-26 Airbus France Systeme de limitation des oscillations en tangage applique a un aeronef.
US20100301170A1 (en) * 2009-05-29 2010-12-02 Arin Boseroy Control system for actuation system
FR2973776B1 (fr) * 2011-04-07 2013-04-05 Messier Bugatti Architecture de systeme de freinage pour aeronef.
FR2982822B1 (fr) * 2011-11-22 2014-08-01 Messier Bugatti Dowty Procede de gestion du freinage d'un aeronef permettant de limiter son tangage
RU2484279C1 (ru) * 2011-12-19 2013-06-10 Николай Евгеньевич Староверов Способ повышения эффективности торможения самолета на пробеге и повышения безопасности при взлете и посадке и устройство для его реализации
CN102582602B (zh) * 2012-03-05 2014-12-31 西安航空制动科技有限公司 一种飞机碳刹车盘湿态下刹车效率的控制方法
GB201315012D0 (en) 2013-08-22 2013-10-02 Airbus Uk Ltd Aircraft autonomous pushback
CN103612750A (zh) * 2013-11-20 2014-03-05 渭南高新区晨星专利技术咨询有限公司 一种飞机防滑刹车控制方法
US10648455B2 (en) * 2014-10-14 2020-05-12 Twingtec Ag Flying apparatus
US9731813B2 (en) * 2014-11-12 2017-08-15 The Boeing Company Methods and apparatus to control aircraft horizontal stabilizers
EP3448749B1 (en) * 2016-04-25 2020-07-01 Bombardier Inc. Aircraft pitch control system with electronically geared elevator
US10086925B2 (en) * 2016-07-13 2018-10-02 Embraer S.A. Use of automatic pitch control to improve braking performance
CN108398883B (zh) * 2018-02-27 2021-02-09 北京控制工程研究所 一种rlv进场着陆轨迹快速推演及确定方法
CN109157847B (zh) * 2018-11-06 2023-11-24 大连理工大学 一种基于碳杆的固定翼航模结构及安装方法
RU2722597C1 (ru) * 2019-10-18 2020-06-02 Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФГУП "ЦАГИ") Способ торможения летательного аппарата при посадке
CN111976963A (zh) * 2020-07-08 2020-11-24 西安航空制动科技有限公司 一种6轮车架主起落架飞机电传刹车控制系统及方法
US11897597B2 (en) * 2020-07-20 2024-02-13 The Boeing Company Flap pressure shape biasing
WO2025030231A1 (en) * 2023-08-10 2025-02-13 Safran Landing Systems Canada Inc. Pitch attitude control system for increasing aircraft braking efficiency

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB754405A (en) * 1954-04-13 1956-08-08 Goodyear Tire & Rubber Apparatus for landing aircraft
FR2542277B1 (fr) * 1983-03-08 1985-06-28 Messier Hispano Sa Procede et dispositif de commande du freinage d'un aeronef lors de l'atterrissage des qu'il a pris contact avec le sol d'une piste par ses trains d'atterrissage principaux et quand le train avant n'a pas encore pris contact avec le sol
US4646242A (en) * 1984-01-27 1987-02-24 The Boeing Company Aircraft automatic braking system
US4646254A (en) * 1984-10-09 1987-02-24 Gte Government Systems Corporation Noise threshold estimating method for multichannel signal processing
JPH01106765A (ja) * 1987-10-19 1989-04-24 Yokogawa Electric Corp アンチスキッドブレーキシステム
DE3803015A1 (de) * 1988-02-02 1989-08-10 Pfister Gmbh Verfahren und system zum betrieb eines luftfahrzeugs
RU2009077C1 (ru) * 1991-12-16 1994-03-15 Мамулин Андрей Викторович Устройство для управления торможением колес транспортного средства
EP0754405A1 (en) * 1995-07-21 1997-01-22 Tiziano Faccia Improved machine for shredding and mixing fibrous products for technical use in zoo
JPH09164932A (ja) * 1995-12-15 1997-06-24 Aisin Seiki Co Ltd 車両の運動制御装置
US5823479A (en) * 1996-05-20 1998-10-20 The Boeing Company Landing attitude modifier for airplane
US6220676B1 (en) * 1997-05-09 2001-04-24 The B. F. Goodrich Company Antiskid control of multi-wheel vehicles using coupled and decoupled Kalman filtering incorporating pitch weight transfer

Also Published As

Publication number Publication date
CN101052564A (zh) 2007-10-10
EP1807304A1 (fr) 2007-07-18
JP4714221B2 (ja) 2011-06-29
RU2341409C1 (ru) 2008-12-20
WO2006048519A1 (fr) 2006-05-11
CA2581436A1 (fr) 2006-05-11
CA2581436C (fr) 2012-05-29
ATE389582T1 (de) 2008-04-15
BRPI0516920B1 (pt) 2018-01-16
DE602005005513D1 (de) 2008-04-30
FR2877312B1 (fr) 2007-01-12
DE602005005513T2 (de) 2009-04-23
EP1807304B1 (fr) 2008-03-19
FR2877312A1 (fr) 2006-05-05
JP2008518821A (ja) 2008-06-05
CN100509557C (zh) 2009-07-08
US20090065636A1 (en) 2009-03-12
US7708223B2 (en) 2010-05-04

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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

B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]
B21F Lapse acc. art. 78, item iv - on non-payment of the annual fees in time

Free format text: REFERENTE A 16A ANUIDADE.

B24J Lapse because of non-payment of annual fees (definitively: art 78 iv lpi, resolution 113/2013 art. 12)

Free format text: EM VIRTUDE DA EXTINCAO PUBLICADA NA RPI 2640 DE 10-08-2021 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDA A EXTINCAO DA PATENTE E SEUS CERTIFICADOS, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.