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BR112022011925A2 - Sistema de controle de freio de aeronave e método para controlar a guinada durante a frenagem da aeronave - Google Patents

Sistema de controle de freio de aeronave e método para controlar a guinada durante a frenagem da aeronave

Info

Publication number
BR112022011925A2
BR112022011925A2 BR112022011925A BR112022011925A BR112022011925A2 BR 112022011925 A2 BR112022011925 A2 BR 112022011925A2 BR 112022011925 A BR112022011925 A BR 112022011925A BR 112022011925 A BR112022011925 A BR 112022011925A BR 112022011925 A2 BR112022011925 A2 BR 112022011925A2
Authority
BR
Brazil
Prior art keywords
yaw
aircraft
brake control
control system
braking
Prior art date
Application number
BR112022011925A
Other languages
English (en)
Inventor
L Hill James
N Roe David
Burkhalter Kurt
Robert Piercy Quickfall Benjamin
Original Assignee
Meggitt Aircraft Braking Systems Corp
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 Meggitt Aircraft Braking Systems Corp filed Critical Meggitt Aircraft Braking Systems Corp
Publication of BR112022011925A2 publication Critical patent/BR112022011925A2/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60T—VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF; BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL; ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL; PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OF VEHICLES; VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES
    • B60T11/00—Transmitting braking action from initiating means to ultimate brake actuator without power assistance or drive or where such assistance or drive is irrelevant
    • B60T11/10—Transmitting braking action from initiating means to ultimate brake actuator without power assistance or drive or where such assistance or drive is irrelevant transmitting by fluid means, e.g. hydraulic
    • B60T11/16—Master control, e.g. master cylinders
    • B60T11/20—Tandem, side-by-side, or other multiple master cylinder units
    • B60T11/21—Tandem, side-by-side, or other multiple master cylinder units with two pedals operating on respective circuits, pressures therein being equalised when both pedals are operated together, e.g. for steering
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60T—VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF; BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL; ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL; PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OF VEHICLES; VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES
    • B60T7/00—Brake-action initiating means
    • B60T7/02—Brake-action initiating means for personal initiation
    • B60T7/04—Brake-action initiating means for personal initiation foot actuated
    • B60T7/042—Brake-action initiating means for personal initiation foot actuated by electrical means, e.g. using travel or force sensors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60T—VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF; BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL; ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL; PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OF VEHICLES; VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES
    • B60T8/00—Arrangements for adjusting wheel-braking force to meet varying vehicular or ground-surface conditions, e.g. limiting or varying distribution of braking force
    • B60T8/17—Using electrical or electronic regulation means to control braking
    • B60T8/1701—Braking or traction control means specially adapted for particular types of vehicles
    • B60T8/1703—Braking or traction control means specially adapted for particular types of vehicles for aircrafts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60T—VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF; BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL; ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL; PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OF VEHICLES; VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES
    • B60T8/00—Arrangements for adjusting wheel-braking force to meet varying vehicular or ground-surface conditions, e.g. limiting or varying distribution of braking force
    • B60T8/17—Using electrical or electronic regulation means to control braking
    • B60T8/1755—Brake regulation specially adapted to control the stability of the vehicle, e.g. taking into account yaw rate or transverse acceleration in a curve
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60T—VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF; BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL; ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL; PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OF VEHICLES; VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES
    • B60T8/00—Arrangements for adjusting wheel-braking force to meet varying vehicular or ground-surface conditions, e.g. limiting or varying distribution of braking force
    • B60T8/32—Arrangements for adjusting wheel-braking force to meet varying vehicular or ground-surface conditions, e.g. limiting or varying distribution of braking force responsive to a speed condition, e.g. acceleration or deceleration
    • B60T8/321—Arrangements for adjusting wheel-braking force to meet varying vehicular or ground-surface conditions, e.g. limiting or varying distribution of braking force responsive to a speed condition, e.g. acceleration or deceleration deceleration
    • B60T8/325—Systems specially adapted for aircraft
    • 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
    • B64C25/426—Braking devices providing an automatic sequence of braking
    • 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
    • B64C25/44—Actuating mechanisms
    • B64C25/46—Brake regulators for preventing skidding or aircraft somersaulting
    • 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
    • B64C25/44—Actuating mechanisms
    • B64C25/48—Actuating mechanisms differentially operated for steering purposes

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transportation (AREA)
  • Regulating Braking Force (AREA)

Abstract

SISTEMA DE CONTROLE DE FREIO DE AERONAVE E MÉTODO PARA CONTROLAR A GUINADA DURANTE A FRENAGEM DA AERONAVE. Apresenta um sistema de controle de freio de aeronave que acomoda a guinada desejada para direção, enquanto elimina substancialmente a guinada indesejada. O sistema avalia os sinais de comando de freio do piloto, os sinais correspondentes aos parâmetros da aeronave e os sinais com base nos parâmetros de controle de freio, determinando a partir deles uma quantidade de guinada desejada pelo piloto. A taxa de guinada instantânea é monitorada e comparada com a taxa de guinada desejada. Um sinal de erro correspondente à diferença entre as taxas de guinada instantânea e real é calculado e esse sinal de erro é empregado para modificar um diferencial de frenagem entre os freios direito e esquerdo para eliminar ou reduzir substancialmente a guinada indesejada.
BR112022011925A 2019-12-20 2020-12-18 Sistema de controle de freio de aeronave e método para controlar a guinada durante a frenagem da aeronave BR112022011925A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201962951500P 2019-12-20 2019-12-20
PCT/US2020/065877 WO2021127352A1 (en) 2019-12-20 2020-12-18 Yaw reduction system and method for aircraft braking

Publications (1)

Publication Number Publication Date
BR112022011925A2 true BR112022011925A2 (pt) 2022-09-06

Family

ID=76476736

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112022011925A BR112022011925A2 (pt) 2019-12-20 2020-12-18 Sistema de controle de freio de aeronave e método para controlar a guinada durante a frenagem da aeronave

Country Status (6)

Country Link
US (1) US11834160B2 (pt)
EP (1) EP4077076B1 (pt)
BR (1) BR112022011925A2 (pt)
CA (1) CA3161846A1 (pt)
ES (1) ES3014193T3 (pt)
WO (1) WO2021127352A1 (pt)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114671012A (zh) * 2022-03-31 2022-06-28 西安航空制动科技有限公司 一种基于防滑同步的飞机防滑刹车系统及防偏航控制方法
GB2626530A (en) * 2023-01-19 2024-07-31 Airbus Operations Ltd System for controlling aircraft ground manoeuvres

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3839818A (en) * 1973-10-18 1974-10-08 E Heggedal Glider with automatically releasing foldable wings
US5456523A (en) * 1994-01-19 1995-10-10 Mcdonnell Douglas Corporation Multi-wheel brake system
US5671899A (en) * 1996-02-26 1997-09-30 Lockheed Martin Corporation Airborne vehicle with wing extension and roll control
US6056237A (en) * 1997-06-25 2000-05-02 Woodland; Richard L. K. Sonotube compatible unmanned aerial vehicle and system
US6183051B1 (en) * 1999-02-01 2001-02-06 Aircraft Braking Systems Corp. Fail safe electrical brake control system for aircraft
US6882920B2 (en) * 2003-04-29 2005-04-19 Goodrich Corporation Brake control system
US8016366B2 (en) * 2006-06-02 2011-09-13 Goodrich Corporation Differential brake control and weighted average wheel speed for brake control system
FR2924831B1 (fr) * 2007-12-11 2010-11-19 Airbus France Procede et dispositif de generation d'un ordre de vitesse de lacet pour un aeronef roulant au sol
US8386094B2 (en) * 2009-01-29 2013-02-26 Hydro-Aire, Inc. Taxi brake inhibit system
US9227608B2 (en) * 2009-08-12 2016-01-05 Meggitt Aircraft Braking Systems Decentralized electric brake system
GB2505942B (en) * 2012-09-17 2015-06-10 Blue Bear Systems Res Ltd Morphing foil or wing
US9296468B1 (en) * 2012-09-21 2016-03-29 Brandebury Tool Company, Inc. Aerial vehicle with separation of winged surfaces in first and second flexed states
US9896194B2 (en) * 2014-05-28 2018-02-20 Goodrich Corporation Autobraking system with course trajectory adjustment
US9555873B1 (en) * 2015-11-11 2017-01-31 Area-I Inc. Aerial vehicle with deployable components
US10300897B2 (en) * 2017-05-15 2019-05-28 Goodrich Corporation Brake load balance and runway centering techniques
US10259435B2 (en) * 2017-05-15 2019-04-16 Goodrich Corporation Deceleration pedal control for braking systems

Also Published As

Publication number Publication date
US11834160B2 (en) 2023-12-05
CA3161846A1 (en) 2021-06-24
WO2021127352A1 (en) 2021-06-24
US20230094913A1 (en) 2023-03-30
EP4077076A1 (en) 2022-10-26
EP4077076B1 (en) 2025-02-05
ES3014193T3 (en) 2025-04-21
EP4077076A4 (en) 2023-08-23

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