BRPI0802621A2 - sistema de proteção contra estol, turbulência, baixa velocidade e elevada atitude - Google Patents

sistema de proteção contra estol, turbulência, baixa velocidade e elevada atitude Download PDF

Info

Publication number
BRPI0802621A2
BRPI0802621A2 BRPI0802621-1A BRPI0802621A BRPI0802621A2 BR PI0802621 A2 BRPI0802621 A2 BR PI0802621A2 BR PI0802621 A BRPI0802621 A BR PI0802621A BR PI0802621 A2 BRPI0802621 A2 BR PI0802621A2
Authority
BR
Brazil
Prior art keywords
flight
turbulence
automatic
control system
low speed
Prior art date
Application number
BRPI0802621-1A
Other languages
English (en)
Inventor
Fabricio Reis Caldeira
Dagfinn Gangsaas
Souza Alvaro Vitor Polati De
Eduardo Da Silva Martins
Marco Tulio Sguerra Vita
Jose Marcio Vieira Dias Jr
Marcos Vinicius Campos
Original Assignee
Embraer Aeronautica Sa
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 Embraer Aeronautica Sa filed Critical Embraer Aeronautica Sa
Publication of BRPI0802621A2 publication Critical patent/BRPI0802621A2/pt
Publication of BRPI0802621B1 publication Critical patent/BRPI0802621B1/pt

Links

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0816Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
    • G05D1/0833Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability using limited authority control

Landscapes

  • Engineering & Computer Science (AREA)
  • Computer Security & Cryptography (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Feedback Control In General (AREA)
  • Traffic Control Systems (AREA)

Abstract

SISTEMA DE PROTEçãO CONTRA ESTOL, TURBULêNCIA, BAIXA VELOCIDADE E ELEVADA ALTITUDE. A presente invenção apresenta um sistema de controle de vóo que move elevadores de acordo com um comando de piloto somado a um comando automático. O sistema de controle d.e vóo monitora um conjunto de parâmetros de vóo para determinar se o veículo de vóo está operando dentro de um envoltório permitido. O sistema de controle de vóo incorpora proteções automáticas pelo comando de elevador automático se o veículo de vóo estiver perto de seus limites de envoltório. A implementação não-limitativa ilustrativa exemplificativa provê proteções automáticas para proteger o veículo de vóo contra baixas velocidades, elevadas atitude, stol e turbulências.
BRPI0802621A 2007-09-04 2008-07-02 sistema de proteção contra estol, turbulência, baixa velocidade e elevada atitude BRPI0802621B1 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/849,501 US8165733B2 (en) 2007-09-04 2007-09-04 Stall, buffeting, low speed and high attitude protection system
PCT/BR2008/000189 WO2009030005A2 (en) 2007-09-04 2008-07-02 Stall, buffeting, low speed and high attitude protection systems

Publications (2)

Publication Number Publication Date
BRPI0802621A2 true BRPI0802621A2 (pt) 2011-08-30
BRPI0802621B1 BRPI0802621B1 (pt) 2020-04-14

Family

ID=40408742

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0802621A BRPI0802621B1 (pt) 2007-09-04 2008-07-02 sistema de proteção contra estol, turbulência, baixa velocidade e elevada atitude

Country Status (5)

Country Link
US (2) US8165733B2 (pt)
EP (1) EP2188144B8 (pt)
CN (2) CN101939187B (pt)
BR (1) BRPI0802621B1 (pt)
WO (1) WO2009030005A2 (pt)

Families Citing this family (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8165733B2 (en) * 2007-09-04 2012-04-24 Embraer S.A. Stall, buffeting, low speed and high attitude protection system
US9156546B2 (en) * 2008-03-11 2015-10-13 The Boeing Company Active-inceptor tactile-cueing hands-off rate-limit
JP5594996B2 (ja) * 2009-09-14 2014-09-24 三菱重工業株式会社 航空機の操縦システム
DE102010035825A1 (de) * 2010-08-30 2012-03-01 Liebherr-Aerospace Lindenberg Gmbh Steuerorgansystem und Vorrichtung zur Erzeugung eines virtuellen Echtzeitmodells
USD702622S1 (en) * 2010-12-02 2014-04-15 OAO Head Company of The Financial-Industrial Group “Rossiiskii Aviatsionnyi Konsortium” Airplane
PE20141399A1 (es) 2011-01-30 2014-10-24 Elbit Systems Ltd Limitacion dinamica de inclinaciones de superficies de control de vuelo monobloque durante condiciones de susceptibilidad a entrada en perdida
US8742973B1 (en) * 2011-09-22 2014-06-03 Rockwell Collins, Inc. System and method of determining increased turbulence susceptibility with elapsed flight time
FR2986065B1 (fr) * 2012-01-23 2015-04-17 Airbus Operations Sas Procede et dispositif d'affichage d'informations d'assiette sur un avion lors d'un decollage.
US8653990B2 (en) * 2012-06-18 2014-02-18 The Boeing Company Stall management system
FR3012112B1 (fr) * 2013-10-22 2017-04-21 Ratier Figeac Soc Procede de surveillance de fonctionnement d'un dispositif de pilotage d'aeronef et dispositif de pilotage d'aeronef ainsi surveille
USD747259S1 (en) * 2014-10-13 2016-01-12 Gulfstream Aerospace Corporation Pair of aircraft wings
US9845146B2 (en) * 2015-10-23 2017-12-19 The Boeing Company Zoom climb prevention system for enhanced performance
US10261518B2 (en) * 2015-11-12 2019-04-16 Embraer S.A. Method and apparatus for protecting aircraft maximum lift capability
CN105468008B (zh) * 2015-12-12 2018-03-02 中国航空工业集团公司西安飞机设计研究所 一种飞机迎角保护控制方法
US9989972B2 (en) * 2016-02-22 2018-06-05 The Boeing Company Systems and methods to prevent an aircraft from tail contact with the ground
US10752339B2 (en) * 2016-03-18 2020-08-25 The Boeing Company Customizing aircraft performance systems and methods
CN106347636B (zh) * 2016-08-30 2019-03-01 中国航空工业集团公司西安飞行自动控制研究所 一种推杆失速保护控制方法
US10481615B2 (en) * 2017-03-01 2019-11-19 Bell Textron Inc. Rotorcraft control mode transition smoothing
US11067981B2 (en) 2017-03-01 2021-07-20 Textron Innovations, Inc. Aircraft control mode transition smoothing
US10228692B2 (en) 2017-03-27 2019-03-12 Gulfstream Aerospace Corporation Aircraft flight envelope protection and recovery autopilot
US10605822B2 (en) * 2017-06-12 2020-03-31 The Boeing Company System for estimating airspeed of an aircraft based on a weather buffer model
US10921824B2 (en) * 2017-08-31 2021-02-16 Embraer S.A. Attitude fine tracking system for manual aircraft control
US10671090B2 (en) * 2017-09-01 2020-06-02 Embraer S.A. Automatic command for lift control devices
JP7106160B2 (ja) * 2018-03-27 2022-07-26 株式会社Acsl 無人航空機
CA3037923C (en) * 2018-03-29 2025-12-09 Bombardier Inc. System and method for improving the operation of an aircraft
US11480980B2 (en) 2018-09-19 2022-10-25 Rosemount Aerospace Inc. Aircraft anti-spin systems
US11194345B2 (en) 2019-09-11 2021-12-07 The Boeing Company Systems and methods for pitch axis envelope limiting of an aircraft
US11841713B2 (en) * 2020-01-07 2023-12-12 Gulfstream Aerospace Corporation Controllers and aircraft with takeoff stall protection system
CN111959799B (zh) * 2020-07-24 2023-10-20 中国航空工业集团公司西安飞行自动控制研究所 一种民用支线客机的失速保护方法
CN112357060B (zh) * 2020-10-29 2022-08-02 天津腾云智航科技有限公司 一种固定翼无人机襟翼高程收敛控制方法
CN117330084B (zh) * 2023-12-01 2024-02-23 中国航空工业集团公司西安飞机设计研究所 一种民用飞机姿态包线确定方法

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3033496A (en) * 1959-09-23 1962-05-08 Honeywell Regulator Co Control apparatus
US3345018A (en) * 1965-05-24 1967-10-03 Honeywell Inc Dirigible craft control apparatus
US3584814A (en) * 1967-07-18 1971-06-15 Bell Aerospace Corp Stability and control augmentation system
WO1984001345A1 (en) * 1982-09-30 1984-04-12 Boeing Co Total energy based flight control system
US4849900A (en) * 1986-05-02 1989-07-18 The Boeing Company Flight control system and method
US5446666A (en) * 1994-05-17 1995-08-29 The Boeing Company Ground state-fly state transition control for unique-trim aircraft flight control system
US5596499A (en) * 1995-02-21 1997-01-21 The Boeing Company Control law mode switching between rate command and attitude command control systems
US5722620A (en) * 1995-05-15 1998-03-03 The Boeing Company Aircraft pitch-axis stability and command augmentation
US5746392A (en) * 1995-05-15 1998-05-05 The Boeing Company Autopilot/flight director underspeed protection system
CN1230721C (zh) * 1996-08-22 2005-12-07 波音公司 飞机俯仰增稳和指令增控系统
US6062513A (en) * 1998-09-14 2000-05-16 The Boeing Company Total energy based flight control system
US6246929B1 (en) * 1999-06-16 2001-06-12 Lockheed Martin Corporation Enhanced stall and recovery control system
US6236914B1 (en) * 1999-06-16 2001-05-22 Lockheed Martin Corporation Stall and recovery control system
US6422517B1 (en) * 1999-12-02 2002-07-23 Boeing Company Aircraft tailstrike avoidance system
FR2841008B1 (fr) * 2002-06-12 2004-08-20 Airbus France Procede et systeme de pilotage d'un aeronef
US6885917B2 (en) * 2002-11-07 2005-04-26 The Boeing Company Enhanced flight control systems and methods for a jet powered tri-mode aircraft
FR2852683B1 (fr) * 2003-03-19 2005-05-20 Airbus France Procede et dispositif d'aide au pilotage d'un aeronef lors d'une approche de non precision pendant une phase d'atterrissage.
FR2874204B1 (fr) * 2004-08-13 2007-12-14 Airbus France Sas Systeme de commande de vol electriques pour les gouvernes de profondeur d'un aeronef
US7742846B2 (en) * 2006-06-02 2010-06-22 Sikorsky Aircraft Corporation Surface contact override landing scheme for a FBW rotary-wing aircraft
US8165733B2 (en) * 2007-09-04 2012-04-24 Embraer S.A. Stall, buffeting, low speed and high attitude protection system

Also Published As

Publication number Publication date
EP2188144B8 (en) 2018-02-21
CN101939187A (zh) 2011-01-05
WO2009030005A3 (en) 2010-02-04
CN103324190B (zh) 2016-02-10
US20090062973A1 (en) 2009-03-05
CN103324190A (zh) 2013-09-25
CN101939187B (zh) 2015-06-24
US20110054720A1 (en) 2011-03-03
US8214089B2 (en) 2012-07-03
EP2188144A4 (en) 2011-12-21
WO2009030005A2 (en) 2009-03-12
EP2188144B1 (en) 2017-10-18
WO2009030005A8 (en) 2010-11-18
EP2188144A2 (en) 2010-05-26
BRPI0802621B1 (pt) 2020-04-14
US8165733B2 (en) 2012-04-24

Similar Documents

Publication Publication Date Title
BRPI0802621A2 (pt) sistema de proteção contra estol, turbulência, baixa velocidade e elevada atitude
WO2008070944A3 (en) Flight control system
BR112015032242A2 (pt) vidro anti-solar
BRPI1107019A8 (pt) Sistema para controlar uma porta, e método para executar uma função de segurança no controle de uma porta
BR112013021765A2 (pt) sistema de controle de aeronave, aeronave, programa de controle de aeronave e método para o controle de aeronave
WO2011147571A3 (en) A device for an adjustable flap of a wing
BR112013027237A2 (pt) escalonamento de limites de empuxo modificado para controle de assimetria de empuxo
ATE544673T1 (de) Klappbarer kantenzaun einer hinterkantklappe und betriebsverfahren
WO2008036618A3 (en) Automatic heading control system for tiltrotor aircraft and helicopters
BR112015003889A2 (pt) mecanismo de rotor de sustentação e aeronave de decolagem e aterrissagem vertical
BR112015024149A2 (pt) estrutura de suporte leve, método para produzir uma estrutura de suporte leve e um painel em sanduíche de compósito, e, painel em sanduíche de compósito
BR112017004139A2 (pt) multi-rotor com asa inclinada
BR112013033075A2 (pt) método e sistema para o controle da velocidade do motor e de maquinário de engenharia do tipo lança de guindaste
WO2008065664A3 (en) Flight control cockpit modes in ducted fan vtol vehicles
BR112013029847A2 (pt) simbologia de velocidade de voo baseada em inclinação e potência não confiável de mostrador de voo primário
BR112014008198A2 (pt) válvula de controle sanguíneo de múltiplo uso contendo frestas circunferênciais
BR112017026456A2 (pt) uso da direção assistida para compensar os efeitos negativos introduzidos por um diferencial de deslizamento limitado
DE502007005892D1 (de) N klappenwirbel beeinflussenden vorrichtung
BR112012015635A2 (pt) avião e sistema de controle de um avião propelido por pelo menos um motor a jato alojado em uma nacela.
BR112018071313A2 (pt) sistema e método de controle de acelerador
BR112013022291A2 (pt) método de operar de maneira simultânea atuadores para movimentar flaps de aeronave, um dispositivo de acionamento de flap de aeronave e uma aeronave dotada de tal dispositivo
BRPI0509558A (pt) sistemas e métodos que empregam um sistema que evita colisão a fim de aumentar a percepção de um piloto
BR112015002669A2 (pt) método, programa e sistema de controle para controlar a pré-carga de um rolamento de uma turbina eólica, e turbina eólica compreendendo tal sistema de controle
BR112015030654A2 (pt) dispositivo de controle para motor de combustão interna
BR112014006543A2 (pt) sistema de microprocessador com ambiente de tempo de execução seguro

Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B25D Requested change of name of applicant approved

Owner name: EMBRAER S.A. (BR/SP)

B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 10 (DEZ) ANOS CONTADOS A PARTIR DE 14/04/2020, OBSERVADAS AS CONDICOES LEGAIS.