BR112013029847A2 - simbologia de velocidade de voo baseada em inclinação e potência não confiável de mostrador de voo primário - Google Patents

simbologia de velocidade de voo baseada em inclinação e potência não confiável de mostrador de voo primário

Info

Publication number
BR112013029847A2
BR112013029847A2 BR112013029847A BR112013029847A BR112013029847A2 BR 112013029847 A2 BR112013029847 A2 BR 112013029847A2 BR 112013029847 A BR112013029847 A BR 112013029847A BR 112013029847 A BR112013029847 A BR 112013029847A BR 112013029847 A2 BR112013029847 A2 BR 112013029847A2
Authority
BR
Brazil
Prior art keywords
tilt
symbology
unreliable
flight
display power
Prior art date
Application number
BR112013029847A
Other languages
English (en)
Other versions
BR112013029847B1 (pt
Inventor
Adam Marshall Thoreen
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Publication of BR112013029847A2 publication Critical patent/BR112013029847A2/pt
Publication of BR112013029847B1 publication Critical patent/BR112013029847B1/pt

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C23/00Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
    • G01C23/005Flight directors

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Navigation (AREA)
  • Traffic Control Systems (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

resumo patente de invenção: "simbologia de velocidade de voo baseada em inclinação e potência não confiável de mostrador de voo primário". a presente invenção refere-se a um sistema para exibir comandos de guia baseados em inclinação e potência e informação de trajetória de voo, para uma variedade de modos de exibição (subida, cruzeiro, descida, aterragem) a pilotos, em resposta a situações em que os dados aéreos medidos não são confiáveis. esta informação é apresentada de maneira intuitiva e prática exatamente quando e onde necessária no mostrador de voo primário. as informações exibidas mudam dinamicamente em resposta aos parâmetros da aeronave.
BR112013029847-2A 2011-05-25 2012-04-17 método e sistema para exibir informações a um piloto de aeronave durante voo real ou simulado BR112013029847B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/115,450 2011-05-25
US13/115,450 US8665120B2 (en) 2011-05-25 2011-05-25 Primary flight display pitch- and power-based unreliable airspeed symbology
PCT/US2012/033931 WO2012161890A1 (en) 2011-05-25 2012-04-17 Primary flight display pitch- and power-based unreliable airspeed symbology

Publications (2)

Publication Number Publication Date
BR112013029847A2 true BR112013029847A2 (pt) 2016-12-13
BR112013029847B1 BR112013029847B1 (pt) 2021-01-12

Family

ID=46051927

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112013029847-2A BR112013029847B1 (pt) 2011-05-25 2012-04-17 método e sistema para exibir informações a um piloto de aeronave durante voo real ou simulado

Country Status (8)

Country Link
US (1) US8665120B2 (pt)
EP (2) EP2715287B1 (pt)
JP (1) JP6012718B2 (pt)
CN (1) CN103562682B (pt)
AU (1) AU2012259346B2 (pt)
BR (1) BR112013029847B1 (pt)
CA (1) CA2826592C (pt)
WO (1) WO2012161890A1 (pt)

Families Citing this family (39)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8761970B2 (en) * 2008-10-21 2014-06-24 The Boeing Company Alternative method to determine the air mass state of an aircraft and to validate and augment the primary method
JP5916283B2 (ja) * 2010-07-01 2016-05-11 三菱重工業株式会社 表示装置、操縦支援システム、及び表示方法
US8977413B2 (en) * 2012-03-07 2015-03-10 Ge Aviation Systems Llc Methods for derated thrust visualization
FR2988835B1 (fr) * 2012-03-28 2015-01-30 Dassault Aviat Procede de determination d'un etat de credibilite de mesures de capteurs d'un aeronef et systeme correspondant
US9128109B1 (en) * 2012-08-20 2015-09-08 The Boeing Company Method and system for detecting errors in indicated air speed
FR2998873B1 (fr) * 2012-11-30 2016-10-14 Airbus Aide au pilotage d'un aeronef en situation de decrochage
FR3008499B1 (fr) * 2013-07-12 2015-08-07 Airbus Operations Sas Procede et dispositif d'affichage en temps reel d'une consigne d'assiette sur un aeronef lors d'un pilotage manuel.
US20150162001A1 (en) * 2013-12-10 2015-06-11 Honeywell International Inc. System and method for textually and graphically presenting air traffic control voice information
US10094668B2 (en) 2014-10-09 2018-10-09 Honeywell International Inc. Systems and methods for producing two independent dissimilar attitude solutions, two independent dissimilar inertial solutions or both from one improved navigation device
US9688416B2 (en) * 2014-10-20 2017-06-27 Honeywell International Inc System and method for isolating attitude failures in aircraft
JP6179000B2 (ja) * 2014-10-27 2017-08-16 エスゼット ディージェイアイ テクノロジー カンパニー リミテッドSz Dji Technology Co.,Ltd 飛行情報を提供する方法、プログラム及び端末
KR101671687B1 (ko) * 2014-12-18 2016-11-03 한국항공우주산업 주식회사 항공기의 지형추적비행용 디스플레이 방법 및 장치
US9964960B2 (en) * 2015-08-19 2018-05-08 Sikorsky Aircraft Corporation Hover attitude trim for vehicle
US10043402B1 (en) * 2015-09-04 2018-08-07 Rockwell Collins, Inc. Flight path cross check
CN105241475B (zh) * 2015-09-24 2017-11-03 江西洪都航空工业集团有限责任公司 一种远距离气体压力快速精确控制方法
FR3045015B1 (fr) * 2015-12-09 2017-12-22 Thales Sa Procede d'affichage d'un "indicateur de directeur d'attitude" dans un systeme de visualisation de tete pour aeronef
FR3046229A1 (fr) * 2015-12-29 2017-06-30 Thales Sa Procede de representation graphique d'une vue synthetique tridimensionnelle du paysage exterieur dans un systeme de visualisation de bord pour aeronef
US9862499B2 (en) * 2016-04-25 2018-01-09 Airbus Operations (S.A.S.) Human machine interface for displaying information relative to the energy of an aircraft
WO2017208179A1 (en) 2016-05-31 2017-12-07 Bombardier Inc. Displaying performance limitations in aircraft display
US9969503B2 (en) * 2016-07-21 2018-05-15 Rockwell Collins, Inc. Head-up display (HUD) stall recovery symbology
US10229606B2 (en) 2016-08-24 2019-03-12 Gulfstream Aerospace Corporation Controllers and aircraft with pitch and flight path based flight director modes
FR3066755B1 (fr) * 2017-05-23 2019-06-07 Airbus Operations Procede et dispositif de surveillance et d'estimation de parametres relatifs au vol d'un aeronef.
CN107238366B (zh) * 2017-05-26 2023-02-28 成都凯天电子股份有限公司 风标式迎角空速传感器保护装置
US10605822B2 (en) * 2017-06-12 2020-03-31 The Boeing Company System for estimating airspeed of an aircraft based on a weather buffer model
CA2972498C (en) * 2017-06-28 2024-01-23 Bombardier Inc. Takeoff pitch guidance system and method
US10175698B1 (en) * 2017-09-11 2019-01-08 Honeywell International Inc. Automatic flight control systems and methods
US10677879B2 (en) * 2017-09-15 2020-06-09 The Boeing Company Depression angle reference tracking system
US10460613B2 (en) * 2017-09-26 2019-10-29 Honeywell International Inc. Method and system for displaying an alignment symbol for indicating deviations between ownship runway course heading and tracking
US10690555B2 (en) 2017-10-17 2020-06-23 Sikorsky Aircraft Corporation Composite airspeed indicator display for compound aircrafts
USD888069S1 (en) * 2018-02-08 2020-06-23 Sikorsky Aircraft Corporation Flight display screen or portion thereof with graphical user interface including a composite indicator
USD881206S1 (en) 2018-02-08 2020-04-14 Sikorsky Aircraft Corporation Flight display screen or portion thereof with graphical user interface including a composite indicator
US10302451B1 (en) 2018-02-20 2019-05-28 The Boeing Company Optimizing climb performance during takeoff using variable initial pitch angle target
US10948511B2 (en) * 2018-03-05 2021-03-16 Honeywell International Inc. Apparatus and method for verifying operation of air data probes
EP3841020B1 (en) * 2018-08-21 2023-01-04 Safran Passenger Innovations, LLC Systems and methods of determining flight phase / motion status of an aircraft
US10957207B2 (en) 2018-09-27 2021-03-23 Honeywell International Inc. Systems and methods for associating critical flight reference data with a flight path vector symbol
US11003196B2 (en) * 2018-12-07 2021-05-11 The Boeing Company Flight control system for determining a common mode pneumatic fault
CN111204469B (zh) * 2019-12-04 2023-06-23 中国航空工业集团公司成都飞机设计研究所 一种飞行能量变化显示系统及显示位置确定方法
US11577853B2 (en) * 2021-04-13 2023-02-14 William M. Fisher Aircraft angle of attack and sideslip angle indicator
CN118603130A (zh) * 2024-08-06 2024-09-06 中国航空工业集团公司沈阳飞机设计研究所 一种飞机飞行姿态感知动态显示方法及装置

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5039037A (en) 1989-09-11 1991-08-13 The Boeing Company Throttle control system having manual and automatic modes of operation
US5029778A (en) * 1989-09-11 1991-07-09 The Boeing Company Throttle control system having real-time-computed thrust vs throttle position function
US5382954A (en) 1993-05-27 1995-01-17 Honeywell Inc. Resolution advisory display instrument for TCAS guidance
US6745113B2 (en) * 2002-06-07 2004-06-01 The Boeing Company Method and system for autoflight information display
EP1462767B1 (en) 2003-02-27 2014-09-03 The Boeing Company Aircraft guidance system and method providing perspective flight guidance
US7342515B2 (en) * 2005-10-12 2008-03-11 Honeywell International, Inc. Hybrid centered head-down aircraft attitude display and method for calculating displayed drift angle limit
FR2903788B1 (fr) * 2006-07-11 2008-11-14 Thales Sa Viseur tete haute a affichage securise
US8761970B2 (en) 2008-10-21 2014-06-24 The Boeing Company Alternative method to determine the air mass state of an aircraft and to validate and augment the primary method
JP5690127B2 (ja) * 2010-12-14 2015-03-25 川崎重工業株式会社 飛行制御装置およびこれを備える飛行体

Also Published As

Publication number Publication date
CN103562682A (zh) 2014-02-05
US20120299753A1 (en) 2012-11-29
AU2012259346A1 (en) 2013-08-29
BR112013029847B1 (pt) 2021-01-12
WO2012161890A1 (en) 2012-11-29
JP2014516006A (ja) 2014-07-07
CA2826592C (en) 2016-02-02
EP2715287B1 (en) 2019-11-13
AU2012259346B2 (en) 2015-05-07
CA2826592A1 (en) 2012-11-29
EP3693705A1 (en) 2020-08-12
EP2715287A1 (en) 2014-04-09
CN103562682B (zh) 2016-03-16
JP6012718B2 (ja) 2016-10-25
US8665120B2 (en) 2014-03-04

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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]
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: 20 (VINTE) ANOS CONTADOS A PARTIR DE 17/04/2012, OBSERVADAS AS CONDICOES LEGAIS.