BR0314374A - Dispositivo eletrônico não linear de exibição de parâmetros dinâmicos para aeronaves - Google Patents

Dispositivo eletrônico não linear de exibição de parâmetros dinâmicos para aeronaves

Info

Publication number
BR0314374A
BR0314374A BR0314374-0A BR0314374A BR0314374A BR 0314374 A BR0314374 A BR 0314374A BR 0314374 A BR0314374 A BR 0314374A BR 0314374 A BR0314374 A BR 0314374A
Authority
BR
Brazil
Prior art keywords
dynamic parameter
aircraft
display device
parameter display
electronic dynamic
Prior art date
Application number
BR0314374-0A
Other languages
English (en)
Other versions
BR0314374B1 (pt
Inventor
John Maris
Original Assignee
Marinvent 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 Marinvent Corp filed Critical Marinvent Corp
Publication of BR0314374A publication Critical patent/BR0314374A/pt
Publication of BR0314374B1 publication Critical patent/BR0314374B1/pt

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01D—MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
    • G01D7/00—Indicating measured values
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C23/00—Combined 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Navigation (AREA)
  • Traffic Control Systems (AREA)
  • Control Of Indicators Other Than Cathode Ray Tubes (AREA)
  • Indicating Measured Values (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Controls And Circuits For Display Device (AREA)
  • Steroid Compounds (AREA)
  • Indication And Recording Devices For Special Purposes And Tariff Metering Devices (AREA)

Abstract

"DISPOSITIVO ELETRôNICO NãO LINEAR DE EXIBIçãO DE PARâMETROS DINâMICOS PARA AERONAVES". A presente invenção refere-se a um método e um aparelho que são divulgados para mostrar um parâmetro dinâmico de uma aeronave, o aparelho compreendendo uma unidade de exibição recebendo um sinal de exibição e mostrando uma escala que muda dinamicamente e não-linearmente de acordo com um algoritmo de exibição selecionado, a unidade de exibição ainda mostrando um ponteiro apontando para a referida escala de acordo com uma leitura do referido parâmetro dinâmico, assim, enfatizando uma faixa da referida leitura do referido parâmetro dinâmico.
BRPI0314374-0A 2002-10-04 2003-09-26 "aparelho e método para exibir um parâmetro dinâmico de uma aeronave" BR0314374B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US41580702P 2002-10-04 2002-10-04
US60/415,807 2002-10-04
PCT/CA2003/001424 WO2004031833A2 (en) 2002-10-04 2003-09-26 Electronic non-linear aircraft dynamic parameter display

Publications (2)

Publication Number Publication Date
BR0314374A true BR0314374A (pt) 2005-11-29
BR0314374B1 BR0314374B1 (pt) 2015-01-13

Family

ID=32069906

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0314374-0A BR0314374B1 (pt) 2002-10-04 2003-09-26 "aparelho e método para exibir um parâmetro dinâmico de uma aeronave"

Country Status (11)

Country Link
US (1) US7062364B2 (pt)
EP (1) EP1546655B1 (pt)
JP (1) JP4246155B2 (pt)
CN (1) CN100547353C (pt)
AT (1) ATE320588T1 (pt)
AU (1) AU2003266895A1 (pt)
BR (1) BR0314374B1 (pt)
CA (1) CA2494050C (pt)
DE (1) DE60304053T2 (pt)
ES (1) ES2260639T3 (pt)
WO (1) WO2004031833A2 (pt)

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US7412308B2 (en) * 2003-10-07 2008-08-12 Universal Avionics Systems Corp. Dynamic VSI display
DE102004045094B4 (de) * 2004-09-17 2012-05-03 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren zum automatischen Generieren von grafisch dargestellten Anzeigeinstrumenten
WO2006041479A1 (en) * 2004-10-07 2006-04-20 Universal Avionics Systems Corporation Dynamic vsi display
DE102006013695A1 (de) * 2006-03-24 2007-09-27 Robert Bosch Gmbh Elektro-optische Ausgabeeinheit sowie Messgerät mit einer elektro-optischen Ausgabeeinheit
US20090189787A1 (en) * 2008-01-30 2009-07-30 Honeywell International Inc. System and method for generating an altimeter mis-set alert on a primary flight display
EP2177882B1 (en) * 2008-10-20 2016-03-16 Volvo Car Corporation A display device for a vehicle
US20120010765A1 (en) * 2010-07-07 2012-01-12 Honeywell International Inc. System for displaying a procedure to an aircraft operator during a flight of an aircraft
US9529010B2 (en) 2013-06-17 2016-12-27 Honeywell International Inc. Flight deck display systems and methods for visually indicating low speed change conditions during takeoff and landing
FR3010975B1 (fr) * 2013-09-20 2015-11-06 Thales Sa Systeme d'affichage d'informations d'aide a la navigation d'un aeronef et ecran primaire de vol pour un aeronef
US9950805B2 (en) * 2015-10-26 2018-04-24 The Boeing Company Aircraft engine fan speed display improvements for enhanced monitoring and thrust setting ability
US9669941B1 (en) * 2016-01-31 2017-06-06 Rockwell Collins, Inc. Weather indicator system and method
CN106970644B (zh) * 2017-05-16 2019-10-22 西安爱生技术集团公司 一种无人机高度显控方法
CN108168520A (zh) * 2017-12-19 2018-06-15 中联重科股份有限公司 倾角指示器、倾角指示方法、装置和工程机械
US20210009281A1 (en) * 2019-07-08 2021-01-14 Honeywell International Inc. System and method for adjusting a dynamic scale indicator on a flight display of an aircraft
FR3129719B1 (fr) 2021-11-29 2024-02-16 Airbus Helicopters Indicateur de hauteur ayant une échelle de hauteur linéaire par morceaux

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US3806934A (en) * 1972-08-07 1974-04-23 Teledyne Inc Inertial lead vertical speed indicator/glide slope director
DE2724860C2 (de) * 1977-06-02 1979-04-12 Bodenseewerk Geraetetechnik Gmbh, 7770 Ueberlingen Fahrtanzeigeinstrument für Flugzeuge
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Also Published As

Publication number Publication date
JP4246155B2 (ja) 2009-04-02
AU2003266895A8 (en) 2004-04-23
EP1546655B1 (en) 2006-03-15
BR0314374B1 (pt) 2015-01-13
WO2004031833A3 (en) 2004-07-15
EP1546655A2 (en) 2005-06-29
CA2494050C (en) 2011-10-18
JP2006501097A (ja) 2006-01-12
ES2260639T3 (es) 2006-11-01
CA2494050A1 (en) 2004-04-15
DE60304053T2 (de) 2006-11-09
CN1688868A (zh) 2005-10-26
AU2003266895A1 (en) 2004-04-23
ATE320588T1 (de) 2006-04-15
US20040113816A1 (en) 2004-06-17
US7062364B2 (en) 2006-06-13
WO2004031833A2 (en) 2004-04-15
CN100547353C (zh) 2009-10-07
DE60304053D1 (de) 2006-05-11

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B06A Patent application procedure suspended [chapter 6.1 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
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