WO2004031833A3 - Electronic non-linear aircraft dynamic parameter display - Google Patents

Electronic non-linear aircraft dynamic parameter display Download PDF

Info

Publication number
WO2004031833A3
WO2004031833A3 PCT/CA2003/001424 CA0301424W WO2004031833A3 WO 2004031833 A3 WO2004031833 A3 WO 2004031833A3 CA 0301424 W CA0301424 W CA 0301424W WO 2004031833 A3 WO2004031833 A3 WO 2004031833A3
Authority
WO
WIPO (PCT)
Prior art keywords
dynamic parameter
parameter display
electronic non
aircraft dynamic
displaying
Prior art date
Legal status (The legal status 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 status listed.)
Ceased
Application number
PCT/CA2003/001424
Other languages
French (fr)
Other versions
WO2004031833A2 (en
Inventor
John Maris
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Marinvent Corp
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
Priority to JP2004540400A priority Critical patent/JP4246155B2/en
Priority to EP03747776A priority patent/EP1546655B1/en
Priority to CA2494050A priority patent/CA2494050C/en
Priority to DE60304053T priority patent/DE60304053T2/en
Priority to AU2003266895A priority patent/AU2003266895A1/en
Priority to BRPI0314374-0A priority patent/BR0314374B1/en
Publication of WO2004031833A2 publication Critical patent/WO2004031833A2/en
Publication of WO2004031833A3 publication Critical patent/WO2004031833A3/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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

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

Abstract

A method and apparatus is disclosed for displaying a dynamic parameter of an aircraft, the apparatus comprises a display unit receiving a display signal and displaying a scale that changes dynamically and non-linearly in accordance with a selected display algorithm, the display unit further displaying a pointer pointing (36) to said scale (32) in accordance with a reading of said dynamic parameter, thereby emphasizing a range of said reading of said dynamic parameter.
PCT/CA2003/001424 2002-10-04 2003-09-26 Electronic non-linear aircraft dynamic parameter display Ceased WO2004031833A2 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
JP2004540400A JP4246155B2 (en) 2002-10-04 2003-09-26 Electronic nonlinear aircraft dynamic parameter display
EP03747776A EP1546655B1 (en) 2002-10-04 2003-09-26 Electronic non-linear aircraft dynamic parameter display
CA2494050A CA2494050C (en) 2002-10-04 2003-09-26 Electronic non-linear aircraft dynamic parameter display
DE60304053T DE60304053T2 (en) 2002-10-04 2003-09-26 NONLINEAR ELECTRONIC DISPLAY DYNAMIC PLANE PARAMETERS
AU2003266895A AU2003266895A1 (en) 2002-10-04 2003-09-26 Electronic non-linear aircraft dynamic parameter display
BRPI0314374-0A BR0314374B1 (en) 2002-10-04 2003-09-26 "DEVICE AND METHOD FOR DISPLAYING A DYNAMIC PARAMETER OF AN AIRCRAFT"

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US41580702P 2002-10-04 2002-10-04
US60/415,807 2002-10-04

Publications (2)

Publication Number Publication Date
WO2004031833A2 WO2004031833A2 (en) 2004-04-15
WO2004031833A3 true WO2004031833A3 (en) 2004-07-15

Family

ID=32069906

Family Applications (1)

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

Country Status (11)

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

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US7205907B2 (en) * 2003-09-15 2007-04-17 Universal Avionics Systems Corporation Non linear tape display
US7095338B2 (en) * 2003-10-07 2006-08-22 Ted Naimer TCAS VSI display
US7412308B2 (en) * 2003-10-07 2008-08-12 Universal Avionics Systems Corp. Dynamic VSI display
DE102004045094B4 (en) * 2004-09-17 2012-05-03 Deutsches Zentrum für Luft- und Raumfahrt e.V. Method for automatically generating graphically displayed display instruments
WO2006041479A1 (en) * 2004-10-07 2006-04-20 Universal Avionics Systems Corporation Dynamic vsi display
DE102006013695A1 (en) * 2006-03-24 2007-09-27 Robert Bosch Gmbh Electro-optical display unit for hand-held length measuring device e.g. roller-tape, has digital display comprising variable scale with scale point and numerical value, where orientation of scale is changed relative to display unit
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 (en) * 2013-09-20 2015-11-06 Thales Sa NAVIGATION INFORMATION DISPLAY SYSTEM FOR AN AIRCRAFT AND PRIMARY FLIGHT SCREEN FOR AN AIRCRAFT
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 (en) * 2017-05-16 2019-10-22 西安爱生技术集团公司 A method for displaying and controlling the height of an unmanned aerial vehicle
CN108168520A (en) * 2017-12-19 2018-06-15 中联重科股份有限公司 Inclination indicator, inclination indicating method, device and construction machinery
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 (en) 2021-11-29 2024-02-16 Airbus Helicopters Pitch indicator having a piecewise linear pitch scale
US12499770B2 (en) 2023-06-26 2025-12-16 Honeywell International Inc. System and method to intuitively represent the separation of aircraft traffic
USD1110350S1 (en) 2024-08-26 2026-01-27 Marinvent Corporation Display screen or portion thereof with animated graphical user interface
USD1109176S1 (en) 2024-08-26 2026-01-13 Marinvent Corporation Display screen or portion thereof with animated graphical user interface

Citations (4)

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DE2724860B1 (en) * 1977-06-02 1978-08-10 Bodenseewerk Geraetetech Airspeed indicator instrument
US5289185A (en) * 1990-09-05 1994-02-22 Aerospatiale Societe Nationale Industrielle Process for displaying flying aid symbols on a screen on board an aircraft
US6112141A (en) * 1997-10-15 2000-08-29 Dassault Aviation Apparatus and method for graphically oriented aircraft display and control
WO2002007094A2 (en) * 2000-07-17 2002-01-24 Honeywell International Inc. Methods and apparatus for viewing information on a display

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US3806934A (en) * 1972-08-07 1974-04-23 Teledyne Inc Inertial lead vertical speed indicator/glide slope director
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Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2724860B1 (en) * 1977-06-02 1978-08-10 Bodenseewerk Geraetetech Airspeed indicator instrument
US5289185A (en) * 1990-09-05 1994-02-22 Aerospatiale Societe Nationale Industrielle Process for displaying flying aid symbols on a screen on board an aircraft
US6112141A (en) * 1997-10-15 2000-08-29 Dassault Aviation Apparatus and method for graphically oriented aircraft display and control
WO2002007094A2 (en) * 2000-07-17 2002-01-24 Honeywell International Inc. Methods and apparatus for viewing information on a display

Also Published As

Publication number Publication date
CA2494050A1 (en) 2004-04-15
EP1546655B1 (en) 2006-03-15
JP4246155B2 (en) 2009-04-02
ATE320588T1 (en) 2006-04-15
EP1546655A2 (en) 2005-06-29
CA2494050C (en) 2011-10-18
BR0314374B1 (en) 2015-01-13
US20040113816A1 (en) 2004-06-17
AU2003266895A8 (en) 2004-04-23
CN100547353C (en) 2009-10-07
ES2260639T3 (en) 2006-11-01
CN1688868A (en) 2005-10-26
BR0314374A (en) 2005-11-29
WO2004031833A2 (en) 2004-04-15
DE60304053D1 (en) 2006-05-11
JP2006501097A (en) 2006-01-12
US7062364B2 (en) 2006-06-13
AU2003266895A1 (en) 2004-04-23
DE60304053T2 (en) 2006-11-09

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