WO2005034368A3 - Non linear tape display - Google Patents

Non linear tape display Download PDF

Info

Publication number
WO2005034368A3
WO2005034368A3 PCT/US2004/030080 US2004030080W WO2005034368A3 WO 2005034368 A3 WO2005034368 A3 WO 2005034368A3 US 2004030080 W US2004030080 W US 2004030080W WO 2005034368 A3 WO2005034368 A3 WO 2005034368A3
Authority
WO
WIPO (PCT)
Prior art keywords
display
nonlinear scale
non linear
linear tape
tape display
Prior art date
Application number
PCT/US2004/030080
Other languages
French (fr)
Other versions
WO2005034368A2 (en
Inventor
Joachim Laurent Naimer
Sam Hyatt
Jim Brannen
Tom Lawrence
Original Assignee
Universal Avionics Sys 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 Universal Avionics Sys Corp filed Critical Universal Avionics Sys Corp
Publication of WO2005034368A2 publication Critical patent/WO2005034368A2/en
Publication of WO2005034368A3 publication Critical patent/WO2005034368A3/en

Links

Classifications

    • 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

Abstract

A graphical display of a nonlinear scale emulating the view of a mechanical drum gauge. The nonlinear scale may be used for the display of aircraft flight data including airspeed, altitude, heading, and other aircraft data suitable for presentation on a nonlinear scale. The nonlinear scale may scroll to display current aircraft data.
PCT/US2004/030080 2003-09-15 2004-09-15 Non linear tape display WO2005034368A2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/662,485 US7205907B2 (en) 2003-09-15 2003-09-15 Non linear tape display
US10/662,485 2003-09-15

Publications (2)

Publication Number Publication Date
WO2005034368A2 WO2005034368A2 (en) 2005-04-14
WO2005034368A3 true WO2005034368A3 (en) 2005-07-14

Family

ID=34274113

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2004/030080 WO2005034368A2 (en) 2003-09-15 2004-09-15 Non linear tape display

Country Status (2)

Country Link
US (1) US7205907B2 (en)
WO (1) WO2005034368A2 (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7834779B2 (en) * 2005-06-29 2010-11-16 Honeywell International Inc. System and method for increasing visibility of critical flight information on aircraft displays
FR2903183B1 (en) * 2006-06-29 2008-09-12 Thales Sa METHOD FOR MANAGING THE DISPLAY OF A ROTATING COUNTER
US20090240396A1 (en) * 2008-03-19 2009-09-24 John T. Sullivan Pit road display
US9829341B1 (en) * 2008-06-26 2017-11-28 Rockwell Collins, Inc. System and method for providing flight cues for the navigation function required time of arrival (RTA)
US8160755B2 (en) * 2008-09-30 2012-04-17 Honeywell International Inc. Displaying air traffic symbology based on relative importance
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
DE102014212061B4 (en) * 2014-06-24 2023-12-28 Volkswagen Ag Method and device for displaying a vehicle-specific parameter in a vehicle as well as a combination instrument and vehicle
US10712843B2 (en) * 2014-07-29 2020-07-14 Naver Corporation Method and apparatus for controlling display of scrolled content by modifying the content as the content is being scrolled to a designed location and computer program for executing the method
CN108536376B (en) * 2017-12-13 2021-01-05 太原航空仪表有限公司 Simulation roller wheel display method for machine-mounted liquid crystal display
US10640230B2 (en) * 2018-04-04 2020-05-05 Jurgen R. Ihns Cockpit pressurization and oxygen warning system
FR3129719B1 (en) 2021-11-29 2024-02-16 Airbus Helicopters Pitch indicator having a piecewise linear pitch scale

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4860007A (en) * 1988-01-15 1989-08-22 The Boeing Company Integrated primary flight display
US5412382A (en) * 1993-12-30 1995-05-02 Honeywell Inc. Integrated electronic primary flight display
US5739771A (en) * 1995-12-18 1998-04-14 Honeywell Inc. Ambiguous dial indicator with saturating setpoints
US5844504A (en) * 1997-07-22 1998-12-01 Rockwell International Compressed circle flight display
US6112141A (en) * 1997-10-15 2000-08-29 Dassault Aviation Apparatus and method for graphically oriented aircraft display and control
US6686851B1 (en) * 2000-08-25 2004-02-03 Rockwell Collins Altitude tape and integral vertical speed indicator

Family Cites Families (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3668622A (en) 1970-05-21 1972-06-06 Boeing Co Flight management display
US4247843A (en) 1978-08-23 1981-01-27 Sperry Corporation Aircraft flight instrument display system
US4774670A (en) 1985-04-29 1988-09-27 Lockheed Corporation Flight management system
US4750127A (en) 1985-10-31 1988-06-07 The Boeing Company Energy compensated target speed for aircraft descent
US4914733A (en) 1987-10-30 1990-04-03 Allied-Signal, Inc. Traffic advisory-instantaneous vertical speed display
US5227786A (en) 1989-06-30 1993-07-13 Honeywell Inc. Inside/out perspective format for situation awareness displays
US5185606A (en) 1990-05-08 1993-02-09 Fokker Aircraft B.V. Primary flight display presenting resolution advisory information provided by a traffic alert and collision avoidance system
US5179377A (en) 1990-12-31 1993-01-12 Honeywell Inc. Tcas view display format with horizontal trend
US5248968A (en) 1991-12-06 1993-09-28 The Boeing Company Tcas ii pitch guidance control law and display symbol
US5250947A (en) 1992-03-16 1993-10-05 Honeywell Inc. Altitude tape for aircraft displays
US5382954A (en) 1993-05-27 1995-01-17 Honeywell Inc. Resolution advisory display instrument for TCAS guidance
US5493309A (en) 1993-09-24 1996-02-20 Motorola, Inc. Collison avoidance communication system and method
US5668542A (en) 1995-07-03 1997-09-16 The United States Of America As Represented By The Secretary Of The Air Force Color cockpit display for aircraft systems
FR2742226B1 (en) 1995-12-08 1998-02-06 Eurocopter France VERTICAL ALTITUDE AND SPEED INDICATOR FOR AIRCRAFT
US5739770A (en) 1996-01-16 1998-04-14 Honeywell Inc. Off-path descent guidance by a flight management system
US5872526A (en) 1996-05-23 1999-02-16 Sun Microsystems, Inc. GPS collision avoidance system
US5920321A (en) 1996-09-30 1999-07-06 Rockwell International Corporation Flight management system with 3-dimensional flight path display
CA2202409C (en) * 1997-04-11 1998-04-07 Carl W. Millard Howgozit airspeed indicator system
US6085150A (en) 1997-07-22 2000-07-04 Rockwell Collins, Inc. Traffic collision avoidance system
US6259378B1 (en) 1997-09-22 2001-07-10 Sandel Avionics Display system for airplane cockpit or other vehicle
US6154151A (en) 1998-06-16 2000-11-28 Rockwell Collins, Inc. Integrated vertical situation display for aircraft
US6145151A (en) * 1998-06-23 2000-11-14 Herron; Harold F. Ergonomic brush and handle therefor
US6271768B1 (en) 1998-12-30 2001-08-07 Honeywell Inc. Vertical speed indicator/traffic resolution advisory display for TCAS
US6683541B2 (en) 1999-01-21 2004-01-27 Honeywell International Inc. Vertical speed indicator and traffic alert collision avoidance system
US6571155B2 (en) 2001-07-02 2003-05-27 The Boeing Company Assembly, computer program product and method for displaying navigation performance based flight path deviation information
US20030132860A1 (en) 2001-09-21 2003-07-17 Honeywell International, Inc. Interface for visual cueing and control for tactical flightpath management
CA2494050C (en) 2002-10-04 2011-10-18 Marinvent Corporation Electronic non-linear aircraft dynamic parameter display
US6879887B2 (en) 2003-04-02 2005-04-12 Honeywell International Inc. Low speed range indicator

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4860007A (en) * 1988-01-15 1989-08-22 The Boeing Company Integrated primary flight display
US5412382A (en) * 1993-12-30 1995-05-02 Honeywell Inc. Integrated electronic primary flight display
US5739771A (en) * 1995-12-18 1998-04-14 Honeywell Inc. Ambiguous dial indicator with saturating setpoints
US5844504A (en) * 1997-07-22 1998-12-01 Rockwell International Compressed circle flight display
US6112141A (en) * 1997-10-15 2000-08-29 Dassault Aviation Apparatus and method for graphically oriented aircraft display and control
US6686851B1 (en) * 2000-08-25 2004-02-03 Rockwell Collins Altitude tape and integral vertical speed indicator

Also Published As

Publication number Publication date
US20050057377A1 (en) 2005-03-17
WO2005034368A2 (en) 2005-04-14
US7205907B2 (en) 2007-04-17

Similar Documents

Publication Publication Date Title
EP2151669A3 (en) System and method for displaying constraint information on a graphical aircraft instrument tape element
WO2006134256A3 (en) Method and system for assisting flight control of a low-flying aircraft
WO2005013204A3 (en) Flight situation presentation system and method
WO2006132713A3 (en) Integrated hover display with augmented approach to hover symbology cueing for degraded visual environmental conditions
WO2005034368A3 (en) Non linear tape display
WO2006099395A3 (en) System and method for displaying information using a compass
WO2001046647A3 (en) Method, apparatus and computer program product for estimating airplane attitude with reduced sensor set
WO2005120954A3 (en) System and method for monitoring aircraft engine health and determining engine power available, and applications thereof
WO2003007021A3 (en) Constant altitude weather and all weather display
WO2006115873A3 (en) System and method for displaying the protected airspace associated with a circle-to-land maneuver
WO2008024130A3 (en) Methods and systems for displaying navigation procedure information
EP1816439A3 (en) Heading awareness symbology for track centered primary flight displays
EP2696171A3 (en) Aircraft systems and methods for displaying weather information along a flight path
BRPI0512473A (en) aircraft backup display device, method to assist piloting of an aircraft and aircraft
WO2007038587A3 (en) Company and contact information system and method
WO2008064191A3 (en) Visual display system for an aircraft
WO2002059547A3 (en) Egpws cutoff altitude for helicopters
AP1773A (en) Airborne geophysical measurements.
NZ603049A (en) Temporary formatting and charting of selected data
WO2002029363A3 (en) Simultaneous textual display of an original and a modified flight plan
WO2009016693A1 (en) Map display system, map display device, and map display method
WO2007075481A3 (en) System and method for converting voice weather data into data for display in an aircraft cockpit
ATE530877T1 (en) BACKUP INSTRUMENT FOR AIRCRAFT
WO2007048931A3 (en) Method for setting an aircraft barometric altitude
US9981753B2 (en) Composite normalized angle of attack indicating system

Legal Events

Date Code Title Description
AK Designated states

Kind code of ref document: A2

Designated state(s): AE AG AL AM AT AU AZ BA BB BG BR BW BY BZ CA CH CN CO CR CU CZ DE DK DM DZ EC EE EG ES FI GB GD GE GH GM HR HU ID IL IN IS JP KE KG KP KR KZ LC LK LR LS LT LU LV MA MD MG MK MN MW MX MZ NA NI NO NZ OM PG PH PL PT RO RU SC SD SE SG SK SL SY TJ TM TN TR TT TZ UA UG US UZ VC VN YU ZA ZM ZW

AL Designated countries for regional patents

Kind code of ref document: A2

Designated state(s): GM KE LS MW MZ NA SD SL SZ TZ UG ZM ZW AM AZ BY KG KZ MD RU TJ TM AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LU MC NL PL PT RO SE SI SK TR BF BJ CF CG CI CM GA GN GQ GW ML MR NE SN TD TG

121 Ep: the epo has been informed by wipo that ep was designated in this application
DPEN Request for preliminary examination filed prior to expiration of 19th month from priority date (pct application filed from 20040101)
122 Ep: pct application non-entry in european phase