WO2005050601A3 - Display systems for a device - Google Patents

Display systems for a device Download PDF

Info

Publication number
WO2005050601A3
WO2005050601A3 PCT/US2004/023167 US2004023167W WO2005050601A3 WO 2005050601 A3 WO2005050601 A3 WO 2005050601A3 US 2004023167 W US2004023167 W US 2004023167W WO 2005050601 A3 WO2005050601 A3 WO 2005050601A3
Authority
WO
WIPO (PCT)
Prior art keywords
images
acoustic level
sensors
level
display system
Prior art date
Application number
PCT/US2004/023167
Other languages
French (fr)
Other versions
WO2005050601A2 (en
Inventor
Barry Berson
Bialecki Larry
Buck Peter
Morgenstern John
Original Assignee
Supersonic Aerospace Int
Barry Berson
Bialecki Larry
Buck Peter
Morgenstern John
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
Priority claimed from US10/615,634 external-priority patent/US7486291B2/en
Priority claimed from US10/616,145 external-priority patent/US7312725B2/en
Priority claimed from US10/619,848 external-priority patent/US6905091B2/en
Priority claimed from US10/706,672 external-priority patent/US7982767B2/en
Application filed by Supersonic Aerospace Int, Barry Berson, Bialecki Larry, Buck Peter, Morgenstern John filed Critical Supersonic Aerospace Int
Priority to EP04817726A priority Critical patent/EP1661117A4/en
Publication of WO2005050601A2 publication Critical patent/WO2005050601A2/en
Publication of WO2005050601A3 publication Critical patent/WO2005050601A3/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
    • G01C23/005—Flight directors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D43/00—Arrangements or adaptations of instruments
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00—Equipment not otherwise provided for
    • B64D47/08—Arrangements of cameras

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Controls And Circuits For Display Device (AREA)
  • Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)

Abstract

A display system for operating a device receives images from sensors (110) that represent scenery outside the device and is configured to detect moving objects in the images, as well as fuse (222) the images to a single viewpoint (224). The display system generates a plurality of mutually exclusive windows (120, 122, 124) which include a common user interface and display area (706, 714, 718). The system receives information regarding current flight conditions of the device such as an aircraft and determines the acoustic level of the sonic boom and/or other noise generated. The current acoustic level is compared to a desired level (904), and various cues are displayed (928) to operators regarding corrective actions to the acoustic level. A cleaning mechanism (1224) removes obstructions from a transparent aperture on a housing (1212) enclosing the sensors.
PCT/US2004/023167 2003-07-08 2004-07-01 Display systems for a device WO2005050601A2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP04817726A EP1661117A4 (en) 2003-07-08 2004-07-01 Display systems for a device

Applications Claiming Priority (8)

Application Number Priority Date Filing Date Title
US10/615,634 US7486291B2 (en) 2003-07-08 2003-07-08 Systems and methods using enhanced vision to provide out-the-window displays for a device
US10/615,634 2003-07-08
US10/616,145 2003-07-08
US10/616,145 US7312725B2 (en) 2003-07-08 2003-07-08 Display system for operating a device with reduced out-the-window visibility
US10/619,848 2003-07-14
US10/619,848 US6905091B2 (en) 2003-07-14 2003-07-14 System and method for controlling the acoustic signature of a device
US10/706,672 US7982767B2 (en) 2003-11-11 2003-11-11 System and method for mounting sensors and cleaning sensor apertures for out-the-window displays
US10/706,672 2003-11-11

Publications (2)

Publication Number Publication Date
WO2005050601A2 WO2005050601A2 (en) 2005-06-02
WO2005050601A3 true WO2005050601A3 (en) 2006-04-06

Family

ID=34623988

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2004/023167 WO2005050601A2 (en) 2003-07-08 2004-07-01 Display systems for a device

Country Status (2)

Country Link
EP (1) EP1661117A4 (en)
WO (1) WO2005050601A2 (en)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2903787B1 (en) * 2006-07-11 2008-11-14 Thales Sa DEVICE FOR GENERATING THE EMERGENCY FUNCTION IN A HIGH HEAD VIEWFINDER
US8019489B2 (en) 2006-12-20 2011-09-13 The Boeing Company Methods and systems for displaying messages from a plurality of sources
DE102010042956A1 (en) 2010-10-26 2012-04-26 Airbus Operations Gmbh Method and arrangement for determining a load on an aircraft structure
US9376983B2 (en) * 2012-11-30 2016-06-28 Honeywell International Inc. Operations support systems and methods with acoustics evaluation and control
FR3028498B1 (en) * 2014-11-14 2018-06-01 Airbus Operations DEVICE FOR CONTROLLING A PUSHING REGIME OF AT LEAST ONE AIRCRAFT ENGINE.
US10793266B2 (en) * 2016-11-14 2020-10-06 Boom Technology, Inc. Commercial supersonic aircraft and associated systems and methods
WO2018183994A1 (en) * 2017-03-31 2018-10-04 Area 2601, LLC Computer-based systems and methods for facilitating aircraft approach
US10699584B2 (en) 2018-03-02 2020-06-30 Honeywell International Inc. Systems and methods for sonic boom aware flight planning

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4887298A (en) * 1988-06-15 1989-12-12 Renkus-Heinz Electronic circuit for sensing disconnect or failure of a power output sense line in an audio power system
US20010048763A1 (en) * 2000-05-30 2001-12-06 Takeshi Takatsuka Integrated vision system
US6405975B1 (en) * 1995-12-19 2002-06-18 The Boeing Company Airplane ground maneuvering camera system
US6466235B1 (en) * 1999-09-08 2002-10-15 Rockwell Collins, Inc. Method and apparatus for interactively and automatically selecting, controlling and displaying parameters for an avionics electronic flight display system

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5551649A (en) 1989-10-20 1996-09-03 Fokker Aircraft B.V. Propeller blade position controller
US5189929A (en) * 1992-03-09 1993-03-02 United Technologies Corporation System and method for transmission gearbox noise control utilizing localized oil cooling/heating
US5927648A (en) * 1996-10-17 1999-07-27 Woodland; Richard Lawrence Ken Aircraft based sensing, detection, targeting, communications and response apparatus
US5742336A (en) * 1996-12-16 1998-04-21 Lee; Frederick A. Aircraft surveillance and recording system
US20030067542A1 (en) * 2000-10-13 2003-04-10 Monroe David A. Apparatus for and method of collecting and distributing event data to strategic security personnel and response vehicles

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4887298A (en) * 1988-06-15 1989-12-12 Renkus-Heinz Electronic circuit for sensing disconnect or failure of a power output sense line in an audio power system
US6405975B1 (en) * 1995-12-19 2002-06-18 The Boeing Company Airplane ground maneuvering camera system
US6466235B1 (en) * 1999-09-08 2002-10-15 Rockwell Collins, Inc. Method and apparatus for interactively and automatically selecting, controlling and displaying parameters for an avionics electronic flight display system
US20010048763A1 (en) * 2000-05-30 2001-12-06 Takeshi Takatsuka Integrated vision system

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
GUELL J.: "FLILO (Flying Infrared for Low-level Operations) an Enhanced Vision System", IEEE AES SYSTEMS MAG., September 2000 (2000-09-01), pages 31 - 35, XP002988590 *
NASA: "NASA´s High-Speed Research Program, The eXternal Visibility System Concept", September 1998 (1998-09-01), pages 3 PAGES, XP002988591, Retrieved from the Internet <URL:http://oea.larc.nasa.gov/PAIS/HSR-Cockpit.html> *

Also Published As

Publication number Publication date
EP1661117A2 (en) 2006-05-31
EP1661117A4 (en) 2009-01-21
WO2005050601A2 (en) 2005-06-02

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