Method and apparatus for displaying aircraft engine...

Communications: electrical – Aircraft alarm or indicating systems – Nonalarm flight indicator

Reexamination Certificate

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

C340S945000, C340S963000, C701S029000

Reexamination Certificate

active

07142131

ABSTRACT:
A method and system for displaying aircraft engine information. In one embodiment, the method includes directing the display of an icon that represents a qualitative, overall operational state of an aircraft engine, with the overall operational state being determined from a plurality of engine operating parameters. The method can further include directing a change in the display of the icon when the overall operational state of the aircraft engine changes from a first overall operational state to a second operational state. In a further aspect of this embodiment, the change in the characteristic of the icon can include a change in the color or other visual characteristic of the icon, and the color or other visual characteristic of the icon can correspond directly to instructions to the pilot for actions suggested or required as a result of the current engine operational state.

REFERENCES:
patent: 3191147 (1965-06-01), Majendie
patent: 4196474 (1980-04-01), Buchanan et al.
patent: 4212064 (1980-07-01), Forsythe et al.
patent: 4247843 (1981-01-01), Miller
patent: 4274096 (1981-06-01), Dennison
patent: 4325123 (1982-04-01), Graham
patent: 4792906 (1988-12-01), King
patent: 4860007 (1989-08-01), Konicke
patent: 4899284 (1990-02-01), Lewis
patent: 5050081 (1991-09-01), Abbott et al.
patent: 5070458 (1991-12-01), Gilmore et al.
patent: 5329277 (1994-07-01), Dougan et al.
patent: 5337982 (1994-08-01), Sherry
patent: 5420582 (1995-05-01), Kubbat
patent: 5454074 (1995-09-01), Hartel et al.
patent: 5499025 (1996-03-01), Middleton et al.
patent: 5668542 (1997-09-01), Wright
patent: 5715163 (1998-02-01), Bang
patent: 5739769 (1998-04-01), Vladimir et al.
patent: 5844503 (1998-12-01), Riley et al.
patent: 5875998 (1999-03-01), Gleine
patent: 5940013 (1999-08-01), Vladimir et al.
patent: 5978715 (1999-11-01), Briffe
patent: 6057786 (2000-05-01), Briffe
patent: 6085129 (2000-07-01), Schardt
patent: 6098014 (2000-08-01), Kranz
patent: 6112141 (2000-08-01), Briffe
patent: 6118385 (2000-09-01), Leard et al.
patent: 6188937 (2001-02-01), Sherry
patent: 6246320 (2001-06-01), Monroe
patent: 6262720 (2001-07-01), Jeffrey et al.
patent: 6278913 (2001-08-01), Jiang
patent: 6314366 (2001-11-01), Farmakis et al.
patent: 6346892 (2002-02-01), DeMers et al.
patent: 6362750 (2002-03-01), Castor
patent: 6381519 (2002-04-01), Snyder
patent: 6389333 (2002-05-01), Hansman
patent: 6443399 (2002-09-01), Yount et al.
patent: 6542796 (2003-04-01), Gibbs et al.
patent: 6556902 (2003-04-01), Ing et al.
patent: 6636786 (2003-10-01), Partel
patent: 6697718 (2004-02-01), Le Draoullec et al.
patent: 6720891 (2004-04-01), Chen
patent: 6745113 (2004-06-01), Griffin
patent: 6753891 (2004-06-01), Chohan et al.
patent: 2002/0016654 (2002-02-01), Ing et al.
patent: 2002/0033837 (2002-03-01), Munro
patent: 2003/0058134 (2003-03-01), Sherry
patent: 2003/0132860 (2003-07-01), Feyereisen
patent: 2004/0059474 (2004-03-01), Boorman
patent: 2004/0183697 (2004-09-01), Rogers et al.
patent: 2004/0254691 (2004-12-01), Subelet
patent: 2006/0004496 (2006-01-01), Tucker et al.
patent: 3315386 (1984-10-01), None
patent: 0 286 120 (1988-10-01), None
patent: 0 370 640 (1990-05-01), None
patent: 0 489 521 (1992-06-01), None
patent: 21848306 (2002-03-01), None
patent: 2817831 (2002-06-01), None
patent: 886136 (1962-01-01), None
patent: WO-02/24530 (2002-03-01), None
Presentation by Airbus Industries personnel on Jun. 10, 2002 (12 pages).
Peugeot 406 Handbook, Automobiles Peugeot, Paris, France, May 14, 1998 (pp. 30 and 38).
European Search Report for European Patent Application No. EP 03 07 7100, The Boeing Company, Oct. 28, 2003 (2 pages).
U.S. Appl. No. 10/746,883, Boorman.
U.S. Appl. No. 10/746,912, Boorman.
U.S. Appl. No. 10/787,644, Tafs et al.
U.S. Appl. No. 10/798,749, Sandell et al.
U.S. Appl. No. 10/814,369, Chen et al.
U.S. Appl. No. 10/814,494, Gunn et al.
U.S. Appl. No. 10/815,034, Crane et al.
777 Flight Deck (1 page); http://www.meriweather.com/777/777—main.html; [Accessed Jan. 28, 2003].
Hutchins, Edwin, “The Integrated Mode Management Interface,” Department of Cognitive Science, University of California, San Diego, Sep. 17, 1996.
Lindenfeld, Ron, “What is an FMS?”, Flight Management Systems (5 pages); http://www.ultranet.com/˜marzgold//FAQ-FMS.html; [Accessed Jun. 3, 2002].
Meriweather's Flight Deck Acronyms & Definitions (4 pages); http://www.meriweather.com/fd/def.html; [Accessed Jun. 3, 2002].
U.S. Appl. No. 10/860,760, Sikora et al.

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Method and apparatus for displaying aircraft engine... does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Method and apparatus for displaying aircraft engine..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Method and apparatus for displaying aircraft engine... will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-3676151

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.