Aeronautics and astronautics – Aircraft control – Automatic
Reexamination Certificate
2011-01-25
2011-01-25
Ellis, Christopher P (Department: 3644)
Aeronautics and astronautics
Aircraft control
Automatic
C244S199300, C244S180000, C340S968000
Reexamination Certificate
active
07874522
ABSTRACT:
Systems and methods for tracing aircraft vortices. One method includes directing a tracer from a first aircraft into a vortical flow generated by the first aircraft. The method can further include detecting a characteristic corresponding to the presence of the tracer directed into the vortical flow. Based at least in part on the detected characteristic, the method can include directing the flight of the first aircraft, or a second aircraft following the first aircraft, or both.
REFERENCES:
patent: 2477461 (1949-07-01), Lee
patent: 2650781 (1953-09-01), Taylor
patent: 3012740 (1958-04-01), Wagner
patent: 3090584 (1963-05-01), Kuchemann et al.
patent: 3480234 (1969-11-01), Cornish
patent: 3596854 (1971-08-01), Haney, Jr.
patent: 3604661 (1971-09-01), Mayer, Jr.
patent: 3692259 (1972-09-01), Yuan
patent: 3761929 (1973-09-01), Wyatt
patent: 3841587 (1974-10-01), Freed
patent: 3845918 (1974-11-01), White, Jr.
patent: 3881669 (1975-05-01), Lessen
patent: 3936013 (1976-02-01), Yuan
patent: 3974986 (1976-08-01), Johnstone
patent: 3984070 (1976-10-01), Patterson, Jr.
patent: 3997132 (1976-12-01), Erwin
patent: 4137764 (1979-02-01), Hallock et al.
patent: 4359640 (1982-11-01), Geiger
patent: 4477042 (1984-10-01), Griswold, II
patent: 4735503 (1988-04-01), Werner et al.
patent: 4860976 (1989-08-01), McFadden et al.
patent: 5150859 (1992-09-01), Ransick
patent: 5158251 (1992-10-01), Taylor
patent: 5173706 (1992-12-01), Urkowitz
patent: 5208600 (1993-05-01), Rubin
patent: 5262773 (1993-11-01), Gordon
patent: 5492289 (1996-02-01), Nosenchuck et al.
patent: 5541591 (1996-07-01), Bush
patent: 5634613 (1997-06-01), McCarthy
patent: 5657009 (1997-08-01), Gordon
patent: 5724040 (1998-03-01), Watnick
patent: 5755408 (1998-05-01), Schmidt et al.
patent: 5758823 (1998-06-01), Glezer et al.
patent: 5806807 (1998-09-01), Haney
patent: 5813625 (1998-09-01), Hassan et al.
patent: 5838007 (1998-11-01), Wang
patent: 5845874 (1998-12-01), Beasley
patent: 5918835 (1999-07-01), Gerhardt
patent: 5938404 (1999-08-01), Domzalski et al.
patent: 5957413 (1999-09-01), Glezer et al.
patent: 5988522 (1999-11-01), Glezer et al.
patent: 6062076 (2000-05-01), Johari et al.
patent: 6070461 (2000-06-01), Gjessing et al.
patent: 6082679 (2000-07-01), Crouch et al.
patent: 6123145 (2000-09-01), Glezer et al.
patent: 6129309 (2000-10-01), Smith et al.
patent: 6138955 (2000-10-01), Gutmark et al.
patent: 6177888 (2001-01-01), Cabot et al.
patent: 6184816 (2001-02-01), Zheng et al.
patent: 6283406 (2001-09-01), Remington et al.
patent: 6378807 (2002-04-01), Tomioka
patent: 6394397 (2002-05-01), Ngo et al.
patent: 6422518 (2002-07-01), Stuff et al.
patent: 6424408 (2002-07-01), Ooga et al.
patent: 6425553 (2002-07-01), Smith et al.
patent: 6471477 (2002-10-01), Hassan et al.
patent: 6513761 (2003-02-01), Huenecke
patent: 6554607 (2003-04-01), Glezer et al.
patent: 6629674 (2003-10-01), Saddoughi et al.
patent: 6668638 (2003-12-01), Huang et al.
patent: 6703945 (2004-03-01), Kuntman et al.
patent: 6963291 (2005-11-01), Holforty et al.
patent: 7017862 (2006-03-01), Fischbach
patent: 7100875 (2006-09-01), Shmilovich et al.
patent: 7104143 (2006-09-01), Powell
patent: 7333030 (2008-02-01), Baranov et al.
patent: 2002/0024652 (2002-02-01), Ooga
patent: 2003/0222795 (2003-12-01), Holforty et al.
patent: 2005/0105540 (2005-05-01), Baumann et al.
patent: 2006/0244637 (2006-11-01), Baranov et al.
patent: 2007/0034746 (2007-02-01), Shmilovich et al.
patent: 2007/0045476 (2007-03-01), Shmilovich et al.
patent: 2007/0051855 (2007-03-01), Shmilovich et al.
patent: 2007/0103340 (2007-05-01), Baranov et al.
patent: 2008/0035784 (2008-02-01), Meserole et al.
patent: 2008/0035789 (2008-02-01), Lewis et al.
patent: 2008/0042013 (2008-02-01), Shmilovich et al.
patent: 2009/0173835 (2009-07-01), Shmilovich et al.
patent: 1756541 (1970-04-01), None
patent: 10039109 (2002-02-01), None
patent: 0689990 (1996-01-01), None
Choroba et al. “The Concept of Integrated Air Traffic Control Wake Vortex Safety andCapacity System,” IEEE Oct. 2003, vol. 1, pp. 684-688.
International Search Report and Written Opinion for PCT/US07/016394; Applicant: The Boeing Company; mailed Oct. 29, 2008, 15 pages.
Holzapfel, Frank, “Analysis of Wake Vortex Decay Mechanisms in the Atmosphere,” Aerospace Science and Technology 7, 2003, pp. 263-375.
“Wake Data and Safety Assessment Methods,” 1st Workshop WakeNet2-Europe (organised in collaboration with WakeNet-USA), London, Heathrow Control Tower, Nov.11-12, final Aug. 11, 2003, 18 pages.
Langevin, Gail., “Wake-Vortex Hazard,” NASA Verified to 2004 by Wayback Machine.
Lewellen, D.C. et al., “Large-Eddy Simulations and Lidar Measurements of Vortex-Pair Breakup in Aircraft Wakes,” Aug. 8, 1998, AIAA Journal, vol. 36 No. 8, pp. 1439-1445.
Rodenhiser, R., “An Ultrasonic Method for Aircraft Wake Vortex Detection,” Aug. 30, 2005, 115 pgs, Worcester Polytechnic Institute.
Sauvage, L., et al., “WB Separations Technology Case, Preparation of Wake Vortex Detection Technology Case, Eurocontrol EEC TRSC52/2004, Public Summary Report,” 29 pgs, Mar. 2005, Leosphere, Paris, France.
Socrates Wake Vortex Tection and Tracking: A Technical Status Report, Nov. 22, 2004, 29 pgs, Flight Safety Technology, Lockheed Martin.
Tank, W., “Airplane wake detection iwth a VHF cw bistatic radar,” Jan. 1997, 13 pgs, AIAA Meeting Papers, American Institute of Aeronautics and Astronautics, Inc.
Wall, Robert, “Airbus Cries Foul in A380 Wake Vortex Debate,” 2 pgs, http://www.aviationow.com/search/AvnowSearchResult.do?reference, accessed Jan. 10, 2006.
Dunn Michael J.
Lewis Michael S.
Meserole Jere S.
Tillotson Brian J.
Ellis Christopher P
Perkins Coie LLP
The Boeing Company
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