Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils
Reexamination Certificate
2006-08-04
2009-12-01
Collins, Timothy D (Department: 3643)
Aeronautics and astronautics
Aircraft sustentation
Sustaining airfoils
C244S00100R, C343S708000
Reexamination Certificate
active
07624951
ABSTRACT:
An aircraft has a fuselage and a pair of wings joined to the fuselage at a dihedral angle. A wing extension, such as an angled winglet or a wing-tip pod, is joined to a distal end of each of the wings. A top-surface antenna lies in each of the top surfaces, and a bottom-surface antenna lies in each of the bottom surfaces. The antennas are preferably flat-panel antennas such as phased-array antennas.
REFERENCES:
patent: 4714215 (1987-12-01), Jupp et al.
patent: 6577272 (2003-06-01), Madden
patent: 6653980 (2003-11-01), Ceccom et al.
patent: 6873296 (2005-03-01), Langley et al.
patent: 6954182 (2005-10-01), Knapp
patent: 7019681 (2006-03-01), Pellett et al.
patent: 2008/0210822 (2008-09-01), Hanusa et al.
Goff Joshua T.
Kraft John R.
Rowe Frank J.
Stevens Jason A.
Collins Timothy D
Hawker Beechcraft Corporation
Lerner David Littenberg Krumholz & Mentlik LLP
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