Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils
Reexamination Certificate
2006-05-23
2006-05-23
Eldred, J. Woodrow (Department: 3644)
Aeronautics and astronautics
Aircraft sustentation
Sustaining airfoils
C244S216000, C244S204000
Reexamination Certificate
active
07048235
ABSTRACT:
A swept aircraft wing includes a leading airfoil element and a trailing airfoil element. At least one full-span slot is defined by the wing during at least one transonic condition of the wing. The full-span slot allows a portion of the air flowing along the lower surface of the leading airfoil element to split and flow over the upper surface of the trailing airfoil element so as to achieve a performance improvement in the transonic condition.
REFERENCES:
patent: 2177798 (1939-10-01), Bechereau
patent: 2772058 (1956-11-01), Grant
patent: 2908454 (1959-10-01), De Wolff
patent: 3259341 (1966-07-01), Steidl
patent: 3638886 (1972-02-01), Zimmer
patent: 3653611 (1972-04-01), Trupp et al.
patent: 4015787 (1977-04-01), Maieli et al.
patent: 4117996 (1978-10-01), Sherman
patent: 4353517 (1982-10-01), Rudolph
patent: 4441675 (1984-04-01), Boehringer et al.
patent: 4498646 (1985-02-01), Proksch et al.
patent: 4533096 (1985-08-01), Baker et al.
patent: 4575030 (1986-03-01), Gratzer
patent: 4576347 (1986-03-01), Opsahl
patent: 4856735 (1989-08-01), Lotz et al.
patent: 5082208 (1992-01-01), Matich
patent: 5088661 (1992-02-01), Whitener
patent: 5178348 (1993-01-01), Bliesner
patent: 5265830 (1993-11-01), Allen
patent: 5551651 (1996-09-01), Hendrickson
patent: 5680124 (1997-10-01), Bedell et al.
patent: 5686907 (1997-11-01), Bedell et al.
patent: 5788190 (1998-08-01), Siers
patent: 6293497 (2001-09-01), Kelley-Wickemeyer et al.
patent: 6328265 (2001-12-01), Dizdarevic
patent: 6592072 (2003-07-01), Gregg, III et al.
patent: 0 838 394 (1998-04-01), None
Application of Mini-Trailing-Edge Devices in the Awiator Project, H. Hansen, Airbus Deutschland, EGAG, Hunefeldstr. 1-5, D-28199 Bremen, Germany.
Optimization Techniques in Airfoil Design, Mark Drela, MIT Aero & Astro.
PCT International Search Report for App. No. PCT/US03/32060, dated Feb. 18, 2004, 4 pages.
Campbell Richard L.
McLean James D.
Witkowski David P.
Eldred J. Woodrow
Harness & Dickey & Pierce P.L.C.
The Boeing Company
LandOfFree
Slotted aircraft wing does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Slotted aircraft wing, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Slotted aircraft wing will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-3613573