Aeronautics and astronautics – Aircraft structure – Ice prevention
Reexamination Certificate
2006-06-27
2006-06-27
Dinh, Tien (Department: 3644)
Aeronautics and astronautics
Aircraft structure
Ice prevention
Reexamination Certificate
active
07066431
ABSTRACT:
The present invention relates to apparatus for influencing fluid flow over a surface, and more particularly, but not exclusively, to turbulent boundary layer flow drag reduction for an aircraft. The present invention provides such apparatus including a plasma generator comprising a first electrode and a signal generator, the apparatus being operable to drive the first electrode with a pulsed signal generated by the signal generator thereby to cause a change in direction of the flow of the fluid over the surface.
REFERENCES:
patent: 3095163 (1963-06-01), Hill
patent: 3162398 (1964-12-01), Meyer et al.
patent: 3224375 (1965-12-01), Hoff
patent: 3360220 (1967-12-01), Meyer
patent: 5669583 (1997-09-01), Roth
patent: 5917286 (1999-06-01), Scholl et al.
patent: 5938854 (1999-08-01), Roth
patent: 5941481 (1999-08-01), Snarski
patent: 6200539 (2001-03-01), Sherman et al.
patent: 6220549 (2001-04-01), Tsunoda et al.
patent: 6805325 (2004-10-01), Malmuth et al.
patent: 6888314 (2005-05-01), Krichtafovitch et al.
patent: 1 031 925 (1953-06-01), None
patent: 1134446 (1968-11-01), None
patent: 2 208 656 (1989-04-01), None
patent: 94/00342 (1994-01-01), None
Johnson Graham A
Scott Simon J
Thornton Edward
Airbus UK Limited
Dinh Tien
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