Winglet

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Reexamination Certificate

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Details

C244S199100

Reexamination Certificate

active

07988099

ABSTRACT:
A winglet for an aircraft wing is provided. The winglet has an airflow control arrangement, for example in the form of a trailing edge flap (20) by means of which lift generated by the winglet can be varied. The control arrangement desirably forms part of a manoeuvre load alleviation system (22) for the aircraft.

REFERENCES:
patent: 2557829 (1951-06-01), Lavelle
patent: 2697568 (1954-12-01), Powers
patent: 3144220 (1964-08-01), Kittelson
patent: 4455004 (1984-06-01), Whitaker, Sr.
patent: 4457479 (1984-07-01), Daude
patent: 4545552 (1985-10-01), Welles
patent: 4722499 (1988-02-01), Klug
patent: 4796192 (1989-01-01), Lewis
patent: 5100081 (1992-03-01), Thomas
patent: 5156358 (1992-10-01), Gerhardt
patent: 5988563 (1999-11-01), Allen
patent: 6042059 (2000-03-01), Bilanin et al.
patent: 6484968 (2002-11-01), Felker
patent: 6578798 (2003-06-01), Dizdarevic et al.
patent: 6673402 (2004-01-01), Wildenrotter et al.
patent: 196410 (1923-04-01), None
patent: 390201 (1933-03-01), None
patent: 576125 (1946-03-01), None
patent: 819919 (1959-09-01), None
Definition of the term “winglet” from www.merriam-webster.com.
Definition of the term “fixed” from www.merriam-webster.com.

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