Aircraft wet wing

Details Aircraft wet wing Aircraft wet wing

2005-04-22

2008-10-28

Collins, Timothy D (Department: 3643)

Aeronautics and astronautics

Aircraft structure

Fuselage and body construction

C244S00100R, C244S13400A

Reexamination Certificate

active

07441725

ABSTRACT:
An aircraft wing (12) comprising a structural casing (14) defining a leading edge, a fuel cell (16) within the structural casing (14), a deicer (18) having electrical lines which receive a supply of electrical power from an onboard power source, and a trip line (20). The trip line (20) is positioned to receive early contact upon impact of the wing by a bird or other foreign object and disruption of the trip line triggers termination of the supply of electrical power to the deicer (18).

REFERENCES:
patent: 4581504 (1986-04-01), Hamel, Sr.
patent: 4814931 (1989-03-01), Kugelman et al.
patent: 5089926 (1992-02-01), Kugelman
patent: 5481139 (1996-01-01), Lucas
patent: 2004/0212940 (2004-10-01), Kugelman et al.
patent: 2004/0222701 (2004-11-01), Kugelman
patent: 497163 (1938-12-01), None
patent: 2001314026 (2001-11-01), None
GB0607497.5; Great Britain Search Report dated Jul. 26, 2006.

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