Aircraft high-lift system with overload protection

Details Aircraft high-lift system with overload protection Aircraft high-lift system with overload protection

2007-03-27

2007-03-27

Collins, Timothy D. (Department: 3643)

Aeronautics and astronautics

Aircraft sustentation

Sustaining airfoils

C060S431000

Reexamination Certificate

active

10788160

ABSTRACT:
The invention concerns an aircraft high-lift system with a drive system, components for transmitting the drive energy over the entire wing span to drive stations of individual segments of landing flap/slat flap systems, and with overload protection. According to the invention, the overload protection consists of electrical load sensors positioned at the drive-energy in-take points of the individual power trains on the flaps.

REFERENCES:
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patent: 4745815 (1988-05-01), Klopfenstein
patent: 4786013 (1988-11-01), Pohl
patent: 4858491 (1989-08-01), Shube
patent: 5409188 (1995-04-01), Takagi et al.
patent: 6616096 (2003-09-01), Witton et al.
patent: 3800647 (1989-07-01), None
patent: 1065487 (2001-01-01), None
patent: WO2004/008097 (2004-01-01), None
htt://www.omega.com/literature/transactions/volume3/load3.html, “Load Cell Designs”.
http://www.omega.com/literature/transactions/volume3/load3.html, “Load Cell Designs”.

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