Leading edge systems and methods for aerospace vehicles
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United States of America Patent
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Apr 23, 2019
Grant Date -
Jan 25, 2018
app pub date -
Jul 20, 2016
filing date -
Jul 20, 2016
priority date (Note) -
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Abstract
There is provided a leading edge system for an aerospace vehicle. The leading edge system has at least one structural member. The leading edge system further has a plurality of removable modules removably attached to the at least one structural member. Each removable module has a hollow box substructure and at least one flange portion disposed along a first end of the hollow box substructure. The leading edge system further has a plurality of first attachment elements configured for attaching the at least one flange portion of the removable module to a first end portion of the at least one structural member. The leading edge system further has a plurality of second attachment elements configured for attaching a second end of the hollow box substructure opposite the flange portion, to a second end portion of the at least one structural member opposite the first end portion.
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