There is provided a leading edge system (10) 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 (42) and at least one flange portion disposed along a first end (52) of the hollow box substructure. The leading edge system further has a plurality of first attachment elements (70) configured for attaching the at least one flange portion (54) 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 (74) 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.
СПОСОБЫ И СИСТЕМЫ ДЛЯ ПЕРЕДНИХ КРОМОК АЭРОКОСМИЧЕСКИХ ТРАНСПОРТНЫХ СРЕДСТВ
2018-10-22
Patent
Electronic Resource
Russian
СИСТЕМЫ И СПОСОБЫ ВОЗВРАТА ДЛЯ БЕСПИЛОТНЫХ ПОДВОДНЫХ ТРАНСПОРТНЫХ СРЕДСТВ
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European Patent Office | 2017