Abstract: Admixture generation determination includes: obtaining ancestry assignment information associated with an individual's genotype data, the ancestry assignment information at least indicating that a portion of the individual's genotype data is deemed to be associated with a specific ancestry; determining the individual's genetic ancestry summary data corresponding to the specific ancestry; estimating an admixture generation associated with the specific ancestry, the admixture generation indicating a most recent generation or a most recent generation range from which the individual has at least one non-admixed ancestor of the specific ancestry, the estimation including a maximum likelihood determination based at least in part on the individual's genetic ancestry summary data and a recombination model; and outputting the estimated admixture generation.

Abstract: Estimating parental contribution of ancestry includes: obtaining a set of ancestry assignment data associated with an individual's genotype data, at least some of the ancestry assignment data indicating that one or more segments of the individual's genotype data is deemed to be associated with a specific ancestry; determining whether in the individual's genotype data there is at least one confirmed region of overlapping ancestry assignment associated with the specific ancestry; in the event that it is determined that there is at least one confirmed region of overlapping ancestry assignment associated with the specific ancestry: specifying that parental contribution of the specific ancestry is made by both parents of the individual; in the event that it is determined that there is no confirmed region of overlapping ancestry assignment associated with the specific ancestry: statistically determining whether the parental contribution to the specific ancestry is made by only one parent of the individual or by bot

Abstract: Ancestry deconvolution includes obtaining unphased genotype data of an individual; phasing, using one or more processors, the unphased genotype data to generate phased haplotype data; using a learning machine to classify portions of the phased haplotype data as corresponding to specific ancestries respectively and generate initial classification results; and correcting errors in the initial classification results to generate modified classification results.

Abstract: Estimating parental contribution of ancestry includes: obtaining a set of ancestry assignment data associated with an individual's genotype data, at least some of the ancestry assignment data indicating that one or more segments of the individual's genotype data is deemed to be associated with a specific ancestry; determining whether in the individual's genotype data there is at least one confirmed region of overlapping ancestry assignment associated with the specific ancestry; in the event that it is determined that there is at least one confirmed region of overlapping ancestry assignment associated with the specific ancestry: specifying that parental contribution of the specific ancestry is made by both parents of the individual; in the event that it is determined that there is no confirmed region of overlapping ancestry assignment associated with the specific ancestry: statistically determining whether the parental contribution to the specific ancestry is made by only one parent of the individual or by bot

Abstract: Admixture generation determination includes: obtaining ancestry assignment information associated with an individual's genotype data, the ancestry assignment information at least indicating that a portion of the individual's genotype data is deemed to be associated with a specific ancestry; determining the individual's genetic ancestry summary data corresponding to the specific ancestry; estimating an admixture generation associated with the specific ancestry, the admixture generation indicating a most recent generation or a most recent generation range from which the individual has at least one non-admixed ancestor of the specific ancestry, the estimation including a maximum likelihood determination based at least in part on the individual's genetic ancestry summary data and a recombination model; and outputting the estimated admixture generation.

Abstract: Estimating parental contribution of ancestry includes: obtaining a set of ancestry assignment data associated with an individual's genotype data, at least some of the ancestry assignment data indicating that one or more segments of the individual's genotype data is deemed to be associated with a specific ancestry; determining whether in the individual's genotype data there is at least one confirmed region of overlapping ancestry assignment associated with the specific ancestry; in the event that it is determined that there is at least one confirmed region of overlapping ancestry assignment associated with the specific ancestry: specifying that parental contribution of the specific ancestry is made by both parents of the individual; in the event that it is determined that there is no confirmed region of overlapping ancestry assignment associated with the specific ancestry: statistically determining whether the parental contribution to the specific ancestry is made by only one parent of the individual or by bot

Abstract: Ancestry deconvolution includes obtaining unphased genotype data of an individual; phasing, using one or more processors, the unphased genotype data to generate phased haplotype data; using a learning machine to classify portions of the phased haplotype data as corresponding to specific ancestries respectively and generate initial classification results; and correcting errors in the initial classification results to generate modified classification results.

Abstract: The stiffening frames (14) of an aircraft fuselage (2) remain continuous while passing through an upper panel (5) of the wing box and extend over the ribs (3) situated in that box. The overall mechanical strength of the assembly is improved, despite the notches it is necessary to make in the panel (5).

Abstract: An aircraft structure includes a wing spar (10), with orbital frames (24, 24?, 24?) arranged in transverse planes, right and left horizontal spars (26) connected to the wing spar (10) at the upper panel (14) of the spar respectively to the right and to the left of the spar, and for each right or left horizontal spar (26), a triangular panel (50) that includes a wall (60), a first edge arranged at the horizontal spar (26), a second side arranged at the wing spar (10), and a third side at which a first rectilinear oblique reinforcement (62) connecting the horizontal spar (26) and the wing spar (10) is provided, characterized in that the triangular panel (50) includes at least one second rectilinear oblique reinforcement (64) that connects the horizontal spar (26) and the wing spar (10).

Abstract: A device for sectioning an electrical circuit is provided. The device includes a housing having two main sectioning terminals and, in the housing, a first member for sectioning a first electrical connection between the two main sectioning terminals, an automatic control, under the action of an electrical signal, of the first sectioning member from the closed position to the open position thereof, and a manual control member for resetting the first sectioning member from the open position to the closed position thereof. The device also includes, in the housing, two secondary sectioning terminals and a second sectioning member movable between a position for opening and a position for closing a second electrical connection between the two secondary sectioning terminals, the second sectioning member being coupled to the first sectioning member, commutation of the first sectioning member bringing about commutation of the second sectioning member.

Abstract: The stiffening frames (14) of an aircraft fuselage (2) remain continuous while passing through an upper panel (5) of the wing box and extend over the ribs (3) situated in that box. The overall mechanical strength of the assembly is improved, despite the notches it is necessary to make in the panel (5).

Abstract: An aircraft structure includes a wing spar (10), with orbital frames (24, 24?, 24?) arranged in transverse planes, right and left horizontal spars (26) connected to the wing spar (10) at the upper panel (14) of the spar respectively to the right and to the left of the spar, and for each right or left horizontal spar (26), a triangular panel (50) that includes a wall (60), a first edge arranged at the horizontal spar (26), a second side arranged at the wing spar (10), and a third side at which a first rectilinear oblique reinforcement (62) connecting the horizontal spar (26) and the wing spar (10) is provided, characterized in that the triangular panel (50) includes at least one second rectilinear oblique reinforcement (64) that connects the horizontal spar (26) and the wing spar (10).

Abstract: A device for sectioning an electrical circuit is provided. The device includes a housing having two main sectioning terminals and, in the housing, a first member for sectioning a first electrical connection between the two main sectioning terminals, an automatic control, under the action of an electrical signal, of the first sectioning member from the closed position to the open position thereof, and a manual control member for resetting the first sectioning member from the open position to the closed position thereof. The device also includes, in the housing, two secondary sectioning terminals and a second sectioning member movable between a position for opening and a position for closing a second electrical connection between the two secondary sectioning terminals, the second sectioning member being coupled to the first sectioning member, commutation of the first sectioning member bringing about commutation of the second sectioning member.

Abstract: A device for joining, in particular, composite structure elements with metallic structure elements of an aircraft. The device includes a junction element, provided with a first longitudinal partition wall fastened to a metallic panel, integral with a stiffener comprising a vertical core and at least one baseplate, with a second longitudinal partition wall, fastened to a composite panel, and with a lower branch to which are connected the proximal extremities of the said first and second longitudinal partition walls. The device further includes a first fitting element, provided with a first pick-up fitting body on the said stiffener and with a first heel and a second fitting element, provided with a second pick-up fitting body on the composite panel, and with a second heel, the heels of the fitting elements being fastened to the lower branch, on both sides of the lower branch, opposite each other.

Abstract: A device for joining, in particular, composite structure elements with metallic structure elements of an aircraft, comprising a junction element, provided with a first longitudinal partition wall fastened to a metallic panel, integral with a stiffener comprising a vertical core and at least one baseplate, with a second longitudinal partition wall, fastened to a composite panel, and with a lower branch to which are connected the proximal extremities of the said first and second longitudinal partition walls, the device comprising, moreover, a first fitting element, provided with a first pick-up fitting body on the said stiffener and with a first heel and a second fitting element, provided with a second pick-up fitting body on the composite panel, and with a second heel, the heels of the fitting elements being fastened to the lower branch, on both sides of the lower branch, opposite each other.

Abstract: Polyamide-based thermoplastic compositions comprising by weight:

Abstract: Polyamide-based thermoplastic compositions comprising by weight: 50 to 99% of a polyamide (A1), 1 to 50% of a catalyzed polyamide (A2), 0 to 40% of a plasticizer, 0 to 60%, preferably 0 to 30%, of a flexible modifier, the total being 100%, are useful for manufacturing articles, for example, flexible pipes.