Assertion: radome | /r/CapableOf | come into contact
Facets:
value: with the fuselage
type: OTHER
Source sentences:
text: 2 shows a perspective view of such a radome, particularly its periphery 3 that can come into contact with the fuselage 1 of the aircraft.
text: Preferably, said single axis along which the radome is positioned by each of said second fasteners is approximately perpendicular to the tangent to the perimeter of the radome at the point at which the distance between firstly said perimeter of the radome that can come into contact with the fuselage and secondly the longitudinal axis of said fastener is minimum.
text: a1) fix a set of fittings inside said radome, distributed close to the perimeter of this radome coming into contact with the aircraft fuselage; b1) choose a subset of fittings distributed among the set of fittings fixed to the radome in step a1) and fix a convex-shaped part corresponding to a first fastener, as described above, onto each of the fittings of said subset; b2) fix a convex-shaped part corresponding to a second fastener, as described above, on each of the fittings placed during step a1) and not belonging to the subset chosen in step b1), orienting said convex-shaped part such that said single axis contained in a plane perpendicular to the longitudinal axis of this fastener, according to which said second fastener positions the radome is approximately perpendicular to the tangent to the perimeter of the radome at the point at which the distance between firstly said perimeter of the radome that can come into contact with the fuselage and secondly the longitudinal axis of said fastener is minimum; c) fix concave-shaped parts on a fuselage frame, so that these concave-shaped parts are facing each of said convex-shaped parts when the radome is in its planned position on the aircraft; d) put guide rods into position on each of the convex-shaped parts corresponding to first fasteners put into position during step b1); e) offer up the radome in front of the fuselage and insert said guide rods placed in step d) into the concave-shaped parts corresponding to them fixed on the fuselage in step c) until said guide rods pass through said concave-shaped parts; f) put a locking device into position at the end of each of said guide rods so as to secure placement of the radome on the aircraft fuselage; g) put a screw into position in each of the concave-shaped parts of the second fasteners, through the face of said concave part opposite its face in contact with the convex part fixed to the radome and screw this screw into this convex part; h) remove the guide rods from the first fasteners and replace them with screws in the same way as for the second fasteners (step g)).
text: Four first fasteners 10 are arranged on the inside of the radome close to the perimeter 3 of the radome that can come into contact with the aircraft fuselage.