Radome and device for attaching said radome to an aircraft
A radome and aircraft technology, applied in the field of radome, can solve problems such as spending more time, and achieve the effect of being conducive to support and high resistance
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[0040] figure 1 and FIG. 2 : The radome ( 1 ) according to the invention comprises a double curvature surface ( 12 ) made of a material capable of transmitting electromagnetic waves, preferably a honeycomb type composite material. The radome (1) comprises a rigid one-piece ring (11) extending from a junction end (10) fixed to the aircraft fuselage to the location of a locking device (20). This rigid one-piece ring maintains the consistency of the shape of the radome—in particular during opening of the radome, for example during inspection or maintenance operations on a radar arranged below the radome.
[0041] The rigidity of the ring (11) also means that the radome can remain fixed to the fuselage with a reduced number of fuselage anchoring and locking points. On the other hand, the stiffness of the ring does not allow a complete smoothing and adjustment of the shape of the junctional end (10) to the shape of the fuselage. In order to allow the junctional ring of the radom...
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