Abstract: A lifting surface comprising a movable discontinuity located in the surface of the lifting surface. The movable discontinuity is movable between an active position in which the movable discontinuity acts as vortex generator, and a passive position in which the movable discontinuity is integrated into the surface of the lifting surface without acting as vortex generator. The lifting surface may be in an elevator, the elevator being rotatable around a hinge line with respect to the rest of the lifting surface. A bar is rigidly joined to the elevator. The bar, the elevator and the movable discontinuity are configured such that when the elevator rotates with respect to the rest of the lifting surface, the bar moves the movable discontinuity that departs from the surface of the lifting surface, acting as a vortex generator.

Abstract: A latch is disclosed herein.

Abstract: A latch is disclosed herein. The latch having: a fork bolt movably mounted to the latch for movement between an open position and a closed position; a detent lever movably mounted to the latch for movement between a latched position and a released position, wherein the detent lever prevents the fork bolt from moving from the closed position to the open position when the detent lever is in the latched position; a hold open lever configured to engage and retain the detent lever when it moves from the latched position to the released position; and wherein the fork bolt is configured to disengage the hold open lever from the detent lever when the fork bolt travels away from the closed position.

Abstract: An aircraft stabilizer (15, 17) with an enlarged area of laminar flow. The lateral skins (45a, 45b; 65a, 65b) of its torsion box (43; 63) include joggled areas (53a, 53b; 73a, 73b) as attachment areas of its leading edge (41; 61) which are arranged in a rearward position with respect to the forward most spar of the stabilizer (15, 17).

Abstract: A lightweight shield for aircraft protection against threat of high energy impacts, which comprises, a structural layer that has a first side and a second side, the first side being intended for receiving the impact, and a ballistic material layer for absorbing high energy impacts, having a first side and a second side. The first side of the ballistic material layer is faced to the second side of structural layer and joined to the structural layer via a progressively detachable interface and, the second side of the ballistic material layer is a free surface.

Abstract: A pressure bulkhead for an aircraft comprising a fuselage. The pressure bulkhead comprises an inflatable element, suitable for being filled with air, which in turn comprises a cover which delimits an inner zone. The pressure bulkhead further comprises a seal suitable for providing an airtight seal between the cover and the fuselage of the aircraft.

Abstract: A leading edge for an airfoil comprising a torsion box, the leading edge comprising a leading plate and a first inflatable element suitable for being filled with air. The leading plate comprises a convex side and a concave side. The first inflatable element is in contact with at least part of the concave side, thus reinforcing the leading plate. An airfoil comprising such a leading edge is also provided.

Abstract: An external part of an aircraft (such as a fairing) comprising a skin made with flexible materials attached to rigid supporting elements (such as longerons and frames) arranged in, at least, two directions. The skin comprises inner inflatable panels in all bays delimited by the rigid supporting elements and/or an external inflatable panel. The skin is joined to the supporting elements so that its external surface complies with aerodynamic requirements.

Abstract: The present disclosure refers to a multi-spar torsion box structure comprising a plurality of spars of composite material arranged to form a multi-cell structure with two or more cells extending span-wise at the torsion box, and upper and lower skin covers of composite material respectively joined to upper and lower surfaces of the multi-cell structure. The structure further comprises at least one belt-like reinforcing element extending on the outer perimeter of the torsion box, and fixed to the upper and lower surfaces of the multi-cell structure, and transversely arranged with respect to the span-wise direction of the torsion box. The belt-like reinforcing element is made of a metallic or a composite material. The present disclosure can advantageously be used in the manufacture of aircrafts lifting surfaces, such as horizontal tail planes (HTP) or wings.

Abstract: A latch is provided including a fork bolt configured to rotate between an unlatched position and a latched position. A bellcrank lever is operably coupled to the fork bolt via a detent lever. The bellcrank lever has an engagement ledge located adjacent a slot of the bellcrank lever. The engagement shelf prevents movement of a gear configured to move the detent lever via movement of the bellcrank lever.

Abstract: A latch including a locking lever pivotally mounted to the latch. The latch also including an intermittent lever pivotally coupled to the locking lever at a first end, wherein movement of the locking lever causes a movement of the intermittent lever. A gear is pivotally coupled to a second end of the locking lever such that rotation of the gear causes movement of the locking lever. The locking lever is formed from a resilient material and has an area of reduced thickness reproducing a spring effect. Movement of the second end of the locking lever with respect to the first end of the locking lever creates a biasing force in the locking lever.

Abstract: A latch having: a fork bolt movably mounted thereto; a detent lever movably mounted thereto, wherein the detent lever prevents the fork bolt from moving from a closed position to an open position when the detent lever is in a latched position; a bell crank lever movably mounted to the latch for movement between a first position and a second position, wherein the bell crank lever moves the detent lever from the latched position to the released position as the bell crank lever moves from the first position to the second position; a release lever movably mounted to the latch for movement between a first position and a second position; and an intermittent pin operatively coupled to bell crank lever and the release lever, wherein movement of the release lever is not transferred to the bell crank lever when the intermittent pin is in the second position.

Abstract: A latch is disclosed herein.

Abstract: The invention concerns a method for beneficiation of fly ash particles comprising: determining the heat value of the fly ash particles; comparing the determined heat value of the fly ash particles with a minimum heat value K; feeding an inlet of a combustor (5) with a feed material comprising the fly ash particles and, in case the determined heat value is lower than the minimum heat value K, fuel in sufficient quantity to assure that the heat value of the raw material is greater than or equal to the minimum heat value K; supplying an upstream airflow to the combustor (5) so as to carry the feed material in suspension from the inlet to an outlet of the combustor; operating the combustor (5) at a temperature of at least 700° C.; collecting beneficiated fly ash particles from the airflow at the outlet of the combustor (5). The invention also concerns an installation for implementation of the said method.

Abstract: A latch is provided, the latch having: a fork bolt that moves between an unlatched position and a latched position; a first detent lever that that cooperates with the fork bolt and moves between an engaged position and a disengaged position; a hold open lever for biasing against the first detent lever when the first detent lever is in the released position; and a single switch that is activated only when the first detent lever is moved from the engaged position towards the disengaged position and when the fork bolt moves from the unlatched position towards the latched position, wherein the latch does not have any other switches.

Abstract: A latch is disclosed herein. The latch having: a fork bolt movably mounted to the latch for movement between an open position and a closed position; a detent lever movably mounted to the latch for movement between a latched position and a released position, wherein the detent lever prevents the fork bolt from moving from the closed position to the open position when the detent lever is in the latched position; a hold open lever configured to engage and retain the detent lever when it moves from the latched position to the released position; and wherein the fork bolt is configured to disengage the hold open lever from the detent lever when the fork bolt travels away from the closed position.

Abstract: A latch is provided including a fork bolt configured to rotate between an unlatched position and a latched position. A bellcrank lever is operably coupled to the fork bolt via a detent lever. The bellcrank lever has an engagement ledge located adjacent a slot of the bellcrank lever. The engagement shelf prevents movement of a gear configured to move the detent lever via movement of the bellcrank lever.

Abstract: A polarizer screen for a satellite communications terminal, comprising a plurality of layers separated by dielectric material, each layer having a grid of parallel metal strips and a periodic distribution of interleaved metal dipoles, wherein a first set of dipoles is arranged to be perpendicular to the metal strips and a second set of dipoles is arranged to be parallel to the metal strips such that any linearly polarized electromagnetic waves that pass through the screen are converted into orthogonal circular polarization in different frequency bands.

Abstract: A latch including a locking lever pivotally mounted to the latch. The latch also including an intermittent lever pivotally coupled to the locking lever at a first end, wherein movement of the locking lever causes a movement of the intermittent lever. A gear is pivotally coupled to a second end of the locking lever such that rotation of the gear causes movement of the locking lever. The locking lever is formed from a resilient material and has an area of reduced thickness reproducing a spring effect. Movement of the second end of the locking lever with respect to the first end of the locking lever creates a biasing force in the locking lever.

Abstract: A compartment latch is shown. It includes a fork bolt that moves between an open position and a closed position and a first detent lever that that cooperates with the fork bolt and that moves between a latched position and a released position. A support for holding the fork bolt and the detent lever is also provided. A second detent lever for biasing against the first detent lever when the first detent lever is in the released position is provided. The second detent lever is connected to the support at a hinge.