Abstract: Described herein is a receiver for a navigation system, which receives a navigation signal modulated with a pseudorandom sequence along a line-of-sight path and reflected paths. The receiver includes a delay-locked loop, which generates a local sequence, and a first correlator and a second correlator, which operate in open-loop mode and generate a first correlation signal.

Abstract: The present invention provides apparatus for processing and regenerating the signals of telecommunication satellites, for meshed communications on multi-beam coverage between standard DVB-RCS and DVB-S2 user terminals and apparatus for filtering and routing the signals transferred between ground terminals.

Abstract: The present invention relates to propellant tanks for space platforms, launchers and every sort of space transport craft.

Abstract: An actuation system which implements a three-dimensional rectilinear guide with high rectilinear features and it provides stability and stiffness to the moved object by supporting it in a not operating initial phase, particularly suitable to the translation of reflectors for satellite antennas along a predetermined axis in order to obtain the zooming effect thereof on the radiation diagram of the antenna itself.

Abstract: Isostatic deployable support structure for antenna reflectors for vehicles characterized in that it is constituted by six supports hinged to each of their ends in three points on the structure of the vehicle and in three points on the structure of the reflector, in which: —two out of the three points of hinging on the structure of the reflector are positioned in points that are diametrically symmetrical with respect to the plane of symmetry of the antenna optics, and the third one is positioned on the plane of symmetry of the antenna optics, at the end of the reflector that is closer to the illumination system of the reflector; —two out the three points of hinging on the structure of the vehicle are positioned in points that are symmetrical with respect to the plane of symmetry of the antenna optics, as distant as possible, in the area between the reflector and the illumination system, and the third one is positioned on the plane of symmetry of the antenna optics, above the side of the illumination system tha

Abstract: The invention consists of a communication system that relays a satellite signal inside railway tunnels and relays the signals transmitted inside said tunnels towards the satellite, in such a way as to assure to vehicles transiting inside the tunnels a perfect transmission and reception quality even in the absence of satellite visibility. The system is based on a fixed terminal, for gallery illumination, connected to a fixed satellite station, and on a mobile terminal installed on the vehicle, connected to a mobile satellite terminal. The system automatically effects a switching action between satellite channel and radio channel in the tunnel, and vice versa, to assure the continuity of the vehicle-satellite connection. The system finds elective application for railway vehicles.

Abstract: Thin film coating for transferring antistatic characteristics to the surface on which it is placed, in particular antenna surfaces, in order to prevent electrical charge accumulations on it and discharge phenomenon.

Abstract: An actuation system which implements a three-dimensional rectilinear guide with high rectilinear features and it provides stability and stiffness to the moved object by supporting it in a not operating initial phase, particularly suitable to the translation of reflectors for satellite antennas along a predetermined axis in order to obtain the zooming effect thereof on the radiation diagram of the antenna itself.

Abstract: Isostatic deployable support structure for antenna reflectors for vehicles characterized in that it is constituted by six supports hinged to each of their ends in three points on the structure of the vehicle and in three points on the structure of the reflector, in which: —two out of the three points of hinging on the structure of the reflector are positioned in points that are diametrically symmetrical with respect to the plane of symmetry of the antenna optics, and the third one is positioned on the plane of symmetry of the antenna optics, at the end of the reflector that is closer to the illumination system of the reflector; —two out the three points of hinging on the structure of the vehicle are positioned in points that are symmetrical with respect to the plane of symmetry of the antenna optics, as distant as possible, in the area between the reflector and the illumination system, and the third one is positioned on the plane of symmetry of the antenna optics, above the side of the illumination system tha

Abstract: A panoramic telescope of the type having a body 3 to be mounted on a vehicle, a head-piece 9 attached to the body and rotating with respect thereto. A window 11 is provided for observing the external scenery. Inside the head-piece is a mirror 13 for deflecting the incoming beam from the window towards an optical detector.

Abstract: A panoramic periscope includes a central body (3, 3A) and a rotating head-piece (9) supported on the central body. Inside the central body, an optical path (21, 23, 101, 105, 109, 111, 113) for an optical beam (F,) coming from the head-piece (9) is provided. A viewing module (17) receives the optical beam, for observing the external scenery. A laser telemeter (19) is provided and, along the optical path, a separator element (10S) with an inner dichroic surface (105A) is passed through by the optical beam coming from the head-piece (9). The inner dichroic surface (105A) separates a laser beam coming from the head-piece (9) and deviating it towards a separate optical path (107) which conveys the laser beam towards the laser telemeter (19). The separator element (105) has an entry surface (105I) and an exit surface (105U) which are parallel with one another and passed through by the optical beam (FV), the surfaces being perpendicular to the optical beam (FV).

Abstract: An infrared image sensor, in particular one of the interlaced parallel scanning type, is described. The infrared image sensor has an optical focusing system for focusing an image on a matrix of sensitive elements (55) for the detection of the image. A collimator unit (5) forms a focal plane. The collimator unit is disposed at the entry of the sensor. At least one thermal reference (33), whose image is projected on the matrix (55), is disposed on the optical path of the image inside the sensor.

Abstract: A panoramic telescope of the type having a body 3 to be mounted on a vehicle, a head-piece 9 attached to the body and rotating with respect thereto. A window 11 is provided for observing the external scenery. Inside the head-piece is a mirror 13 for deflecting the incoming beam from the window towards an optical detector.

Abstract: A helicopter rotor brake having a disk connected angularly to a helicopter rotor; a brake caliper having friction members cooperating with the disk; and an actuating device for moving the brake caliper, parallel to the plane of the disk, between a work position engaging the disk and wherein the brake caliper may be operated to brake the rotor, and a safety position releasing the disk and wherein any possibility of the friction members interacting with the disk is prevented.

Abstract: A rotating mat for switching equipment, fitted with one or more holding flaps and elements capable of exerting a recalling force on the mat when the flaps are on the transmission rollers, wherein the elements which exert the recalling force are flexible elements attached to the mat's surface at the point of anchoring the flaps.

Abstract: Two different powders, one ceramic and the other of polymer particles, are fed separately into a jet of plasma of a conventional torch of a plasma spraying device by means of separate supply devices having respective powder injectors. The injection parameters of the two powders are established independently to achieve effective fusion of the ceramic particles and prevent complete combustion of the polymer particles. More specifically, the ceramic powder is injected along the axis of the jet of plasma, while the polymer powder is injected into a peripheral portion of the jet, at a predetermined distance from the jet axis, so that some of the polymer particles are incorporated in the ceramic coating deposited on a component for coating; and the polymer is subsequently removed by medium-temperature heat treatment to leave a porous ceramic coating with excellent thermal insulation properties.

Abstract: A releasable coupling for a power transmission line to a tail rotor of a foldable-tail-section helicopter, the coupling having a first and a second coupling assembly fitted respectively to the body and the tail of the helicopter, and which cooperate with each other when the tail is in the work position; the two coupling assemblies having respective transmission members in turn having respective radial toothings cooperating telescopically with each other, and respective conical male and female lead-in members which are brought into contact with each other prior to the respective toothings to guide connection of the transmission members; at least one of the transmission members being supported orientably.

Abstract: The monitoring method includes the steps of: acquiring a signal from an acceleration sensor; calculating a transform in the frequency domain of the signal to obtain a sequence of samples; acquiring a sample in the sequence of samples; calculating an actual amplitude value of the acquired sample; calculating a relative deviation between the actual amplitude value of the acquired sample and a reference amplitude value; and comparing the relative deviation with at least one predetermined threshold to immediately detect any irregularity in, and so prevent in-flight failure of, the helicopter transmission assembly.

Abstract: The monitoring method includes the steps of: acquiring a signal from an acceleration sensor associated with an epicyclic assembly; sampling the signal at a predetermined sampling frequency to obtain an initial sequence of samples; dividing the samples in the initial sequence into groups, each defined by a predetermined number of samples; acquiring predetermined groups of samples; filtering the acquired groups of samples to obtain an intermediate sequence of samples; processing the intermediate sequence of samples to obtain a final sequence of samples; calculating a sixth-order moment of the final sequence of samples; and comparing the sixth-order moment with at least one predetermined threshold to detect any vibrational irregularity in the epicyclic assembly of the helicopter.