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61.发明申请公开(公告)号：US20220388779A1
公开(公告)日：2022-12-08
申请号：US17774262
申请日：2020-11-06
Applicant: LEONARDO S.P.A.
Inventor： Andrea BRIANO , Simone CASTAGNO , Giacomo CONTI , Andrea PARODI
Abstract: Closure system for connecting two contiguous transport units in a convoy for the transport of goods, the closure system comprising an accordion-shaped element configured to change the length thereof along a longitudinal axis of the convoy and comprising a central portion and a pair of outer portions placed on opposite sides with respect to said axis, the thickness of the accordion-shaped element decreasing from the central portion to the outer portions.
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公开(公告)号：US11498667B2
公开(公告)日：2022-11-15
申请号：US16754270
申请日：2018-10-30
Applicant: LEONARDO S.P.A.
Inventor： Giuseppe Quaranta , Federico Savorgnan , Pierangelo Masarati , Luigi Bottasso , Attilio Colombo
IPC: B64C27/00
Abstract: A rotor for a hover-capable aircraft is described, comprising: a hub rotatable about an axis and, in turn, comprising a plurality of blades; a mast connectable to a drive member of the aircraft and operatively connected to the hub to drive the hub in rotation about the axis; and damping means for damping vibrations transmitted to the mast, which comprise a mass designed to oscillate in a plane transversal to the axis so as to contain flexural vibrations of the mast generated by rotation of the blades; the damping means also comprise elastic means having a desired stiffness along the axis and operatively connected to the mass to contain vibration of the mast along the axis.
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63.发明申请公开(公告)号：US20220343787A1
公开(公告)日：2022-10-27
申请号：US17761062
申请日：2020-09-18
Applicant: LEONARDO S.P.A.
Inventor： Roberto CICCARELLI , Emanuele ROVEA , Francesco OLLOSU , Paolo RIGATO
IPC: G09B9/24
Abstract: A system for evaluating an operator in a training mission on a training element, including a first processing unit configured to receive and process first data to generate converted data according to an operating frequency; a second processing unit configured to receive and process the converted data and mission support data according to the operating frequency to generate second data; and a third processing unit configured to receive and compare the converted data with the second data according to the operating frequency such to generate, based on said comparison, response data. Response data comprise visualisation data and the evaluation system further includes a graphic process unit configured to receive visualisation data and generate a map of the operating environment wherein the training element operates.
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公开(公告)号：US20220250741A1
公开(公告)日：2022-08-11
申请号：US17627445
申请日：2020-06-25
Applicant: LEONARDO S.P.A.
Inventor： Luigi Bottasso , Ermanno Fosco , Paolo Pisani , Francesco Vincenzo , Francesco Rosa , Francesco Braghin , Gabriele Cazzulani , Simone Cinquemani
IPC: B64C27/00
Abstract: A rotor for an aircraft is described that has a mast, an attenuating device to attenuate the transmission of vibrations from the mast in a plane orthogonal to the first axis; and a transmission device interposed between the mast and the attenuating device; the attenuating device comprises a first and a second mass unit with a first and a second mass rotatable about the first axis with a first and a second rotational speed, two control units operable to cause an additional rotation of at least one of the first and second masses and a first and a second support assembly carrying the first and second masses; each control unit controls the angle between the first and second masses and each control unit comprises: a belt coupled to the support assembly and a drive unit coupled to the first belt, to cause the rotation of the first support assembly with respect to said transmission device.
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65.发明申请公开(公告)号：US20220177152A1
公开(公告)日：2022-06-09
申请号：US17598534
申请日：2020-03-27
Applicant: LEONARDO S.p.A.
Inventor： Marco VERCELLESI
Abstract: A method for manufacturing a sound-absorbing panel with a sandwich structure for reducing noise impact of an aeronautic engine includes providing a first skin of a thermoplastic polymeric material, making a plurality of micro-holes through the first skin by mechanical punching of the first skin, securing the first skin to a central layer by arranging a structural adhesive layer between the first skin and the central layer and/or by a thermal weld between the first skin and the central layer, and securing the central layer to a second skin by arranging a structural adhesive layer between the central layer and the second skin and/or by a thermal weld between the central layer and the second skin.
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Patent Agency Ranking
公开(公告)号：US20220146225A1
公开(公告)日：2022-05-12
申请号：US17433556
申请日：2020-02-24
Applicant: LEONARDO S.P.A.
Inventor： Giordano BENEDINI , Valter BENZONI , Tiziano BETTELLI , Stefano CONTI , Mattia FORCINA , Enrico SARIOLI
Abstract: A breech block assembly for a firearm includes a guiding element having a slide adapted to slide along a guide in an actuation system of the breechblock assembly driven by a motor. A shutting element shuts an opening in a breech ring of the firearm. A percussion pin is pushed by an elastic element slide along a longitudinal axis, as a function of the firing cycle of the firearm to an axial hole in the shutting element. The percussion pin is shaped to partially come out of the axial hole of the shutting element for firing a piece of ammunition. The breechblock assembly comprises a control system for controlling the percussion pin. The control system controls the operability and the movement of the percussion pin independently of a firing cycle of the firearm.
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公开(公告)号：US11329353B2
公开(公告)日：2022-05-10
申请号：US16818307
申请日：2020-03-13
Applicant: LEONARDO S.p.A.
Inventor： Yuri Gassani
Abstract: An electrochemical-type power supply source for use in marine environment, is provided with: an electrochemical stack, which generates electric power in the presence, internally, of an electrolytic fluid; a first tank, designed to contain electrolytic fluid at a first temperature; a second tank, designed to contain electrolytic fluid at a second temperature, lower than the first temperature; a thermostatic valve, that mixes electrolytic fluid at a lower temperature with electrolytic fluid at a higher temperature, for generating a mixed electrolytic fluid to be introduced into the electrochemical stack at a controlled temperature for generating a desired electric power. The electrochemical power supply is further provided with an auxiliary tank, adapted to contain electrolytic fluid at a third temperature, higher than the first temperature; and the thermostatic valve is connected to the auxiliary tank and receives, at an input, the electrolytic fluid at the third temperature.
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公开(公告)号：US20220106031A1
公开(公告)日：2022-04-07
申请号：US17312286
申请日：2019-10-31
Applicant: LEONARDO S.P.A.
Inventor： Pierre Abdel Nour , Matteo Pecoraro
Abstract: An aircraft is described that comprises: a fuselage with a first axis of longitudinal extension; and a tail portion arranged at a tail end of the fuselage; the tail portion comprises two surfaces arranged in a V-shape, inclined to each other and symmetrical with respect to the first axis; each surface comprises an associated winglet arranged transversely with respect to the surface and fixed with respect to the surface.
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公开(公告)号：US20220073201A1
公开(公告)日：2022-03-10
申请号：US17414499
申请日：2019-11-28
Applicant: LEONARDO S.P.A.
Inventor： Daniele Podda , Andrea Gabrielli , Roberto Regonini , Federico Montagna , Stefano Poggi
Abstract: An aircraft is described comprising: a support element; a shaft rotating about an axis; a pair of oblique rolling bearings mounted so as to couple the shaft to the support element (rotatingly about the axis; the rolling bearings comprising: respective first races cooperating radially in contact with a first component (defined by one from the support element and the shaft; respective second races cooperating radially in contact with a second component (defined by the other from the support element and the shaft; and respective pluralities of rolling elements adapted to roll on the first and second races; the aircraft further comprises a pair of preloaded elastic members, which couple the first races to the first component respectively, axially and in an elastically yielding manner.
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公开(公告)号：US20220024572A1
公开(公告)日：2022-01-27
申请号：US17312301
申请日：2019-10-31
Applicant: LEONARDO S.P.A.
Inventor： Roberto Vanni , Andrea Antoni
Abstract: A vertical take-off and/or landing aircraft comprising: a fuselage having a longitudinal axis; a pair of semi-wings protruding from the fuselage in a transversal direction with respect to the longitudinal axis; a pair of a predetermined breaking areas of the semi-wings defining respective preferred rupture sections at which the respective semi-wings are designed to break, during operation, in a controlled way moving along a preferred collapse trajectory in the event of impact; and at least one fluidic line configured to convey at least one service fluid from and/or towards at least one said semi-wing and crossing at least one of said preferred rupture sections; the aircraft comprises a self-sealing coupling movable between a first configuration in which it enables the flow of said service fluid from and/or towards the semi-wing, and a second configuration in which it prevents the above-mentioned flow and the spilling of the service fluid from the fluidic line; the self-sealing coupling is movable from the first to the second configuration via the movement of the semi-wing along the preferred collapse trajectory.
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