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公开(公告)号：US20190193850A1
公开(公告)日：2019-06-27
申请号：US16328069
申请日：2017-09-07
Applicant: LEONARDO S.P.A.
Inventor： Luigi Maria Bottasso
CPC classification number: B64C27/463 , B64C27/04 , B64C27/59 , B64C27/72 , B64C2027/7211
Abstract: A rotor for a hover-capable aircraft is described that comprises: a hub rotatable about a first axis and at least two blades hinged to the hub; each blade comprises a main portion hinged to the hub and a tip portion, which is arranged radially outermost with respect to first axis with respect to the corresponding main portion; the tip portion of each blade is movable with respect to the corresponding main portion of that blade; the tip portion of each blade is selectively movable with respect to the corresponding main portion of that blade between a first position, in which it defines a dihedral or anhedral angle with respect to the corresponding main portion; and a second position, in which it defines a positive or negative sweep angle with respect to the corresponding main portion.
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32.发明申请公开(公告)号：US20190135444A1
公开(公告)日：2019-05-09
申请号：US16180132
申请日：2018-11-05
Applicant: LEONARDO S.P.A.
Inventor： Antonio BRELATI , Girolamo BRELATI , Rosario DEL GIUDICE , Tommaso ROMANO
Abstract: A damage recovery system of a fuselage of an aircraft, comprising: a tank containing a polyurethane foam; a main duct fluidically coupled to the tank to receive the foam; secondary ducts fluidically coupled to the main duct; and distribution means adapted to allow an outflow of the foam from the secondary ducts. Graphene powder can be mixed and added to the polyurethane foam. In flight, a possible leak (crack or hole) in the fuselage is plugged by the polyurethane foam with graphene powder.
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公开(公告)号：US20190092448A1
公开(公告)日：2019-03-28
申请号：US16086579
申请日：2017-03-17
Applicant: LEONARDO S.P.A.
Inventor： Aurelio Calcedonio BOSCARINO , Alberto BECCARO , Pierclaudio IAIA , Nicola Italo CATINO , Diego CURLETTO , Davide DE SIMONE , Luciana LO VERDE , Paolo DI STEFANO , Silva REGIS , Riccardo BARGETTO
Abstract: An aerial vehicle includes a fuselage situated at the center and a main wing body having a pair of half-wings extending on transversely opposite sides of the fuselage. Each half-wing includes an orientable horizontal surface or plane, which acts as an aerodynamic control, and a fixed winglet.
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公开(公告)号：US20180372439A1
公开(公告)日：2018-12-27
申请号：US15775495
申请日：2016-11-08
Applicant: LEONARDO S.P.A.
Inventor： Mauro PELLEGRI
Abstract: A turret includes a firearm, which is configured to shoot munitions. A support assembly supports the firearm and is configured to move the firearm about an azimuthal rotation or swiveling axis (Y) and about a zenithal rotation or elevation axis (X). A munition guidance device mounts on the support assembly and is configured to direct a precision-guided munition, which is shot by the firearm towards a target. A protection apparatus is mounted on the support assembly and is configured to assume: a covering condition, in which the protection apparatus hides the munition guidance device on the inside of the support assembly; and an opening condition, in which the protection apparatus exposes the munition guidance device on the outside of the support assembly.
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公开(公告)号：US20180164066A1
公开(公告)日：2018-06-14
申请号：US15577665
申请日：2016-05-27
Applicant: LEONARDO S.P.A.
Inventor： Gian Battista LEONESIO , Paoloandrea CASTELLETTI , Gianmario GREGORINI
Abstract: A firearm support system is adapted to be installed in a vehicle, in particular an aircraft. The vehicle includes a compartment to accommodate the crew. The compartment has: a bearing surface, an upper structure rising above the bearing surface, and an opening, through which a firearm shoots. The support system includes: an anchoring portion, for being fixed to the upper structure and located in the compartment; a mobile support, which is coupled to the anchoring portion in a mobile manner, is adapted for receiving the firearm, and allows the firearm to move between an operating position, in which the firearm is ready to shoot through the opening, and a non-operating position, in which the firearm is retracted.
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Patent Agency Ranking
公开(公告)号：US20170324156A1
公开(公告)日：2017-11-09
申请号：US15524490
申请日：2014-11-06
Applicant: LEONARDO S.p.A.
Inventor： Stefano Pacetti , Leopoldo Infante , Mario Teglia , Emanuele Tiribelli , Flavio Troiani
IPC: H01Q1/40 , C09D199/00 , C09D123/26
CPC classification number: H01Q1/40 , C09D123/00 , C09D123/26 , C09D199/00 , H01Q9/16
Abstract: Disclosed herein is a method for applying a conformal coating to one or more radio frequency elements of an antenna or antenna array. Said method is characterized in that the conformal coating is based on a thermoplastic material produced from a mixture comprising a thermoplastic polymer and an olive pomace.
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公开(公告)号：US20170198814A1
公开(公告)日：2017-07-13
申请号：US15326408
申请日：2015-07-17
Applicant: LEONARDO S.p.A.
Inventor： Dario Colombo , Giuseppe Gasparini , Paolo Pisani
IPC: F16J15/34
CPC classification number: F16J15/3412
Abstract: A sealing ring for a seal assembly is described that comprises: a main body rotating about an axis; and a first surface, which is defined by the main body, extends transversely to the axis and is suitable for abutting against a further sealing ring in a direction parallel to the axis; the first surface comprises a plurality of grooves forming respective hydropads; the grooves are delimited by a first edge and a second edge facing one another; the first edge and the second edge delimit the grooves in a circumferential direction to said axis; at least one of the first edge and the second edge is shaped like an elliptical arc, which has coincident or separate foci;comprises first grooves and second grooves alternating with one another in a circumferential direction to said axis and staggered from each other in a radial direction to said axis.
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公开(公告)号：US20170137120A1
公开(公告)日：2017-05-18
申请号：US15323653
申请日：2015-07-03
Applicant: LEONARDO S.p.A.
CPC classification number: B64C27/001 , B64C27/12 , B64C27/82 , B64C2027/002
Abstract: A helicopter is described that comprises: a rotor; a fuselage; a drive transmission unit operatively connected to the rotor; a support body, which supports the transmission unit; and constraining means interposed between the support body and the fuselage; the constraining means in turn comprise a crosspiece connected in a fixed manner with respect to the support body and having a first lying plane; the crosspiece is formed in part by a metallic material and in part by a visco-elastic material.
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公开(公告)号：US20250083825A1
公开(公告)日：2025-03-13
申请号：US18568374
申请日：2022-05-24
Applicant: LEONARDO S.P.A.
Inventor： Riccardo Bianco Mengotti
Abstract: A series of convertible aircrafts with a core with an airframe defining a first axis is described; a first, a second, a third, a fourth, a fifth and a sixth rotor which are rotatable about respective first, second, third, fourth, fifth and sixth axis, and operable independently of each other so as to generate respectively a first, a second, a third, a fourth, a fifth and a sixth thrust value independent of each other; the core comprises an electric power source and electric motors which are connected to said first, second, third, fourth, fifth and sixth rotor; each aircraft of the series comprises a module associated with a respective architecture and interfaced with said core.
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40.发明授权公开(公告)号：US12134468B2
公开(公告)日：2024-11-05
申请号：US17789325
申请日：2020-12-24
Applicant: LEONARDO S.P.A.
Inventor： Paolo Pisani , Federico Montagna , Roberto Regonini , Daniele Podda
Abstract: An aircraft is described comprising a transmission unit with a first module and a lubrication system; the first module comprises a casing and a movable member; the lubrication system comprises a header, a nozzle fed with the lubricating fluid and designed to feed the lubricating fluid inside the casing of the first module, a collection tank for the lubricating fluid injected by the nozzle, and recirculation means designed to cause the recirculation of the lubricating fluid from the collection tank to the feed header; the first module comprises a valve available in a first configuration, in which it enables the outflow of said lubricating fluid from said module to the recirculation means when the pressure of the lubricating fluid inside the header is greater than a threshold value; and in a second configuration, in which it fluidically isolates the module from the recirculation means when the pressure of the lubricating fluid inside the header is less than the threshold value.
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