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公开(公告)号：US20160340025A1
公开(公告)日：2016-11-24
申请号：US14717666
申请日：2015-05-20
Applicant: MECAER AVIATION GROUP S.p.A.
Inventor： Andrea TENDOLA , Vittorio LIGNAROLO
CPC classification number: B64C13/28 , B64C13/503 , B64F5/00
Abstract: An aircraft hybrid flight control system comprising a manual control element, a mechanical transmission interposed between the manual control element and a control surface, an electromechanical actuator and a coupling unit configured to connect selectively the control surface to the mechanical transmission in a manual control mode and to the electromechanical actuator in a fly-by-wire control mode; the coupling unit is configured to maintain the mechanical transmission in a condition of substantial continuity with said control surface even in fly-by-wire mode, but for a freedom of relative motion of pre-set amplitude.
Abstract translation: 一种飞行器混合飞行控制系统，包括手动控制元件，插入在手动控制元件和控制表面之间的机械传动装置，机电致动器和耦合单元，其被配置为以手动控制模式选择性地将控制表面连接到机械传动装置， 以逐线控制方式连接到机电致动器; 联接单元被配置为即使在线控模式下仍然保持机械传动处于与所述控制表面相当连续的状态，而是为了预设幅度的相对运动的自由度。
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公开(公告)号：US12151828B2
公开(公告)日：2024-11-26
申请号：US18273232
申请日：2022-01-21
Applicant: MECAER AVIATION GROUP S.P.A.
Inventor： Francesco Lovo , Giorgio Santero , Sergio Spezzacatena
Abstract: A door for an aircraft is configured to be selectively closed on a frame. The door includes a safety system for an anchoring element. The safety system includes a source of light radiations and a receptor of said radiations, the source being integral with the door and the receptor being integral with the anchoring element. The receptor is optically connected to signalling apparatus that signals the positioning of the anchoring element in the second operating condition when the receptor receives the light radiation from the source.
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Patent Agency Ranking
公开(公告)号：US10011087B2
公开(公告)日：2018-07-03
申请号：US15212245
申请日：2016-07-17
Applicant: MECAER AVIATION GROUP S.p.A.
Inventor： Vincenzo Massarelli , Valentina Canala
IPC: B32B3/12 , B32B3/18 , B32B7/12 , B64C1/40 , G10K11/168 , G10K11/172 , B32B5/18 , B32B27/06 , B32B37/06 , B32B37/08 , B32B37/14 , B64C1/06 , B32B5/02 , B32B27/08 , B32B27/12 , B32B27/34 , B32B27/38 , B32B3/10 , B32B7/04 , B64C1/00
CPC classification number: B32B3/12 , B32B5/02 , B32B5/18 , B32B7/12 , B32B27/06 , B32B27/065 , B32B27/08 , B32B27/12 , B32B27/34 , B32B27/38 , B32B37/06 , B32B37/08 , B32B37/142 , B32B2260/021 , B32B2260/046 , B32B2262/106 , B32B2266/0207 , B32B2307/102 , B32B2307/3065 , B32B2307/546 , B32B2307/718 , B32B2307/72 , B32B2307/732 , B32B2605/003 , B32B2605/18 , B64C1/066 , B64C1/40 , G10K11/168 , G10K11/172
Abstract: Panel for soundproofing aircraft interiors comprising a first and a second layer and an intermediate layer of damping material placed between the first and second layer along a neutral axis of the soundproofing panel. The first and the second layer each comprising a structural layer and a surface layer placed on the opposite side to the intermediate layer and connected thereto, adhering continuously by means of an adhesive layer, the intermediate layer extends for the entire area of the panel and is connected to the structural layers of the first and second layer. The intermediate layer comprises a polymer foam material having a uniform thickness less than 2 mm and weight of less than 1.2 kg/m2.
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公开(公告)号：US20170015081A1
公开(公告)日：2017-01-19
申请号：US15212245
申请日：2016-07-17
Applicant: MECAER AVIATION GROUP S.p.A.
Inventor： VINCENZO MASSARELLI , VALENTINA CANALA
IPC: B32B3/12 , B32B7/12 , B32B37/14 , B64C1/40 , B32B37/08 , B32B27/06 , B64C1/06 , B32B5/18 , B32B37/06
CPC classification number: B32B3/12 , B32B5/02 , B32B5/18 , B32B7/12 , B32B27/06 , B32B27/065 , B32B27/08 , B32B27/12 , B32B27/34 , B32B27/38 , B32B37/06 , B32B37/08 , B32B37/142 , B32B2260/021 , B32B2260/046 , B32B2262/106 , B32B2266/0207 , B32B2307/102 , B32B2307/3065 , B32B2307/546 , B32B2307/718 , B32B2307/72 , B32B2307/732 , B32B2605/003 , B32B2605/18 , B64C1/066 , B64C1/40 , G10K11/168 , G10K11/172
Abstract: Panel for soundproofing aircraft interiors comprising a first and a second layer and an intermediate layer of damping material placed between the first and second layer along a neutral axis of the soundproofing panel. The first and the second layer each comprising a structural layer and a surface layer placed on the opposite side to the intermediate layer and connected thereto, adhering continuously by means of an adhesive layer, the intermediate layer extends for the entire area of the panel and is connected to the structural layers of the first and second layer. The intermediate layer comprises a polymer foam material having a uniform thickness less than 2 mm and weight of less than 1.2 kg/m2.
Abstract translation: 用于隔离飞机内部的面板包括沿着隔音板的中性轴线放置在第一和第二层之间的第一层和第二层以及阻尼材料的中间层。 第一层和第二层各自包括结构层和位于与中间层相反的一侧并与之连接的表面层，其通过粘合剂层连续粘合，中间层延伸面板的整个区域，并且是 连接到第一和第二层的结构层。 中间层包括均匀厚度小于2mm且重量小于1.2kg / m 2的聚合物泡沫材料。
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公开(公告)号：US20240109669A1
公开(公告)日：2024-04-04
申请号：US18273232
申请日：2022-01-21
Applicant: MECAER AVIATION GROUP S.P.A.
Inventor： Francesco Lovo , Giorgio Santero , Sergio Spezzacatena
CPC classification number: B64D45/00 , B64C1/1407 , E05B17/10 , E05C9/063
Abstract: A door for an aircraft configured to be selectively closed on a frame, the door comprising a safety system for an anchoring element, the safety system comprising a source of light radiations and a receptor of said radiations, the source being integral with the door and the receptor being integral with the anchoring element, said receptor being optically connected to signalling means, signalling the positioning of the anchoring element in the second operating condition when the receptor receives the light radiation from the source.
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公开(公告)号：US20200223524A1
公开(公告)日：2020-07-16
申请号：US16647206
申请日：2018-09-14
Applicant: MECAER AVIATION GROUP S.P.A.
Inventor： Vincenzo MASSARELLI
Abstract: Aircraft comprising a fuselage, which in turn comprises an outer wall insulating from the outside an inner volume of the aircraft and an inner wall with respect to the outer wall defining a first volume pressurized at a first pressure level, the inner wall and the outer wall being separated from each other by a second volume and being connected by connection means housed in the second volume, this latter being pressurized to a second pressure level, which is at least one order of magnitude lower than the first level.
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公开(公告)号：US10000275B2
公开(公告)日：2018-06-19
申请号：US14717666
申请日：2015-05-20
Applicant: MECAER AVIATION GROUP S.p.A.
Inventor： Andrea Tendola , Vittorio Lignarolo
CPC classification number: B64C13/30 , B64C13/341 , B64F5/00
Abstract: An aircraft hybrid flight control system comprising a manual control element, a mechanical transmission interposed between the manual control element and a control surface, an electromechanical actuator and a coupling unit configured to connect selectively the control surface to the mechanical transmission in a manual control mode and to the electromechanical actuator in a fly-by-wire control mode; the coupling unit is configured to maintain the mechanical transmission in a condition of substantial continuity with said control surface even in fly-by-wire mode, but for a freedom of relative motion of pre-set amplitude.
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