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51. 发明公开

EP2645055A1 Method for evaluating the structural compatibility of an aircraft for use on rough runways 有权转让
标题翻译：用于评估使用不均匀的跑道的飞机的结构相容性方法
公开(公告)号：EP2645055A1
公开(公告)日：2013-10-02
申请号：EP13161497.6
申请日：2013-03-27
申请人： Alenia Aermacchi S.p.A.
发明人： Piccolo, Antonio , Mastroianni, Gaetana , Migliore, Sandro
IPC分类号： G01B21/30 , G08G5/00
CPC分类号： E01C9/00 , G01B21/30 , G08G5/00
摘要： A method for evaluating the structural compatibility of an aircraft (2) for use on a runway (5) having a profile with one or more roughnesses (7, 8) in the form of bumps and/or dips, comprising the steps of: generating (102) a first equivalent bump height curve (25) indicative of the elevation and/or depression of the one of more roughnesses of the runway with respect to a reference value; comparing (106) the first equivalent bump height curve with a second equivalent bump height curve indicative of elevation and/or depression limit values of reference roughnesses such that, when the aircraft encounters said reference roughnesses, it remains within the envelope of admissible loads; generating (103) a first power spectral density curve by means of spectral analysis of the profile of the runway; comparing (107) the first power spectral density curve with a second power spectral density curve (60) relating to a profile of a reference runway such that, when the aircraft runs along this reference runway, it remains within the envelope of admissible loads; verifying (108) if the first equivalent bump height curve (25) develops entirely within the first acceptability region and if the first power spectral density curve develops entirely within the second acceptability region; and authorizing or denying (112, 114, 116) the aircraft the use of the runway, on the basis of the result of said step of verifying (108).
摘要翻译：性评价（5）上具有一个或多个粗糙度的轮廓的跑道中使用的飞行器（2）的结构的相容性的方法（7,8）中凸块和/或凹陷，其包括以下步骤的形式：生成（102）的第一等效凸块高度的曲线（25）表示仰角和/或跑道的相对于参考值的粗糙度中的一个的凹陷; 比较（106）与指示仰角和/或寻求其的参考粗糙度抑郁极限值，当飞机遇到所述参考粗糙度的第二等效凸块高度曲线的第一等效凸块高度的曲线，但它仍然可容许的负载的包络线之内; 生成（103）由所述跑道的轮廓的频谱分析的装置的第一功率谱密度曲线; 比较（107）与第二功率谱密度曲线（60）的第一功率谱密度曲线与一个参考跑道检查的是，当飞机沿着该参考跑道运行时，它仍然是可容许的负载的包络内的一个简档; 验证（108），如果第一等效凸块高度的曲线（25）完全开发出的第一区域和可接受范围内，如果第一功率谱密度曲线的第二区域内的可接受完全开发出; 和授权或拒绝（112，114，116）的飞机上使用跑道的，验证（108）的所述步骤的结果的基础上。

52. 发明授权

EP2324369B1 TEST ARRANGEMENT FOR A LASER THREATS IDENTIFYING SYSTEM OF AN AIRCRAFT 有权转让
标题翻译：试验安排了一种用于识别飞行器激光威胁
公开(公告)号：EP2324369B1
公开(公告)日：2013-08-21
申请号：EP09749187.2
申请日：2009-09-08
申请人： Alenia Aermacchi S.p.A.
发明人： RUSSO, Francesco , BARLETTA, Alessandro
IPC分类号： F41H11/02 , G01S7/497 , G01S7/495
CPC分类号： G01S7/495 , F41H11/02 , G01S7/4818 , G01S7/497

53. 发明授权

EP2217430B1 APPARATUS FOR THE INFUSION OF RESIN INTO A PREFORM IN A CLOSED MOULD 有权转让
标题翻译：设备，用于空白以封闭形式树脂输注
公开(公告)号：EP2217430B1
公开(公告)日：2013-06-05
申请号：EP08847432.5
申请日：2008-10-29
申请人： Alenia Aermacchi S.p.A.
发明人： DE VITA, Vincenzo , BENEVENTI, Francesco , RAFFONE, Marco
IPC分类号： B29C70/44 , B29C70/48 , B29C70/54
CPC分类号： B29C70/548 , B29C67/0037 , B29C70/443 , B29C70/48 , B29C70/546 , B29L2031/005 , B29L2031/3082

54. 发明公开

EP2592000A1 Fuel tank for aircraft provided with a fuel heating system, and fuel heating system for aircraft fitted with such a tank 有权转让
标题翻译：用于与燃料加热系统和燃料加热系统用于飞行器飞机燃油箱具有这样的罐
公开(公告)号：EP2592000A1
公开(公告)日：2013-05-15
申请号：EP12191682.9
申请日：2012-11-07
申请人： Alenia Aermacchi S.p.A.
发明人： Moscatelli, Antonio , Paternoster, Massimiliano , Magaldi, Marco
IPC分类号： B64D13/06 , B64D37/34 , B64D37/06
CPC分类号： B64D37/34 , B64D13/06 , B64D37/06 , F28D15/0266 , Y02T50/56
摘要： The fuel tank (10) is made as a flexible multilayer tank, wherein a cavity (16) is provided between two adjacent layers (10a, 10b) of the tank (10) and defines a path that extends along a bottom wall of the tank (10) between an inlet opening (18) and an outlet opening (20) of the tank (10). The path defined by the cavity (16) is intended to be passed through by a hot fluid in order to transfer heat to the fuel contained in the tank (10). Advantageously used as hot fluid is a fluid in vapour phase made available by a two-phase fluid heat exchanger (30), said fluid in vapour phase being cooled through the cavity (16) and leaving the outlet opening (20) of the tank (10) as fluid in liquid phase.

55. 发明公开

EP2511082A2 Method for manufacturing products made of composite material with a closed-section sandwich structure 有权
标题翻译：一种用于制备的产品具有的夹层结构具有封闭部分由复合材料制成的过程
公开(公告)号：EP2511082A2
公开(公告)日：2012-10-17
申请号：EP12163763.1
申请日：2012-04-11
申请人： Alenia Aermacchi S.p.A.
发明人： Pitzolu, Ruggero
IPC分类号： B29C70/46 , B29C70/86
CPC分类号： B29C70/865 , B29C70/46
摘要： A matched mould curing apparatus (10) defining a moulding cavity is provided; two sets of layers (16, 26) of curable, fibre-reinforced, thermosetting composite material are laminated on the lower forming tool (11) and upper forming tool (12). Closed-cell foam core segments (15a-15d) are provided and placed adjacent to each other on the layers (16). The core segments are oversized with respect to the nominal size determined by the moulding cavity in the closed condition, minus the thickness of the layers (16, 26) of composite material. A controlled temperature is applied firstly so as to allow plastic deformation of the core segments (15a-15d), but without closing completely the matched mould. The temperature and pressure are then applied so as to cause complete closure of the matched mould (10, 11, 12) and curing of the laminated layers (16, 26).
摘要翻译：定义模腔的匹配模具固化装置（10）设置; 固化的，纤维增强的，热固性复合材料的两组层（16，26）被层叠在下部成形工具（11）和上部成形工具（12）。闭孔泡沫芯段（15A-15D）被提供，并放置在相邻的海誓山盟上的各层（16）。芯段是过大的相对于标称尺寸确定性由模腔在关闭状态开采，减去复合材料的层（16，26）的厚度。受控的温度被首先施加，从而允许芯段（15A-15D）的塑性变形，但没有完全关闭调用匹配模具。然后，将温度和压力被施加，以使匹配的模具（10，11，12）和固化叠层（16，26）的完全闭合。

56. 发明授权

EP2017077B1 Process for manufacturing a sound-absorbing panel for aircrafts 有权
标题翻译：一种生产用于飞行器吸音板的方法
公开(公告)号：EP2017077B1
公开(公告)日：2012-09-12
申请号：EP08157673.8
申请日：2008-06-05
申请人： Alenia Aermacchi S.p.A.
发明人： Midali, Alberto , Aliverti, Mauro , Roccati, Mauro , Ferrante, Pier Giorgio
IPC分类号： B32B38/04 , B32B3/12 , B32B37/14 , F02C7/045
CPC分类号： B32B37/146 , B32B2038/047 , B32B2307/102 , B32B2605/18 , F02C7/045 , Y02T50/672

57. 发明授权

EP1962442B1 A method and system for the remote control of aircraft 有权转让
标题翻译：方法和系统，用于飞机的遥控
公开(公告)号：EP1962442B1
公开(公告)日：2012-07-11
申请号：EP08150946.5
申请日：2008-02-01
申请人： Alenia Aermacchi S.p.A.
发明人： Spensatellu, Tonino
IPC分类号： H04B7/185
CPC分类号： H04B7/18506 , H04L1/08 , H04L12/40176 , H04L2012/4028

58. 发明公开

EP2404745A1 Method for making hollow stiffening elements 有权
标题翻译： Verfahren zur Herstellung von hohlen Versteifungselementen
公开(公告)号：EP2404745A1
公开(公告)日：2012-01-11
申请号：EP11172788.9
申请日：2011-07-06
申请人： Alenia Aermacchi S.p.A.
发明人： Midali, Alberto , Bottero, Luca , Duccini, Gianni , Gregori, Massimo
IPC分类号： B29D99/00 , B29C70/50 , B29C33/56 , B29C33/68 , B29C61/02
CPC分类号： B29C33/68 , B29C33/56 , B29C61/02 , B29C63/42 , B29C70/504 , B29D99/0014
摘要： Method for making hollow stiffening elements with co-curing technique on a structure made of composite material 1 comprising the use of at least a lamination and polymerization spindle 2 upon which it is positioned at least a rolled section 3. This rolled section 3 forms at least a hollow structure 11 where there is the spindle 2, comprising the following operational phases: coating the spindle 2 with at least a first anti-adherent layer 41; coating the spindle 2 with at least a second heat-shrinking layer 42; heating the coated spindle 2; positioning the spindle 2 on the surface of the structure 1; laminating the surface 1 through at least a rolled section 3; heating the structure 1 with at least a positioned rolled section 3; extracting the spindle 2 from the hollow structure 11.
摘要翻译：在由复合材料1制成的结构上制造具有共固化技术的中空加强元件的方法，包括至少使用至少层压和聚合主轴2，至少位于轧制部分3上。该轧制部分3至少形成具有主轴2的中空结构11，包括以下操作阶段：用至少第一抗粘附层41涂覆主轴2; 用至少第二热收缩层42涂覆主轴2; 加热涂层心轴2; 将心轴2定位在结构1的表面上; 通过至少轧制部分3层压表面1; 用至少定位的轧制部分3加热结构1; 从中空结构11取出主轴2。

59. 发明公开

EP2291310A2 COUPLING FOR INDUCING HIGH TEMPERATURE DROPS BETWEEN CONNECTED PARTS ON AN AIRCRAFT 有权
标题翻译：离合器GENERATING相关零件的强温废物在一个平面上
公开(公告)号：EP2291310A2
公开(公告)日：2011-03-09
申请号：EP09746129.7
申请日：2009-05-01
申请人： Alenia Aermacchi S.p.A.
发明人： PREMAZZI, Marco , GARUCIO, Federico
IPC分类号： B64C1/38 , B64C1/40 , B64D29/00 , B64D33/02 , B64D15/02 , B64D15/12
CPC分类号： B64C1/38 , B64C1/40 , B64D15/02 , B64D15/12 , B64D29/00 , B64D33/02 , B64D2033/0233 , B64D2033/0273 , B64D2033/0286 , Y10T16/52 , Y10T16/555
摘要： Coupling for inducing high temperature drops on parts of an aircraft comprising an edge portion (2) subjected to high temperature and a bearing structure (3) having limited capacity to resist against high temperatures. Such coupling comprises at least one hinge (4) having low heat conductivity.

60. 发明公开

EP3068926A1 METHOD FOR MANUFACTURING AN AIRCRAFT COMPONENT EQUIPPED WITH A PROTECTION AGAINST ABRASION AND HEAT, AND AIRCRAFT COMPONENT MANUFACTURED THROUGH SAID METHOD 审中-公开
标题翻译：方法用于生产具有保护，禁止磨损和发热AN航空器部件，并根据该方法生产的飞机部件
公开(公告)号：EP3068926A1
公开(公告)日：2016-09-21
申请号：EP14806446.2
申请日：2014-11-10
申请人： Alenia Aermacchi S.p.A.
发明人： BOTTERO, Luca , GREGORI, Massimo
IPC分类号： C25D5/54
CPC分类号： C25D5/54 , B64C1/38 , B64C3/36 , B64C2001/0072 , B64C2001/0081 , C25D3/12 , C25D3/562 , C25D7/00 , C25D21/12
摘要： A method includes providing an aircraft component including a substrate made of composite material and a polymeric matrix; and applying a protective coating made of metallic material to the substrate. The protective coating is applied to the polymeric matrix by an electrolytic deposition process.

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