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1. 发明公开

EP2340994A1 Helicopter control stick support assembly 有权转让
标题翻译： BefestigungsvorrichtungfüreinenHubschraubersteuerknüppel
公开(公告)号：EP2340994A1
公开(公告)日：2011-07-06
申请号：EP09425543.7
申请日：2009-12-30
申请人： Agusta S.p.A.
发明人： Bandera, Gian Luigi
IPC分类号： B64C13/06
CPC分类号： B64C13/06
摘要： A support assembly (4) for helicopter control sticks (5) has a supporting structure (6); an instrument panel (20) fixed to the supporting structure (6); and a connecting device (30) for connecting the sticks (5) to the supporting structure (6). The connecting device (30) has a longitudinally elongated arm (31) fitted on one end (33) with the sticks (5); and the arm (31) slides to move the sticks to/from the supporting structure (6), and rotates about a horizontal axis (10) to adjust the height of the sticks (5).
摘要翻译：用于直升机控制棒（5）的支撑组件（4）具有支撑结构（6）; 固定到所述支撑结构（6）上的仪表板（20）; 以及用于将棒（5）连接到支撑结构（6）的连接装置（30）。连接装置（30）具有与杆（5）一体地装配在一端（33）上的纵向细长臂（31）。并且所述臂（31）滑动以使所述棒与所述支撑结构（6）移动，并且围绕水平轴线（10）旋转以调节所述棒（5）的高度。

2. 发明公开

EP2223854A1 Helicopter rotor 有权转让
标题翻译： Hubschrauberrotor
公开(公告)号：EP2223854A1
公开(公告)日：2010-09-01
申请号：EP09425077.6
申请日：2009-02-25
申请人： Agusta S.p.A.
发明人： Nannoni, Fabio , Ballerio, Dante , Abdel Nour, Pierre , Colombo, Attilio
IPC分类号： B64C27/35 , B64C27/51
CPC分类号： B64C27/32 , B64C27/35 , B64C27/51 , B64C27/635
摘要： A rotor (3, 3') for a helicopter (1), having a drive shaft (10) rotating about a first axis (A); a hub (11) angularly integral with the drive shaft (10) about the first axis (A); and at least two blades (12) projecting from the hub (11) on opposite sides of the first axis (A) and elongated along respective second axes (B) crosswise to the first axis (A); each blade (12) is movable with respect to the hub (11) and to the other blade (12) about a respective third axis (C) crosswise to the respective second axis (B); the rotor (3, 3') has at least two dampers (40) for damping oscillation of respective blades (12) about the respective third axes (C), and which have respective first portions (41) movable integrally with the respective blades (12) about the respective third axes (C); and the dampers (40) have respective second portions (42; 46a, 46b) connected elastically to the respective first portions (41) and functionally to each other.
摘要翻译：一种用于直升机（1）的转子（3,3'），具有围绕第一轴线（A）旋转的驱动轴（10）; 围绕第一轴线（A）与驱动轴（10）成一体的轮毂（11）; 以及至少两个叶片（12），其从所述轮毂（11）在所述第一轴线（A）的相对侧上突出并沿着与所述第一轴线（A）交叉的相应的第二轴线（B）延伸; 每个叶片（12）可相对于轮毂（11）和与另一个叶片（12）相对于与相应的第二轴线（B）交叉的相应的第三轴线（C）移动; 转子（3,3'）具有至少两个阻尼器（40），用于阻止相应的叶片（12）围绕相应的第三轴线（C）的振动，并且具有相应的第一部分（41）可与各个叶片 12）关于相应的第三轴线（C）; 并且所述阻尼器（40）具有彼此弹性地连接到相应的第一部分（41）并且在功能上彼此连接的相应的第二部分（42; 46a，46b）。

3. 发明公开

EP2133266A8 Aircraft wing 有权转让
标题翻译：飞机机翼
公开(公告)号：EP2133266A8
公开(公告)日：2010-05-19
申请号：EP09162227.4
申请日：2009-06-09
申请人： Agusta S.p.A.
发明人： Pancotti, Santino , Ballerio, Dante
IPC分类号： B64C27/04 , B64D7/02
CPC分类号： F41A9/34 , B64C27/04 , B64C2025/325 , B64D7/04 , F41A9/79
摘要： A wing (4) for an aircraft (1) having at least one weapon (8), and a feed duct (13) for feeding the weapon (8) with ammunition (9) supplied in the form of a belt (10); the wing (4) has a compartment (20) for housing a portion (54) of the belt (10) and connectable to a loading opening (14) of the feed duct (13).

4. 发明公开

EP2133266A2 Aircraft wing 有权转让
标题翻译： Flugzeug
公开(公告)号：EP2133266A2
公开(公告)日：2009-12-16
申请号：EP09162227.4
申请日：2009-06-09
申请人： Agusta S.p.A.
发明人： Pancotti, Santino , Ballerio, Dante
IPC分类号： B64C27/04 , B64D7/02
CPC分类号： F41A9/34 , B64C27/04 , B64C2025/325 , B64D7/04 , F41A9/79
摘要： A wing (4) for an aircraft (1) having at least one weapon (8), and a feed duct (13) for feeding the weapon (8) with ammunition (9) supplied in the form of a belt (10); the wing (4) has a compartment (20) for housing a portion (54) of the belt (10) and connectable to a loading opening (14) of the feed duct (13).
摘要翻译：用于具有至少一个武器（8）的飞机（1）的翼（4）和用于以武器（8）形式供给武器（8）的进给管（13），所述弹药（9）以皮带（10）的形式提供; 机翼（4）具有用于容纳皮带（10）的一部分（54）并且可连接到进给管道（13）的装载开口（14）的隔间（20）。

5. 发明公开

EP2133265A1 Helicopter 有权转让
标题翻译： Hubschrauber
公开(公告)号：EP2133265A1
公开(公告)日：2009-12-16
申请号：EP08425408.5
申请日：2008-06-10
申请人： Agusta S.p.A.
发明人： Nannoni, Fabio , Ballerio, Dante , Scandroglio, Alessadro
IPC分类号： B64C27/04 , B64D33/02 , B64D33/08
CPC分类号： B64D33/08 , B64C27/04 , B64C2025/325 , B64D7/08 , B64D33/02
摘要： A helicopter (1) having a drive (6) in turn having an air intake conduit (12); a main rotor (3) connected functionally to the drive (6); and a transmission (9) interposed functionally between the main rotor (3) and the drive (6) and housed in a housing (23). The helicopter (1) has at least one air intake (20) in turn having : a first inlet (21) connected fluidically to the intake conduit (12); at least one second inlet (22) connected fluidically to the housing (23); and deflecting means (30) interacting, in use, with an airflow (F) to divide the airflow (F) into a first and a second airflow. The air intake (20) also has guide means (31, 32, 37, 53) for guiding the first airflow along a first path (P) extending from the deflecting means (30) to the first inlet (21), and for guiding the second airflow along a second path (Q) separate from the first path (P) and extending from the deflecting means (30) to the second inlet (22).
摘要翻译：具有驱动器（6）的直升机（1）又具有进气管道（12）; 与所述驱动器（6）功能连接的主转子（3）; 以及功能上介于主转子（3）和驱动器（6）之间并容纳在壳体（23）中的变速器（9）。直升机（1）具有至少一个进气口（20），其具有：与进气管道（12）流体连接的第一入口（21）; 至少一个与所述壳体（23）流体连接的第二入口（22）; 和偏转装置（30）在使用中与气流（F）相互作用以将气流（F）分成第一和第二气流。进气口（20）还具有引导装置（31,32,37,53），用于沿着从偏转装置（30）延伸到第一入口（21）的第一路径（P）引导第一气流，并且用于引导沿第二路径（Q）的第二气流与第一路径（P）分离并且从偏转装置（30）延伸到第二入口（22）。

6. 发明授权

EP1628877B1 CRASHWORTHINESS STRUCTURE AND METHOD 失效转让
标题翻译：施工和方法耐撞
公开(公告)号：EP1628877B1
公开(公告)日：2009-09-02
申请号：EP04739418.4
申请日：2004-05-26
申请人： Politecnico Di Milano , Agusta S.p.A.
发明人： ANGHILERI, Marco
IPC分类号： B64C27/00 , B64C27/04 , B64D37/06 , B64D25/00
CPC分类号： B64C1/062 , B64C27/006 , B64C27/04 , B64C2001/0072 , B64C2001/0081 , B64D25/00 , B64D37/06 , B64D45/0015 , B64D2045/005 , Y02T50/43
摘要： What is described is a locally yielding structure (1) with high energy absorption for aeronautical applications, the said structure being substantially closed and substantially rigid, characterized in that at least one wall (3) of the said substantially closed structure comprises at least one vent valve (8) which can be opened when a pressure exceeding a predetermined value is present within the substantially closed structure (1). In a particularly advantageous application, the invention is used in connection with a helicopter tank and enables the subfloor to be used to absorb energy by being deformed during any impact on the ground. The present invention is also advantageous for limiting the damage caused by explosions in an aircraft fuselage.

7. 发明授权

EP1965091B1 Transmission joint 有权转让
标题翻译：传力接头
公开(公告)号：EP1965091B1
公开(公告)日：2009-07-29
申请号：EP07425103.4
申请日：2007-02-27
申请人： Agusta S.p.A.
发明人： Gasparini, Giuseppe , Scaltritti, Diego , Bianchi, Andrea
IPC分类号： F16D3/76
CPC分类号： F16D3/77 , F16D3/76

8. 发明授权

EP1930237B1 Deformable floor substructure for a helicopter 有权转让
标题翻译：变形的基本结构用于直升机
公开(公告)号：EP1930237B1
公开(公告)日：2009-07-29
申请号：EP08151467.1
申请日：2005-10-21
申请人： Agusta S.p.A.
发明人： Poggi, Stefano
IPC分类号： B64C1/00 , B64C1/18 , B64C27/00
CPC分类号： F16F7/12 , B64C1/062 , B64C1/18 , B64C27/006

9. 发明授权

EP1568604B1 Helicopter 有权转让
标题翻译：直升机
公开(公告)号：EP1568604B1
公开(公告)日：2007-08-29
申请号：EP05101148.4
申请日：2005-02-16
申请人： Agusta S.p.A.
发明人： Pancotti, Santino
IPC分类号： B64C5/02 , B64C5/08 , B64C23/06
CPC分类号： B64C27/82 , B64C23/069 , B64C2027/8281 , Y02T50/164
摘要： A helicopter (1) having a fuselage (2); and two rear wings (6) located on opposite sides of the fuselage (2) and having winglets (7), each projecting transversely from a free end of the relative wing (6).

10. 发明授权

EP1640266B1 Helicopter rotor with a vibration damping device 有权
标题翻译：直升机旋翼与振动阻尼器
公开(公告)号：EP1640266B1
公开(公告)日：2007-04-18
申请号：EP04425726.9
申请日：2004-09-28
申请人： Agusta S.p.A.
发明人： Pancotti, Santino
IPC分类号： B64C27/32 , B64C27/35 , B64C27/51
CPC分类号： B64C27/35 , B64C27/32 , B64C27/51

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