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81 条记录 (耗时 0.014 秒)

    Combined scavenging roots pump and feed pump
    51.
    发明公开
    Combined scavenging roots pump and feed pump 有权
    润滑油泵

    公开(公告)号：EP2085616A1

    公开(公告)日：2009-08-05

    申请号：EP08425041.4

    申请日：2008-01-29

    申请人： Agusta S.p.A.

    发明人： Colombo, Dario ,  Gasparini, Giuseppe

    IPC分类号： F04C2/08 ,  F04C2/12 ,  F04C2/18 ,  F04C11/00 ,  F04C15/00 ,  F16N13/20 ,  B64C27/12 ,  F01D25/20

    CPC分类号： F04C11/006 ,  F01D25/20 ,  F01M2001/123 ,  F04C2/084 ,  F04C2/086 ,  F04C2/126 ,  F04C2/18 ,  F04C15/0076 ,  Y02T50/671

    摘要： A lubricating pump (1) having a first stage (5) and a second stage (10); the first stage (5) in turn has an intake (6) connectable hydraulically to a tank (4) of lubricating fluid, and a delivery outlet (7) connectable hydraulically to a lubricated member (3); the first stage (5) compresses the lubricating fluid from the tank (4) to a pressure for supply to the member (3); the second stage (10) in turn has an inlet (11) connectable hydraulically to a casing (9) housing the member (3), and an outlet (13) connectable hydraulically to the tank (4); the second stage (10) feeds the lubricating fluid in the casing (9) back into the tank (4); the second stage (10) is a Roots type, and has a first and a second rotor (31, 32) rotating about respective axes (B, C) to feed the lubricating fluid from the inlet (11) to the outlet (13); and the first and second rotor (31, 32) are operated by the first stage (5).

    Device and method for protecting an aircraft component from collision with flying objects
    52.
    发明公开
    Device and method for protecting an aircraft component from collision with flying objects 有权
    装置和方法用于保护飞行器组件从碰撞飞行物体

    公开(公告)号：EP2014551A1

    公开(公告)日：2009-01-14

    申请号：EP07425425.1

    申请日：2007-07-09

    申请人： Agusta S.p.A.

    发明人： Anghileri, Marco

    IPC分类号： B64D33/02 ,  F02C7/05

    CPC分类号： B64D33/02 ,  B64D2033/022 ,  F02C7/055 ,  Y02T50/672

    摘要： A device (1) for protecting an aircraft component from collision with a flying object (9), the device having : a main member (2) rotating about an axis (A) and subject to collision with a flying object; and diverting means (8) connected angularly to the main member (2), also subject to collision with the flying object (9), and designed, in the event of collision of the main member (2) with the flying object (9), to reduce the axial momentum of the flying object (9) and divert the flying object (9) radially with respect to the axis (A).

    摘要翻译： 一种用于在飞机构件保护从碰撞飞行物体的装置（1）（9），具有该设备：（2）关于轴线（A）并受与飞行物体碰撞旋转围绕主部件; 和转向装置（8）角度地连接到所述主件（2），即是受与飞行物体（9），并且设计碰撞，在与所述飞行物体的主要构件（2）的碰撞的情况下（9） ，为了减少飞行物体（9）的轴向动量并转移所述飞行物体（9）沿径向相对于所述轴线（A）。

    Transmission joint
    53.
    发明公开
    Transmission joint 有权
    Übertragungsgelenk

    公开(公告)号：EP1965091A1

    公开(公告)日：2008-09-03

    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

    摘要： A transmission joint (1, 1', 1", 1"') for angularly connecting a first and a second member (2, 2', 2"; 4, 4', 4", 4"'), and having a coupling member (5a, 5b; 5a', 5b'; 5a", 5b" ; 5"') interposed functionally between the first and second member (2, 2', 2"; 4, 4', 4", 4"') and extending about an axis (A); the coupling member (5a, 5b; 5a', 5b'; 5a", 5b"; 5"') has : a first portion (6, 6', 6", 6"') connectable angularly to the first member (2,2',2''), a second portion (7, 7', 7", 7"') connectable angularly to the second member (4, 4', 4", 4"') and located radially outwards of the first portion (6, 6', 6", 6"'), and an intermediate portion (8, 8', 8", 8"') interposed radially between the first and second portion (6, 6', 6", 6"'; 7,7',7",7"') and elongated in a direction (D) crosswise to the axis (A); the intermediate portion (8, 8', 8", 8"') of the coupling member (5a, 5b; 5a', 5b'; 5a", 5b"; 5"') has, from the first portion (6, 6', 6", 6"') to the second portion (7, 7', 7", 7"'), a first portion (9, 9', 9", 9"') decreasing in thickness crosswise to the direction (D), and a second portion (10, 10', 10", 10"') of constant thickness. ( Figure 2 )

    摘要翻译： 1.一种用于将第一和第二构件（2,2'，2“; 4,4'，4”，4“'）成角度地连接的传动接头（1,1'，1”，1“'） 功能上介于第一和第二构件（2,2'，2“; 4,4'，4”，4“之间）的连接构件（5a，5b; 5a'，5b'; 5a”，5b“; 5” '）并且围绕轴线（A）延伸;联接构件（5a，5b; 5a'，5b'; 5a“，5b”; 5“'）具有：第一部分（6,6'，6”，6 与第一构件（2,2'，2“）成角度地连接的第二部分（7,7'，7”，7“）可与第二构件（4,4'，4”）成角度地连接， ，4“'），并且位于第一部分（6,6'，6”，6“'）的径向向外的位置，以及位于第一和第二部分之间的中间部分（8,8'，8”，8“ 第二部分（6,6'，6“，6”'; 7,7'，7“，7”'）并沿与轴线（A）交叉的方向（D）细长; 所述连接构件（5a，5b; 5a'，5b'; 5a“，5b”; 5“'）的中间部分（8,8'，8”，8“'） 6“，6”，6“'）延伸到第二部分（7,7'，7”，7“'），第一部分（9,9'，9”，9“'） 方向（D）和具有恒定厚度的第二部分（10,10'，10“，10”'）（图2）

    Helicopter
    57.
    发明公开
    Helicopter 有权
    Hubschrauber

    公开(公告)号：EP1568604A1

    公开(公告)日：2005-08-31

    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).

    摘要翻译： 具有机身（2）的直升机（1）; 以及位于机身（2）的相对侧上的两个后翼（6），并且具有小翼（7），每个后翼从相对翼（6）的自由端横向伸出。

    Helicopter rotor hub, and rotor featuring such a hub
    59.
    发明公开
    Helicopter rotor hub, and rotor featuring such a hub 有权
    Hubschrauberrotornbee，和转子mit einer solchen Nabe

    公开(公告)号：EP1371554A1

    公开(公告)日：2003-12-17

    申请号：EP03013282.3

    申请日：2003-06-12

    申请人： Agusta S.p.A.

    发明人： Pancotti, Santino

    IPC分类号： B64C27/00 ,  B64C27/32

    CPC分类号： B64C27/32 ,  B64C27/35 ,  B64C27/48

    摘要： There is described a hub (2) for a helicopter rotor (1), having a main body (4), and a number of connecting members (5) projecting from the main body (4) and for the connection of respective blades (3); the main body (4) and the connecting members (5) being defined by separate components connectable to one another by releasable fastening means (6).

    摘要翻译： 描述了一种用于直升机转子（1）的毂（2），具有主体（4）和从主体（4）突出并连接各个叶片（3）的多个连接构件（5） ）; 主体（4）和连接构件（5）由通过可释放的紧固装置（6）彼此连接的分开的部件限定。