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1. 发明公开

EP3045763A1 GUMMI-METALL-HÜLSENLAGER 有权
公开(公告)号：EP3045763A1
公开(公告)日：2016-07-20
申请号：EP15003466.8
申请日：2015-12-05
申请人： AUDI AG
发明人： Conrad, Thomas , Roland, Jörg
IPC分类号： F16F1/38 , F16C27/06 , F16F1/393
CPC分类号： F16F1/3835 , F16C27/063 , F16F1/38 , F16F1/3863 , F16F1/393
摘要： Die Erfindung betrifft Gummi-Metall-Hülsenlager (10), umfassend eine Außenhülse (12) mit einer ersten Außenkante (12a) und einer in axialer Richtung (a) betrachtet gegenüberliegend angeordneten zweiten Außenkante (12b), eine konzentrisch zur Außenhülse (12) angeordnete Innenhülse (14), sowie eine zwischen der Außenhülse (12) und der Innenhülse (14) liegende und konzentrisch zu diesen angeordnete und durch jeweils eine Elastomerschicht (18, 20) mit diesen verbundene Zwischenhülse (16). Die Erfindung zeichnet sich dadurch aus, dass die Außenkanten (12a, 12b) der Außenhülse (12) jeweils mindestens zwei abschnittsweise radial nach innen eingedrückte Außenkantenbereiche (12-1, 12-2) aufweist.
摘要翻译：橡胶金属套筒轴承包括外套筒，当从轴向方向观察时，外套筒具有与第一外边缘相对的第一外边缘和第二外边缘。第一和第二外边缘各自具有设置有径向向内凹入的外边缘区域的至少一个部分。内套筒与外套筒同心地设置，并且中间套筒同心地设置在外套管和内套筒之间，并且经由第一弹性体层与第二弹性体层连接到外套筒。

2. 发明公开

EP2868501A4 BALL JOINT 有权
标题翻译： KUGELGELENK
公开(公告)号：EP2868501A4
公开(公告)日：2016-02-17
申请号：EP13809449
申请日：2013-03-20
申请人： ILJIN CO LTD
发明人： LEE YOUNG-CHUN , KWON TAE-SUNG , KIM HYUN-WOO
IPC分类号： B60G21/05 , B60G7/02 , F16C11/06 , F16F1/393
CPC分类号： F16C11/06 , B60G7/005 , B60G2204/416 , F16C11/0614 , F16C11/0671 , F16C2326/05 , F16F1/393 , Y10T403/32721

3. 发明授权

EP1704345B1 ROTARY WING AIRCRAFT ROD END AND METHOD OF MAKING A HELICOPTER VEHICLE ROD END WITH A PRECOCKED ORIENTATION 失效
标题翻译：挥杆平面杆端并产生一个直升机杆头具有预倾斜取向方法
公开(公告)号：EP1704345B1
公开(公告)日：2012-03-07
申请号：EP05726379.0
申请日：2005-01-14
申请人： LORD CORPORATION
发明人： JAMES, Frank, O. , RAJECKI, Christopher, F.
IPC分类号： F16F1/393 , B64C27/56 , B64C27/59
CPC分类号： F16F1/40 , B64C27/56 , B64C27/58 , B64C27/59 , F16C7/04 , F16C11/0614 , F16C11/083 , F16F1/393 , Y10T29/49885 , Y10T29/4998 , Y10T29/49982 , Y10T403/47
摘要： The invention provides a rotary wing aircraft helicopter vehicle rod end and method of making a rod end. The rotary wing aircraft rod end includes a nonelastomeric inner member having an outer bonding surface segment and an axial bore with a center bore axis, a nonelastomeric outer member having an inner bonding surface segment and an axial bore center bore axis, and molded in place alternating elastomeric shims and nonelastomeric shims connecting the nonelastomeric inner member to the nonelastomeric outer member. The rod end includes a first inner elastomeric shim bonded to the nonelastomeric inner member outer bonding surface segment and to a first inner nonelastomeric shim and a second outer elastomeric shim bonded to the nonelastomeric outer member inner bonding surface segment and to a second outer nonelastomeric shim. The nonelastomeric inner member has a molded misalignment rotary wing aircraft rod end orientation with the outer nonelastomeric outer member.

4. 发明公开

EP2259935A1 REACTION ROD ARRANGEMENT 有权
标题翻译：反应杆安排
公开(公告)号：EP2259935A1
公开(公告)日：2010-12-15
申请号：EP08719433.8
申请日：2008-04-07
申请人： Kongsberg Automotive AS
发明人： BJOERKGARD, Sven , ANDERSEN, Dagfinn
IPC分类号： B60G7/00 , B60G9/00 , F16C11/06 , F16C27/06
CPC分类号： B60G7/005 , B60G9/022 , B60G2200/315 , B60G2204/148 , B60G2204/41 , B60G2204/416 , B60G2206/013 , B60G2206/11 , B60G2206/73 , F16C11/0614 , F16C2326/05 , F16F1/393
摘要： The present invention refers to a reaction rod arrangement, in particular a V-stay suspension, for a vehicle including a bushing (1), wherein the bushing (1) comprises a rigid core member (3) having a bearing portion (9) and defining a longitudinal axis (z), and an elastomer body (11) being arranged on at least a portion of the radially outer surface of the bearing portion (9), characterised in that the bearing portion (9) comprises a first and a second tapering portion (37, 39), wherein the first tapering portion (37) tapers towards one axial end of the bearing portion (9) and the second tapering portion (39) tapers towards the other opposite axial end of the bearing portion (9), wherein the axial extension of the bearing portion (9) is larger than its maximal radial extension with respect to the longitudinal axis (z), and wherein the elastomer body (11) is movably arranged on the bearing portion (9) such that the elastomer body (11) is able to perform a rotational movement about the longitudinal axis (z) relative to the rigid core member (3) and a tilting movement about an axis perpendicular to the longitudinal axis (z) relative to the rigid core member (3).
摘要翻译：本发明涉及一种用于包括衬套（1）的车辆的反作用杆装置，特别是V形支撑悬架，其中衬套（1）包括具有支承部分（9）的刚性芯体构件（3），以及（9）的径向外表面的至少一部分上设置有弹性体本体（11），其特征在于，所述轴承部分（9）包括第一和第二轴承部分其特征在于，所述第一锥形部分（37）朝向所述轴承部分（9）的一个轴向端部逐渐变细，并且所述第二锥形部分（39）朝向所述轴承部分（9）的另一个相对的轴向端部逐渐变细，，其中轴承部分（9）的轴向延伸大于其相对于纵向轴线（z）的最大径向延伸，并且其中弹性体本体（11）可移动地布置在轴承部分（9）上，使得弹性体（11）能够进行围绕其的旋转运动（3）相对于所述刚性核心部件（3）的纵向轴线（z）以及围绕垂直于所述纵向轴线（z）的轴线的倾斜运动。

5. 发明授权

EP1487650B1 COUPLING 有权
公开(公告)号：EP1487650B1
公开(公告)日：2010-05-05
申请号：EP03708741.8
申请日：2003-03-10
申请人： Kongsberg Automotive ASA
发明人： BJORKGARD, Sven
IPC分类号： B60G7/00
CPC分类号： F16F1/393 , B60G7/005 , B60G9/022 , B60G2200/315 , B60G2204/143 , B60G2204/148 , B60G2204/41 , B60G2204/416 , B60G2204/43 , Y10T403/455

6. 发明公开

EP2112064A2 Spherical elastomeric bearing with improved shim thickness 有权
标题翻译： Kugelförmiges，elastomeres Lager mit verbesserter Ausgleichsscheibendicke
公开(公告)号：EP2112064A2
公开(公告)日：2009-10-28
申请号：EP09005377.8
申请日：2009-04-15
申请人： Sikorsky Aircraft Corporation
发明人： Cunningham, Robert , Byrnes, Francis Edward
IPC分类号： B64C27/35
CPC分类号： B64C27/35 , F16F1/393 , Y10T403/32737
摘要： An elastomeric spherical bearing (30) includes a multiple of shims (38), at least two of which have different thicknesses. In one exemplary embodiment, each of the shims (38) has a different thickness with a generally equivalent stress on each shim (38).
摘要翻译：弹性球面轴承（30）包括多个垫片（38），其中至少两个具有不同的厚度。在一个示例性实施例中，每个垫片（38）具有不同的厚度，在每个垫片（38）上具有大致相等的应力。

7. 发明授权

EP1499510B2 DREIECKLENKER 有权
标题翻译： A-ARM
公开(公告)号：EP1499510B2
公开(公告)日：2009-10-14
申请号：EP03709607.0
申请日：2003-02-12
申请人： ZF Lemförder GmbH
发明人： BUHL, Reinhard , RICHTER, Reinhard , COSSMANN, Uwe , KUNZE, Ralf , BUBLIES, Holger , KNOPP, Sören
IPC分类号： B60G7/00 , F16F1/393 , F16C11/06
CPC分类号： F16F1/393 , B60G7/001 , B60G7/005 , B60G2200/315 , B60G2204/143 , B60G2204/148 , B60G2204/416 , B60G2206/124 , B60G2206/91 , F16C11/0614 , F16C2326/05 , Y10T403/32737
摘要： A wishbone (1) is disclosed, for the suspension of axles on motor vehicles to give a jointed connection of a vehicle axle to a vehicle chassis, with two control arms (2, 3), connected together to the vehicle axle by means of a joint housing (6) for a rubber/metal bearing (11) to fix the wishbone (1), formed in common by the control arms (2, 3), whereby the rubber/metal bearing (11) comprises a swivel pin (12) with a ball surface and an elastomeric body (14) enclosing the swivel pin (12), at least in the region of the ball surface, housed in a recess (16) within the joint housing (6). Two press rings (17, 18) are arranged within the recess (16) in the joint housing (6) on the axial outer side of the elastomeric body (14), which may be displaced towards each other by means of a tensioning device, using interposed stop surfaces (22) on the joint housing (6) against the opposing outer sides of the press rings (17, 18). By means of said particular embodiment the rubber/metal bearing can be tensioned in both the axial and the radial direction, such as to permit larger forces to be transmitted due to the greater rigidity thus achieved.

8. 发明授权

EP1811195B1 Gelenklager, insbesondere zur Lagerung von Achslenkern in Kraftfahrzeugen 有权
标题翻译：球面滑动轴承，特别是用于控制臂的机动车辆中的存储
公开(公告)号：EP1811195B1
公开(公告)日：2008-11-26
申请号：EP06012219.9
申请日：2006-06-14
申请人： Jörn GmbH
发明人： Zawadzki, Bernd
IPC分类号： F16F1/387
CPC分类号： F16F1/393

9. 发明公开

EP1818195A1 Koppelstange für eine Stabilisatorenanordnung 审中-公开
标题翻译： Koppelstangefüreine Stabilisatorenanordnung
公开(公告)号：EP1818195A1
公开(公告)日：2007-08-15
申请号：EP07002803.0
申请日：2007-02-09
申请人： Muhr und Bender KG
发明人： Scharioth, Rüdiger
IPC分类号： B60G21/055 , B60G7/00 , F16C11/06 , F16F1/393
CPC分类号： F16F1/393 , B60G7/001 , B60G7/005 , B60G21/0551 , B60G2204/1224 , B60G2204/41 , B60G2204/416 , B60G2204/422 , B60G2206/017 , B60G2206/11 , B60G2206/427 , B60G2206/82092 , F16C7/04 , F16C11/083 , F16C2326/05 , Y10T403/32631 , Y10T403/32713
摘要： Koppelstange, insbesondere für eine Stabilisatoranordnung in einem Kraftfahrzeug, die jeweils an ihren Enden Gelenke 19, 20 aufweist, bei der zumindest eines der Gelenke 19, 20 der Koppelstange 17, 18 ein Elastomer-Metall-Gelenk ist, das aus einem innenliegenden Kugelelement 35, 45, einem ringförmigen Elastomerelement 40, 50 und einem außenliegenden Hülsenteil 37, 47 besteht, wobei das Elastomerelement 40, 50 mit dem Kugelelement 35, 45 und dem Hülsenteil 37, 47 jeweils fest verbunden ist.
摘要翻译：连接杆在其端部具有接头（19,20）。杆（17,18）的接头由弹性体金属接头制成，弹性体金属接头由内侧（35,45）上的球形元件，圆形弹性体元件（40,50）和外部壳体部分（37， 47）。弹性体元件与球元件相连，壳体部分牢固地连接。

10. 发明公开

EP1704345A1 ROTARY WING AIRCRAFT ROD END AND METHOD OF MAKING A HELICOPTER VEHICLE ROD END WITH A PRECOCKED ORIENTATION 失效
标题翻译：挥杆平面杆端并产生一个直升机杆头具有预倾斜取向方法
公开(公告)号：EP1704345A1
公开(公告)日：2006-09-27
申请号：EP05726379.0
申请日：2005-01-14
申请人： LORD CORPORATION
发明人： JAMES, Frank, O. , RAJECKI, Christopher, F.
IPC分类号： F16F1/393 , B64C27/56 , B64C27/59
CPC分类号： F16F1/40 , B64C27/56 , B64C27/58 , B64C27/59 , F16C7/04 , F16C11/0614 , F16C11/083 , F16F1/393 , Y10T29/49885 , Y10T29/4998 , Y10T29/49982 , Y10T403/47
摘要： The invention provides a rotary wing aircraft helicopter vehicle rod end and method of making a rod end. The rotary wing aircraft rod end includes a nonelastomeric inner member having an outer bonding surface segment and an axial bore with a center bore axis, a nonelastomeric outer member having an inner bonding surface segment and an axial bore center bore axis, and molded in place alternating elastomeric shims and nonelastomeric shims connecting the nonelastomeric inner member to the nonelastomeric outer member. The rod end includes a first inner elastomeric shim bonded to the nonelastomeric inner member outer bonding surface segment and to a first inner nonelastomeric shim and a second outer elastomeric shim bonded to the nonelastomeric outer member inner bonding surface segment and to a second outer nonelastomeric shim. The nonelastomeric inner member has a molded misalignment rotary wing aircraft rod end orientation with the outer nonelastomeric outer member.

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