CN202833642U - Rubber supporting bearing - Google Patents
Rubber supporting bearing Download PDFInfo
- Publication number
- CN202833642U CN202833642U CN 201220432358 CN201220432358U CN202833642U CN 202833642 U CN202833642 U CN 202833642U CN 201220432358 CN201220432358 CN 201220432358 CN 201220432358 U CN201220432358 U CN 201220432358U CN 202833642 U CN202833642 U CN 202833642U
- Authority
- CN
- China
- Prior art keywords
- spherical
- flat
- metal spacer
- metal
- rubber layer
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 229910052751 metal Inorganic materials 0.000 claims abstract description 106
- 239000002184 metal Substances 0.000 claims abstract description 106
- 125000006850 spacer group Chemical group 0.000 claims abstract description 105
- 150000003624 transition metals Chemical class 0.000 claims abstract description 22
- 229910052723 transition metal Inorganic materials 0.000 claims abstract description 19
- 239000010410 layer Substances 0.000 claims description 78
- 230000007704 transition Effects 0.000 claims description 5
- 239000003292 glue Substances 0.000 claims description 2
- 239000002356 single layer Substances 0.000 claims 1
- 230000006835 compression Effects 0.000 abstract description 10
- 238000007906 compression Methods 0.000 abstract description 10
- 150000001875 compounds Chemical class 0.000 abstract description 2
- 238000005516 engineering process Methods 0.000 abstract description 2
- 239000010935 stainless steel Substances 0.000 description 6
- 229910001220 stainless steel Inorganic materials 0.000 description 6
- 229910000838 Al alloy Inorganic materials 0.000 description 4
- 239000012790 adhesive layer Substances 0.000 description 4
- 239000000463 material Substances 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 238000000465 moulding Methods 0.000 description 3
- 229910001069 Ti alloy Inorganic materials 0.000 description 2
- 238000013016 damping Methods 0.000 description 2
- 238000010068 moulding (rubber) Methods 0.000 description 2
- 238000013040 rubber vulcanization Methods 0.000 description 2
- 238000004073 vulcanization Methods 0.000 description 2
- 229910000851 Alloy steel Inorganic materials 0.000 description 1
- 230000003139 buffering effect Effects 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
Images
Landscapes
- Support Of The Bearing (AREA)
Abstract
本实用新型属于弹性轴承复合技术,涉及一种橡胶支撑轴承。橡胶支撑轴承包括小接头、一组球形金属隔片、中间过渡金属件、若干层平板金属隔片及隔片之间的橡胶层、大接头。球形金属隔片与小接头之间、球形金属隔片与中间过渡金属件之间及各球形金属隔片之间均通过橡胶层经硫化粘接成一体,平板金属隔片与中间过渡金属件之间、平板金属隔片与大接头之间及平板金属隔片之间也通过橡胶层经硫化粘接成一体,且球形金属隔片胶层总厚度与平板金属隔片胶层总厚度比值在1.0~10.0之间。本实用新型具有使轴承压缩刚度与径向刚度在较大载荷范围内实现刚度匹配,结构简单、设计自由灵活等优点。
The utility model belongs to the compound technology of elastic bearings and relates to a rubber supporting bearing. The rubber support bearing includes a small joint, a group of spherical metal spacers, an intermediate transition metal piece, several layers of flat metal spacers and rubber layers between the spacers, and a large joint. Between the spherical metal spacer and the small joint, between the spherical metal spacer and the intermediate transition metal piece, and between the spherical metal spacers are vulcanized and bonded together through the rubber layer. The space between the flat metal spacer and the large joint and between the flat metal spacers are vulcanized and bonded together through the rubber layer, and the ratio of the total thickness of the rubber layer of the spherical metal spacer to the total thickness of the flat metal spacer is 1.0 ~10.0. The utility model has the advantages of making the compression stiffness and radial stiffness of the bearing realize stiffness matching within a relatively large load range, simple structure, free and flexible design, and the like.
Description
技术领域 technical field
本实用新型属于弹性轴承复合技术,涉及一种橡胶支撑轴承。The utility model belongs to the composite technology of elastic bearings and relates to a rubber supporting bearing.
背景技术 Background technique
直升机旋翼系统中均采用减振装置,通常采用弹性轴承结构来减小旋翼摆振对机身的影响,可承受大的离心载荷和大的挥舞摆振变距,有效减小机身的振动,避免直升机产生地面共振和空中共振,大大提高了直升机的安全性和舒适性,此外,采用弹性轴承结构可以大幅提高桨叶及旋翼系统的使用寿命,从而延长整机的使用寿命,是旋翼系统中的关键功能构件。Helicopter rotor systems all use vibration damping devices, usually using elastic bearing structures to reduce the impact of rotor shimmy on the fuselage, which can withstand large centrifugal loads and large flapping shimmy pitch, effectively reducing the vibration of the fuselage. It avoids the ground resonance and air resonance of the helicopter, which greatly improves the safety and comfort of the helicopter. In addition, the use of elastic bearing structure can greatly improve the service life of the blade and rotor system, thereby prolonging the service life of the whole machine. key functional components.
现有技术橡胶支撑轴承包括球形金属隔片、平板金属隔片及隔片之间的橡胶层和大小接头、中间过渡金属件。其中,大接头为平板金属结构,平板结构胶层总厚度过大使得弹性轴承径向刚度偏低,对径向刚度要求较大的场合,该结构难以同时满足径向刚度和轴向刚度的设计要求。The rubber support bearing in the prior art includes spherical metal spacers, flat metal spacers, rubber layers between the spacers, large and small joints, and intermediate transition metal pieces. Among them, the large joint is a flat metal structure, and the total thickness of the adhesive layer of the flat structure is too large, so that the radial stiffness of the elastic bearing is relatively low. When the radial stiffness is required, it is difficult for this structure to meet the design of radial stiffness and axial stiffness at the same time. Require.
实用新型内容 Utility model content
本实用新型的目的是:提出一种能够实现压缩刚度与径向刚度在较大范围内实现匹配的橡胶支撑轴承。The purpose of the utility model is to propose a rubber support bearing capable of matching the compression stiffness and the radial stiffness in a relatively large range.
本实用新型的技术方案是:一种橡胶支撑轴承,其包括小接头、一组球形金属隔片、中间过渡金属件、若干层平板金属隔片、大接头,所述球形金属隔片由球形橡胶层粘接成一体,且粘接为一体的球形金属隔片一端与小接头相连,另一端与中间过渡金属件相连,所述平板金属隔片之间由平板橡胶层粘接为一体,且粘接为一体的平板金属隔片一端与中间过渡金属件相连,另一端与大接头相连,其中,球形橡胶层总厚度与平板橡胶层总厚度比值在1.0~10.0之间。The technical scheme of the utility model is: a rubber supporting bearing, which includes a small joint, a group of spherical metal spacers, an intermediate transition metal piece, several layers of flat metal spacers, and a large joint. The spherical metal spacers are made of spherical rubber The layers are bonded together, and one end of the bonded spherical metal spacer is connected to the small joint, and the other end is connected to the intermediate transition metal piece. The flat metal spacers are bonded together by the flat rubber layer, and the glued One end of the integrally connected flat metal spacer is connected to the intermediate transition metal piece, and the other end is connected to the large joint, wherein the ratio of the total thickness of the spherical rubber layer to the total thickness of the flat rubber layer is between 1.0 and 10.0.
所述球形金属隔片的层数为4~10层,平板金属隔片为1~6层。The number of layers of the spherical metal spacer is 4-10 layers, and that of the flat metal spacer is 1-6 layers.
所述球形金属隔片、平板金属隔片的厚度为0.5mm~1.5mm,厚度公差控制在±0.1mm。The thickness of the spherical metal spacer and the flat metal spacer is 0.5 mm to 1.5 mm, and the thickness tolerance is controlled at ±0.1 mm.
球形金属隔片胶层厚度和平板橡胶层厚度为0.5mm~2.0mm。The thickness of the rubber layer of the spherical metal spacer and the thickness of the flat rubber layer are 0.5 mm to 2.0 mm.
各球形金属隔片为同球心,球形金属隔片从小接头到中间过度金属结构之间的面积逐渐变大,最小的球形金属隔片与小接头之间、最大的一层球形隔片与中间过度金属结构之间及各球形隔片之间均通过橡胶层经硫化粘接成一体。Each spherical metal spacer is concentric, and the area between the spherical metal spacers from the small joint to the middle transitional metal structure gradually becomes larger, between the smallest spherical metal spacer and the small joint, between the largest spherical metal spacer and the middle The transitional metal structures and the spherical spacers are vulcanized and bonded together through the rubber layer.
大接头与平板橡胶层之间的具有金属凸台。There is a metal boss between the large joint and the flat rubber layer.
所述大接头、小接头、球形金属隔片、平板金属隔片及中间过渡金属件的正中心均开有通孔,经胶层粘接成一个整体后各通孔同轴。There are through holes in the center of the large joints, small joints, spherical metal spacers, flat metal spacers and intermediate transition metal parts, and the through holes are coaxial after being bonded into a whole by the adhesive layer.
所述各球形橡胶层厚度应保证均匀并同球心,各平板橡胶层厚度应保证均匀并相互平行。The thickness of each spherical rubber layer should be guaranteed to be uniform and concentric with the center of the sphere, and the thickness of each flat rubber layer should be guaranteed to be uniform and parallel to each other.
球形金属隔片在球面与卷边的过渡处采取圆角处理,内圆半径R1取R0.5mm~R3mm,外圆半径R2取R0.5mm~R4mm。The spherical metal spacer is rounded at the transition between the spherical surface and the curling edge. The inner circle radius R1 is R0.5mm-R3mm, and the outer circle radius R2 is R0.5mm-R4mm.
本实用新型的优点是:本实用新型橡胶支撑轴承采用多层球形轴承与多层柱形轴承复合,通过控制球形金属隔片、平板金属隔片的层数及各胶层的厚度,在保持接口和外观尺寸不变的前提下,可在较大载荷范围内实现压缩刚度和径向刚度的匹配,满足直升机旋翼系统对弹性轴承压缩刚度、挥舞刚度、扭转刚度和径向刚度的不同设计要求,且该设计自由灵活,结构简单,加工成本低,成型容易。The utility model has the advantages that: the rubber support bearing of the utility model adopts multi-layer spherical bearing and multi-layer cylindrical bearing compound, and by controlling the number of layers of the spherical metal spacer and the flat metal spacer and the thickness of each rubber layer, the interface is maintained Under the premise of keeping the appearance size unchanged, the compression stiffness and radial stiffness can be matched within a large load range, meeting the different design requirements of the helicopter rotor system for elastic bearing compression stiffness, flapping stiffness, torsional stiffness, and radial stiffness. Moreover, the design is free and flexible, the structure is simple, the processing cost is low, and the forming is easy.
附图说明 Description of drawings
图1是本实用新型橡胶支撑轴承第一实施方式的结构示意图。Fig. 1 is a schematic structural view of the first embodiment of the rubber support bearing of the present invention.
图2是图1的俯视图。FIG. 2 is a top view of FIG. 1 .
图3是图1的仰视图。Fig. 3 is a bottom view of Fig. 1 .
图4为图1的A-A剖视图。Fig. 4 is a sectional view along line A-A of Fig. 1 .
图5为球形金属隔片卷边剖视图。Fig. 5 is a cross-sectional view of the curling of the spherical metal spacer.
图6是本实用新型橡胶支撑轴承第二实施方式的结构示意图。Fig. 6 is a schematic structural view of the second embodiment of the rubber support bearing of the present invention.
图7是图6的B-B剖视图。Fig. 7 is a B-B sectional view of Fig. 6 .
其中,1-小接头,2-球形橡胶层,3-球形金属隔片,4-中间过渡金属件,5-平板橡胶层,6-平板金属隔片,7-大接头,8-金属凸台。Among them, 1-small joint, 2-spherical rubber layer, 3-spherical metal spacer, 4-intermediate transition metal piece, 5-flat rubber layer, 6-flat metal spacer, 7-large joint, 8-metal boss .
具体实施方式 Detailed ways
下面对本实用新型做进一步详细说明。Below the utility model is described in further detail.
参见图1~图4,其中,图1是本实用新型橡胶支撑轴承第一实施方式的结构示意图,图2是图1的俯视图,图3是图1的仰视图,图4为图1的A-A剖视图。本实施方式中,所述橡胶支撑轴承包括一组球形金属隔片、若干层平板金属隔片及隔片之间的橡胶层和大小接头、中间过渡金属件。Referring to Figures 1 to 4, where Figure 1 is a schematic structural view of the first embodiment of the rubber support bearing of the present invention, Figure 2 is a top view of Figure 1, Figure 3 is a bottom view of Figure 1, and Figure 4 is A-A of Figure 1 cutaway view. In this embodiment, the rubber support bearing includes a group of spherical metal spacers, several layers of flat metal spacers, rubber layers between the spacers, large and small joints, and intermediate transition metal pieces.
所述的一组球形金属隔片3经球形橡胶层2硫化粘接成一体后,各球形金属隔片是同球心的,各球形金属隔片的厚度是均匀的,球形金属隔片从小接头到中间过渡金属件之间面积逐渐变大,最小的球形金属隔片与小接头之间、最大的一层球形金属隔片与中间过渡金属件之间及各球形金属隔片之间均通过橡胶层经硫化粘接成一体。After the group of
所述的平板金属隔片6的厚度是均匀的,经平板橡胶层5硫化粘接成一体后各隔片之间相互平行,且最下方的平板金属隔片经橡胶层与中间过渡金属件相胶结,最上方的平板金属隔片经橡胶层与大接头相胶结,并经硫化粘接成一体。The thickness of the
所述的大接头7、小接头1、球形金属隔片3、平板金属隔片6及中间过渡金属件4的正中心均开有圆孔,所有金属件经胶层粘接成一个整体后各金属件的中心圆孔同轴。The center of the
所述的球形橡胶层2、平板橡胶层5厚度可以相同,也可以不同,各球形橡胶层厚度应保证均匀并同球心,各平板橡胶层5厚度应保证均匀并相互平行。但球形橡胶层总厚度与平板橡胶层总厚度比值控制在1.0~10.0之间,从而以在较大载荷范围内,实现压缩刚度和径向刚度的匹配。The thickness of the
所述球形金属隔片的层数为4~10层,平板金属隔片为1~6层。所述球形金属隔片3、平板金属隔片6的厚度为0.5mm~2mm,厚度公差控制在±0.1mm,其材质为不锈钢、合金钢、铝合金或钛合金。所述大接头7、小接头1、中间过渡金属件4的材质为不锈钢、铝合金、钛合金。The number of layers of the spherical metal spacer is 4-10 layers, and that of the flat metal spacer is 1-6 layers. The thickness of the
所述球形金属隔片3在球面与卷边的过渡处应进行圆角处理,如图5所示,在工艺满足的条件下应尽量减小内圆半径R1、外圆半径R2的尺寸,通常R1根据金属件厚度和成型工艺取R0.5mm~R3mm,R2取R0.5mm~R4mm。The
本实用新型的工作原理是:橡胶支撑轴承的大接头7和小接头1分别与直升机的轴承袖套和柔性梁连接。桨叶旋转引起的动载经柔性梁传递到小接头,然后经各橡胶层逐级传递到大接头,各橡胶层的变形对动载起到缓冲过渡作用,从而减小机身的振动。由于桨叶旋转引起的动载传递到轴承小接头时表现为同时承受离心、扭转、挥舞、径向上的复杂叠加交变载荷,轴承的使用寿命通常表现为橡胶层出现疲劳裂纹并逐渐加深扩展最终导致轴承失效,而橡胶层的疲劳裂纹与叠加交变载荷下的等效应变关系密切,某一方向的刚度过高,会影响轴承的整体减振性能,刚度过低,会导致橡胶层应变过大,降低轴承的使用寿命,因此根据桨叶的实际动载对轴承均会给出各方向的刚度指标要求,本实用新型在满足轴承接口及基本外观尺寸的前提下,通过控制球形金属隔片胶层总厚度与平板金属隔片胶层总厚度的比例,实现了在较大范围内压缩刚度和径向刚度的匹配,同时对扭转刚度和挥舞刚度没有大的影响,可对轴承提出的不同刚度设计指标进行灵活优化设计,满足刚度性能设计要求。The working principle of the utility model is: the
实施例一Embodiment one
一种橡胶支撑轴承,如图1~图5所示。小接头1、大接头7、中间过渡金属件4为铝合金材料,球形金属隔片3为不锈钢材料,厚度均为0.6mm,厚度公差范围控制在±0.1mm以内,一组球形金属隔片为7片,从小接头到中间过渡金属件面积逐级增大,各球形金属隔片外缘均带有卷边,在成型过程中通过卷边及中心定位销对隔片定位来精确控制各球形金属隔片保持同球心、同轴,从而保证各球形橡胶层同球心及厚度均匀。A rubber support bearing, as shown in Figures 1 to 5. The small joint 1, the
平板金属隔片6为不锈钢材料制成的平板圆形隔片,厚度均为0.6mm,厚度公差范围控制在±0.1mm以内,各平板金属隔片形状及尺寸均相同,平板金属隔片一共2层,各平板橡胶层的厚度均匀性及胶层间的平行度由平板金属隔片平面度及精密成型模具共同保证。另外,大接头与平板橡胶层之间的具有金属凸台,以用于调节控制平板橡胶层厚度。The
小接头1中心开有螺纹孔用于装配时连接,螺纹孔贯穿小接头1,在其他金属件的中心开有通孔,球形金属隔片3、平板金属隔片6的中心通孔与其外缘应有良好的同轴性,经橡胶硫化成型后,所有金属件的中心孔保持同轴。There is a threaded hole in the center of the small joint 1 for connection during assembly. The threaded hole runs through the small joint 1 and has a through hole in the center of other metal parts. The center through hole of the
与各球形金属隔片相连接的胶层厚度相同,与各平板圆形隔片相连接的胶层厚度相同,球形橡胶层2总厚度与平板橡胶层5总厚度比值为3.5。The thickness of the rubber layer connected to each spherical metal spacer is the same, and the thickness of the rubber layer connected to each flat circular spacer is the same. The ratio of the total thickness of the
球形金属隔片3在球面与卷边的过渡处进行圆角处理,R1为2mm,R2为3mm。The
试验测得该结构轴承的压缩刚度为4660N/mm,径向刚度为236N/mm,压缩刚度与径向刚度的比值为19.7,能够满足较大径向载荷条件下的刚度匹配设计要求。According to the test, the compression stiffness of the structural bearing is 4660N/mm, the radial stiffness is 236N/mm, and the ratio of compression stiffness to radial stiffness is 19.7, which can meet the stiffness matching design requirements under the condition of large radial load.
实施例二Embodiment two
一种橡胶支撑轴承,如图6、图7所示。小接头1、大接头7、中间过渡金属件4为铝合金材料,球形金属隔片3为不锈钢材料,厚度均为0.6mm,厚度公差范围控制在±0.1mm以内,一组球形金属隔片为7片,从小接头到中间过渡金属件面积逐级增大,各球形金属隔片外缘均带有卷边,在成型过程中通过卷边及中心定位销对隔片定位来精确控制各球形金属隔片保持同球心、同轴,从而保证各球形橡胶层同球心及厚度均匀。A rubber support bearing, as shown in Figure 6 and Figure 7. The small joint 1, the
平板金属隔片6为不锈钢材料制成的平板圆形隔片,厚度均为0.6mm,厚度公差范围控制在±0.1mm以内,各平板圆形隔片形状及尺寸均相同,平板圆形隔片一共4层,各平板橡胶层的厚度均匀性及胶层间的平行度由平板金属隔片平面度及精密成型模具共同保证。The
小接头1中心开有螺纹孔用于装配时连接,螺纹孔贯穿小接头1,在其他金属件的中心开有通孔,球形金属隔片3、平板圆形隔片6的中心通孔与其外缘应有良好的同轴性,经橡胶硫化成型后,所有金属件的中心孔保持同轴。There is a threaded hole in the center of the small joint 1 for connection during assembly. The threaded hole runs through the small joint 1 and has a through hole in the center of other metal parts. The edge should have good coaxiality. After rubber vulcanization and molding, the central holes of all metal parts should remain coaxial.
与各球形金属隔片相连接的胶层厚度相同,与各平板圆形隔片相连接的胶层厚度相同,球形橡胶层2总厚度与平板橡胶层5总厚度比值为1.5。The thickness of the rubber layer connected to each spherical metal spacer is the same, and the thickness of the rubber layer connected to each flat circular spacer is the same. The ratio of the total thickness of the
球形金属隔片3在球面与卷边的过渡处进行了圆角处理,R1为2mm,R2为3mm。The
试验测得该结构轴承的压缩刚度为3070N/mm,径向刚度为120N/mm,压缩刚度与径向刚度的比值为25.6,能够满足较小径向载荷条件下的刚度匹配设计要求。The test results show that the compression stiffness of the structural bearing is 3070N/mm, the radial stiffness is 120N/mm, and the ratio of compression stiffness to radial stiffness is 25.6, which can meet the stiffness matching design requirements under the condition of small radial load.
Claims (9)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 201220432358 CN202833642U (en) | 2012-08-28 | 2012-08-28 | Rubber supporting bearing |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 201220432358 CN202833642U (en) | 2012-08-28 | 2012-08-28 | Rubber supporting bearing |
Publications (1)
Publication Number | Publication Date |
---|---|
CN202833642U true CN202833642U (en) | 2013-03-27 |
Family
ID=47945355
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN 201220432358 Expired - Lifetime CN202833642U (en) | 2012-08-28 | 2012-08-28 | Rubber supporting bearing |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN202833642U (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102829079A (en) * | 2012-08-28 | 2012-12-19 | 中国航空工业集团公司北京航空材料研究院 | Rigidity matching rubber supporting bearing |
CN104236906A (en) * | 2014-08-26 | 2014-12-24 | 中国直升机设计研究所 | Device for testing radial rigidity of tail rotor steady bearings |
US10330148B2 (en) | 2014-02-26 | 2019-06-25 | Airbus Helicopters Deutschland GmbH | Bearing arrangement with a first bearing layer and a second bearing layer |
US12060148B2 (en) | 2022-08-16 | 2024-08-13 | Honeywell International Inc. | Ground resonance detection and warning system and method |
-
2012
- 2012-08-28 CN CN 201220432358 patent/CN202833642U/en not_active Expired - Lifetime
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102829079A (en) * | 2012-08-28 | 2012-12-19 | 中国航空工业集团公司北京航空材料研究院 | Rigidity matching rubber supporting bearing |
CN102829079B (en) * | 2012-08-28 | 2015-07-15 | 中国航空工业集团公司北京航空材料研究院 | Rigidity matching rubber supporting bearing |
US10330148B2 (en) | 2014-02-26 | 2019-06-25 | Airbus Helicopters Deutschland GmbH | Bearing arrangement with a first bearing layer and a second bearing layer |
CN104236906A (en) * | 2014-08-26 | 2014-12-24 | 中国直升机设计研究所 | Device for testing radial rigidity of tail rotor steady bearings |
CN104236906B (en) * | 2014-08-26 | 2017-06-23 | 中国直升机设计研究所 | A kind of tail-rotor spring bearing radial rigidity test device |
US12060148B2 (en) | 2022-08-16 | 2024-08-13 | Honeywell International Inc. | Ground resonance detection and warning system and method |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN102829079B (en) | Rigidity matching rubber supporting bearing | |
CN202833642U (en) | Rubber supporting bearing | |
CN101936337A (en) | Spherical elastic bearing for helicopter rotor wing and molding method thereof | |
CN110701186B (en) | A combined elastic bearing | |
CN102795338A (en) | Micro unmanned aerial vehicle carbon fiber rotor wing and preparation method thereof | |
US20020154940A1 (en) | Device for damped elastic connection and method of manufacturing it | |
CA2790085C (en) | Elastomeric bearing with tapered shims | |
JP2015530535A (en) | Elastic seesaw bearing | |
CN101596786A (en) | A kind of ball hinged rubber elastic element assembling mode and product | |
US4365936A (en) | Laminated elastomeric bearing unit | |
CN104632885A (en) | Rubber elastic bearing | |
CN105757118B (en) | A kind of anti-radial load long-life rubber bearing | |
CN102729580B (en) | Self-pumping and the adhesive bond system from filling | |
CN102011798B (en) | Spherical elastic bearing and injecting method in forming process of spherical elastic bearing | |
CN205315489U (en) | Long -life rubber support bearing | |
CN204366722U (en) | A kind of float support frame | |
CN108266475B (en) | Axial nonlinear stiffness adjustment laminated spring of traction spherical hinge and adjustment method | |
CN113459602B (en) | A lightweight corrugated sandwich composite bearing cylinder | |
CN110081077B (en) | A kind of high radial stability elastic bearing | |
CN207683645U (en) | The compound carrier wheel of endless-track vehicle | |
CN110107646A (en) | A kind of stable long-life viscoelastic damper of high radial | |
CN112178052A (en) | Laminated rubber and metal elastic bearing | |
CN205853799U (en) | Longitudinal composite material plate spring assembly | |
CN108253058B (en) | Nonlinear variable-rigidity adjusting rubber metal spherical hinge | |
CN202779427U (en) | Bent whole concave die |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CP03 | Change of name, title or address | ||
CP03 | Change of name, title or address |
Address after: 100095 box 81, Haidian District, Beijing Patentee after: AECC BEIJING INSTITUTE OF AERONAUTICAL MATERIALS Address before: 100095 box 81, Haidian District, Beijing Patentee before: AVIC BEIJING INSTITUTE OF AERONAUTICAL MATERIALS |
|
TR01 | Transfer of patent right | ||
TR01 | Transfer of patent right |
Effective date of registration: 20210531 Address after: No. 5 Yongxiang North Road, Haidian District, Beijing 100094 Patentee after: Beijing Aeronautical Materials Research Institute Co.,Ltd. Address before: 100095 box 81, Haidian District, Beijing Patentee before: AECC BEIJING INSTITUTE OF AERONAUTICAL MATERIALS |
|
CP01 | Change in the name or title of a patent holder | ||
CP01 | Change in the name or title of a patent holder |
Address after: No. 5 Yongxiang North Road, Haidian District, Beijing 100094 Patentee after: Beijing Aviation Materials Research Institute Co.,Ltd. Address before: No. 5 Yongxiang North Road, Haidian District, Beijing 100094 Patentee before: Beijing Aeronautical Materials Research Institute Co.,Ltd. |
|
CX01 | Expiry of patent term | ||
CX01 | Expiry of patent term |
Granted publication date: 20130327 |