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    • 1. 发明申请
    • PROPYLENE-BASED POLYMER COMPOSITIONS FOR GRIP APPLICATIONS
    • 用于GRIP应用的基于丙烯的聚合物组合物
    • WO2016154770A1
    • 2016-10-06
    • PCT/CN2015/000210
    • 2015-03-27
    • EXXONMOBIL CHEMICAL PATENTS INC.
    • XU, JiehuiCHEN, Xin
    • C08L23/10C08K3/00B29C45/00
    • C08L23/14B29C45/0001C08L2205/02C08L2205/035C08L23/10
    • The present invention is related to a grip composition comprising 5 to 10 wt%of a polymer blend modifier, having a weight average molecular weight of 10, 000 to 100, 000 g/mole, 65 to 75 wt%of a propylene-based elastomer, having a weight average molecular weight of 100, 000 to 300, 000 g/mole, and a mineral powder. The polymer blend modifier comprises a first propylene-based polymer and a second propylene-based polymer, where the first and second propylene-based polymers are different and are individually selected from a homopolymer of propylene or a copolymer of propylene and ethylene or a C 4 to C 10 alpha-olefin. The composition further comprises 5 to 10 wt%of a propylene polymer, which is a homopolymer of propylene or a copolymer of propylene units with from 0.5 to 4 wt%ethylene or C 4 to C 10 alpha-olefin comonomer derived units.
    • 本发明涉及包含5至10重量%的聚合物共混改性剂的握把组合物,其重均分子量为10,000至100,000g / mol,65至75wt%的丙烯类弹性体 ,重均分子量为100,000〜300,000g / mol,和矿物粉末。 聚合物共混改性剂包括第一丙烯类聚合物和第二丙烯类聚合物,其中第一和第二丙烯类聚合物不同,并且分别选自丙烯均聚物或丙烯与乙烯的共聚物或C4至 C10α-烯烃。 该组合物还包含5至10重量%的丙烯聚合物,其是丙烯的均聚物或具有0.5至4重量%乙烯或C 4至C 10α-烯烃共聚单体衍生单元的丙烯单元的共聚物。
    • 3. 发明申请
    • TRIM ELEMENT FOR MOTOR VEHICLE ADAPTED TO OPTIMUM DEPLOYMENT OF INFLATABLE BAG DEVICE
    • 适用于最佳部署可充气袋装置的电机车辆元件
    • WO2012045197A1
    • 2012-04-12
    • PCT/CN2010/001580
    • 2010-10-09
    • FAURECIA INTERIEUR INDUSTRIEWANG, KevinMEZIERE, JérômeMUNCH, Thierry
    • WANG, KevinMEZIERE, JérômeMUNCH, Thierry
    • B60R21/205
    • B60R21/205B60R13/0206B60R21/2165B60R2021/21652
    • The object of the invention is a trim element (10) for a motor vehicle comprising a rigid supporting member (12), a flexible covering member (14) covering the supporting member (12), and a rigid frame (16). The covering member (14) comprises a skin (26) intended to be visible by an occupant of the passenger compartment of the motor vehicle, and the supporting member (12) comprises at least one aperture (22) allowing deployment of an inflatable bag device outwards from the trimming member (10). The frame (16) is attached to the supporting member (12) on the periphery of said aperture (22) through several attachment means (20). A flap (18) covers the aperture (22) while being jointed with said frame (16). The frame (16) comprises a continuous rib (34) extending from the frame (16) into the covering member. The rib (34) extends along at least one portion of the frame (16) and includes one portion above at least one portion of the attachment means (20).
    • 本发明的目的是用于机动车辆的装饰元件(10),其包括刚性支撑构件(12),覆盖支撑构件(12)的柔性覆盖构件(14)和刚性框架(16)。 覆盖构件(14)包括旨在由机动车辆的乘客舱的乘客可见的皮肤(26),并且支撑构件(12)包括至少一个孔(22),允许展开可充气袋装置 从修剪构件(10)向外。 框架(16)通过几个附接装置(20)附接到所述孔(22)的周边上的支撑构件(12)上。 翼片(18)在与所述框架(16)接合的同时覆盖所述孔(22)。 框架(16)包括从框架(16)延伸到覆盖构件中的连续肋(34)。 肋(34)沿着框架(16)的至少一部分延伸并且包括在附接装置(20)的至少一部分上方的一个部分。
    • 4. 发明申请
    • DROOP PANEL LINKAGE
    • DROOP面板链接
    • WO2011143794A1
    • 2011-11-24
    • PCT/CN2010/000729
    • 2010-05-21
    • AIRBUS S.A.S.YUE, Haikuo
    • YUE, Haikuo
    • B64C9/04B64C9/16
    • B64C9/04B64C9/16B64C9/32B64C2009/143Y02T50/44
    • A droop panel linkage (2) for aircraft comprises a lever arm (5), a main lever (4), a main tube (7) and at least one drive strut (6). The lever arm (5) is pivotally attached at a first end to a flap (3) and is pivotally connected at a second end to a first end of the main lever (4), wherein a second end of the main lever (4) is provided with a first engagement means for engaging with a second engagement means incorporated into or associated with the main tube (7). The main tube (7) is pivotally connected at each end to a proximal end of the drive strut (6), wherein a distal end of the drive strut (6) is pivotally attached to a droop panel (1). Preferably, the main lever (4) is configured as a single-lever type of main lever. As a result of such configuration, the total weight of the droop panel linkage (2) is reduced and the weight penalty of the overall construction is mitigated.
    • 用于飞行器的下垂面板连杆机构(2)包括杠杆臂(5),主杆(4),主管(7)和至少一个驱动支柱(6)。 杠杆臂(5)在第一端处枢转地附接到翼片(3),并且在第二端枢转地连接到主杆(4)的第一端,其中主杆(4)的第二端 设置有用于与并入或与主管(7)相关联的第二接合装置接合的第一接合装置。 主管(7)在每个端部枢转地连接到驱动支柱(6)的近端,其中驱动支柱(6)的远端枢转地附接到下垂面板(1)。 优选地,主杠杆(4)构造为单杠杆式主杆。 作为这种结构的结果,下垂面板连杆(2)的总重量减小,整体结构的重量减轻得到缓解。
    • 10. 发明申请
    • INJECTION MOULD PRODUCT EJECTION APPARATUS AND METHOD
    • 注射模具产品喷射装置和方法
    • WO2012129726A1
    • 2012-10-04
    • PCT/CN2011/000549
    • 2011-03-30
    • FAURECIA INNENRAUM SYSTEME GMBHLIESEN, Martin
    • LIESEN, Martin
    • B29C45/40B29C33/44
    • B29C45/40B29C45/401B29C2045/4057B29C2045/4063
    • An injection mould product ejection apparatus (16) comprising: an ejection element (20); and a displacing member for displacing the ejection element between a retracted moulding position (P1) and a first extended ejection position; characterised in that: the ejection element is an ejection assembly and comprises: a) an inner ejection sub- assembly (26), and b) an outer ejection bush (32) surrounding the inner ejection sub¬ assembly, said displacing member comprises: a collective displacing member (40), for displacing the whole ejection assembly from the retracted moulding position to an intermediate ejection position, and a sub-assembly displacing member (44, 48, 56), for converting the ejection assembly from the intermediate ejection position to the first extended ejection position by extending the sub-assembly relative to the outer ejection bush.
    • 一种注射模具产品喷射装置(16),包括:喷射元件(20); 以及用于使弹出元件在缩回的模制位置(P1)和第一延伸喷射位置之间移动的移位构件; 其特征在于:所述喷射元件是喷射组件,包括:a)内部喷射子组件(26),以及b)围绕所述内部喷射子组件的外部喷射衬套(32),所述移位构件包括: 用于将整个喷射组件从缩回的模制位置移动到中间喷射位置的组合移动构件(40),以及用于将喷射组件从中间喷射位置转换成中间喷射位置的子组件移动构件(44,48,56) 所述第一延伸喷射位置通过相对于所述外部喷射衬套延伸所述子组件。