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1.发明申请MOUNTING FOR LOCKING A VANE BY MEANS OF THE BLADE THEREOF DURING MACHINING OF THE ROOT OF SAID VANE 审中-公开用于在加工车窗时根据其叶片的方式锁定风扇的安装公开(公告)号：US20130015618A1
公开(公告)日：2013-01-17
申请号：US13582205
申请日：2011-02-28
IPC分类号： B23Q3/06
摘要： A mounting for locking a turbine engine vane that includes a root and at least one portion outside the root. The mounting can machine the outside portion on a machine tool and includes a stationary jaw for receiving the vane, the jaw including at least six points that form abutments and define a positioning reference system for the vane. The mounting also includes a movable jaw to ensure, during machining the outside portion, holding the vane against the stationary jaw by a clamping mechanism onto the vane root. The movable jaw includes a first clamping mechanism exerting pressure on one of the surfaces of the root, the pressure being substantially perpendicular to the surface. The stationary jaw includes a second clamping mechanism exerting pressure on the leading or trailing edge of the root, the pressure being substantially oriented in the direction of the trailing or leading edge of the root.
摘要翻译： 用于锁定涡轮发动机叶片的安装件，其包括根部和根部外部的至少一个部分。 安装件可以加工机床上的外部部分并且包括用于接收叶片的固定夹爪，所述夹爪包括至少六个点，所述至少六个点形成邻接并且限定用于叶片的定位参考系。 安装件还包括可移动夹爪，以确保在加工外部部分期间，通过夹紧机构将叶片抵靠在叶片根部上的固定夹爪。 可移动夹爪包括在根部的一个表面上施加压力的第一夹紧机构，该压力基本上垂直于该表面。 固定夹爪包括在根部的前缘或后缘施加压力的第二夹紧机构，该压力基本上沿着根部的后缘或前缘的方向定向。
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公开(公告)号：US20120232652A1
公开(公告)日：2012-09-13
申请号：US13412221
申请日：2012-03-05
申请人： Rolando Mora , Salvador Dada , Juan Jose Chacon
发明人： Rolando Mora , Salvador Dada , Juan Jose Chacon
IPC分类号： A61F2/12
CPC分类号： A61F2/12 , A61F2240/001 , B29C41/02 , B29C41/22
摘要： An implantable soft tissue prosthesis device comprising a silicone elastomer-shell filled with silicone gel or liquid, which among the layers that constitute its shell includes a barrier layer formed of a low permeability silicone, which impedes the bleeding or diffusion of the silicone gel from the inside of the implant to its surroundings through the shell. This barrier layer is given a coloration different to the other layers of the shell, making it visible in the finished product. The coloration of the barrier layer gives the fabricator of the implant as well as to medical personnel, the possibility to identify the presence of the barrier layer and its homogeneity, improving the safety of the device.
摘要翻译： 一种植入式软组织假体装置，其包括填充有硅凝胶或液体的硅氧烷弹性体 - 壳体，构成其壳体的层之间包括由低渗透性硅氧烷形成的阻挡层，其阻止硅凝胶的渗出或扩散 植入物内部通过外壳到其周围。 该阻挡层被赋予与壳的其它层不同的着色，使其在成品中可见。 阻挡层的着色给植入物的制造者以及医务人员提供了识别阻挡层的存在及其均匀性的可能性，从而提高了装置的安全性。
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3.发明申请EQUIPMENT COMPRISING A ROTATABLE CRADLE AND INTENDED FOR ENCASING THE AIRFOIL OF A TURBINE BLADE IN ORDER TO MACHINE THE ROOT 有权装有可旋转的砂浆的设备，旨在用于在机器的基础上订购涡轮叶片的空气公开(公告)号：US20130174420A1
公开(公告)日：2013-07-11
申请号：US13824777
申请日：2011-10-14
CPC分类号： B23Q3/063 , B23Q3/086 , F01D25/285 , Y10T29/49336
摘要： An equipment for coating an airfoil of a turbine blade of a turbine engine in a coating block, including a base on which a molding block is positioned for flow of the coating metal, the molding block including a cavity defining a reference plane on the block for positioning the block in space, wherein the base also includes a cradle supporting the blade via six bearing points defining an orientation plane representative of an angular position of the airfoil relative to a root of the blade. The cradle is rotatably movable relative to the base about an axis oriented so as to be substantially parallel to a direction of a leading edge of the blade, to enable a modification in an angle formed between the reference and orientation planes.
摘要翻译： 一种用于在喷涂块中涂覆涡轮发动机的涡轮叶片的翼型的设备，包括其上定位有用于流动涂层金属的模制块的基座，模制块包括限定块上的参考平面的腔，用于 将所述块定位在空间中，其中所述基座还包括通过六个轴承点支撑所述叶片的支架，所述六个支承点限定了代表所述翼型件相对于所述叶片的根部的角位置的取向平面。 托架可相对于基座绕可转动地移动，该轴线定向成基本上平行于叶片的前缘的方向，从而能够改变在参考平面和定向平面之间形成的角度。
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4.发明授权Equipment comprising a rotatable cradle and intended for encasing the airfoil of a turbine blade in order to machine the root 有权设备包括可旋转托架并且用于封装涡轮机叶片的翼型件以加工根部公开(公告)号：US09205522B2
公开(公告)日：2015-12-08
申请号：US13824777
申请日：2011-10-14
CPC分类号： B23Q3/063 , B23Q3/086 , F01D25/285 , Y10T29/49336
摘要： An equipment for coating an airfoil of a turbine blade of a turbine engine in a coating block, including a base on which a molding block is positioned for flow of the coating metal, the molding block including a cavity defining a reference plane on the block for positioning the block in space, wherein the base also includes a cradle supporting the blade via six bearing points defining an orientation plane representative of an angular position of the airfoil relative to a root of the blade. The cradle is rotatably movable relative to the base about an axis oriented so as to be substantially parallel to a direction of a leading edge of the blade, to enable a modification in an angle formed between the reference and orientation planes.
摘要翻译： 一种用于在喷涂块中涂覆涡轮发动机的涡轮叶片的翼型的设备，包括其上定位有用于流动涂层金属的模制块的基座，模制块包括限定块上的参考平面的腔，用于 将所述块定位在空间中，其中所述基座还包括通过六个轴承点支撑所述叶片的支架，所述六个支承点限定了代表所述翼型件相对于所述叶片的根部的角位置的取向平面。 托架可相对于基座绕可转动地移动，该轴线定向成基本上平行于叶片的前缘的方向，从而能够改变在参考平面和定向平面之间形成的角度。
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5.发明授权公开(公告)号：US10112275B2
公开(公告)日：2018-10-30
申请号：US13582205
申请日：2011-02-28
摘要： A mounting for locking a turbine engine vane that includes a blade and at least one portion outside the blade is provided. The mounting can machine the outside portion on a machine tool and includes a stationary jaw for receiving the vane, the jaw including at least six points that form abutments and define a positioning reference system for the vane. The mounting also includes a movable jaw to ensure, during machining the outside portion, holding the vane against the stationary jaw by a clamping mechanism onto the vane blade. The movable jaw includes a first clamping mechanism exerting pressure on one of the surfaces of the blade, the pressure being substantially perpendicular to the surface. The stationary jaw includes a second clamping mechanism exerting pressure on the leading or trailing edge of the blade, the pressure being substantially oriented in the direction of the trailing or leading edge of the blade.
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