-
公开(公告)号：US5116218A
公开(公告)日：1992-05-26
申请号：US622647
申请日：1990-12-05
CPC分类号： B29C53/824 , B29C33/44 , B29C33/485
摘要： Molding apparatus, for example for molding components of polymerized resin without drawing, comprises a mold defined by a mold wall having a first thermal expansion coefficient, and a die including a die wall having a second thermal expansion coefficient greater than the said first coefficient, a molding operation being carried out by inserting the die into the mold at a first temperature, heating the die and the mold to a second temperature higher than the first temperature, and subsequently cooling the die and the mold after a component has been molded. In accordance with the invention, the die wall includes a plurality of separate sectors which are pivotally mounted on a common support member and which are arranged and dimensioned such that, at the second temperature, the radially outer faces of the sectors adjoin one another contiguously to define the molding face of the die wall.
摘要翻译： 成型装置，例如用于模制未拉伸的聚合树脂的组分，包括由具有第一热膨胀系数的模具壁定义的模具和包括具有大于所述第一系数的第二热膨胀系数的模具壁的模具， 通过在第一温度下将模具插入模具中进行成型操作，将模具和模具加热至高于第一温度的第二温度，随后在模制成型后冷却模具和模具。 根据本发明，模具壁包括多个单独的扇区，其可枢转地安装在共同的支撑构件上，并且其布置和尺寸被设计成使得在第二温度下，扇形体的径向外表面彼此邻接地连接到 限定模具壁的模制面。
-
12.发明授权
公开(公告)号：US4907743A
公开(公告)日：1990-03-13
申请号：US269725
申请日：1988-11-10
CPC分类号： F23R3/60 , F02K1/04 , F02K1/80 , F05D2230/642
摘要： Two coaxial bodies of revolution made of materials having distinctly different expansion coefficients are joined together to form an assembly by fixing means comprising at least three resilient brackets of trapezoidal shape, the larger end of each bracket having a flanged edge secured at at least two points by hollow rivets to a metal ring and by bolts extending through the rivets to the body with the higher expansion coefficient, and the smaller end of each bracket being secured by at least one bolt to the body with the lower expansion coefficient in a manner which imposes a cold prestress on the bracket.
摘要翻译： 由具有明显不同的膨胀系数的材料制成的两个旋转同轴体连接在一起，以通过包括至少三个梯形形状的弹性支架的固定装置形成组件，每个支架的较大端具有通过在至少两个点处固定的凸缘 空心铆钉到金属环，并且以螺栓延伸穿过铆钉到具有较高膨胀系数的主体，并且每个支架的较小端部以至少一个螺栓固定到具有较低膨胀系数的体系，其方式为施加 支架上的冷预应力。
-
13.发明授权Turbo-machine with device for automatically controlling the rate of flow of turbine ventilation air 失效涡轮机具有用于自动控制涡轮机通风空气流量的装置
公开(公告)号：US4805398A
公开(公告)日：1989-02-21
申请号：US103417
申请日：1987-10-01
CPC分类号： F01D5/082 , F01D11/18 , F01P7/02 , F02C7/18 , Y02T50/672 , Y02T50/676
摘要： A device for automatically controlling the rate of flow of turbine ventilation air in a turbo-machine comprises two superimposed ceramic rings which are split and are each fixed at a single point to a metal support so that differential expansion of the support and the two rings in response to the operating conditions of the turbo-machine causes the registry of peripherally disposed slots in the ceramic rings to vary and thereby control the rate of ventilation air flow therethrough in accordance with the turbo-machine operating conditions.
摘要翻译： 用于自动控制涡轮机中的涡轮机通风空气的流量的装置包括两个叠置的陶瓷环，它们分开并且分别固定在金属支撑件上的一个点上，使得支撑件和两个环的不同膨胀 对涡轮机的操作条件的响应导致陶瓷环中外围设置的槽的注册表变化，从而根据涡轮机操作条件控制通过其中的通风空气的速率。
-
14.发明授权
公开(公告)号：US4674951A
公开(公告)日：1987-06-23
申请号：US770247
申请日：1985-08-28
IPC分类号： F04D27/02
CPC分类号： F02K7/075 , F04D27/0215 , F04D27/023 , Y02T50/672
摘要： A ring of an annular valve assembly is movable in the direction of its longitudinal axis and is intended for an axial compressor blow-off arrangement. The ring takes the form of an axially orientated channel-section member having a first annular skin of concave section nested in a second annular skin also of concave section. A cavity filled with a synthetic resin filler is defined by the two skins. The blow-off arrangement for an axial-flow compressor of a turbo-jet engine, which incorporates this ring, comprises an annular opening with which the ring cooperates to re-form the wall of the air flow when the blow-off arrangement is inoperative.
摘要翻译： 环形阀组件的环可以在其纵向轴线的方向上移动，并且用于轴向压缩机吹出装置。 该环采取轴向定向的通道截面构件的形式，其具有嵌在第二环形表皮中的凹部的第一环形表皮，也是凹形部分。 填充有合成树脂填料的空腔由两个表皮限定。 涡轮喷气发动机的轴流式压缩机的排放装置，其结合了该环，包括环形开口，当排放装置不起作用时，该环与该空气合流以重新形成空气流的壁 。
-
公开(公告)号：US4546606A
公开(公告)日：1985-10-15
申请号：US491372
申请日：1983-05-04
申请人： Jean G. Bouiller , Marc F. B. Buisson , Gerard E. A. Jourdain , Denis J. M. Sandelis , Yves R. A. Urruty
发明人： Jean G. Bouiller , Marc F. B. Buisson , Gerard E. A. Jourdain , Denis J. M. Sandelis , Yves R. A. Urruty
CPC分类号： F02K3/075 , F01D17/162 , Y10T137/87442
摘要： The control device comprises at least one control ring to which one end ofn elbow lever is articulated. The vane pivot of alternating vanes is fixed at the intersection of the arms of the elbow levers. The other end of each elbow lever is connected by a rod to the end of a straight lever, the other end of which is fixed to the pivot of an adjacent vane. The circumferential movement of the ring causes the pivots of the adjacent vanes to pivot in opposite directions. Two other embodiments have two rings.
摘要翻译： 控制装置包括至少一个控制环，肘杆的一端被铰接到该控制环上。 交替叶片的叶片枢轴固定在肘杆臂的交叉处。 每个肘杆的另一端通过杆连接到直杆的端部，另一端固定在相邻叶片的枢轴上。 环的圆周运动导致相邻叶片的枢轴在相反的方向枢转。 另外两个实施例具有两个环。
-
16.发明授权Nozzle for a jet engine containing an adjustable convergent-divergent portion 失效用于喷气发动机的喷嘴，其包含可调节的收敛 - 发散部分
公开(公告)号：US5520336A
公开(公告)日：1996-05-28
申请号：US237399
申请日：1981-01-13
IPC分类号： F02K1/12
CPC分类号： F02K1/12 , F02K1/1223 , F05D2250/323 , F05D2250/324 , Y02T50/671
摘要： A nozzle comprises: a set of first flaps articulated to a rigid structure, and forming a convergent; a set of second flaps each articulated to a corresponding first flap, and forming a divergent; a set of third flaps each of which is connected at a position between two adjacent second flaps and which is, on the one hand, articulated to the rigid structure and, on the other hand, linked to each of the two adjacent second flaps by carrier linked to the aforesaid third flap by a ball joint.
摘要翻译： 喷嘴包括：一组铰接到刚性结构的第一翼片，并且形成会聚; 一组第二翼片，每个第二翼片铰接到相应的第一翼片，并形成发散; 一组第三翼片，每个翼片连接在两个相邻的第二翼片之间的位置，并且一方面铰接到刚性结构，另一方面通过载体连接到两个相邻的第二翼片中的每一个 通过球形接头连接到上述第三挡板。
-
17.发明授权Variable geometry flame trap device for use in an after-burner device of a gas turbine 失效用于燃气轮机的后燃烧器装置的可变几何形状的火焰捕集装置
公开(公告)号：US5269138A
公开(公告)日：1993-12-14
申请号：US16074
申请日：1993-02-10
CPC分类号： F23R3/22
摘要： A variable geometry flame trap device for use in an after-burner device of a gas turbine, which is not exposed to deformation forces during its use in the after-burner mode. This is achieved with a plurality of flame trap plate pairs (21), positioned downstream of the turbine at the outlet of a primary air flow duct (9) and mounted so as to pivot on a plurality of diffuser arms (19) located at the outlet of a secondary air flow duct (7), characterized in that the plates (21) of each pair are made from a composite material and in that they have a cam projecting from their facing faces (42), said two cams (43) bearing on one another.
摘要翻译： 一种用于燃气轮机的后燃烧器装置的可变几何型火焰捕集装置，其在后燃烧器模式中的使用期间不会受到变形力的影响。 这是通过多个阻气板对（21）来实现的，其位于涡轮机的主要空气流动管道（9）的出口的下游，并且安装成在位于所述主要空气流动管道（9）处的多个扩散器臂 二次气流管道（7）的出口，其特征在于，每对的板（21）由复合材料制成，并且它们具有从其相对面（42）突出的凸轮，所述两个凸轮（43） 彼此相依。
-
公开(公告)号：US4778109A
公开(公告)日：1988-10-18
申请号：US133886
申请日：1987-12-16
CPC分类号： F02K1/006 , F02K1/1223 , F02K1/1292 , F02K1/62
摘要： An adjustable two-dimensional nozzle is disclosed in which simplified control means are located away from the flow of gasses through the nozzle. The nozzle includes a movable frame located outside of fixed sidewalls and has pivotally attached thereto a pair of upstream or converging nozzle flaps. Upstream edges of the upstream flaps are attached to the movable frame such that the flaps pivot about axes extending substantially perpendicular to the longitudinal axis of the nozzle. Downstream or diverging flaps are attached to the downstream edges of the upstream flaps such that these flaps also pivot about axes extending substantially perpendicular to the longitudinal axis of the nozzle. A cam member extends between each of the movable frames and each downstream flap to control the angular variations of the flaps during movement of the frame. The flap arrangements are symmetrically arranged with respect to a plane passing through the longitudinal axis of the nozzle, such that translational movement of the frames will alter the cross-section of the nozzle in a symmetrical manner with respect to the plane. If the frame is rotated about its pivot attachment, the nozzle flaps will be asymmetrically adjusted and may be utilized to vector the thrust of the gasses emanating from the nozzle.
摘要翻译： 公开了一种可调节的二维喷嘴，其中简化的控制装置位于远离气体流经喷嘴的位置。 喷嘴包括位于固定侧壁外侧的可移动框架，并且可旋转地附接有一对上游或会聚的喷嘴襟翼。 上游翼片的上游边缘附接到可移动框架，使得翼片围绕基本上垂直于喷嘴的纵向轴线延伸的轴线枢转。 下游或发散的翼片附接到上游翼片的下游边缘，使得这些翼片也围绕基本上垂直于喷嘴的纵向轴线延伸的轴线枢转。 凸轮构件在每个可移动框架和每个下游翼片之间延伸以在框架移动期间控制翼片的角度变化。 翼片装置相对于穿过喷嘴的纵向轴线的平面对称地布置，使得框架的平移运动将相对于平面以对称的方式改变喷嘴的横截面。 如果框架绕其枢轴附件旋转，则喷嘴挡板将被不对称地调节，并且可以用于对从喷嘴发出的气体的推力进行矢量化。
-
公开(公告)号：US4679982A
公开(公告)日：1987-07-14
申请号：US773226
申请日：1985-09-06
IPC分类号： F04D27/02
CPC分类号： F04D27/0215 , F04D27/023
摘要： A ring or other annular assembly is supported within a compressor casing by means of one or more resiliently deformable bodies of elastomeric material adhered between two rigid plates. One of the rigid plates is secured to the ring, the other to the compressor casing, and both plates are disposed parallel to the direction of movement of the ring. Preferably, the resiliently deformable body is made up of an alternating stack of the elastomeric plates and rigid plates adhered together, and parallel with the first two rigid plates which secured the body to the ring and the casing. A compressor of a gas turbine plant incorporates an antisurge blow-off valve mechanism in the form of a slot formed in the outer wall defining the flow path and an annular assembly movable axially of the plant to close and open the slot.
摘要翻译： 环或其它环形组件通过粘附在两个刚性板之间的一个或多个弹性体材料的弹性变形体支撑在压缩机壳体内。 一个刚性板被固定到环上，另一个固定到压缩机壳体，并且两个板平行于环的移动方向设置。 优选地，弹性变形体由弹性体板和粘合在一起的刚性板的交替堆叠构成，并且平行于将主体固定到环和壳体上的前两个刚性板。 燃气轮机设备的压缩机包括形成在限定流路的外壁中的狭槽形式的防喘振排气阀机构，以及可移动到工厂轴向以闭合和打开槽的环形组件。
-
公开(公告)号：US5593278A
公开(公告)日：1997-01-14
申请号：US568223
申请日：1983-12-30
申请人： Gerard E. A. Jourdain , Jean-Paul Lagrange , Gerard M. F. Mandet , Jacques H. Mouchel , Jean-Philippe E. Richard , Marcel R. Soligny
发明人： Gerard E. A. Jourdain , Jean-Paul Lagrange , Gerard M. F. Mandet , Jacques H. Mouchel , Jean-Philippe E. Richard , Marcel R. Soligny
CPC分类号： F01D11/18 , F01D25/246 , Y02T50/67 , Y02T50/671
摘要： The disclosed invention relates to a sealing device for the rotor blades of a gas turbine engine which permits real time adjustment to be made of the clearances between the rotor blade tips and the sealing structure. The sealing shroud around the turbine wheel is formed of sectors, each sector being attached to a monolithic short response time ring and a monolithic long response time ring. Ventilating air from upstream of the turbine wheel is directed onto the rings such that the sectors are caused to radially expand or contract in compliance with the expansion or contraction of the tips of the rotor blades during stabilized and transient engine operational modes. A small positive clearance between the sealing sectors and the blade tips is maintained throughout the range of the engine's operation.
摘要翻译： 所公开的本发明涉及一种用于燃气涡轮发动机的转子叶片的密封装置，其允许由转子叶片尖端和密封结构之间的间隙进行实时调节。 涡轮机轮周围的密封罩由扇形部分组成，每个扇形部分连接到单片短响应时间环和单片长响应时间环。 涡轮机叶轮上游的通风空气被引导到环上，使得在稳定和瞬态的发动机操作模式期间，这些扇区在转子叶片的尖端的膨胀或收缩下被引起径向膨胀或收缩。 在发动机运行的整个范围内，保持密封扇区和叶片尖端之间的小的正间隙。
-
-
-
-
-
-
-
-
-
搜索结果
26 条记录 (耗时 0.015 秒)
