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31.发明申请公开(公告)号：US20100028138A1
公开(公告)日：2010-02-04
申请号：US11778928
申请日：2007-07-17
IPC分类号： F04D29/58
CPC分类号： F02C7/18 , F01D5/046 , F02C3/08 , F05D2260/221 , Y02T50/675 , Y02T50/676
摘要： A system for ventilating a downstream cavity of an impeller of a centrifugal compressor in a turbomachine, this cavity being delimited by the downstream face of the impeller and by an annular end-piece of a diffuser and being ventilated by taking air from the outlet of the compressor, the system comprising at least one annular deflector mounted in this cavity in order to oppose the rise of hot air along the downstream face of the impeller and in order to cause the diverted hot air to be driven by the air taken from the outlet of the compressor.
摘要翻译： 一种用于使涡轮机中的离心压缩机的叶轮的下游空腔通风的系统，该空腔由叶轮的下游面和扩散器的环形端部限定，并且通过从 压缩机，所述系统包括安装在该空腔中的至少一个环形偏转器，以便抵抗沿着叶轮的下游面的热空气的上升，并且使得转向的热空气被从 压缩机。
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公开(公告)号：US20090202341A1
公开(公告)日：2009-08-13
申请号：US12333478
申请日：2008-12-12
申请人： Antoine Robert, Alain BRUNET , Claude CHOMEL , Sebastien JUSTE , Emmanuel HOURADOU , Dominique RAULIN , Frederic RENAULT , Julien SEDLAK
发明人： Antoine Robert, Alain BRUNET , Claude CHOMEL , Sebastien JUSTE , Emmanuel HOURADOU , Dominique RAULIN , Frederic RENAULT , Julien SEDLAK
CPC分类号： F01D11/18 , F01D17/105 , F01D25/145 , F01D25/246 , F02C6/08 , F04D29/522 , Y02T50/671 , Y02T50/675
摘要： The invention relates to a turbomachine module comprising a device to improve radial clearances, comprising an outer casing (22), an inner casing (21) and at least one shock absorbing ring (5) connecting the casings, the module also comprising an annular cavity (43) on the downstream side of the ring (5), with a passage (42) formed in it through which an airflow (4) is drawn off from the primary flow (Fp). According to the invention, the device to improve radial clearances comprises a thermal inertia control device for the shock absorbing ring mounted on the shock absorbing ring (5), downstream from it, this device comprising at least one coat of thermal insulation (8), and at least partly delimiting the annular cavity (43) on the downstream side of it (43).
摘要翻译： 本发明涉及一种包括改进径向间隙的装置的涡轮机模块，包括外壳（22），内壳（21）和连接壳体的至少一个减震环（5），所述模块还包括环形空腔 （5）的下游侧具有在其中形成有通道（42）的通道（43），通过该通道从气流（Fp）排出气流（4）。 根据本发明，用于改善径向间隙的装置包括安装在减震环（5）上的减震环的热惯性控制装置，在其下游，该装置包括至少一层隔热层（8）， 并且至少部分地限定其下游侧（43）上的环形空腔（43）。
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公开(公告)号：US20090155056A1
公开(公告)日：2009-06-18
申请号：US12332685
申请日：2008-12-11
IPC分类号： F01B25/00
CPC分类号： F04D29/545 , F04D27/0215
摘要： A turbomachine compressor, such as a high-pressure compressor, including air bleed means comprising a duct having a suction end opening out into an outer casing of the compressor level with a rotor wheel and a stator stage of the compressor, a screen sheet of annular shape being mounted radially inside the casing facing a portion of the suction end of the duct so as to make the bleeding of air uniform over 360° around the axis of the compressor.
摘要翻译： 一种涡轮机压缩机，例如高压压缩机，包括排气装置，其包括具有吸入端的管道，该吸入端与压缩机级的外壳开口，转子轮和压缩机的定子级，环形筛网 形状被径向地安装在壳体内面向管道的吸入端的一部分，以使空气的渗出在压缩机的轴线周围均匀地超过360°。
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34.发明授权Expansion device for oral reconstruction and method for the installation of the expansion device under a patient's gum in order to carry out oral reconstruction in cases of bone loss 失效用于口腔重建的扩张装置和用于在患者牙龈下安装扩张装置的方法，以便在骨丢失的情况下进行口腔重建
公开(公告)号：US5695338A
公开(公告)日：1997-12-09
申请号：US403805
申请日：1995-05-15
申请人： Antoine Robert
发明人： Antoine Robert
摘要： An expansion device for oral reconstruction formed by a closed pouch made of a film provided at one point with an additional thickness and a protective feature against being perforated right through, characterized in that the protective feature is a concave cover portion within the pouch and is positioned so as to be facing the additional thickness, bonded directly to each side of the additional thickness but not on its entire periphery.
摘要翻译： PCT No.PCT / FR93 / 00890 Sec。 371日期1995年5月15日 102（e）日期1995年5月15日PCT提交1993年9月15日PCT公布。 公开号WO94 / 06368 日期1994年3月31日一种用于口腔重建的膨胀装置，由封闭的小袋形成，该薄膜由一个具有附加厚度的膜提供，并具有防止穿透的保护特征，其特征在于，保护特征是凹形盖部分 并且被定位成面向附加的厚度，直接粘附在附加厚度的每一侧，而不是在其整个周边上。
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