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1.发明授权Turbo aero engine equipped with means facilitating adjustment of plays of the stator and between the stator and rotor 失效涡轮喷气发动机配备有便于调整定子和定子与转子之间的作用的装置
公开(公告)号：US5288206A
公开(公告)日：1994-02-22
申请号：US974899
申请日：1992-11-12
申请人： Alain M. L. Bromann , Jean-Louis Charbonnel , Pierre Debeneix , Daniel J. Marey , Jacky Naudet , Thierry J. M. Niclot , Yann J. M. Rigaud
发明人： Alain M. L. Bromann , Jean-Louis Charbonnel , Pierre Debeneix , Daniel J. Marey , Jacky Naudet , Thierry J. M. Niclot , Yann J. M. Rigaud
CPC分类号： F01D11/24 , F01D25/246 , F01D25/26 , F05D2240/11
摘要： A turbjet engine includes various elements for adjustment of play of the stator by having the stator heated or cooled by a gas. The outer housing to which the ferrule bearing the fixed vane stages is secured may be formed of two skins between which the gas is injected. The ferrule may be composed of sectors extending over one circumference fraction and fixed via their center and simply guided at their extremity; finally, it is possible to provide sealing devices between the outer housing and the support bearing surfaces of the ribs of the ferrule elements. The volume between the ferrule and the housing is then sectioned and is able to receive separate gas feedings for play adjustment.
摘要翻译： 涡轮喷气发动机包括通过使定子被气体加热或冷却来调节定子的游隙的各种元件。 固定有固定叶片级的套圈的外壳可由两个外壳形成，气体被注入。 套管可以由在一个圆周分数上延伸并且经由它们的中心固定的部分组成，并且在其末端简单地被引导; 最后，可以在外壳和套圈元件的肋的支撑承载表面之间提供密封装置。 然后，套圈和壳体之间的体积被分段，并且能够接收用于游戏调节的单独的气体供给。
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2.发明授权Turbomachine stator having a double skin casing including means for preventing gas flow longitudinally therethrough 失效涡轮机定子，其具有双皮肤外壳，包括用于防止气体纵向流过其中的装置
公开(公告)号：US5320484A
公开(公告)日：1994-06-14
申请号：US055068
申请日：1993-04-29
申请人： Jean-Louis Charbonnel , Pierre Debeneix , Christopher C. Glynn , Daniel J. Marey , Jean-Pierre A. J. Mourlan , Jacky S. Naudet , Gerard Receveur , Yann J. M. Rigaud , Roger C. Walker
发明人： Jean-Louis Charbonnel , Pierre Debeneix , Christopher C. Glynn , Daniel J. Marey , Jean-Pierre A. J. Mourlan , Jacky S. Naudet , Gerard Receveur , Yann J. M. Rigaud , Roger C. Walker
CPC分类号： F01D25/26 , F01D11/005
摘要： A turboshaft engine in which the stator comprises an outer casing surrounding a ring formed by a number of ring elements each having an apertured rib which spaces the element from the casing, the ribs dividing the space between the casing and the ring into separate compartments, and each rib having a sealing element disposed alongside it to cover the apertures and seal one compartment from the next. The casing and the ring are fixed together by virtue of bolts which have their axes inclined to the radial direction so that tightening the bolts causes the casing to press radially on the sealing elements at the same time as pressing them axially against the respective ribs.
摘要翻译： 一种涡轮轴发动机，其中定子包括围绕由多个环形元件形成的环的外壳，每个环形元件具有将元件与壳体隔开的多孔肋，将外壳和环之间的空间分隔成独立的隔间， 每个肋具有密封元件，沿着密封元件设置以覆盖孔并将一个隔室与下一个隔室密封。 壳体和环通过螺栓固定在一起，该螺栓的轴线相对于径向方向倾斜，使得紧固螺栓使得壳体在密封元件上径向挤压，同时将其按压在相应的肋上。
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公开(公告)号：US06918745B2
公开(公告)日：2005-07-19
申请号：US10451626
申请日：2002-01-03
CPC分类号： F01D9/044 , F01D25/246 , F04D29/542
摘要： The invention relates to an axial compressor stator for a gas turbine, the stator having a rigid, external, annular frame and axially juxtaposed rings configured within the frame and bearing annuli of stationary vanes. The rings are defined by arcuate segments affixed to the frame. The inside walls of the arcuate segments externally define the aerodynamic conduit for the compressed gaseous fluid. The arcuate segments are brazed segments that include a honeycomb component sandwiched between an inner sheetmetal bounding the aerodynamic conduit and an outer sheetmetal. The outer sheetmetal solely connects the arcuate segments to the frame.
摘要翻译： 本发明涉及一种用于燃气轮机的轴向压缩机定子，该定子具有刚性的外部环形框架和轴向并置的环，该环构造在框架内并具有静止叶片的环形空间。 环由固定在框架上的弧形段限定。 弧形段的内壁外部限定用于压缩气态流体的空气动力学导管。 弧形段是钎焊段，其包括夹在界定空气动力学管道的内部金属板和外部金属板之间的蜂窝构件。 外部金属板单独将弓形段连接到框架。
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公开(公告)号：US20050008477A1
公开(公告)日：2005-01-13
申请号：US10838295
申请日：2004-05-05
IPC分类号： F02C7/042 , F01D17/16 , F04D29/56 , F16C19/30 , F16C19/32 , F16C19/54 , F16C25/08 , F16C33/36 , F04D15/00
CPC分类号： F16C19/54 , F01D17/16 , F01D17/162 , F04D29/563 , F16C19/30
摘要： A guide device for guiding a variable-pitch blade, in particular in a turbomachine compressor, the blade having a pivot formed by a cylindrical axial shank (6) mounted in a cylindrical housing (10) of a casing and pivotally guided about an axis in said housing by bearings, the device being characterized in that said bearings are abutment bearings (14, 15) with conical rollers (17), the axes of the rollers being substantially perpendicular to the pivot axis of the blade.
摘要翻译： 引导装置，用于引导可变桨距叶片，特别是在涡轮机压缩机中，所述叶片具有由安装在壳体的圆柱形壳体（10）中的圆柱形轴向轴（6）形成的枢轴，并绕轴线 所述装置的特征在于，所述轴承是具有锥形辊（17）的邻接轴承（14,15），所述辊的轴线基本上垂直于所述叶片的枢转轴线。
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5.发明授权公开(公告)号：US07112041B2
公开(公告)日：2006-09-26
申请号：US10885778
申请日：2004-07-08
申请人： Pierre Debeneix , Arnaud Langlois , Erick Boston , Alain Leman , Vincent Garnier , Jacques Audet
发明人： Pierre Debeneix , Arnaud Langlois , Erick Boston , Alain Leman , Vincent Garnier , Jacques Audet
IPC分类号： F01D17/16
CPC分类号： F01D17/162
摘要： A device for guiding pivoting of variable-pitch vanes in a turbomachine, each vane having a pivot formed by a cylindrical axial shank which is guided in a cylindrical chimney of the casing and in a cylindrical orifice of a stationary element which surrounds the outside of the casing and which is centered and fixed relative thereto. The invention improves pivotal guidance of variable-pitch vanes.
摘要翻译： 用于引导涡轮机中的可变节流叶片的枢转的装置，每个叶片具有由圆柱形轴向轴构成的枢轴，所述枢轴在壳体的圆柱形烟囱中被引导并且围绕在壳体外部的固定元件的圆柱形孔中 并且相对于其而居中和固定。 本发明改进了可变节距叶片的枢纽指导。
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6.发明申请公开(公告)号：US20050042079A1
公开(公告)日：2005-02-24
申请号：US10885778
申请日：2004-07-08
申请人： Pierre Debeneix , Arnaud Langlois , Erick Boston , Frederic Leman , Vincent Garnier , Jacques Audet
发明人： Pierre Debeneix , Arnaud Langlois , Erick Boston , Frederic Leman , Vincent Garnier , Jacques Audet
CPC分类号： F01D17/162
摘要： A device for guiding pivoting of variable-pitch vanes in a turbomachine, each vane having a pivot formed by a cylindrical axial shank which is guided in a cylindrical chimney of the casing and in a cylindrical orifice of a stationary element which surrounds the outside of the casing and which is centered and fixed relative thereto. The invention improves pivotal guidance of variable-pitch vanes.
摘要翻译： 用于引导涡轮机中的可变节流叶片的枢转的装置，每个叶片具有由圆柱形轴向轴构成的枢轴，所述枢轴在壳体的圆柱形烟囱中被引导并且围绕在壳体外部的固定元件的圆柱形孔中 并且相对于其而居中和固定。 本发明改进了可变节距叶片的枢纽指导。
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公开(公告)号：US06575697B1
公开(公告)日：2003-06-10
申请号：US09868902
申请日：2001-10-17
申请人： Jean-Baptiste Arilla , Sylvie Coulon , Pierre Debeneix , Florence Irène Noëlle Leutard , Paul Rodrigues , Patrice Jean Marc Rosset
发明人： Jean-Baptiste Arilla , Sylvie Coulon , Pierre Debeneix , Florence Irène Noëlle Leutard , Paul Rodrigues , Patrice Jean Marc Rosset
IPC分类号： F01D1108
CPC分类号： F01D11/08 , F01D11/005 , F01D25/246
摘要： A joint between a turbine ring. The ring is jointed to a spacer of the turbine by a joint including hooks which fit together on one side, and an abutment of flanges as well as a mortise and tenon joint on the other side. According to the joint, the tenon and mortise are separated from the flanges in abutment to limit the plays in the axial direction, produced by design or by expansions, to increase mechanical strength and simplify manufacturing.
摘要翻译： 涡轮环之间的接头。 环通过包括在一侧配合的钩的接头以及在另一侧上的法兰以及榫接头和榫头接头的接头连接到涡轮的间隔件。 根据接头，榫头和榫眼与法兰的邻接分离，限制了设计或扩展产生的轴向作用，增加机械强度，简化制造。
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公开(公告)号：US5259183A
公开(公告)日：1993-11-09
申请号：US899909
申请日：1992-06-17
申请人： Pierre Debeneix
发明人： Pierre Debeneix
CPC分类号： B64D27/18 , B64D27/26 , F02C7/20 , B64D2027/268 , F05D2230/642
摘要： The exhaust casing of a turbojet engine has a polygonal cross-section and carries at least three hanging lugs provided with holes designed to receive fixing axles of a rear suspension structure for the engine. The axes of these holes are situated at vertices of the polygon defined by the cross-section of the casing, and this polygon is regular except at the position of each of the hanging lugs, where it is deformed to displace the respective vertex radially outward.
摘要翻译： 涡轮喷气发动机的排气外壳具有多边形横截面并且承载至少三个悬挂凸耳，其设置有用于接收用于发动机的后悬架结构的固定轴的孔。 这些孔的轴线位于由壳体的横截面限定的多边形的顶点处，并且该多边形是规则的，除了在每个悬挂凸耳的位置处，其被变形以使各顶点径向向外移位。
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9.发明授权
公开(公告)号：US4373421A
公开(公告)日：1983-02-15
申请号：US187069
申请日：1980-09-15
摘要： An emergency aerosol lubrication device, particularly for airborne engines which includes a mechanism for placing a certain quantity of oil in reserve, an operator-controlled mechanism for atomizing oil in an aerosol container, which is connected to the points to be lubricated, a member for supplying the atomization mechanism with oil drawn from the reserve, and a mechanism for keeping the reserve oil at a suitable temperature.
摘要翻译： 一种紧急气溶胶润滑装置，特别是用于机载发动机的紧急气溶胶润滑装置，其包括用于将一定量的油放置在储备中的机构，用于雾化与待润滑点相连的气溶胶容器中的油的操作者控制机构，用于 向雾化机构供给从储备中抽出的油，以及将储备油保持在合适温度的机构。
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10.发明授权Device for blocking a ring for axially retaining a blade, associated rotor disk and retaining ring, and rotor and aircraft engine comprising them 有权用于阻挡用于轴向保持叶片，相关联的转子盘和保持环的环以及包括它们的转子和飞机发动机的装置公开(公告)号：US07290988B2
公开(公告)日：2007-11-06
申请号：US11466987
申请日：2006-08-24
IPC分类号： F01D5/30
CPC分类号： F01D5/3015 , F01D5/326 , F01D11/006 , F05D2230/64 , F05D2260/30
摘要： A device for rotationally blocking a retaining ring (20) on a rotor disk (10) includes successive first (162, 262) and second (164, 264) blocking hooks of the disk (10), at least one cleat (302, 304, 306) of the retaining ring (20) arranged close to a split (24) in the ring (20). The position of the at least one cleat (302, 304, 306) on the retaining ring (20) is such that, when the retaining ring (20) is in place in a groove (22) situated in the rotor disk (10), the at least one cleat (302, 304, 306) is in abutment against the first blocking hook (162, 262), and the split (24) is covered by the second blocking hook (164, 264).
摘要翻译： 用于旋转地阻挡转子盘（10）上的保持环（20）的装置包括盘（10）的连续的第一（162,262）和第二（164,264）阻挡钩，至少一个防滑钉（302,304） ，所述保持环（20）的靠近所述环（20）中的分割（24）的位置，306。 所述保持环（20）上的所述至少一个防滑板（302,304,306）的位置使得当所述保持环（20）位于转子盘（10）中的凹槽（22）中时， 所述至少一个防滑钉（302,304,306）与所述第一阻挡钩（162,262）抵接，并且所述裂口（24）被所述第二阻挡钩（164,264）覆盖。
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