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1. 发明授权

US07147434B2 Nozzle ring with adhesive bonded blading for aircraft engine compressor 有权
标题翻译：用于飞机发动机压缩机的带有粘合剂叶片的喷嘴环
公开(公告)号：US07147434B2
公开(公告)日：2006-12-12
申请号：US10876610
申请日：2004-06-28
申请人： Claude Marcel Mons , Sandra Andrieu , Manuel Girard , Francois Pierre Georges Maurice Ribassin
发明人： Claude Marcel Mons , Sandra Andrieu , Manuel Girard , Francois Pierre Georges Maurice Ribassin
IPC分类号： F01D9/04
CPC分类号： F04D29/023 , F01D9/042 , F04D29/542 , F05D2230/23 , F05D2300/434 , F05D2300/603 , Y02T50/672 , Y10T29/49323 , Y10T29/49885
摘要： Blades (3) extending radially from the inner shroud (1) to the outer shroud (2) are attached to the inner shroud by means of a sealing cement containing an organic polyimide-based polymer adhesive.
摘要翻译：从内护罩（1）向外护罩（2）径向延伸的刀片（3）通过含有有机聚酰亚胺基聚合物粘合剂的密封胶水附接到内护罩。

2. 发明授权

US07553130B1 Nozzle ring adhesive bonded blading for aircraft engine compressor 有权
标题翻译：用于飞机发动机压缩机的喷嘴环粘合叶片
公开(公告)号：US07553130B1
公开(公告)日：2009-06-30
申请号：US11523522
申请日：2006-09-20
申请人： Claude Marcel Mons , Sandra Andrieu , Manuel Girard , Francois Pierre Georges Maurice Ribassin
发明人： Claude Marcel Mons , Sandra Andrieu , Manuel Girard , Francois Pierre Georges Maurice Ribassin
IPC分类号： F01D9/04
CPC分类号： F04D29/023 , F01D9/042 , F04D29/542 , F05D2230/23 , F05D2300/434 , F05D2300/603 , Y02T50/672 , Y10T29/49323 , Y10T29/49885
摘要： A compressor nozzle ring for an aircraft includes an inner shroud, an outer shroud and a multiplicity of blades extending from the inner shroud to the outer shroud. Each blade passes through the inner shroud and is attached to it with sealing cement containing an organic polymer adhesive. The adhesive is polyimide based.
摘要翻译：用于飞行器的压缩机喷嘴环包括内护罩，外护罩和从内护罩延伸到外护罩的多个刀片。每个叶片穿过内部护罩，并用含有机聚合物粘合剂的密封胶水将其连接到其上。粘合剂是基于聚酰亚胺的。

3. 发明申请

US20090148283A1 NOZZLE RING ADHESIVE BONDED BLADING FOR AIRCRAFT ENGINE COMPRESSOR 有权
标题翻译：喷枪环胶机粘合叶片用于飞机发动机压缩机
公开(公告)号：US20090148283A1
公开(公告)日：2009-06-11
申请号：US11523522
申请日：2006-09-20
申请人： Claude Marcel Mons , Sandra Andrieu , Manuel Girard , Francois Pierre Ribassin
发明人： Claude Marcel Mons , Sandra Andrieu , Manuel Girard , Francois Pierre Ribassin
IPC分类号： F01D5/14
CPC分类号： F04D29/023 , F01D9/042 , F04D29/542 , F05D2230/23 , F05D2300/434 , F05D2300/603 , Y02T50/672 , Y10T29/49323 , Y10T29/49885
摘要： A compressor nozzle ring for an aircraft includes an inner shroud, an outer shroud and a multiplicity of blades extending from the inner shroud to the outer shroud. Each blade passes through the inner shroud and is attached to it with sealing cement containing an organic polymer adhesive. The adhesive is polyimide based.
摘要翻译：用于飞行器的压缩机喷嘴环包括内护罩，外护罩和从内护罩延伸到外护罩的多个刀片。每个叶片穿过内部护罩，并用含有机聚合物粘合剂的密封胶水将其连接到其上。粘合剂是基于聚酰亚胺的。

4. 发明申请

US20110211945A1 METHOD FOR THE MANUFACTURE OF A CIRCULAR REVOLUTION THERMOMECHANICAL PART INCLUDING A TITANIUM-BASED LOAD-BEARING SUBSTRATE LINED WITH STEEL OR SUPERALLOY, A TURBOMACHINE COMPRESSOR HOUSING WHICH IS RESISTANT TO TITANIUM FIRE OBTAINED ACCORDING TO THIS METHOD 审中-公开
标题翻译：用于制造包括以钢或超级合金为基础的基于钛铁的负载轴承衬底的圆形回火温度部件的方法，根据该方法获得的抵抗钛铁矿的涡轮压缩机壳体
公开(公告)号：US20110211945A1
公开(公告)日：2011-09-01
申请号：US13060719
申请日：2009-09-03
申请人： Laurent Ferrer , Claude Marcel Mons
发明人： Laurent Ferrer , Claude Marcel Mons
IPC分类号： F01D25/24 , B21D26/02
CPC分类号： B23P15/00 , B21D39/042 , B21J1/04 , B32B15/013 , F01D25/08 , F01D25/24 , F02C7/25 , F04D29/023 , F04D29/542 , F05D2230/232 , F05D2230/25 , F05D2230/26 , F05D2300/133 , F05D2300/171 , F05D2300/174 , F05D2300/175 , Y02T50/67 , Y02T50/671 , Y02T50/675
摘要： A method for manufacture of a compressor housing which is resistant to a titanium fire (burning titanium). An explosion cladding of a circular blank made of steel, or steel alloy, or superalloy which is incombustible in the presence of a titanium fire is accomplished on a circular blank made from titanium or titanium alloy.
摘要翻译：一种耐钛火（耐燃钛）的压缩机壳体的制造方法。在由钛或钛合金制成的圆形坯料上实现由钢或钢合金制成的圆形坯料的爆炸包层或在钛火存在下不可燃的超合金。

5. 发明授权

US07625176B2 Plain bearing between two parts which are movable with respect to each other 有权
标题翻译：两个部件之间的相对于彼此可移动的平面轴承
公开(公告)号：US07625176B2
公开(公告)日：2009-12-01
申请号：US11279822
申请日：2006-04-14
申请人： Christelle Foucher , Veronique Christiane Giffard , Claude Marcel Mons
发明人： Christelle Foucher , Veronique Christiane Giffard , Claude Marcel Mons
IPC分类号： F04D29/046 , B21D53/10 , F16C33/00
CPC分类号： F04D29/057 , F01D17/162 , F04D29/563 , F05D2230/41 , F05D2300/506 , F16C17/10 , F16C17/26 , F16C33/12 , F16C33/14 , F16C2204/60 , F16C2223/08 , F16C2360/23 , Y10T29/49707
摘要： The present invention relates to a plain bearing between two parts movable with respect to each other, the first part having a first bearing element made from a first metal and the second part having a second bearing element made from a second metal of higher hardness. The first bearing element has a surface layer hardened by strain hardening. As a result of the invention, the wear between the parts can be reduced and their life can be substantially lengthened. The invention can be advantageously applied to cases in which the first part is a variable-setting diffuser blade and the second part is a gas turbine casing.
摘要翻译：本发明涉及可相对于彼此移动的两个部件之间的滑动轴承，第一部件具有由第一金属制成的第一轴承元件，第二部件具有由较高硬度的第二金属制成的第二轴承元件。第一轴承元件具有通过应变硬化硬化的表面层。作为本发明的结果，可以减少部件之间的磨损，并且可以使其寿命显着延长。本发明可以有利地应用于第一部分是可变设定的扩散器叶片并且第二部分是燃气涡轮机壳体的情况。

6. 发明授权

US07597538B2 Thermostructural turbomachine part that is circularly symmetrical about a longitudinal axis, the part including an annular wiper, and a method of manufacture 有权
标题翻译：围绕纵向轴线圆形对称的热结构涡轮机部件，该部件包括环形刮水器，以及制造方法
公开(公告)号：US07597538B2
公开(公告)日：2009-10-06
申请号：US11560131
申请日：2006-11-15
申请人： Claude Marcel Mons , Joël Olivier Alfred Abel Vigneau
发明人： Claude Marcel Mons , Joël Olivier Alfred Abel Vigneau
IPC分类号： F01D11/02
CPC分类号： F16J15/453 , B22F3/1055 , B29C64/153 , B33Y10/00 , B33Y80/00 , F01D11/02 , F04D29/023 , F04D29/102 , F05D2230/31 , F05D2260/95 , F05D2300/611 , F16J15/445 , F16J15/4472 , Y02P10/295 , Y02T50/67
摘要： In the method, a support is provided that presents a base for an annular wiper, and a wiper is built up that presents height that varies around its circumference, by forming a plurality of projecting portions by performing following successive steps: a laser source connected to an optical head focused on a point on the top surface of the base is activated, as is a source of powder connected to the spray nozzle, thereby forming a localized melt at said point, into which the powder is injected, thus forming a localized region of extra thickness; and the optical head and the nozzle are aimed at another point adjacent to said region of extra thickness and the method returns to the preceding step until the layer of material is completed in the angular sector in question.
摘要翻译：在该方法中，提供了一种用于环形刮水器的基座的支撑件，并且通过执行以下连续步骤形成多个突起部分，构建了提供围绕其圆周变化的高度的擦拭器：激光源连接到聚焦在基座的顶表面上的点上的光学头被激活，连接到喷嘴的粉末源也是如此，从而在所述点处形成局部熔体，粉末被注入到其中，从而形成局部区域额外的厚度; 并且光学头和喷嘴瞄准在与所述额外厚度的区域相邻的另一点上，并且该方法返回到前面的步骤，直到材料层在所讨论的角度扇区中完成。

7. 发明申请

US20090185768A1 TURBOMACHINE SHAFT GUIDANCE 有权
标题翻译： TURBOMACHINE SHAFT指导
公开(公告)号：US20090185768A1
公开(公告)日：2009-07-23
申请号：US12357045
申请日：2009-01-21
申请人： Claude Marcel Mons , Laurent Raberin , Jean-Marc Rongvaux , Stephane Rousselin
发明人： Claude Marcel Mons , Laurent Raberin , Jean-Marc Rongvaux , Stephane Rousselin
IPC分类号： F16C27/02
CPC分类号： F01D21/045 , F01D25/164 , F05D2300/505 , F16C19/06 , F16C27/04 , F16C2360/23
摘要： A support for a bearing that guides a shaft in a turbomachine, comprising an annular part made of a shape memory material which retains an initial shape when the load applied to it remains below a threshold value and which deforms, absorbing energy when the applied load becomes at least equal to the threshold value, this annular part being capable of reverting at least approximately to its initial shape when the applied load drops back below the threshold value.
摘要翻译：一种用于在涡轮机中引导轴的轴承的支撑件，包括由形状记忆材料制成的环形部件，当施加到其上的载荷保持初始形状时，其保持低于阈值并且在施加的载荷变为时变形时吸收能量至少等于阈值，当所施加的载荷下降到低于阈值时，该环形部分能够至少近似地恢复到其初始形状。

8. 发明授权

US07448280B2 Method for evaluating the fatigue strength of welded joints 有权
标题翻译：评估焊接接头疲劳强度的方法
公开(公告)号：US07448280B2
公开(公告)日：2008-11-11
申请号：US11833628
申请日：2007-08-03
申请人： Claude Marcel Mons
发明人： Claude Marcel Mons
IPC分类号： G01N3/20
CPC分类号： B23K26/34 , B23K26/32 , B23K31/12 , B23K2103/14 , G01N3/00 , G01N2203/0005 , G01N2203/0066 , G01N2203/0067 , G01N2203/0073
摘要： Method for evaluating the fatigue strength of welded joints produced by melting an alloy using a specified welding technique, which method comprises the following steps: a statistically significant number N of specimens are produced with a welded joint using said welding technique; each of the specimens is subjected to cyclic fatigue tests, with an alternating stress a, until failure; the size of the relevant defect appearing in the fracture plane of the specimens is measured by fractography; a range of defect dimensions for which the probability of measuring by fractography a defect outside the range is less than a predetermined level of probability t is determined from the measured sizes; and the lowest stress σmin liable to cause the specimen to fail with a level of probability t is determined from this range.
摘要翻译：用于通过使用规定的焊接技术对合金进行熔融而得到的焊接接头的疲劳强度进行评价的方法，该方法包括以下步骤：使用所述焊接技术，用焊接接头制造统计学上显着的N个试样; 每个样品进行循环疲劳试验，交替应力a，直到失效; 通过断面测量样品断裂面出现的相关缺陷的大小; 根据测量的尺寸确定通过断层图测量范围之外的缺陷小于预定的概率水平t的缺陷尺寸范围; 并且从该范围确定易于导致样品以概率t水平故障的最低应力σσmin 。

9. 发明授权

US08888448B2 Method for the manufacture of a circular revolution thermomechanical part including a titanium-based load-bearing substrate lined with steel or superalloy, a turbomachine compressor housing which is resistant to titanium fire obtained according to this method 有权
标题翻译：用于制造圆形回转热机械部件的方法，该部件包括衬有钢或超合金的钛基承载基底，根据该方法获得耐钛火的涡轮机压缩机壳体
公开(公告)号：US08888448B2
公开(公告)日：2014-11-18
申请号：US13060748
申请日：2009-09-03
申请人： Laurent Ferrer , Claude Marcel Mons
发明人： Laurent Ferrer , Claude Marcel Mons
IPC分类号： F01D25/24 , F04D29/52 , F04D29/02 , F01D25/08 , B21K3/00 , B32B15/01 , B23P15/00 , F02C7/25 , B21D26/051
CPC分类号： B23P15/00 , B21D26/051 , B21K3/00 , B32B15/013 , F01D25/08 , F01D25/24 , F02C7/25 , F04D29/023 , F04D29/526 , F05D2230/23 , F05D2230/25 , F05D2230/26 , F05D2300/133 , F05D2300/171 , F05D2300/174 , F05D2300/175 , Y02T50/67 , Y02T50/671 , Y02T50/675 , Y10T29/49636 , Y10T29/49805
摘要： A method for manufacture of a compressor housing which is resistant to a titanium fire (burning titanium). A circular blank made of steel, or steel alloy, or superalloy which is incombustible in the presence of a titanium fire is hydroformed against a circular blank made from titanium or titanium alloy.
摘要翻译：一种耐钛火（耐燃钛）的压缩机壳体的制造方法。由钛或钛合金制成的圆形坯料对由钢或钢合金制成的圆形坯料或在钛火存在下不可燃的超耐热合金进行加氢成形。

10. 发明授权

US08881395B2 Method for increasing the coefficient of adhesion between two parts rotating as one with a rotor 有权
标题翻译：增加两个与转子一体旋转的部件之间的粘合系数的方法
公开(公告)号：US08881395B2
公开(公告)日：2014-11-11
申请号：US13055576
申请日：2009-05-13
申请人： Vincent Dessoly , Claude Marcel Mons , Ana Carmen Viguera Sancho
发明人： Vincent Dessoly , Claude Marcel Mons , Ana Carmen Viguera Sancho
IPC分类号： B21K25/00 , F16D1/033 , F01D5/06
CPC分类号： F16D1/033 , F01D5/066 , F05D2230/313 , F05D2230/90 , F05D2250/60 , F05D2250/61 , F05D2250/611 , F05D2300/133 , F05D2300/506 , F16D2300/10 , Y10T29/4932 , Y10T29/49885
摘要： A method for increasing the coefficient of adhesion between two parts that rotate as one with a rotor, for example a turbomachine rotor, those parts pressing against one another via pressing faces. The method includes milling at least one of the pressing faces so as to modify its surface finish and increase its roughness, then covering the or each machined face with a thin layer of a material that is hard and has a high coefficient of friction.
摘要翻译：一种用于增加与转子（例如涡轮机转子）一体旋转的两个部件之间的粘合系数的方法，这些部件通过按压面彼此压靠。该方法包括铣削至少一个按压面以便改变其表面光洁度并增加其粗糙度，然后用难以且具有高摩擦系数的材料的薄层覆盖或每个机加工面。

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