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1. 发明授权

EP2906467B1 HELICE COMPORTANT UNE ECOPE DYNAMIQUE MOBILE 无效转让
标题翻译：用便携式动态铲PROPELLER
公开(公告)号：EP2906467B1
公开(公告)日：2016-08-24
申请号：EP13786687.7
申请日：2013-10-08
申请人： SNECMA
发明人： CHARTIER, Sarah , FABRE, Adrien, Jacques, Philippe , IGEL, Dominik , JACQUEMARD, Christophe , TAJAN, Sébastien
IPC分类号： B64C11/06 , F01D5/08
CPC分类号： F01D5/081 , B64C11/06 , B64D2027/005 , F01D5/3007 , F01D7/00 , F05D2220/30 , F05D2260/20 , Y02T50/66 , Y02T50/672 , Y02T50/673 , Y02T50/676

2. 发明公开

EP3010799A1 PIVOT DE PALE D'HELICE AERIENNE EN FORME DE CALOTTE SPHERIQUE 有权转让
标题翻译：接头，用于中一球冠形螺旋桨叶片
公开(公告)号：EP3010799A1
公开(公告)日：2016-04-27
申请号：EP14735616.6
申请日：2014-06-12
申请人： SNECMA
发明人： TAJAN, Sébastien , FABRE, Adrien, Jacques, Philippe , JACQUEMARD, Christophe , LAURENCEAU, Adrien
IPC分类号： B64C11/34 , F04D29/36
CPC分类号： B64C11/346 , B64C11/06 , B64D2027/005 , F04D29/323 , F04D29/366 , Y02T50/66
摘要： The invention relates to a pivot (30) for an air propeller blade, comprising a rotary support (36) which is to be radially mounted on a propeller hub while being able to pivot about a pivoting axis (Z), a blade support (38) comprising a housing (40) for receiving a blade root, and at least one arm (34a, 34b) extending laterally in relation to the pivoting axis and carrying a balance weight (32) forming a counterweight, the arm and the balance weight having a general geometric form of a spherical cap.

3. 发明授权

EP2324205B1 DISPOSITIF AMORTISSEUR DE VIBRATIONS POUR ATTACHES D'AUBES DE TURBOMACHINE, TURBOMACHINE ET MOTEURS ASSOCIES 有权转让
标题翻译： VIBRATIONSDÄMPFERFOR TURBOMASCHINEN铲文章，叶轮机相关及相关MOTORS
公开(公告)号：EP2324205B1
公开(公告)日：2012-03-21
申请号：EP09804573.5
申请日：2009-08-05
申请人： Snecma
发明人： FABRE, Adrien, Jacques, Philippe
IPC分类号： F01D5/30 , F04D29/32
CPC分类号： F01D5/3092 , F01D5/3007 , F04D29/322 , F05D2300/43 , F05D2300/501 , F05D2300/603 , F05D2300/702 , Y02T50/67 , Y02T50/672 , Y02T50/673
摘要： The present invention relates to a vibration-damping device for a turbomachine blade provided with a blade root (6) which is able to be inserted into a pocket (2) of a carrier disk (1) of a bladed wheel, said device being able to be positioned between said blade root and a retaining wall (14a, 14b) of said pocket. Said device comprises at least one shim (7) consisting of an assembly of layers of rigid materials (8, 10) and of viscoelastic materials (9), and comprising two portions, each forming a lateral branch (7a, 7b) which can be inserted along one of the two retaining walls (14a, 14b), the two lateral branches being connected to one another, so as to constitute a single part, by a third portion forming a shim bottom (7c) of rigid material. It is characterized in that at least one layer of viscoelastic material is positioned between two layers of rigid materials (8, 10).

4. 发明授权

EP3019398B1 PALE D'HÉLICE COMPOSITE POUR AÉRONEF 有权转让
标题翻译：用于飞机的复合螺旋桨叶片
公开(公告)号：EP3019398B1
公开(公告)日：2018-03-28
申请号：EP14742277.8
申请日：2014-06-25
申请人： Snecma
发明人： LAURENCEAU, Adrien , FABRE, Adrien, Jacques, Philippe , GIMAT, Matthieu
IPC分类号： B64C11/26 , B29D99/00
CPC分类号： B64C11/26 , B29C70/24 , B29C70/48 , B29D99/0025 , B29K2063/00 , B29K2105/253 , B29K2307/04 , B29K2715/00 , B29L2031/082 , D03D25/005 , Y02T50/43

5. 发明公开

EP2324205A1 DISPOSITIF AMORTISSEUR DE VIBRATIONS POUR ATTACHES D'AUBES DE TURBOMACHINE, TURBOMACHINE ET MOTEURS ASSOCIES 有权转让
标题翻译： VIBRATIONSDÄMPFERFOR TURBOMASCHINEN铲文章，叶轮机相关及相关MOTORS
公开(公告)号：EP2324205A1
公开(公告)日：2011-05-25
申请号：EP09804573.5
申请日：2009-08-05
申请人： Snecma
发明人： FABRE, Adrien, Jacques, Philippe
IPC分类号： F01D5/30 , F04D29/32
CPC分类号： F01D5/3092 , F01D5/3007 , F04D29/322 , F05D2300/43 , F05D2300/501 , F05D2300/603 , F05D2300/702 , Y02T50/67 , Y02T50/672 , Y02T50/673
摘要： The present invention relates to a vibration-damping device for a turbomachine blade provided with a blade root (6) which is able to be inserted into a pocket (2) of a carrier disk (1) of a bladed wheel, said device being able to be positioned between said blade root and a retaining wall (14a, 14b) of said pocket. Said device comprises at least one shim (7) consisting of an assembly of layers of rigid materials (8, 10) and of viscoelastic materials (9), and comprising two portions, each forming a lateral branch (7a, 7b) which can be inserted along one of the two retaining walls (14a, 14b), the two lateral branches being connected to one another, so as to constitute a single part, by a third portion forming a shim bottom (7c) of rigid material. It is characterized in that at least one layer of viscoelastic material is positioned between two layers of rigid materials (8, 10).

6. 发明公开

EP2300317A1 DISPOSITIF D'ATTACHE D'UNE PALE A CALAGE VARIABLE 有权转让
标题翻译：装置用于固定叶片可变调节
公开(公告)号：EP2300317A1
公开(公告)日：2011-03-30
申请号：EP09797512.2
申请日：2009-07-16
申请人： Snecma
发明人： DAO, Daniel , FABRE, Adrien, Jacques, Philippe , MADEC, Alain, Paul
IPC分类号： B64C11/06
CPC分类号： B64C11/06
摘要： The invention relates to a device for attaching a blade that includes a ferrule (28) mounted about an outer collar (23) of the pivot (15) of the blade (27), and capable of rotating by a sufficient angle so that cleats (30, 31) can close the ends of the pivot notch and maintain therein the base of the blade (27), as well as mobile wedges that facilitate the maintaining of the base in place within the notch. The invention can be used in aircraft machines.

7. 发明授权

EP2300317B1 DISPOSITIF D'ATTACHE D'UNE PALE A CALAGE VARIABLE 有权转让
标题翻译：装置用于固定叶片可变调节
公开(公告)号：EP2300317B1
公开(公告)日：2011-11-09
申请号：EP09797512.2
申请日：2009-07-16
申请人： Snecma
发明人： DAO, Daniel , FABRE, Adrien, Jacques, Philippe , MADEC, Alain, Paul
IPC分类号： B64C11/06
CPC分类号： B64C11/06
摘要： The invention relates to a device for attaching a blade that includes a ferrule (28) mounted about an outer collar (23) of the pivot (15) of the blade (27), and capable of rotating by a sufficient angle so that cleats (30, 31) can close the ends of the pivot notch and maintain therein the base of the blade (27), as well as mobile wedges that facilitate the maintaining of the base in place within the notch. The invention can be used in aircraft machines.

8. 发明公开

EP2555973A1 HÉLICE NON CARÉNÉE POUR TURBOMACHINE 有权转让
标题翻译：不能掩饰转子的燃气涡轮机
公开(公告)号：EP2555973A1
公开(公告)日：2013-02-13
申请号：EP11718449.9
申请日：2011-04-01
申请人： Snecma
发明人： BOURU, Michel, André , FABRE, Adrien, Jacques, Philippe , JABLONSKI, Laurent , MAHIEU, Jean-Noël
IPC分类号： B64C11/06
CPC分类号： F04D29/056 , B64C11/06 , B64D2027/026 , Y02T50/66
摘要： Unshrouded fan with variable-pitch blades the roots (38) of which are each fitted from the outside into a radial housing of an annular rotor element and guided in rotation about their axis by two rolling bearings (76, 94), one of which is borne by an annular segment (54) with cylindrical skirt (56) mounted in a groove (50) of the cylindrical body (40) and by a locking nut (64) screwed onto the cylindrical skirt (56). Said bearing (94) is externally capped by a ring (100) that has external dog teeth (108) engaging with internal dog teeth (112) of the housing to provide axial retention for the ring (100) in the housing. Locking means inserted between the teeth (112) of the housing and those of the ring (100) prevent the ring (100) from turning or from being removed axially from the housing.

9. 发明公开

EP3019398A1 PALE D'HÉLICE COMPOSITE POUR AÉRONEF 有权转让
标题翻译： VERBUNDPROPELLERBLATTFÜREIN FLUGZEUG
公开(公告)号：EP3019398A1
公开(公告)日：2016-05-18
申请号：EP14742277.8
申请日：2014-06-25
申请人： Snecma
发明人： LAURENCEAU, Adrien , FABRE, Adrien, Jacques, Philippe , GIMAT, Matthieu
IPC分类号： B64C11/26 , B29D99/00
CPC分类号： B64C11/26 , B29C70/24 , B29C70/48 , B29D99/0025 , B29K2063/00 , B29K2105/253 , B29K2307/04 , B29K2715/00 , B29L2031/082 , D03D25/005 , Y02T50/43
摘要： The invention relates to an aircraft propeller blade including a structure having an airfoil, consisting of at least one fibrous reinforcement (200) obtained by three-dimensional weaving of threads and made denser by a matrix and a spar (60) including a bulged portion (62) extending outside of the fibrous reinforcement and forming the shank of the blade, and a shaped portion (61) in a recess (206) provided within the fibrous reinforcement (200). The fibrous reinforcement (200) comprises a disconnection area (204) forming the recess (206) inside the fibrous reinforcement (200). The disconnection area (204) leads to the lower portion (220) and the rear edge (230) of the fibrous reinforcement (200) such as to form an opening (231) for inserting the shaped portion (61) of the spar (60) into the recess (206) of the fibrous reinforcement. The opening (231) on the rear edge (230) of the fibrous reinforcement (200) extends over a height (H231) that is shorter than the height (H204) of the recess such as to provide, on said rear edge (230), a retaining portion (232) that is at least partially in contact with the shaped portion (61) of the spar (60).
摘要翻译：一种飞机螺旋桨叶片，包括由至少一片纤维增强材料构成的流线型结构，所述至少一片纤维增强材料通过三维织造纱线并由基体致密化，以及包括延伸到纤维增强件外部并形成叶片根部的扩大部分的翼梁以及存在于布置在纤维增强件内部的壳体中的成形部。纤维增强件包括在纤维增强件内部形成壳体的非互连区域。非互连区域开放到纤维增强件的底部部分和后边缘中，以形成用于将翼梁的成形部分插入纤维增强件的壳体中的开口。存在于纤维增强件的后边缘中的开口在比壳体的高度小的高度上延伸。

10. 发明公开

EP2906467A1 HELICE COMPORTANT UNE ECOPE DYNAMIQUE MOBILE 无效转让
标题翻译：用便携式动态铲PROPELLER
公开(公告)号：EP2906467A1
公开(公告)日：2015-08-19
申请号：EP13786687.7
申请日：2013-10-08
申请人： SNECMA
发明人： CHARTIER, Sarah , FABRE, Adrien, Jacques, Philippe , IGEL, Dominik , JACQUEMARD, Christophe , TAJAN, Sébastien
IPC分类号： B64C11/06 , F01D5/08
CPC分类号： F01D5/081 , B64C11/06 , B64D2027/005 , F01D5/3007 , F01D7/00 , F05D2220/30 , F05D2260/20 , Y02T50/66 , Y02T50/672 , Y02T50/673 , Y02T50/676
摘要： The main subject matter of the invention is a propeller (32) for a turbomachine (1) comprising a plurality of blades (48) and a blade support ring (47) provided with housings (50) each receiving a pivot (52) carrying the root (58) of one of said blades (48), characterised in that at least one of the pivots (52) is combined with at least one dynamic scoop (100), which is designed to be movable between an open position for capturing a cooling air flow (F), and a different closed position, on the basis of the orientation of the corresponding blade (48).

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