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公开(公告)号：US11299989B2
公开(公告)日：2022-04-12
申请号：US16965845
申请日：2019-01-29
摘要： The invention relates to an assembly (1) for a turbine of a turbomachine, comprising: a first rotor disk (20a), a second rotor disk (20b), a part forming a mobile ring (28), comprising a system for preventing rotation of the mobile ring (28) relative to the rotor disks (20a, 20b), said system comprising: a rotor disk securing flange (222) having a plurality of teeth (224) that are distributed circumferentially about the turbomachine longitudinal axis (X-X), and a mobile ring securing flange (282) having a plurality of lugs (284) that are distributed circumferentially about the turbomachine longitudinal axis (X-X), the engagement of the rotor disk securing flange (222) with the mobile ring securing flange (282) ensuring, by means of the teeth (224) and the lugs (284), that the mobile ring (28) does not rotate relative to the rotor disks (20a, 20b).
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公开(公告)号：US11879347B2
公开(公告)日：2024-01-23
申请号：US17919184
申请日：2021-04-13
发明人： Benoit Guillaume Silet , Stéphane Pierre Guillaume Blanchard , Fabien Stéphane Garnier , Thibaud Louis Zaia
CPC分类号： F01D25/14 , F01D25/12 , F05D2260/60
摘要： A turbomachine turbine casing that extend around an axis and includes an annular wall and a cooling device. The annular wall is provided with a casing hook which extends in radial protrusion from an inside of the annular wall. The casing hook allows a mounting, on the turbomachine turbine casing, of ring segments disposed circumferentially end to end around the axis. The cooling device includes a collector duct intended to convey cooling air, the collector duct extending circumferentially around the annular wall. The collector duct has a cooling air inlet and a cooling air outlet. The collector duct and the annular wall have a common portion, which delimits the collector duct and from which the corresponding casing hook extends.
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3.发明授权公开(公告)号：US11753958B2
公开(公告)日：2023-09-12
申请号：US17633834
申请日：2020-08-06
发明人： Simon Nicolas Morliere , Stéphane Pierre Guillaume Blanchard , Nicolas Jean-Marc Marcel Beauquin
CPC分类号： F01D11/24 , F01D25/12 , F01D25/14 , F01D25/28 , F02C7/18 , F05D2220/323 , F05D2250/241 , F05D2260/201 , F05D2260/30
摘要： The present invention relates to a device for cooling, using air jets, an external casing of a turbomachine, comprising a housing for supplying air to cooling tubes of said casing, the housing being provided with an attachment device on the external casing. According to the invention, said attachment device comprises two upstream ball joint retention devices which each connect the housing to the external casing.
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公开(公告)号：US11378014B2
公开(公告)日：2022-07-05
申请号：US17055428
申请日：2019-05-15
发明人： Stéphane Pierre Guillaume Blanchard , Helene Myriam Condat , Nicolas Xavier Trappier , Laurent Paul François Perrot
摘要： A turbomachine includes a low-pressure shaft that drives a fan shaft in rotation by a coupling assembly including a first shaft on which are formed plural first axial grooves, a second shaft on which are formed plural second axial grooves, and a coupling device including rolling elements and an annular cage positioned between the first shaft and the second shaft. The rolling elements are positioned between one of the first axial grooves and one of the second axial grooves to couple in rotation the first and the second shaft. Each first and second groove has a first and a second substantially planar surface inclined with respect to one another and extending along the axis.
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公开(公告)号：US20180066540A1
公开(公告)日：2018-03-08
申请号：US15695725
申请日：2017-09-05
CPC分类号： F01D25/243 , F01D25/16 , F01D25/162 , F01D25/28 , F05D2220/323 , F05D2230/53 , F05D2240/14 , F05D2240/90 , Y02T50/671
摘要： A turbine comprising an intermediate casing axially inserted between an upstream high pressure turbine casing and a downstream low pressure turbine casing and comprising an outer annular shroud from which an annular flange radially extends, characterized in that the downstream end of the high pressure turbine casing and the upstream end of the low pressure turbine casing are attached on the radial annular flange of the intermediate casing.
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公开(公告)号：US20170218781A1
公开(公告)日：2017-08-03
申请号：US15320378
申请日：2015-06-24
CPC分类号： F01D5/3007 , F01D5/02 , F01D5/081 , F01D5/12 , F01D5/3015 , F01D11/005 , F01D11/006 , F05D2220/32 , F05D2260/30 , Y02T50/676
摘要： The invention relates to a rotary assembly for a turbomachine, comprising: a disk (16) having an external periphery exhibiting an alternation of slots (22) and of teeth (20), vanes (14) extending radially from the disk (16), the roots (24) of which are engaged axially and retained radially in the slots (22) of the disk, upstream and/or downstream of the disk, an annular sealing flange (52) of cavities (36) formed radially between, respectively, the roots of the vanes and the bottoms of the slots of the disk, said flange comprising an external part (56) arranged axially facing the upstream and/or downstream ends, respectively, of the teeth of the disk and of the roots of the vanes. According to the invention, the assembly further comprises an intermediate ring (66) which is arranged axially between the flange (52) and the teeth (20) of the disk, and also comprises a seal (70) which is arranged axially between, on the one side, the intermediate ring (6) and, on another side, the teeth (20) of the disk and the vane roots (24).
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公开(公告)号：US11555405B2
公开(公告)日：2023-01-17
申请号：US16704031
申请日：2019-12-05
发明人： Simon Nicolas Morliere , Nicolas Jean-Marc Marcel Beauquin , Stéphane Pierre Guillaume Blanchard , Gaëlle Inès Méganne Moreaux
摘要： A device for holding (101) at least one cooling tube (120) of a turbomachine casing (10) cooling system (100), the holding device including a fixing frame (104), a holding member (160) being configured to hold two cooling tubes (120), and a connection assembly (140) between the holding member (160) and a fixing frame (104), extending on either side of the frame, the connection assembly (160) comprising a connection part (150) extending through an opening (108) of the fixing frame from an outer portion (141) to the inner portion (142) of the connection assembly, the inner portion (142) being disposed between two cooling tubes (120) and secured to the holding member (160) while the outer portion (141) comprises a resilient return member (170) urged in compression towards the fixing frame by the connection part (150).
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公开(公告)号：US10598031B2
公开(公告)日：2020-03-24
申请号：US15698927
申请日：2017-09-08
发明人： Stéphane Pierre Guillaume Blanchard , Joao Antonio Amorim , Maxime Aurélien Rotenberg , Nicolas Xavier Trappier
摘要： A turbine rotor is fitted to a turbomachine and includes disks each containing a coupling portion with recesses each holding a root of a blade, and coupled to one another by a first annular ferrule attached to one of them close to the recesses, and second rotationally coupled ferrules, which are respectively coupled radially to the disks, which each consists of at least two semi-annular sectors, and which form with the associated disk a space which communicates with the recesses of the coupling portion of this latter disk. In addition, each first ferrule includes through-holes enabling air to enter this space, and then the recesses, intended to cool the coupling portion which couples its disk and the blade roots.
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公开(公告)号：US10385706B2
公开(公告)日：2019-08-20
申请号：US15320378
申请日：2015-06-24
摘要： The invention relates to a rotary assembly for a turbomachine, comprising: a disk (16) having an external periphery exhibiting an alternation of slots (22) and of teeth (20), vanes (14) extending radially from the disk (16), the roots (24) of which are engaged axially and retained radially in the slots (22) of the disk, upstream and/or downstream of the disk, an annular sealing flange (52) of cavities (36) formed radially between, respectively, the roots of the vanes and the bottoms of the slots of the disk, said flange comprising an external part (56) arranged axially facing the upstream and/or downstream ends, respectively, of the teeth of the disk and of the roots of the vanes. According to the invention, the assembly further comprises an intermediate ring (66) which is arranged axially between the flange (52) and the teeth (20) of the disk, and also comprises a seal (70) which is arranged axially between, on the one side, the intermediate ring (6) and, on another side, the teeth (20) of the disk and the vane roots (24).
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公开(公告)号：US10301972B2
公开(公告)日：2019-05-28
申请号：US15695725
申请日：2017-09-05
摘要： A turbine comprising an intermediate casing axially inserted between an upstream high pressure turbine casing and a downstream low pressure turbine casing and comprising an outer annular shroud from which an annular flange radially extends, characterized in that the downstream end of the high pressure turbine casing and the upstream end of the low pressure turbine casing are attached on the radial annular flange of the intermediate casing.
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