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公开(公告)号：US07458773B2
公开(公告)日：2008-12-02
申请号：US11202336
申请日：2005-08-12
CPC分类号： F01D25/16 , F01D25/18 , F02C3/067 , F02K3/072 , F05D2230/60 , F05D2230/70 , Y02T50/671
摘要： A turbomachine comprising: a gas generator for producing combustion gas; a turbine section through which the combustion gas passes and comprising first and second rows of contrarotating turbine rotor blades respectively driving first and second low-pressure shafts in rotation; and a fan section comprising a first row of fan blades mounted on a front fan shaft that is connected to an upstream end of the first low-pressure shaft, and a second row of fan blades axially offset from the first row and mounted on a rear fan shaft that is connected to an upstream end of the second low-pressure shaft, the front fan shaft being connected to the upstream end of the first low-pressure shaft via a removable sleeve for transmitting torque.
摘要翻译： 一种涡轮机，包括：用于产生燃烧气体的气体发生器; 涡轮部分，燃烧气体通过该部分，并且包括分别驱动第一和第二低压轴旋转的第一排和第二排反向涡轮转子叶片; 以及风扇部分，包括安装在前风扇轴上的第一排风扇叶片，所述风扇叶片连接到第一低压轴的上游端，以及第二排风扇叶片，其从第一排轴向偏移并安装在后部 风扇轴，其连接到第二低压轴的上游端，前风扇轴经由用于传递扭矩的可拆卸套筒连接到第一低压轴的上游端。
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2.发明申请Turboshaft engine comprising two elements connected to each other with the interposition of a seal 有权涡轮轴发动机包括彼此连接并插入密封件的两个元件公开(公告)号：US20050095123A1
公开(公告)日：2005-05-05
申请号：US10946067
申请日：2004-09-22
申请人： Jean-Claude Taillant , Marc Marchi
发明人： Jean-Claude Taillant , Marc Marchi
CPC分类号： F01D11/005 , F16J15/0887
摘要： Turboshaft engine, such as for example a turbine, comprising a segmented seal between two longitudinally adjacent elements such as, for example, a casing and a ring of sectors of vanes. According to one embodiment, a seal is interposed between a casing and a ring of sectors of vanes and consists of a plurality of flexible segments having a straight deformation zone and a straight fluid-tight bearing zone.
摘要翻译： 涡轮轴发动机，例如涡轮机，包括在两个纵向相邻元件之间的分段密封，例如壳体和叶片扇形环。 根据一个实施例，密封件插入在壳体和叶片扇形环之间，并且由具有直的变形区域和直的流体密封轴承区域的多个柔性段组成。
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公开(公告)号：US07011493B2
公开(公告)日：2006-03-14
申请号：US10790116
申请日：2004-03-02
IPC分类号： F01D25/12
CPC分类号： F01D25/246 , F01D9/04 , F01D11/08
摘要： A turbomachine includes a casing, a rotor, and a plurality of cooled ring segments installed between the casing and the rotor, each ring segment containing a main cooling cavity and being attached to the casing by a fastening device. The fastening device can include a clamping screw positioned more or less radially and pinning the ring segment against the casing. The clamping screw is crossed through by a cooling airway that communicates with the main cooling cavity of the ring segment.
摘要翻译： 涡轮机包括壳体，转子和安装在壳体和转子之间的多个冷却环段，每个环段包含主冷却腔，并通过紧固装置附接到壳体。 紧固装置可以包括多个或多或少径向设置的夹紧螺钉，并将环部分固定在壳体上。 夹紧螺丝通过与环段的主冷却腔连通的冷却气道穿过。
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公开(公告)号：US20050172642A1
公开(公告)日：2005-08-11
申请号：US10513447
申请日：2003-05-16
CPC分类号： F01D5/082 , F02C7/18 , F05D2240/14 , F05D2250/232 , F05D2250/323 , F05D2260/231 , Y02T50/676
摘要： The invention relates to a turbomachine of axis X and comprising, from upstream to downstream, a high pressure compressor whose rotor presents a downstream cone (4), a diffuser (3) extending downstream beside the axis X by an inner casing (5) disposed radially outside said downstream compressor cone, a combustion chamber disposed radially outside said inner diffuser casing, and a high pressure turbine whose rotor is connected to the downstream cone of the compressor by a connection drum, the inner diffuser casing and the downstream compressor cone defining between them an under-chamber cavity that is situated downstream from a discharge labyrinth (13) in which cooling air flows downstream, the turbomachine being characterized in that it also comprises a stator shroud (20) that is installed under the inner diffuser casing (5) downstream from the discharge labyrinth (13).
摘要翻译： 本发明涉及一种轴X的涡轮机，其上游和下游包括一个高压压缩机，该压缩机的转子具有一个下游锥体（4），一个扩散器（3）通过设置在内部壳体（5）的轴线X的下游延伸， 位于所述下游压缩机锥体的径向外侧，设置在所述内部扩散器壳体的径向外侧的燃烧室和转子通过连接鼓连接到压缩机的下游锥体的高压涡轮机，内部扩散器壳体和下游压缩机锥体限定在 它们是位于冷却空气流下游的排放迷宫（13）下游的腔室，涡轮机的特征在于它还包括安装在内部扩散器壳体（5）下方的定子罩（20） 从放电迷宫（13）的下游。
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公开(公告)号：US5816776A
公开(公告)日：1998-10-06
申请号：US791051
申请日：1997-01-28
申请人： Frederic Chambon , Patrick Didier Michel Lestoille , Jacques Henri Mouchel , Jean-Claude Taillant
发明人： Frederic Chambon , Patrick Didier Michel Lestoille , Jacques Henri Mouchel , Jean-Claude Taillant
CPC分类号： F01D11/001 , F01D5/066
摘要： A labyrinth disk includes a main stiffener placed in the middle of the rim immediately below labyrinth elements. Attachment elements are preferably in the form of a bayonet attachment system using teeth fixed on the labyrinth disk crown and teeth fixed on the rotor. Attachment by bolting may optionally be used. The disk may be utilized with turbojets, on the cooling circuit, on the upstream side of the high pressure turbine.
摘要翻译： 迷宫盘包括放置在迷宫元件正下方的边缘中间的主加劲肋。 附接元件优选地是使用固定在迷宫盘冠上的齿和固定在转子上的齿的卡口附接系统的形式。 可以选择使用螺栓连接。 该盘可以与冷却回路上的涡轮喷嘴一起用于高压涡轮机的上游侧。
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公开(公告)号：US20050201859A1
公开(公告)日：2005-09-15
申请号：US10517613
申请日：2003-06-25
CPC分类号： F01D5/081 , F01D5/3015 , F01D11/02 , F02C7/28 , Y02T50/671 , Y02T50/676
摘要： A ventilation circuit of a turbomachine turbine rotor having a turbine disk and an upstream flange disposed upstream from a combustion chamber from which it is spaced apart by a cavity. A first cooling air circuit delivers air into the cavity via main injectors and holes in the flange. A second cooling air circuit delivers air through enclosures delimited by the combustion chamber inner casing and the rotor via a discharge labyrinth, an under-injector labyrinth, and at least one labyrinth downstream from the main injectors between an annular structure and the flange. Three single-wiper labyrinths delimiting two cavities upstream from the venting cavity of the turbine disk are provided downstream from the main injectors. One of the cavities is fed with air from the second circuit upstream from the under-injector labyrinth by bore holes in the annular structure sloping tangentially in the rotation direction of the rotor.
摘要翻译： 具有涡轮机涡轮机转子的通风回路，其具有涡轮盘和设置在燃烧室上游的上游凸缘，所述燃烧室被空腔间隔开。 第一个冷却空气回路通过主注射器和法兰中的孔将空气输送到空腔中。 第二冷却空气回路通过排气迷宫，下注射器迷宫和至少一个迷宫在主喷射器下游的环形结构和凸缘之间的空气通过燃烧室内壳和转子限定的空气。 在主喷射器的下游设置有将涡轮盘的通气腔上游限定两个空腔的三个单刮水器迷宫。 其中一个空腔通过在转子的旋转方向上切向倾斜的环形结构中的钻孔而从喷射器迷宫的上游的第二回路供给空气。
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公开(公告)号：US06916151B2
公开(公告)日：2005-07-12
申请号：US10771540
申请日：2004-02-05
CPC分类号： F01D5/082
摘要： A ventilation device for a high pressure turbine rotor in a turbomachine, the turbine comprising upstream and downstream turbine disks fitted with blades, the device comprising a cooling circuit being supplied by a cooling airflow D taken from the back of the combustion chamber. The circuit is such that the airflow passes through orifices formed in an upstream flange of the upstream disk, such that this airflow circulates in the axial direction towards the downstream side between an inner reaming of the upstream disk and a downstream flange of the downstream disk, the device also comprising a labyrinth inserted between the two disks, such that the airflow is divided into a first flow F1 and a second flow circulating on each side of labyrinth towards the blades.
摘要翻译： 一种用于涡轮机中的高压涡轮转子的通风装置，所述涡轮机包括装配有叶片的上游和下游涡轮盘，所述装置包括由从燃烧室后部取出的冷却气流D供应的冷却回路。 该电路使得气流通过形成在上游盘的上游法兰中的孔，使得该气流在上游盘的内部铰接和下游盘的下游法兰之间沿着轴向方向向下游侧循环， 该装置还包括插入在两个盘之间的迷宫，使得气流被划分成在迷宫的每一侧向叶片循环的第一流F1和第二流。
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公开(公告)号：US20070006569A1
公开(公告)日：2007-01-11
申请号：US11202336
申请日：2005-08-12
IPC分类号： F02K3/04
CPC分类号： F01D25/16 , F01D25/18 , F02C3/067 , F02K3/072 , F05D2230/60 , F05D2230/70 , Y02T50/671
摘要： A turbomachine comprising: a gas generator for producing combustion gas; a turbine section through which the combustion gas passes and comprising first and second rows of contrarotating turbine rotor blades respectively driving first and second low-pressure shafts in rotation; and a fan section comprising a first row of fan blades mounted on a front fan shaft that is connected to an upstream end of the first low-pressure shaft, and a second row of fan blades axially offset from the first row and mounted on a rear fan shaft that is connected to an upstream end of the second low-pressure shaft, the front fan shaft being connected to the upstream end of the first low-pressure shaft via a removable sleeve for transmitting torque.
摘要翻译： 一种涡轮机，包括：用于产生燃烧气体的气体发生器; 涡轮部分，燃烧气体通过该部分，并且包括分别驱动第一和第二低压轴旋转的第一排和第二排反向涡轮转子叶片; 以及风扇部分，包括安装在前风扇轴上的第一排风扇叶片，所述风扇叶片连接到第一低压轴的上游端，以及第二排风扇叶片，其从第一排轴向偏移并安装在后部 风扇轴，其连接到第二低压轴的上游端，前风扇轴经由用于传递扭矩的可拆卸套筒连接到第一低压轴的上游端。
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9.发明授权Turboshaft engine comprising two elements connected to each other with the interposition of a seal 有权涡轮轴发动机包括通过插入密封件彼此连接的两个元件公开(公告)号：US07140840B2
公开(公告)日：2006-11-28
申请号：US10946067
申请日：2004-09-22
申请人： Jean-Claude Taillant , Marc Marchi
发明人： Jean-Claude Taillant , Marc Marchi
IPC分类号： F01D11/00
CPC分类号： F01D11/005 , F16J15/0887
摘要： A turboshaft engine, such as for example a turbine, including a segmented seal between two longitudinally adjacent elements such as, for example, a casing and a ring of sectors of vanes. According to one embodiment, a seal is interposed between a casing and a ring of sectors of vanes and includes a plurality of flexible segments having a straight deformation zone and a straight fluid-tight bearing zone.
摘要翻译： 涡轮轴发动机，例如涡轮机，包括在两个纵向相邻元件之间的分段密封，例如壳体和叶片扇形环。 根据一个实施例，密封件插入在壳体和叶片的扇形环之间，并且包括具有直的变形区域和直的流体密封轴承区域的多个柔性段。
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公开(公告)号：US07036320B2
公开(公告)日：2006-05-02
申请号：US10513447
申请日：2003-05-16
IPC分类号： F02C7/18
CPC分类号： F01D5/082 , F02C7/18 , F05D2240/14 , F05D2250/232 , F05D2250/323 , F05D2260/231 , Y02T50/676
摘要： A turbomachine including a high pressure compressor with a downstream cone, a diffuser extending downstream by an inner casing disposed radially outside the downstream compressor cone, a combustion chamber disposed radially outside the inner diffuser casing, and a high pressure turbine whose rotor is connected to the downstream cone of the compressor by a connection drum, the inner diffuser casing and the downstream compressor cone defining between them an under-chamber cavity that is situated downstream from a discharge labyrinth in which cooling air flows downstream, wherein the engine also includes a stator shroud that is installed under the inner diffuser casing downstream from the discharge labyrinth.
摘要翻译： 一种涡轮机，包括具有下游锥体的高压压缩机，通过设置在下游压缩机锥体径向外侧的内部壳体向下游延伸的扩散器，设置在内部扩散器壳体的径向外侧的燃烧室，以及转子连接到 压缩机的下游锥体通过连接鼓，内部扩散器壳体和下游压缩机锥体在它们之间限定位于冷却空气流下游的排放迷宫下游的腔室，其中发动机还包括定子罩 其安装在排出迷宫下游的内部扩散器壳体的下方。
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