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1.发明申请DEVICE FOR INJECTING A MIXTURE OF AIR AND FUEL, AND COMBUSTION CHAMBER AND TURBOMACHINE PROVIDED WITH SUCH A DEVICE 有权用于喷射空气和燃料混合物的设备，以及提供给这些设备的燃烧室和涡轮机公开(公告)号：US20080000234A1
公开(公告)日：2008-01-03
申请号：US11768421
申请日：2007-06-26
申请人： Patrice Andre COMMARET , Dominique Guezengar , Didier Hippolyte Hernandez , Romain Nicolas Lunel , Pascale Rollet
发明人： Patrice Andre COMMARET , Dominique Guezengar , Didier Hippolyte Hernandez , Romain Nicolas Lunel , Pascale Rollet
IPC分类号： F23R3/04
CPC分类号： F23D11/107 , F23D14/78 , F23D2214/00 , F23R3/12 , F23R3/14 , F23R3/286 , Y02T50/675
摘要： The invention relates to a device for injecting an air/fuel mixture into a combustion chamber, which is to be mounted within a restricted space. This injection device (20) comprises a bowl (70) having an external cylindrical wall (73) continued at its downstream end by a divergent section (74) provided, downstream, with a collar (75) having the form of a ring extending radially outward, the divergent section of the bowl being connected, immediately upstream of the flange, by a connecting wall (76) to a cylindrical ring (77), the cylindrical ring and the connecting wall forming a connection rim oriented in the upstream direction. At least one row of vortex holes (79) is formed in the external cylindrical wall, close to its upstream end, and the connecting wall of the connection rim of the bowl is provided with a row of cooling orifices (81) inclined axially at an angle y to the axis of symmetry of the injection device.
摘要翻译： 本发明涉及一种用于将空气/燃料混合物喷射到要安装在受限空间内的燃烧室中的装置。 该注射装置（20）包括碗（70），其具有外部圆柱形壁（73），该外圆柱形壁（73）在其下游端通过扩散部分（74）延伸，所述扩散部分（74）在下游具有环形形式的环（75） 向外，碗的发散部分通过连接壁（76）直接连接到凸缘的上游，圆柱形环（77），圆柱形环和连接壁形成沿上游方向定向的连接边缘。 至少一排涡流孔（79）形成在外圆柱形壁上，靠近其上游端，并且碗的连接边缘的连接壁设置有一排沿轴向倾斜的冷却孔（81） 与注射装置的对称轴成y角。
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2.发明授权Device for injecting a mixture of air and fuel, and combustion chamber and turbomachine provided with such a device 有权用于喷射空气和燃料的混合物的装置，以及具有这种装置的燃烧室和涡轮机公开(公告)号：US07926281B2
公开(公告)日：2011-04-19
申请号：US11768421
申请日：2007-06-26
申请人： Patrice Andre Commaret , Dominique Guezengar , Didier Hippolyte Hernandez , Romain Nicolas Lunel , Pascale Rollet
发明人： Patrice Andre Commaret , Dominique Guezengar , Didier Hippolyte Hernandez , Romain Nicolas Lunel , Pascale Rollet
CPC分类号： F23D11/107 , F23D14/78 , F23D2214/00 , F23R3/12 , F23R3/14 , F23R3/286 , Y02T50/675
摘要： A device for injecting an air/fuel mixture into a combustion chamber mounted within a restricted space is disclosed. This injection device includes a bowl having an external cylindrical wall continued at its downstream end by a divergent section provided, downstream, with a collar having the form of a ring extending radially outward. The divergent section of the bowl is connected, immediately upstream of the flange, by a connecting wall to a cylindrical ring. The cylindrical ring and the connecting wall form a connection rim oriented in the upstream direction. At least one row of vortex holes is formed in the external cylindrical wall, close to its upstream end, and the connecting wall of the connection rim of the bowl is provided with a row of cooling orifices inclined axially at an angle γ to the axis of symmetry of the injection device.
摘要翻译： 公开了一种用于将空气/燃料混合物注入安装在限制空间内的燃烧室中的装置。 该注射装置包括具有外圆柱形壁的碗，该外壁在其下游端由在下游具有径向向外延伸的环的形式的下游设置的扩散部分延伸。 碗的发散部分在紧邻法兰上游的连接壁连接到圆柱形环上。 圆柱形环和连接壁形成沿上游方向定向的连接边缘。 在外圆柱壁上形成至少一排涡流孔，靠近其上游端，并且碗的连接边缘的连接壁设置有一排冷却孔，该冷却孔轴向以与轴线 注射装置的对称性。
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3.发明申请CHAMBER-BOTTOM BAFFLE, COMBUSTION CHAMBER COMPRISING SAME AND GAS TURBINE ENGINE FITTED THEREWITH 审中-公开箱体底部，包括相同的燃烧室和燃气涡轮发动机公开(公告)号：US20090019856A1
公开(公告)日：2009-01-22
申请号：US12165995
申请日：2008-07-01
IPC分类号： F23R3/42
摘要： The present invention relates to a baffle (10) for the bottom of a combustion chamber of a gas turbine engine, comprising a flat portion of wall (10a) with an opening for an injector of the combustion chamber to pass through, two longitudinal edges (10c, 10d) for the assembly to two adjacent baffles and two transverse edges (10e, 10f), wherein at least one of the edges comprises a joint cover (10d1) arranging a housing (10d10) along said edge for an edge (10′c) of an adjacent baffle (10′) so as to seal the junction between the two edges. The invention also relates to a combustion chamber incorporating said baffles.
摘要翻译： 本发明涉及一种用于燃气涡轮发动机的燃烧室的底部的挡板（10），其包括具有用于燃烧室的喷射器通过的开口的壁（10a）的平坦部分，两个纵向边缘 10e，10d），用于组装到两个相邻的挡板和两个横向边缘（10e，10f），其中至少一个边缘包括沿着所述边缘设置壳体（10d10）的接合盖（10d1），用于边缘（10' c）相邻的挡板（10'），以便密封两个边缘之间的接合部。 本发明还涉及包含所述挡板的燃烧室。
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公开(公告)号：US08875517B2
公开(公告)日：2014-11-04
申请号：US12919772
申请日：2009-02-20
CPC分类号： F02C3/08 , F04D29/441 , F04D29/444 , F23R3/283 , F23R3/60 , Y02T50/671
摘要： A diffuser for a turbine engine that includes two annular webs extending inside one another and connected between them by substantially radial vanes, wherein the downstream peripheral edge of at least one of the webs includes indentions evenly distributed about the longitudinal axis of the diffuser.
摘要翻译： 一种用于涡轮发动机的扩散器，其包括彼此相对延伸并且通过基本上径向的叶片连接在它们之间的两个环形腹板，其中至少一个腹板的下游周边边缘包括围绕扩散器的纵向轴线均匀分布的凹陷。
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公开(公告)号：US20110056207A1
公开(公告)日：2011-03-10
申请号：US12919772
申请日：2009-02-20
CPC分类号： F02C3/08 , F04D29/441 , F04D29/444 , F23R3/283 , F23R3/60 , Y02T50/671
摘要： A diffuser for a turbine engine that includes two annular webs extending inside one another and connected between them by substantially radial vanes, wherein the downstream peripheral edge of at least one of the webs includes indentions evenly distributed about the longitudinal axis of the diffuser.
摘要翻译： 一种用于涡轮发动机的扩散器，其包括彼此相对延伸并且通过基本上径向的叶片连接在它们之间的两个环形腹板，其中至少一个腹板的下游周边边缘包括围绕扩散器的纵向轴线均匀分布的凹陷。
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公开(公告)号：US07661273B2
公开(公告)日：2010-02-16
申请号：US12198386
申请日：2008-08-26
IPC分类号： F02C7/20
CPC分类号： F23R3/283 , F02C3/14 , F05D2230/642 , F05D2250/70 , F05D2260/96 , F23R3/50 , F23R3/60
摘要： Turbomachine with an annular combustion chamber including at its upstream end an annular chamber bottom, and attached at its downstream end by annular flanges to a radially inner casing and outer casing, wherein the upstream end of the chamber is connected to the inner casing or outer casing by elastically deformable bridges.
摘要翻译： 具有环形燃烧室的涡轮机，其上游端部包括环形室底部，并且在其下游端通过环形凸缘附接到径向内壳体和外壳体，其中室的上游端连接到内壳体或外壳体 通过可弹性变形的桥梁。
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公开(公告)号：US20120073259A1
公开(公告)日：2012-03-29
申请号：US13259941
申请日：2010-03-12
IPC分类号： F23R3/50
CPC分类号： F23R3/60 , F01D9/023 , F01D25/243 , F23R3/50 , Y02T50/671
摘要： A turbomachine including an annular combustion chamber, the combustion chamber presenting a connection flange at its downstream end for connection to an outer casing. The connection flange bears axially against the outer casing and is blocked in an axial direction by the upstream end of an inner casing of a high pressure turbine.
摘要翻译： 一种包括环形燃烧室的涡轮机，所述燃烧室在其下游端具有连接凸缘以连接到外壳。 连接法兰轴向抵靠外壳，并通过高压汽轮机内壳的上游端沿轴向阻塞。
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公开(公告)号：US20110113789A1
公开(公告)日：2011-05-19
申请号：US12997266
申请日：2009-06-10
CPC分类号： F23R3/283
摘要： A gas turbine engine combustion chamber including at least one deflector mounted on the chamber end wall and including an opening for a carburetted air supply device. The deflector includes an opening, corresponding to the chamber end wall opening, with an annular cylindrical part for attachment to the wall, the cylindrical part including a mechanical attachment mechanism collaborating with a complementary attachment mechanism on a metal sleeve secured to the wall and a cylindrical centering cup fixed by one end to the sleeve and housed inside the cylindrical part of the deflector.
摘要翻译： 一种燃气涡轮发动机燃烧室，包括安装在室端壁上的至少一个偏转器，并且包括用于碳化空气供应装置的开口。 偏转器包括对应于室端壁开口的开口，具有用于附接到壁的环形圆柱形部分，圆柱形部分包括与固定到壁上的金属套筒上的互补附接机构协作的机械附接机构，以及圆柱形 定心杯由一端固定到套筒上并容纳在偏转器的圆柱形部分内。
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公开(公告)号：US08516830B2
公开(公告)日：2013-08-27
申请号：US12544423
申请日：2009-08-20
CPC分类号： F23R3/283
摘要： A turbomachine combustion chamber including a substantially L-shaped fuel injector and a device for mounting and fastening the injector in an orifice of the casing of the chamber, is disclosed. The device includes an outer collar carried by the injector and a removable annular spacer surrounding the injector and designed to be interposed between the collar of the injector and the casing.
摘要翻译： 公开了一种涡轮机燃烧室，其包括基本上L形的燃料喷射器和用于将喷射器安装并紧固在腔室壳体的孔中的装置。 该装置包括由注射器承载的外部轴环和围绕注射器的可移除的环形间隔件，并被设计成插入在注射器的套环和套管之间。
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10.发明申请FUEL MIXING DEVICE FOR TURBINE ENGINE COMBUSTION CHAMBER COMPRISING IMPROVED AIR FEED MEANS 有权用于涡轮发动机燃烧室的燃料混合装置，包括改进的空气进料装置公开(公告)号：US20120204567A1
公开(公告)日：2012-08-16
申请号：US13503737
申请日：2010-11-03
CPC分类号： F23R3/14 , F23R3/286 , Y02T50/675
摘要： A fuel mixing device for an annular combustion chamber of a turbine engine, including a member for centering a turbine engine injector head, at least one air intake ring including blades allowing swirling of air, a bowl including an annular row of air intake orifices, an annular cavity communicating with the air intake orifices, and channels arranged through the blades to feed air to the annular cavity.
摘要翻译： 一种用于涡轮发动机的环形燃烧室的燃料混合装置，包括用于使涡轮发动机喷射器头定心的构件，包括允许空气旋转的叶片的至少一个进气环，包括空气吸入孔的环形排的碗， 与进气口连通的环形空腔，以及通过叶片布置的通道，以将空气送入环形空腔。
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