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公开(公告)号：EP4372281A1
公开(公告)日：2024-05-22
申请号：EP22425055.5
申请日：2022-11-18
发明人： Licata, Daniele , Amato, Alberto , Alsina Torrent, Armando , Belina, Ivo , Duesing, Michael Klaus
IPC分类号： F23R3/06
CPC分类号： F23R3/005 , F23R3/06 , F23R2900/0304120130101 , F23R2900/0304320130101
摘要： A combustion chamber (3) for a power plant gas turbine assembly (1) wherein the combustion chamber comprises an outer casing (7) and a plurality of heat shielding tile devices (8) supported by the outer casing; wherein at least one shielding tile device comprises: a metallic tile body (9) having an inner face (10) configured for facing the hot gas flow inside the combustion chamber and an opposite outer face (11) configured for facing a plenum obtained between the outer casing and the metallic tile body and fed by cooling air; a first plurality of first cooling pipes (12) fed by the cooling air wherein the first cooling pipes are arranged parallel each other forming a first layer (16) on the outer face of the metallic tile body; a second plurality of second cooling pipes (13) fed by the cooling air wherein the second cooling pipes are arranged parallel each other forming a second layer (17) on the first plurality of first cooling pipes.
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公开(公告)号：EP4198270A1
公开(公告)日：2023-06-21
申请号：EP21425070.6
申请日：2021-12-20
摘要： An exhaust gas casing for a heavy-duty gas turbine engine includes a shell (12) delimiting a hot gas path (13) and having a downstream flange (17); and an annular cooling structure (20), extending around at least a circumferential portion of the shell (12) adjacent to the downstream flange (17) and configured to convey cooling air around the shell (12). The annular cooling structure (20) is inwardly defined by the shell (12) and is outwardly defined by at least an annular cover structure (25, 26) attached to the shell (12).
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公开(公告)号：EP3957827A1
公开(公告)日：2022-02-23
申请号：EP20425031.0
申请日：2020-08-18
摘要： The coating system for a component of a gas turbine engine comprises a bond coat BC layer (2) and a thermal barrier coating TBC layer (3) above the BC layer (2) . The BC layer (2) has a thickness in the range 180-300 micrometers and a roughness Ra of its surface facing the TBC layer (3) in a range 12.8-19.0 micrometers. The TBC layer (3) has a thickness in the range 200-700 micrometers and a porosity in the range 15.0-23.0 vol %. The ends of ranges are included in the ranges.
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公开(公告)号：EP3816405A1
公开(公告)日：2021-05-05
申请号：EP19425077.5
申请日：2019-11-04
摘要： A stator assembly (22) for a gas turbine comprising is provided with:
• a stator ring (24), which extends about a longitudinal axis (A) and comprises an inner edge and an outer edge (29); the outer edge being provided with an annular groove (30); the annular groove (30) defining a leading wall (34) and a trailing wall (35); the trailing wall (34) being provided with an annular trailing radial face (36a) and with an annular trailing axial face (36b);
• a plurality of stator vanes (25) radially arranged and coupled alongside one another to the outer edge (29) of the stator ring (24) so as to close the annular grove (30) and define an annular cooling channel (32);
the stator ring (24) being provided with at least one trailing cooling hole (39) having an inlet (40) facing the annular cooling channel (32) and an outlet (41) arranged on the annular trailing radial face (36b).-
公开(公告)号：EP2948660B1
公开(公告)日：2020-08-26
申请号：EP14714327.5
申请日：2014-01-23
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公开(公告)号：EP3686398A1
公开(公告)日：2020-07-29
申请号：EP19425005.6
申请日：2019-01-28
发明人： Cerasi, Luca , König, Marcel , Elli, Stefano
IPC分类号： F01D9/02
摘要： A seal assembly for a gas turbine comprises at least one main spring configured to be at least partially housed in a seat (19) of a combustor outlet member (17), at least one flexible seal member having a plate portion disposed on an outer side of the main spring and having an outer blade configured to sealingly cooperate with a seat surface, and at least one shield seal member having a plate portion disposed on an outer side of the plate portion of the flexible seal element and a flange configured to contact axially a vane surface under the axial elastic load of the main spring. A corresponding gas turbine comprises an outer casing, a compressor, a plurality of can combustors (10) downstream of the compressor and a turbine downstream of the can combustors (10), the compressor and turbine comprising fixed vanes (14) carried by the outer casing and rotating blades carried by a rotor. The can combustors are spaced around the rotor and produce hot gas by combusting a mixture of air and at least one fuel. The gas turbine includes, for each can combustor, a seal assembly axially interposed between an outlet member (17) of the combustor (10) and at least one turbine vane and radially interposed between an outer hot gas path (12) and an inner space containing higher-pressure cooling air.
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公开(公告)号：EP2741001B1
公开(公告)日：2020-02-05
申请号：EP13196562.6
申请日：2013-12-10
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公开(公告)号：EP3351726A1
公开(公告)日：2018-07-25
申请号：EP18152639.3
申请日：2018-01-19
发明人： TAPPANI, Marco , SCHNEIDER, Andrea
摘要： A blade or vane for a compressor comprises a main body (15; 25) provided with a base face (16; 26), with a top face (17; 27), opposite with respect to the base face (16; 26), and with an outer face (18; 28), which extends between the base face (16; 26) and the top face (17; 27) and defines the airfoil profile of the blade or vane (7; 10; 70; 700); the main body (15; 25) being shaped so as to define along the outer face (18; 28) a leading edge (30), a trailing edge (31), a pressure side (32) and a suction side (33); and at least one appendix (29; 79; 779) arranged in the proximity of the trailing edge (31).
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公开(公告)号：EP3339737A1
公开(公告)日：2018-06-27
申请号：EP17209153.0
申请日：2017-12-20
发明人： MACELLONI, Paolo
CPC分类号： F02C7/24 , B23P6/045 , B23P2700/13 , F05D2220/32 , F05D2240/35 , F05D2300/173 , F05D2300/2261 , F05D2300/5023 , F23M5/02 , F23R3/002 , F23R3/007 , F23R2900/00019
摘要： A thermoinsulating tile for combustion chambers of gas turbines comprises: a thermoinsulating material body (9) having a first face (10) and a second face (11);
a sealed chamber (18) encapsulated in the thermoinsulating material body (9) between the first face (10) and the second face (11) and containing a marker substance (20) in the liquid state at least at a temperature of use of the thermoinsulating tile.
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