公开(公告)号：EP4075111B1

公开(公告)日：2024-09-25

申请号：EP22166638.1

申请日：2022-04-05

IPC分类号： G01J5/00 ,  G01J5/02 ,  G01J5/0875 ,  F23M11/04 ,  F23N5/08 ,  G01J1/04 ,  G01J1/42 ,  F23D14/02 ,  G01N21/72

CPC分类号： G01J5/0205 ,  G01J5/0875 ,  F23M11/042 ,  G01J5/0018 ,  G01N21/72 ,  F23N5/082 ,  G01J1/429 ,  G01J1/0466 ,  F23M11/045 ,  F23N2241/0620200101 ,  F23D14/02 ,  F23C2900/990120130101 ,  F23N2900/0500520130101 ,  F23N2900/0500420130101

公开(公告)号：EP4253840B1

公开(公告)日：2024-09-11

申请号：EP23163666.3

申请日：2023-03-23

IPC分类号： F23L1/02 ,  F23L15/00 ,  F23M5/08 ,  F23H7/08 ,  F23H7/10 ,  F23L15/04 ,  F23H17/08

CPC分类号： F23M5/085 ,  F23L1/02 ,  F23L15/00 ,  F23H7/08 ,  F23H7/10 ,  F23N2221/0820200101 ,  F23L15/04 ,  F23H17/08 ,  F23H2700/00920130101 ,  F23G2203/10120130101

公开(公告)号：EP4425050A1

公开(公告)日：2024-09-04

申请号：EP24158501.7

申请日：2024-02-20

申请人： Valmet Technologies Oy

发明人： LEHTONEN, Pekka ,  LUOMAHARJU, Tero ,  YLI-HEMMINKI, Pasi

IPC分类号： F23M5/08

CPC分类号： F23M5/08

摘要： A wall (200) for a fluidized bed boiler (300). The wall (200) comprises a first heat exchanger pipe (110) comprising a first primary portion (111) and a first secondary portion (112), and a second heat exchanger pipe (120) comprising a second primary portion (121) and a second secondary portion (122). A first gap (221) is arranged between the first secondary portion (112) and the second secondary portion (122), and at least a part of the first secondary portion (112) and at least a part of the second secondary portion (122) extend straight, in parallel, and within an imaginable plane (P). The wall (200) is configured such that particulate material is able to propagate through the first gap (221) from a first side (S1) of the plane (P) to the opposite second side (S2) of the plane (P). The wall (200) comprises a refractory (230) arranged on at least one side of a part of the first secondary portion (112) and a part of the second secondary portion (122). A fluidized bed boiler comprising the wall (200).

公开(公告)号：EP3278027B8

公开(公告)日：2024-03-20

申请号：EP16711857.9

申请日：2016-03-29

发明人： PUCCI, Egidio ,  PROVENZALE, Michele

IPC分类号： F23M5/04 ,  F23R3/00 ,  F23R3/60

公开(公告)号：EP3224921B1

公开(公告)日：2024-03-06

申请号：EP15790343.6

申请日：2015-10-15

发明人： GLESIU, Frederick, Louis ,  DOYLE, John, Patrick ,  HOFFMAN, Alan, Rex ,  HAZELTON, Troy, David

IPC分类号： H02G15/02 ,  H01B3/08 ,  H01B3/40 ,  H01B7/295 ,  F23M11/04 ,  F23N5/08

公开(公告)号：EP4284122A1

公开(公告)日：2023-11-29

申请号：EP21921186.9

申请日：2021-11-04

申请人： Hitachi Zosen Corporation ,  National Institute Of Advanced Industrial Science and Technology

发明人： KAWABATA, Kaoru ,  ISE, Akifumi ,  SEGAWA, Takehiko

IPC分类号： H05H1/24 ,  H04N5/225 ,  H04N7/18 ,  F23M11/04

摘要： A monitoring device in accordance with an aspect of the present invention includes: a lens (4); a cover (5) covering a circumferential surface of the lens (4); and a plasma actuator (7) including a first electrode (71) that generates, toward a center axis (C) of the cover (5), at least one of a plasma (P) generated by a dielectric barrier discharge and an induced jet flow (F), the plasma actuator (7) removing dust (D) with use of at least one of the plasma (P) and the induced jet flow (F).

公开(公告)号：EP3922829B1

公开(公告)日：2023-11-08

申请号：EP21180970.2

申请日：2014-09-16

发明人： BOULDIN, Lee E. ,  MOURA, Dennis M. ,  EASTWOOD, Jonathan J. ,  PACHECO-TOUGAS, Monica

IPC分类号： F02C7/12 ,  F02C7/18 ,  F23R3/42 ,  F23M5/04 ,  F23R3/00 ,  F23R3/06 ,  F23R3/60

公开(公告)号：EP4242520A3

公开(公告)日：2023-11-01

申请号：EP23181568.9

申请日：2014-10-20

申请人： RTX Corporation

发明人： MOURA, Dennis M. ,  REZVANI, Reza

IPC分类号： F23R3/42 ,  F23M5/00 ,  F02C3/14 ,  F02C3/00 ,  F23R3/14 ,  F23R3/28 ,  F23R3/50 ,  F23R3/06

摘要： A combustor for a turbine engine includes an inner liner panel with a multiple of inner dilution passages. The multiple of dilution passages includes a repeating pattern of a first major inner air passage, a minor inner air passage, and a second major inner air passage. A combustor for a turbine engine includes an outer liner panel with a multiple of outer dilution passages. The multiple of outer dilution passages includes a repeating pattern of a first major outer air passage, a first minor outer air passage, a second major outer air passage, and a second minor outer air passage.

公开(公告)号：EP4253840A1

公开(公告)日：2023-10-04

申请号：EP23163666.3

申请日：2023-03-23

申请人： Hitachi Zosen Inova Steinmüller GmbH

发明人： Mozuch, Andreas

IPC分类号： F23L1/02 ,  F23L15/00 ,  F23M5/08 ,  F23H7/08 ,  F23H7/10 ,  F23L15/04 ,  F23H17/08

摘要： Die Erfindung betrifft einen Feuerrost (2a, 2b) für eine Müllverbrennungsanlage, aufweisend einen Rahmen (5) mit Seitenwänden (4a, 4b, 4c, 4d) und verdrehbar am Rahmen (5) gelagerten Torsionswellen (6a, 6b, 6c, 6d), die einen inneren Bereich (5a) des Rahmens (5) zumindest bereichsweise überdecken,
wobei die Torsionswellen (6a, 6b, 6c, 6d) mit einer Rostmechanik (8) wirkverbunden sind, welche dazu eingerichtet ist, die Torsionswellen (6a, 6b, 6c) zu verdrehen, wobei die Rostmechanik (8) an zumindest einer der Seitenwände (4b, 4d) des Rahmens (5) und dabei zumindest teilweise, vorzugsweise vollständig, außerhalb des inneren Bereiches (5a) des Rahmens (5) angeordnet ist.
Erfindungsgemäß ist vorgesehen, dass mindestens eine der Seitenwände (4a, 4b, 4c, 4d) des Rahmens (5) doppelwandig ausgebildet ist, so dass sich in der mindestens einen Seitenwand (4a, 4b, 4c, 4d) ein Innenraum (13a, 13b, 13c, 13d) ausbildet, und
der Rahmen (5) Eintritts-Öffnungen (10a, 10b) und Austritts-Öffnungen (10c, 10d) in der mindestens einen doppelwandigen Seitenwand (4a, 4b, 4c, 4d) aufweist, insbesondere an den Stirnseiten (11a, 11b, 11c, 11d), so dass ein Luftstrom (12) durch den jeweiligen Innenraum (13a, 13b, 13c, 13d) in der mindestens einen doppelwandigen Seitenwand (4a, 4b, 4c, 4d) strömen kann.

公开(公告)号：EP4235030A1

公开(公告)日：2023-08-30

申请号：EP23160757.3

申请日：2020-06-16

申请人： Raytheon Technologies Corporation

发明人： QUACH, San ,  STYBORSKI, Jeremy ,  KARANIAN, Caroline

IPC分类号： F23R3/00 ,  F23R3/06 ,  F23M5/02

摘要： A combustor of a gas turbine engine including a first forward liner panel (72A-1, 74A-1). The forward liner panel including a liner panel forward edge (130), a liner panel aft edge (132) opposite of the liner panel forward edge, and a first liner panel side edge (134) between the liner panel aft edge and the liner panel forward edge. The first liner panel side edge is non-perpendicular to the liner panel forward edge and oriented at an angle about perpendicular to a swirl flow (I, O) in the combustor.