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    CLEANING DEVICE FOR JET ENGINES AND CLEANING METHOD
    4.
    发明公开
    CLEANING DEVICE FOR JET ENGINES AND CLEANING METHOD 审中-公开

    公开(公告)号：EP3513883A1

    公开(公告)日：2019-07-24

    申请号：EP18382028.1

    申请日：2018-01-19

    申请人： Airbus Operations, S.L.U.

    发明人： CHIABRANDO, Marcos, Javier ,  RAMOS PAUL LASTRA, Pedro, Felipe

    IPC分类号： B08B7/02 ,  F01D25/00 ,  F23R3/44 ,  F23J3/02

    摘要： Cleaning device and method for jet engines comprising a vibration generator unit (1) that is fixed to a main body (2) that is operatively connectable with a first end (3') of a vibration transmitter element (3) having an elongated configuration, the vibration transmitter element (3) having likewise a second end (3"), opposite to the first end (3'), the second end (3") being configured to contact a inner side of the combustor (A) of the jet engine, and the vibration transmitter element (3) being able to be introduced across an engine injector hole (B) and a combustor injector hole (A') of the jet engine.

    Duct assembly including a helicoidal structure and gas turbine combustor including the same
    5.
    发明公开
    Duct assembly including a helicoidal structure and gas turbine combustor including the same 审中-公开

    公开(公告)号：EP3457028A1

    公开(公告)日：2019-03-20

    申请号：EP18190356.8

    申请日：2018-08-23

    申请人： Doosan Heavy Industries & Construction Co., Ltd

    发明人： KIM, Geun Cheol

    IPC分类号： F23R3/00 ,  F23R3/04 ,  F23R3/12 ,  F23R3/44

    摘要： A helicoidal structure promotes cooling of a liner (1250) applied in an annular space of a double-shell structure formed of the liner (1250) and a flow sleeve (1270) to cool a duct assembly, by increasing the residence time and cooling area of cooling compressed air (A) on the surface of the liner (1250). The helicoidal structure includes a helicoidal rib (100) protruding from a surface of the liner (1250) to guide the cooling compressed air (A) at a predetermined angle with respect to an axial direction of the liner (1250), the helicoidal rib (100) having cooling holes (200) and forming a first cooling passage (310) along which main-cooling compressed air flows and a plurality of secondary cooling passages (320) along which auxiliary-cooling compressed air flows. The plurality of secondary cooling passages (320) induces a flow of the auxiliary-cooling compressed air through the cooling holes (200), and the flow of the auxiliary-cooling compressed air is derived from a flow of the main-cooling compressed air in the first cooling passage (310).

    COMBUSTOR HAVING A FLOW SLEEVE
    7.
    发明授权
    COMBUSTOR HAVING A FLOW SLEEVE 有权

    公开(公告)号：EP2375161B1

    公开(公告)日：2018-07-25

    申请号：EP11161552.2

    申请日：2011-04-07

    申请人： General Electric Company

    发明人： Chila, Ronald James ,  Watts, Martin Ronald ,  Wu, Sheng-Yi

    IPC分类号： F23R3/02 ,  F23R3/44

    CPC分类号： F23R3/02 ,  F23R3/44 ,  F23R2900/03043

    摘要： A combustor (10) is provided and includes a liner (20) through which fluid fed from at least two injection points flows from a head end (22) to an interior of a transition piece (23), a first one of the at least two injection points being axially proximate to a fluid impenetrable coupling (50) between the liner (20) and the transition piece (23) and defining apertures (60) disposed in fluid communication with a first passage (35) leading to the head end (22), and a second one of the at least two injection points being disposed axially between the apertures (60) and the head end (22) and upstream from the apertures (60) relative to a direction of fluid flow through the first passage (35), the second one of the at least two injection points being formed of openings (100) disposed in fluid communication with a second passage (45) leading to the head end (22).

    BRENNKAMMERGEHÄUSE UND DAMIT AUSGERÜSTETE GASTURBINE
    10.
    发明公开
    BRENNKAMMERGEHÄUSE UND DAMIT AUSGERÜSTETE GASTURBINE 有权
    燃烧室机匣和如此装备燃气轮机

    公开(公告)号：EP2699848A1

    公开(公告)日：2014-02-26

    申请号：EP12717246.8

    申请日：2012-04-16

    申请人： MAN Diesel & Turbo SE

    发明人： ASCHENBRUCK, Emil ,  BRINKMANN, Reiner ,  HOFFMANN, Stefan

    IPC分类号： F23R3/04 ,  F23R3/44

    CPC分类号： F23R3/42 ,  F23M9/02 ,  F23R3/002 ,  F23R3/06 ,  F23R3/44 ,  F23R2900/03041

    摘要： The invention relates to a combustion chamber housing (10) and to a gas turbine (1) equipped therewith, wherein the combustion chamber housing has a flame tube (20) and a cladding tube (30) which surrounds the flame tube and which in the wall thereof has a plurality of through-holes (31) via which air flowing on the outside onto the cladding tube can radially penetrate into an intermediate space (40) formed between the cladding tube and the flame tube. The invention assures uniform distribution of the inflowing air around the flame tube. This is achieved, among other things, by providing a plurality of guide ribs (50), which are distributed in the intermediate space on the circumference of the two tubes and which each extend radially between the cladding tube and flame tube and parallel to a longitudinal direction (LR) of the two tubes such that the intermediate space is divided by the guide ribs into several longitudinal channels (41).