BRENNKAMMER ZUR DAMPFKÜHLUNG EINER BRENNKAMMER
    6.
    发明授权
    BRENNKAMMER ZUR DAMPFKÜHLUNG EINER BRENNKAMMER 有权
    燃烧室燃烧室蒸汽冷却

    公开(公告)号:EP1032791B2

    公开(公告)日:2008-01-23

    申请号:EP98962217.0

    申请日:1998-11-06

    发明人: LIEBE, Roland

    IPC分类号: F23R3/00

    摘要: The invention relates to a wall structure (3) with an intermediate partition (12) between an inner wall (6) and an outer wall (7). An inlet (9) leading to an external cooling area (13) located in between the outer wall and the intermediate partition (12) and an outlet (10) leading to an inner cooling area (10) located in between the intermediate partition (12) and the inner wall (6) are provided for the cooling liquid, especially for cooling vapour (14). The intermediate partition (12) has openings (15) allowing cooling fluid (11) to flow through. The invention further relates to a method for cooling a gas turbine combustion chamber (1) with vapour.

    RINGBRENNKAMMER FÜR EINE GASTURBINE
    7.
    发明公开
    RINGBRENNKAMMER FÜR EINE GASTURBINE 审中-公开
    环燃烧室的燃气涡轮机

    公开(公告)号:EP1446614A1

    公开(公告)日:2004-08-18

    申请号:EP02802992.4

    申请日:2002-11-07

    发明人: LIEBE, Roland

    IPC分类号: F23R3/00 F23R3/50 F23R3/60

    摘要: An annular combustion chamber (RBK) for a gas turbine is disclosed, which permits a sealed air cooling, such that high powers and efficiencies can be achieved with low NOx emissions. The two-piece annular combustion chamber housing (1,3) surrounds a thin-walled sealed liner (4,41), which guides the hot gas escaping from the burners (5) to the turbine inlet (8) in a gas-tight manner. A variable annular chamber (7) is located between the liner and the annular combustion chamber housing (1,3), in which the cooling air is collected as a counter-current to the hot gas and fed to the burners (5) ( closed air cooling ). The surfaces of the liner (4,41) are variably cooled with efficient baffle cooling devices (14) and drilled patterns in (1,3). The thermally-elastic liner constructed from submerged arc-welded rings is axially fixed at the flange (36) only and for the remainder provided with reinforcing circumferential beading. The freely expanding liner (4,41) is otherwise concentrically fixed to the cold annular combustion chamber housing (1,3) by means of elastic tensioning elements (10). The above efficient, economical and simple construction further offers significant service advantages due to the following construction features:- the burners (5) can be completely (dis)assembled from outside without opening the housing. Both the liner (4, 41) and also a ring which integrates the first row of turbine guide vanes in the annular combustion chamber can be removed as service pieces in other words exchanged without opening the turbine and compressor housing and without removal of a rotor.

    BRENNKAMMER SOWIE VERFAHREN ZUR DAMPFKÜHLUNG EINER BRENNKAMMER
    8.
    发明授权
    BRENNKAMMER SOWIE VERFAHREN ZUR DAMPFKÜHLUNG EINER BRENNKAMMER 有权
    燃烧室燃烧室蒸汽冷却

    公开(公告)号:EP1032791B1

    公开(公告)日:2002-08-07

    申请号:EP98962217.0

    申请日:1998-11-06

    发明人: LIEBE, Roland

    IPC分类号: F23R3/00

    摘要: The invention relates to a wall structure (3) with an intermediate partition (12) between an inner wall (6) and an outer wall (7). An inlet (9) leading to an external cooling area (13) located in between the outer wall and the intermediate partition (12) and an outlet (10) leading to an inner cooling area (10) located in between the intermediate partition (12) and the inner wall (6) are provided for the cooling liquid, especially for cooling vapour (14). The intermediate partition (12) has openings (15) allowing cooling fluid (11) to flow through. The invention further relates to a method for cooling a gas turbine combustion chamber (1) with vapour.

    BRENNKAMMER SOWIE VERFAHREN ZUR DAMPFKÜHLUNG EINER BRENNKAMMER
    9.
    发明公开
    BRENNKAMMER SOWIE VERFAHREN ZUR DAMPFKÜHLUNG EINER BRENNKAMMER 有权
    燃烧室和燃烧室蒸汽冷却方法

    公开(公告)号:EP1032791A1

    公开(公告)日:2000-09-06

    申请号:EP98962217.0

    申请日:1998-11-06

    发明人: LIEBE, Roland

    IPC分类号: F23R3/00

    摘要: The invention relates to a wall structure (3) with an intermediate partition (12) between an inner wall (6) and an outer wall (7). An inlet (9) leading to an external cooling area (13) located in between the outer wall and the intermediate partition (12) and an outlet (10) leading to an inner cooling area (10) located in between the intermediate partition (12) and the inner wall (6) are provided for the cooling liquid, especially for cooling vapour (14). The intermediate partition (12) has openings (15) allowing cooling fluid (11) to flow through. The invention further relates to a method for cooling a gas turbine combustion chamber (1) with vapour.