COMPOSITE MATERIAL INLET PLENUM AND GAS TURBINE ENGINE SYSTEM COMPRISING SAID PLENUM
    1.
    发明申请
    COMPOSITE MATERIAL INLET PLENUM AND GAS TURBINE ENGINE SYSTEM COMPRISING SAID PLENUM 审中-公开
    复合材料入口气体和气体涡轮发动机系统

    公开(公告)号:WO2014177658A1

    公开(公告)日:2014-11-06

    申请号:PCT/EP2014/058916

    申请日:2014-04-30

    Abstract: An air inlet plenum for a gas turbine engine is described. The air inlet plenum (3) comprises a hollow body (17) having an air inlet aperture (19) and an air outlet aperture (21) arranged and configured for connection to the gas turbine engine (6). The air inlet plenum (3) comprises at least one removable portion (23L, 23R), which is removable from the hollow body (17) when the air inlet plenum (3) is connected to a gas turbine engine (6). The air inlet plenum is at least partly made of fiber-reinforced plastic.

    Abstract translation: 描述了用于燃气涡轮发动机的进气室。 空气入口通风室(3)包括具有空气入口孔(19)和排气孔(21)的空心体(17),空气出口孔(21)布置和构造成用于连接到燃气涡轮发动机(6)。 空气入口增压室(3)包括至少一个可移除部分(23L,23R),当空气入口增压室(3)连接到燃气涡轮发动机(6)时,该可移除部分可从空心体(17)移除。 空气入口增压室至少部分由纤维增强塑料制成。

    METHODS OF WASHING GAS TURBINE ENGINES AND GAS TURBINE ENGINES
    2.
    发明申请
    METHODS OF WASHING GAS TURBINE ENGINES AND GAS TURBINE ENGINES 审中-公开
    清洗燃气涡轮发动机和燃气涡轮发动机的方法

    公开(公告)号:WO2015082609A1

    公开(公告)日:2015-06-11

    申请号:PCT/EP2014/076562

    申请日:2014-12-04

    Abstract: Washing of the gas turbine engine, during operation of the gas turbine engine, comprises a washing phase that consists in spraying (4) a detergent liquid substance towards the inlet of the compressor (1) of the engine; the mass flow of the detergent liquid substance to be sprayed is set so that the liquid-to-gas ratio at the inlet of the compressor (1) is more than 1% and less than 5% with reference to the rated mass flow of the compressor (1); the washing phase comprises a first sub-phase during which the flow of the detergent liquid substance is increased gradually and a second sub-phase during which the flow of the detergent liquid substance is maintained constant.

    Abstract translation: 燃气涡轮发动机在燃气涡轮发动机运行期间的清洗包括洗涤阶段,其包括将洗涤剂液体物质喷射到发动机的压缩机(1)的入口; 设定要喷射的洗涤剂液体物质的质量流量,使得压缩机(1)入口处的液体与气体的比率相对于所述压缩机(1)的额定质量流量大于1%且小于5% 压缩机(1); 洗涤阶段包括洗涤剂液体物质的流动逐渐增加的第一子阶段和洗涤液体的流动保持恒定的第二子阶段。

    WASHING NOZZLES AND GAS TURBINE ENGINES
    3.
    发明申请
    WASHING NOZZLES AND GAS TURBINE ENGINES 审中-公开
    清洗喷嘴和气体涡轮发动机

    公开(公告)号:WO2015082610A1

    公开(公告)日:2015-06-11

    申请号:PCT/EP2014/076563

    申请日:2014-12-04

    Abstract: The nozzle (4) is used for spraying a liquid substance towards a compressor (1) of a gas turbine engine, and comprises: - an elongated body (20) having an end for ejecting the liquid substance, - a conduit (21) for said liquid substance internal to said elongated body (20) and extending up to said end, - a recess (22) located at said end, wherein said conduit (21) ends in said recess (22); wherein said recess (22) opens towards the lateral surface of said elongated body (20), typically a cylindrical body, and said conduit (21) is tangential to the bottom of said recess (22).

    Abstract translation: 喷嘴(4)用于朝向燃气涡轮发动机的压缩机(1)喷射液体物质,并且包括: - 具有用于喷射液体物质的端部的细长主体(20), - 用于 所述液体物质在所述细长体(20)内部并延伸到所述端部, - 位于所述端部处的凹部(22),其中所述导管(21)终止于所述凹部(22)中。 其中所述凹部(22)朝向所述细长主体(20)的侧表面开口,通常为圆柱体,并且所述导管(21)与所述凹部(22)的底部相切。

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