Trilobe mounting with anti-rotation apparatus for an air duct in a gas
turbine rotor
    1.
    发明授权
    Trilobe mounting with anti-rotation apparatus for an air duct in a gas turbine rotor 失效
    三叶安装在燃气轮机转子中用于空气管道的防旋转装置

    公开(公告)号:US6053697A

    公开(公告)日:2000-04-25

    申请号:US105478

    申请日:1998-06-26

    摘要: An air duct assembly for a gas turbine compressor rotor in a gas turbine engine is described. The rotor includes a compressor spool shaft and at least one stage disk, and the air duct assembly includes an elongate hollow cylindrical air duct configured to couple to a stage disk at a first end of the air duct. The second end of the air duct is configured to couple to the spool shaft. The second end of the air duct includes a plurality of lobes depending radially inward, a spool shaft insert configured to fit into an opening in the spool shaft, and a plurality of pins coupled to the spool shaft insert and configured to extend from the insert and to engage the lobes of the second end of the air duct.

    摘要翻译: 描述了一种用于燃气涡轮发动机中的燃气轮机压缩机转子的空气管道组件。 转子包括压缩机线轴和至少一个级盘,并且空气管道组件包括细长的中空圆柱形空气管道,其被配置为在空气管道的第一端处耦合到平台盘。 风道的第二端构造成联接到卷轴。 空气管道的第二端包括多个沿径向向内的突起,构造成装配到卷筒轴中的开口中的卷轴轴插入件,以及耦合到卷轴轴插入件并被构造成从插入件延伸的多个销 以接合空气管道的第二端的叶片。

    Turbine rotor disk post cooling system
    2.
    发明授权
    Turbine rotor disk post cooling system 失效
    涡轮转子盘后冷却系统

    公开(公告)号:US5388962A

    公开(公告)日:1995-02-14

    申请号:US136143

    申请日:1993-10-15

    IPC分类号: F01D5/08 F01D5/30 F01D11/00

    摘要: The present invention discloses a system for cooling turbine rotor disk posts in a gas turbine engine with a preferred embodiment illustrating an application for a high pressure turbine stage 1 rotor disk. The disk includes a plurality of circumferentially alternating posts and slots disposed about the periphery of the disk with each slot receiving a dovetail of a radially extending blade. The cooling system comprises a plurality of seal bodies with each seal body including a relatively low volume thermal isolation chamber positioned over the top of a corresponding disk post; a plurality of axially extending blade cooling plenums supplied with cooling air with one of the plenums positioned radially inward of each of the blades; a plurality of shallow, radially extending slots formed in a relatively low stressed axially facing surface of each of the blade dovetails for diverting cooling air from the blade cooling plenums to the thermal isolation chambers. Cooling air flows from the blade cooling plenums through the slots into a radially extending plenum which supplies at least one hole in each seal body. The holes are in flow communication with the thermal isolation chambers and are oriented to cause the cooling air to impinge directly on the outer surface of each of the disk posts.

    摘要翻译: 本发明公开了一种用于冷却燃气涡轮发动机中的涡轮机转子盘柱的系统,其中优选实施例示出了用于高压涡轮级1转子盘的应用。 盘包括围绕盘的周边设置的多个周向交替的柱和槽,每个槽容纳径向延伸叶片的燕尾。 冷却系统包括多个密封体,每个密封体包括位于相应的圆柱的顶部上的相对低体积的热隔离室; 多个轴向延伸的叶片冷却气室,其供应有冷却空气,其中一个气室位于每个叶片的径向内侧; 多个浅的,径向延伸的狭槽形成在每个叶片燕尾榫的相对低应力的轴向面对的表面中,用于将冷却空气从叶片冷却风室转移到热隔离室。 冷却空气从叶片冷却气室通过狭槽流入径向延伸的气室,其在每个密封体中提供至少一个孔。 孔与热隔离室流动连通,并且被定向成使得冷却空气直接撞击在每个盘柱的外表面上。

    Liquid-cooled turbine rotor
    3.
    发明授权
    Liquid-cooled turbine rotor 失效
    液冷式涡轮转子

    公开(公告)号:US4184797A

    公开(公告)日:1980-01-22

    申请号:US842407

    申请日:1977-10-17

    摘要: An arrangement is provided for supplying liquid coolant to liquid-cooled turbine buckets of a gas turbine power plant. The buckets have internal coolant passages and the outer rims of turbine discs have coolant channels which communicate coolant from the discs to the passages in the buckets. The forward, intermediate and aft discs with sealing spacers interposed between adjacent discs are mounted on a shaft. The arrangement includes a forward flange, an intermediate flange and an aft flange. The flanges are adjacent to the corresponding discs. The forward and aft flanges, the discs and the spacers have a plurality of aligned axially extending apertures circumferentially disposed about the shaft. Bolts extend through the apertures to secure the discs, spacers and flanges in abutting contact. Each of the interposed spacers cooperates with a corresponding disc to form a circumferentially disposed chamber. In order to supply liquid coolant to the rotor, the shaft includes an axially extending passage for liquid coolant having openings radially inwardly of the flanges for discharging coolant onto the flanges. The flanges direct the coolant, under influence of centrifugal force, to the discs. The discs include means for communicating coolant from the forward flange to a forward chamber, from the intermediate flange to an intermediate chamber and from the aft flange to an aft chamber. The forward, intermediate and aft chambers direct coolant, under influence of centrifugal force, to the outer rim channels in the corresponding discs.

    摘要翻译: 提供了一种用于将液体冷却剂供应到燃气轮机发电厂的液冷涡轮机叶片的装置。 铲斗具有内部冷却剂通道,并且涡轮盘的外缘具有冷却剂通道,其将冷却剂从盘连接到桶中的通道。 具有插入在相邻盘之间的密封垫片的前,中和后盘安装在轴上。 该装置包括前凸缘,中间凸缘和后凸缘。 凸缘与相应的圆盘相邻。 前法兰和后法兰,盘和间隔件具有围绕轴周向设置的多个对准的轴向延伸的孔。 螺栓延伸穿过孔,以将盘,间隔件和凸缘固定在邻接的位置。 每个插入的间隔物与相应的盘配合以形成周向布置的腔室。 为了向转子供应液体冷却剂,轴包括用于液体冷却剂的轴向延伸的通道,其具有用于将冷却剂排放到凸缘上的法兰的径向向内的开口。 法兰将离心力影响下的冷却液引导到圆盘上。 盘包括用于将冷却剂从前法兰连通到前室,从中间凸缘到中间室以及从后凸缘到后室的装置。 前,后,后室在离心力影响下将冷却液直接引向相应光盘的外缘通道。