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    ASSEMBLAGE D'ÉTANCHÉITÉ POUR TURBOMACHINE
    2.
    发明公开
    ASSEMBLAGE D'ÉTANCHÉITÉ POUR TURBOMACHINE 审中-公开
    密封装置用于涡轮机

    公开(公告)号：EP2935897A1

    公开(公告)日：2015-10-28

    申请号：EP13818354.6

    申请日：2013-12-18

    申请人： Turbomeca

    发明人： BRILLET, Christophe, Michel, Georges, Marcel ,  CHABANNE, Pierre ,  GIRARDOT, Julien ,  SCUILLER, Lionel

    IPC分类号： F04D29/063 ,  F04D29/16

    CPC分类号： F04D29/063 ,  F01D11/04 ,  F04D29/083 ,  F04D29/102 ,  F04D29/124 ,  F04D29/162 ,  F05D2220/3217

    摘要： The invention relates to a turbomachine comprising an air compression stage (2) comprising at least one moving compressor wheel (20), an air intake pipe (4) coupled to said air compression stage (2), a first sealing device (54) positioned between a front portion (56) of the moving compressor wheel (20) and the air intake pipe (4) comprising at least one pressure seal (60), a channel (45) for conveying air compressed by the moving wheel (20) and a second sealing device (64) positioned between a rear portion (66) of the moving compressor wheel (20) and the conveyance channel (45) and configured to receive an air flow (F2) coming from the conveyance channel (45), the turbomachine being remarkable in that the second sealing device (64) is configured to allow a withdrawal (F3) of part of the air passing through it and in that the withdrawn air (F3) is conveyed to the pressure seal (60) of the first sealing device (54) so as to keep it pressurized.

    COOLING AIR INTERCOOLING WITH COOLING AIR TAPPED FROM PLURAL LOCATIONS
    9.
    发明公开
    COOLING AIR INTERCOOLING WITH COOLING AIR TAPPED FROM PLURAL LOCATIONS 审中-公开
    KÜHLLUFT-ZWISCHENKÜHLUNG麻省理工学院KÜHLLUFTABGEZAPFUNGVON MEHREREN ORTEN

    公开(公告)号：EP3085924A1

    公开(公告)日：2016-10-26

    申请号：EP16166724.1

    申请日：2016-04-22

    申请人： United Technologies Corporation

    发明人： SUCIU, Gabriel L. ,  CHANDLER, Jesse M. ,  STAUBACH, Joseph Brent ,  MERRY, Brian D.

    IPC分类号： F02C3/13 ,  F02C7/18 ,  F02C9/18

    CPC分类号： F04D29/5826 ,  F01D25/12 ,  F02C3/13 ,  F02C6/08 ,  F02C7/143 ,  F02C7/185 ,  F02C9/18 ,  F04D29/5833 ,  F05D2220/3212 ,  F05D2220/3217 ,  F05D2220/3219 ,  F05D2260/211 ,  F05D2260/213 ,  F05D2260/606 ,  F05D2270/3062 ,  Y02T50/675

    摘要： A gas turbine engine (121) comprises a main compressor section having a high pressure compressor (141) with a downstream most end (140), and more upstream locations (126). A turbine section has a high pressure turbine (144). A first tap taps air from at least one of the more upstream locations (126) in the main compressor section, passes the tapped air through a heat exchanger (122) and then to a cooling compressor (124). The cooling compressor (124) compresses air downstream of the heat exchanger (122). A second tap taps air from a location closer to the downstream most end (140) than the location(s) (126) of the first tap. The first and second tap mix together and are delivered into the high pressure turbine (144). An intercooling system for a gas turbine engine (121) is also disclosed.

    摘要翻译： 燃气涡轮发动机（121）包括主压缩机部分，其具有具有下游最末端（140）的高压压缩机（141）和更多的上游位置（126）。 涡轮部分具有高压涡轮机（144）。 第一分接头从主压缩机部分中的更上游位置（126）中的至少一个上抽出空气，将抽头的空气通过热交换器（122），然后传递到冷却压缩机（124）。 冷却压缩机124将热交换器122的下游的空气压缩。 第二分接头从第一分接头的位置（126）更接近下游最末端（140）的位置敲击空气。 第一和第二抽头混合在一起并被输送到高压涡轮机（144）中。 还公开了一种用于燃气涡轮发动机（121）的中间冷却系统。