Mid-Turbine Frame with Fairing Attachment
    3.
    发明申请
    Mid-Turbine Frame with Fairing Attachment 有权
    带涡流机附件的中型涡轮机架

    公开(公告)号:US20150260057A1

    公开(公告)日:2015-09-17

    申请号:US14438562

    申请日:2013-09-11

    IPC分类号: F01D25/28

    摘要: A mid-turbine frame (MTF) system for a gas turbine engine is disclosed. The MTF includes an inner case, an outer case and a fairing sandwiched between the inner and outer cases. The fairing includes an inner ring spaced apart from and coupled to an outer ring by a plurality of hollow struts. The hollow struts accommodate support rods that connect the inner case to the outer case. Further, the hollow struts act as turning vanes for turning the flow of gases passing from a high pressure turbine (HPT) to a low pressure turbine (LPT) for purposes of providing the correct incidence angle to the first vane of the LPT. The outer ring of the fairing includes a plurality of bosses which receive attachment pins that pass through the outer case for correctly locating the fairing with respect to the outer case and for permitting radial expansion in contraction of the fairing.

    摘要翻译: 公开了一种用于燃气涡轮发动机的中涡轮机架(MTF)系统。 MTF包括夹在内壳和外壳之间的内壳,外壳和整流罩。 整流罩包括通过多个中空支柱间隔开并与外环连接的内圈。 中空支柱适应将内壳连接到外壳的支撑杆。 此外,为了向LPT的第一叶片提供正确的入射角,中空支柱用作转动叶片,用于将从高压涡轮(HPT)通过的气体流转向低压涡轮机(LPT)。 整流罩的外圈包括多个凸台,其接收穿过外壳的连接销,以便正确地将整流罩相对于外壳定位并允许整流罩收缩的径向膨胀。

    Internally cooled spoke
    6.
    发明授权
    Internally cooled spoke 有权
    内部冷却的辐条

    公开(公告)号:US09512738B2

    公开(公告)日:2016-12-06

    申请号:US13753821

    申请日:2013-01-30

    摘要: A turbine engine includes a compressor section, a combustor section in fluid communication with the compressor section, a high pressure turbine in fluid communication with the combustor, a low pressure turbine in fluid communication with the high pressure turbine, and a mid turbine frame located axially between the high pressure turbine and the low pressure turbine. The mid turbine frame includes an outer frame case, an inner frame case, and a plurality of hollow spokes that distribute loads from the inner frame case to the outer frame case. The spokes are hollow to allow cooling airflow to be supplied through the spokes to the inner frame case.

    摘要翻译: 涡轮发动机包括压缩机部分,与压缩机部分流体连通的燃烧器部分,与燃烧器流体连通的高压涡轮机,与高压涡轮机流体连通的低压涡轮机,以及位于轴向 在高压涡轮机和低压涡轮机之间。 中间涡轮机框架包括外框架壳体,内框架壳体和多个中空轮辐,其将负载从内框架壳体分配到外框架壳体。 轮辐是中空的,以允许冷却气流通过轮辐供应到内框架壳体。

    INTERNALLY COOLED SPOKE
    10.
    发明申请
    INTERNALLY COOLED SPOKE 审中-公开
    内部冷却SPOKE

    公开(公告)号:US20140137534A1

    公开(公告)日:2014-05-22

    申请号:US14166320

    申请日:2014-01-28

    IPC分类号: F01D25/14

    摘要: A turbine engine includes a compressor section, a combustor section in fluid communication with the compressor section, a high pressure turbine in fluid communication with the combustor, a low pressure turbine in fluid communication with the high pressure turbine, and a mid turbine frame located axially between the high pressure turbine and the low pressure turbine. The mid turbine frame includes an outer frame case, an inner frame case, and a plurality of hollow spokes that distribute loads from the inner frame case to the outer frame case. The spokes are hollow to allow cooling airflow to be supplied through the spokes to the inner frame case.

    摘要翻译: 涡轮发动机包括压缩机部分,与压缩机部分流体连通的燃烧器部分,与燃烧器流体连通的高压涡轮机,与高压涡轮机流体连通的低压涡轮机,以及位于轴向 在高压涡轮机和低压涡轮机之间。 中间涡轮机框架包括外框架壳体,内框架壳体和多个中空轮辐,其将负载从内框架壳体分配到外框架壳体。 轮辐是中空的,以允许冷却气流通过轮辐供应到内框架壳体。