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A GAS TURBINE ENGINE

机译:燃气轮机

摘要

There is disclosed a turboshaft engine having principal rotational axis and comprising power turbine, tail bearing housing and exhaust collector arranged in axial flow series along said axis. The tail bearing housing has radially central region defining flow chamber for cooling air; and an annular duct defined around the central region and which forms at least part of exhaust flow passage for the flow of exhaust gases from the power turbine to the exhaust collector. The flow chamber is provided in fluid communication with said exhaust collector via at least one exhaust port formed in the tail bearing housing such that the flow of exhaust gases along said exhaust collector during operation of the engine educes flow of cooling air through the central flow chamber by drawing air through the or each exhaust port and into the exhaust collector. A related method of operating a turboshaft engine is also disclosed.
机译:公开了一种涡轮轴发动机,其具有主旋转轴线,并且包括动力涡轮,尾轴承壳体和沿所述轴线成轴向流序列布置的排气收集器。尾部轴承箱具有径向中央区域,该中央区域限定了用于冷却空气的流动室。环形导管围绕中心区域限定,并且该环形导管形成排气流动通道的至少一部分,以用于使排气从动力涡轮机流向排气收集器。流动室设置成通过形成在尾轴承壳体中的至少一个排气口与所述排气收集器流体连通,从而使得在发动机运行期间沿着所述排气收集器的排气流产生通过中央流动室的冷却空气流。通过从每个排气口或每个排气口吸入空气并进入排气收集器。还公开了一种操作涡轮轴发动机的相关方法。

著录项

  • 公开/公告号US2018135448A1

    专利类型

  • 公开/公告日2018-05-17

    原文格式PDF

  • 申请/专利权人 ROLLS-ROYCE PLC;

    申请/专利号US201615567540

  • 发明设计人 BORJA NAVAS;PETER LEYMAN;LEE DAVITT;

    申请日2016-04-29

  • 分类号F01D9/06;F01D9/04;F01D11/06;F01D25/16;F01D25/12;F01D25/30;

  • 国家 US

  • 入库时间 2022-08-21 13:05:17

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