公开(公告)号：US20250052189A1

公开(公告)日：2025-02-13

申请号：US18366249

申请日：2023-08-07

Applicant: General Electric Company

Inventor： Arthur W. Sibbach ,  Rudolf Selmeier ,  Lajith Vijayan ,  Rakshit Tirumala

IPC: F02C3/30 ,  F02K3/06

Abstract: A turbine engine for an aircraft includes a fan that rotates to generate a volume of air, a core turbine engine, a nacelle, and a steam system. The core turbine engine includes a combustor that generates combustion gases, and a turbine including a shaft. The combustor and the turbine define a core air flowpath. The fan is drivingly coupled to the shaft. The nacelle circumferentially surrounds the fan and defines a bypass airflow passage between the nacelle and the core turbine engine. The volume of air flows into the bypass airflow passage as bypass air and flows into the core air flowpath as core air. The steam system extracts water from the combustion gases, vaporizes the water to generate steam, and injects the steam into the core air flowpath to add mass flow to the core air. A bypass ratio of the turbine engine is greater than 18:1.

公开(公告)号：US20140130513A1

公开(公告)日：2014-05-15

申请号：US13673117

申请日：2012-11-09

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Ya-tien Chiu ,  John David Stampfli ,  Rudolf Selmeier

IPC: F02C3/06 ,  F04D19/00 ,  F04D27/00

CPC classification number: F02C3/06 ,  F01D17/162 ,  F04D19/00 ,  F04D21/00 ,  F04D27/002 ,  F04D27/0246 ,  F05D2260/15

Abstract: A compressor section of a gas turbine generally includes a stage of inlet guide vanes positioned adjacent to an inlet of the compressor section and a stage of rotor blades disposed downstream from the inlet guide vanes. A stage of stator vanes is positioned downstream from the stage of rotor blades. The stage of stator blades includes a row of leading guide vanes having a trailing edge. A row of trailing guide vanes coupled to an actuator is disposed between two corresponding adjacent leading guide vanes. Each of the trailing guide vanes includes a trailing edge. The leading edge of each trailing guide vane is disposed upstream of the trailing edge of a corresponding leading guide vane when the trailing guide vane is in an open position and downstream from the trailing edge of the corresponding leading guide vane when the trailing guide vane is in a closed position.

Abstract translation: 燃气涡轮机的压缩机部分通常包括邻近压缩机部分的入口设置的入口引导叶片的台和设置在入口导叶的下游的转子叶片的台。 定子叶片的一级位于转子叶片的下游。 定子叶片的阶段包括一排具有后缘的导向导叶。 连接到致动器的一排尾导叶设置在两个对应的相邻的导向叶片之间。 每个拖尾导叶包括后缘。 当拖尾导叶处于打开位置并且当牵引导叶处于相对应的导向叶片的后缘的下游时，每个拖尾导叶的前缘设置在对应的导向叶片的后缘的上游 关闭位置