Aircraft propulsion system with multi-direction bleed valve

An assembly for an aircraft propulsion system, comprising:

• an engine core including a compressor section, a combustor section, a turbine section and a core flowpath extending sequentially through the compressor section, the combustor section and the turbine section;
• a bypass duct comprising a bypass flowpath outside of the engine core;
• and
• a bleed circuit including a bleed passage and a flow regulator;
• the bleed circuit configured to direct bypass gas through the bleed passage from the bypass flowpath into the core flowpath when the flow regulator is in an open position;
• and
• the bleed circuit configured to cutoff gas flow through the bleed passage between the bypass flowpath and the core flowpath when the flow regulator is in a closed position;
• wherein the flow regulator is configured to move to:
• the open position where the flow regulator opens a first aperture into the bypass duct, and the closed position where the flow regulator closes the first aperture;
• wherein the flow regulator is configured to move to a second open position where the flow regulator opens a second aperture into the bypass duct;
• and
• wherein the flow regulator closes the second aperture when in the closed position.

An assembly for an aircraft propulsion system, comprising:

• an engine core including a compressor section, a combustor section, a turbine section and a core flowpath extending sequentially through the compressor section, the combustor section and the turbine section;
• a bypass duct comprising a bypass flowpath outside of the engine core;
• a bleed passage fluidly coupled with the core flowpath;
• and
• a flow regulator configured to
• fluidly couple the bleed passage with a first opening into the bypass flowpath during a first mode, and fluidly decouple the bleed passage from a second opening into the bypass flowpath during the first mode;
• and
• fluidly couple the bleed passage with the second opening into the bypass flowpath during a second mode, and fluidly decouple the bleed passage from the first opening during the second mode.