Inducer assembly for a turbine engine

A turbine engine comprising:

• a compressor section which receives an ambient air stream and emits a compressed stream;
• a combustion section downstream of the compressor section;
• a turbine section downstream of the combustion section;
• a rotatable drive shaft coupling a portion of the turbine section with a portion of the compressor section and defining a rotational axis for the turbine engine;
• a bypass conduit coupling the compressor section to the turbine section while bypassing at least the combustion section to supply either a portion of the ambient air stream or a portion of the compressed stream to the turbine section to define a bypass stream;
• and
• at least one centrifugal separator fluidly coupled to the bypass stream, the at least one centrifugal separator having:
• a body defining a centerline, wherein the body includes an outer annular wall defining a through passage;
• a center body extending axially along the centerline within the through passage, spaced from the outer annular wall;
• a separator inlet fluidly coupled to the through passage, receiving the bypass stream;
• a fluidly coupled with the turbine section to output a reduced-particle stream that is provided to the turbine section for cooling;
• and
• an angular velocity increaser located within the through passage and coupled to the center body;
• a flow splitter located downstream of the angular velocity increaser, the flow splitter having an inner annular wall spaced radially inwardly from the outer annular wall, wherein the flow splitter is configured to split a radially-outward portion of the bypass stream from a radially-inward portion of the bypass stream such that the radially-outward portion of the bypass stream is a concentrated-particle stream and the radially-inward portion is the reduced-particle stream;
• a first outlet passage defined by the inner annular wall that receives the reduced-particle stream, wherein the first outlet passage fluidly couples an inlet defined by an upstream edge of the inner annular wall and a separator outlet,
• an angular velocity decreaser coupled to the center body and located within the first outlet passage;
• and
• a second outlet passage defined by the outer annular wall and the inner annular wall, wherein the second outlet passage receives the concentrated-particle stream comprising separated particles, wherein the second outlet passage includes a particle outlet located axially downstream of the angular velocity decreaser, and wherein the second outlet passage includes an axially-increasing cross-section, such that a cross-section of the second outlet passage at the inlet is smaller than a cross-section of the second outlet passage downstream of the inlet;
• wherein the center body includes a first diameter measured at the angular velocity increaser and a second diameter measured at a portion of the center body located downstream of the angular velocity increaser and upstream of the angular velocity decreaser, wherein the first diameter is greater than the second diameter.

A turbine engine comprising:

• a compressor section which receives an ambient air stream and emits a compressed stream;
• a combustion section which receives the compressed stream and emits a combustion stream which is at a higher temperature than the compressed stream;
• a turbine section which receives the combustion stream and emits an exhaust stream which is at a lower temperature than the combustion stream;
• a rotatable drive shaft coupling a portion of the turbine section with a portion of the compressor section and defining a rotational axis for the turbine engine;
• a bypass conduit coupling the compressor section to the turbine section while bypassing at least the combustion section to supply either a portion of the ambient air stream or a portion of the compressed stream to the turbine section to define a bypass stream;
• at least one centrifugal separator fluidly coupled to the bypass stream, the at least one centrifugal separator having:
• a body defining a centerline, wherein the body includes an outer annular wall defining a through passage;
• a center body extend axially along the centerline within the through passage, spaced from the outer annular wall;
• a separator inlet fluidly coupled to the through passage, receiving the bypass stream;
• a separator outlet fluidly coupled with the turbine section to output a reduced-particle stream that is provided to the turbine section for cooling;
• an angular velocity increaser located within the through passage and coupled to the center body;
• a flow splitter located downstream of the angular velocity increaser, the flow splitter having an inner annular wall spaced radially-inwardly from the outer annular wall, wherein the flow splitter is configured to split a radially-outward portion of the bypass stream from a radially-inward portion of the bypass stream such that the radially-outward portion of the bypass stream is a concentrated-particle stream and the radially-inward portion is the reduced-particle stream;
• a first outlet passage defined by the inner annular wall that receives the reduced-particle stream, wherein the first outlet passage fluidly couples an inlet defined by an upstream edge of the inner annular wall and the separator outlet, and wherein a portion of the first outlet passage includes an axially-decreasing cross-section;
• an angular velocity decreaser located downstream of the flow splitter;
• and
• a second outlet passage defined by the outer annular wall and the inner annular wall, wherein the second outlet passage receives the concentrated-particle stream comprising separated particles;
• and
• an inducer, wherein a portion of the inner annular wall is received within a flow passage of the inducer.