公开(公告)号：US20220074426A1

公开(公告)日：2022-03-10

申请号：US17014701

申请日：2020-09-08

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： John Schugardt ,  Katherine Smith

IPC: F04D29/44 ,  F02C3/08

Abstract: Turbine engine systems for interstage particle separation in multistage radial compressors are disclosed. The multistage radial compressor system includes an interstage region positioned between a first stage radial compressor and a second stage radial compressor. The interstage region includes a radially-outward oriented section, a longitudinally-oriented section, and a radially-inward oriented section. The radially-outward oriented section transitions to the longitudinally-oriented section at a first approximately 90-degree bend, and the longitudinally-oriented section transitions to the radially-inward oriented section at a second approximately 90-degree bend. The multistage radial compressor system further includes a particle separation system including an extraction slot and an aspiration slot located downstream from the extraction slot. The particle separation system is positioned along the interstage region outside of the air flow path. The extraction slot fluidly connects with a scavenge plenum, and the aspiration slot allows air from the scavenge plenum to recirculate back into the air flow path.

公开(公告)号：US10544693B2

公开(公告)日：2020-01-28

申请号：US15183274

申请日：2016-06-15

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Shakeel Nasir ,  John Schugardt ,  Justin Brown ,  Cristopher Frost

IPC: F01D9/06 ,  F04D29/44 ,  F02C3/04 ,  F04D17/02 ,  F04D29/28 ,  F04D29/32 ,  F04D29/42 ,  F04D29/52 ,  F04D29/54 ,  F01D9/04

Abstract: Provided is a radial diffuser that includes a housing, a plurality of diffuser vanes, and a plurality of deswirl vanes and at least one vane extension providing a service routing. Each of the vane extensions is disposed after a radial section and may extend into or through a transition and into the deswirl cascade. At least a portion of the vane extensions include a service passage extending therethrough. Each service passage is configured to allow a service conduit to extend therethrough without adversely crossing either a diffusion flow passage or a transition flow passage.

公开(公告)号：US10208628B2

公开(公告)日：2019-02-19

申请号：US15085625

申请日：2016-03-30

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Shakeel Nasir ,  John Schugardt ,  Nick Nolcheff ,  John Meier ,  Yogendra Yogi Sheoran ,  Shezan Kanjiyani ,  Daniel Aukland

IPC: F01D25/32 ,  F02C7/36 ,  F04D29/42 ,  F04D29/70

Abstract: A turbine engine incorporating a fine particle separation means includes a radial compressor that rotates about a longitudinal axis, a radially-oriented diffuser located downstream and radially outward, with respect to the longitudinal axis, from the radial compressor, and a flow path positioned downstream and radially outward, with respect to the longitudinal axis, from the diffuser, wherein the flow path comprises an outer annular wall and an inner annular wall between which the compressed air flows, and wherein the flow path comprises an arc the redirects the compressed air from flowing in a substantially radial flow direction to a substantially axial flow direction. The turbine engine further includes an extraction slot in the outer annular wall that fluidly connects with a scavenge plenum, the scavenge plenum being positioned adjacent to and radially outward from the outer annular wall at a position downstream axially along the flow path from the arc.