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公开(公告)号:US11499478B2
公开(公告)日:2022-11-15
申请号:US16952921
申请日:2020-11-19
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Zedic Judd , John Pearson , Douglas Hollingshead , Bradley Tucker , Yogendra Sheoran
Abstract: An asymmetric inlet particle separator for a gas turbine engine includes an inlet having a first cross-sectional shape, and a duct downstream of the inlet. The duct includes a bend upstream from a splitter, a scavenge branch and an engine airflow branch. The splitter is outside of a line of sight from the inlet and the splitter separates the scavenge branch from the engine airflow branch. The asymmetric inlet particle separator includes an annulus downstream of the engine airflow branch configured to be coupled to the gas turbine engine. The annulus has a second cross-sectional shape, and the engine airflow branch transitions from the first cross-sectional shape to the second cross-sectional shape.
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公开(公告)号:US11674527B2
公开(公告)日:2023-06-13
申请号:US16895127
申请日:2020-06-08
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Zedic Judd , Yogendra Sheoran , Morris Anderson , Tyler Crowe
CPC classification number: F04D29/701 , F02C7/00 , F04D29/403 , F04D17/10 , F05D2220/32
Abstract: A ported shroud for a compressor associated with a gas turbine engine includes a primary inlet configured to be in fluid communication with the compressor, and the primary inlet is defined to extend along a central axis of the ported shroud. The ported shroud includes a bellmouth that surrounds the primary inlet, and a port plenum configured to be in fluid communication with the compressor. The port plenum extends along an axis that is transverse to the central axis of the ported shroud and transverse to a direction of fluid flow. The port plenum has a port plenum inlet defined about the axis, and the port plenum inlet is defined through the bellmouth such that a tortuous path is defined to the port plenum inlet. The port plenum including a port plenum outlet downstream from the port plenum inlet configured to be in fluid communication with the compressor.
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公开(公告)号:US20220154641A1
公开(公告)日:2022-05-19
申请号:US16952921
申请日:2020-11-19
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Zedic Judd , John Pearson , Douglas Hollingshead , Bradley Tucker , Yogendra Sheoran
Abstract: An asymmetric inlet particle separator for a gas turbine engine includes an inlet having a first cross-sectional shape, and a duct downstream of the inlet. The duct includes a bend upstream from a splitter, a scavenge branch and an engine airflow branch. The splitter is outside of a line of sight from the inlet and the splitter separates the scavenge branch from the engine airflow branch. The asymmetric inlet particle separator includes an annulus downstream of the engine airflow branch configured to be coupled to the gas turbine engine. The annulus has a second cross-sectional shape, and the engine airflow branch transitions from the first cross-sectional shape to the second cross-sectional shape.
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公开(公告)号:US20210381529A1
公开(公告)日:2021-12-09
申请号:US16895127
申请日:2020-06-08
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Zedic Judd , Yogendra Sheoran , Morris Anderson , Tyler Crowe
Abstract: A ported shroud for a compressor associated with a gas turbine engine includes a primary inlet configured to be in fluid communication with the compressor, and the primary inlet is defined to extend along a central axis of the ported shroud. The ported shroud includes a bellmouth that surrounds the primary inlet, and a port plenum configured to be in fluid communication with the compressor. The port plenum extends along an axis that is transverse to the central axis of the ported shroud and transverse to a direction of fluid flow. The port plenum has a port plenum inlet defined about the axis, and the port plenum inlet is defined through the bellmouth such that a tortuous path is defined to the port plenum inlet. The port plenum including a port plenum outlet downstream from the port plenum inlet configured to be in fluid communication with the compressor.
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