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公开(公告)号:US20220318973A1
公开(公告)日:2022-10-06
申请号:US17217427
申请日:2021-03-30
Applicant: Raytheon Technologies Corporation
Inventor: Amit Surana , Sudarshan N. Koushik , Kenji Homma
Abstract: A method for determining structural vibration mode characteristics includes preparing a digital image correlation (DIC) dataset for the component, applying a dynamic mode decomposition (DMD) technique to the DIC dataset to determine a plurality of DMD modes, selecting at least one dominant DMD mode from the plurality of DMD modes, classifying each of the at least one selected dominant DMD mode as a standing wave or a traveling wave, and determining structural vibration mode characteristics of the component by extracting the structural vibration mode characteristics from each of the at least one selected dominant DMD mode having a standing wave classification
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公开(公告)号:US11781485B2
公开(公告)日:2023-10-10
申请号:US17535270
申请日:2021-11-24
Applicant: RAYTHEON TECHNOLOGIES CORPORATION
Inventor: Julian Winkler , Kenji Homma , Craig Aaron Reimann , Jeffrey Michael Mendoza
CPC classification number: F02C7/24 , F02C7/045 , F23R3/002 , B32B2307/10 , F05D2240/35 , F05D2260/964 , F23R2900/00014 , F23R2900/03045
Abstract: A noise attenuation panel for a structure within a propulsion system includes a first plurality of unit cells; and a second plurality of unit cells, the second plurality of unit cells merged within the first plurality of unit cells, the first plurality of unit cells including a first periodic structure having a first unit cell, a second unit cell, a third unit cell and a fourth unit cell, each of the first unit cell, the second unit cell, the third unit cell and the fourth unit cell including a central body interconnected via a plurality of lateral tubes extending from the central body, the first periodic structure forming a first lateral layer of unit cells.
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公开(公告)号:US20230160343A1
公开(公告)日:2023-05-25
申请号:US17535270
申请日:2021-11-24
Applicant: RAYTHEON TECHNOLOGIES CORPORATION
Inventor: Julian Winkler , Kenji Homma , Craig Aaron Reimann , Jeffrey Michael Mendoza
CPC classification number: F02C7/24 , F23R3/002 , F23R2900/00014 , F23R2900/03045 , F05D2240/35 , F05D2260/964
Abstract: A noise attenuation panel for a structure within a propulsion system includes a first plurality of unit cells; and a second plurality of unit cells, the second plurality of unit cells merged within the first plurality of unit cells, the first plurality of unit cells including a first periodic structure having a first unit cell, a second unit cell, a third unit cell and a fourth unit cell, each of the first unit cell, the second unit cell, the third unit cell and the fourth unit cell including a central body interconnected via a plurality of lateral tubes extending from the central body, the first periodic structure forming a first lateral layer of unit cells.
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公开(公告)号:US20230117838A1
公开(公告)日:2023-04-20
申请号:US17503285
申请日:2021-10-16
Applicant: RAYTHEON TECHNOLOGIES CORPORATION
Inventor: Craig Aaron Reimann , Julian Winkler , Kenji Homma , Jeffrey Michael Mendoza , Ramons A. Reba
Abstract: An acoustic attenuation structure for a gas turbine engine includes a periodic structure having a first unit cell, the first unit cell having a first central body and a first axial tube disposed on the first central body and a second axial tube disposed on the first central body, opposite the first axial tube, each of the first axial tube and the second axial tube being in fluid communication with one another through the first central body.
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公开(公告)号:US20240210354A1
公开(公告)日:2024-06-27
申请号:US18088280
申请日:2022-12-23
Applicant: Raytheon Technologies Corporation
Inventor: Julian Winkler , Kenji Homma , Jeffrey L. Cipolla
CPC classification number: G01N29/02 , G01N29/24 , G01N2291/022 , G01N2291/106
Abstract: A resonator array panel includes a perforated first sheet, a second sheet, and a resonator core. The perforated first sheet includes a first sheet body. The second sheet includes a second sheet body. The second sheet body includes a second exterior side surface and a second interior side surface. The first resonator core is disposed between the perforated first sheet and the second sheet. The first resonator core includes a first plurality of sidewalls. The first plurality of sidewalls forms a first plurality of resonators between the perforated first sheet and the second sheet. The first plurality of resonators includes a first resonator. The first resonator includes a first viscoelastic body disposed within the first resonator cavity.
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公开(公告)号:US11565496B2
公开(公告)日:2023-01-31
申请号:US17067235
申请日:2020-10-09
Applicant: Raytheon Technologies Corporation
Inventor: John A. Sharon , Kenji Homma , Justin R. Hawkes , Paul R. Braunwart , Ellen Y. Sun
IPC: B32B3/28 , B32B15/04 , B32B5/02 , B32B15/02 , B32B15/14 , B32B15/18 , B32B15/20 , B32B27/12 , B32B3/26 , B64C1/40 , B64D33/02
Abstract: A structural panel includes a first skin, a second skin and a core. The core is connected to the first skin and the second skin. The core includes a corrugated sheet of wire mesh that includes a plurality of corrugations. Each of the corrugations extends vertically between and engages the first skin and the second skin.
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公开(公告)号:US20210023810A1
公开(公告)日:2021-01-28
申请号:US17067235
申请日:2020-10-09
Applicant: Raytheon Technologies Corporation
Inventor: John A. Sharon , Kenji Homma , Justin R. Hawkes , Paul R. Braunwart , Ellen Y. Sun
IPC: B32B3/28 , B32B15/04 , B32B5/02 , B32B15/02 , B32B15/14 , B32B15/18 , B32B15/20 , B32B27/12 , B32B3/26 , B64C1/40
Abstract: A structural panel includes a first skin, a second skin and a core. The core is connected to the first skin and the second skin. The core includes a corrugated sheet of wire mesh that includes a plurality of corrugations. Each of the corrugations extends vertically between and engages the first skin and the second skin.
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公开(公告)号:US11928811B2
公开(公告)日:2024-03-12
申请号:US17217427
申请日:2021-03-30
Applicant: Raytheon Technologies Corporation
Inventor: Amit Surana , Sudarshan N. Koushik , Kenji Homma
Abstract: A method for determining structural vibration mode characteristics includes preparing a digital image correlation (DIC) dataset for the component, applying a dynamic mode decomposition (DMD) technique to the DIC dataset to determine a plurality of DMD modes, selecting at least one dominant DMD mode from the plurality of DMD modes, classifying each of the at least one selected dominant DMD mode as a standing wave or a traveling wave, and determining structural vibration mode characteristics of the component by extracting the structural vibration mode characteristics from each of the at least one selected dominant DMD mode having a standing wave classification.
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公开(公告)号:US11830467B2
公开(公告)日:2023-11-28
申请号:US17503285
申请日:2021-10-16
Applicant: RAYTHEON TECHNOLOGIES CORPORATION
Inventor: Craig Aaron Reimann , Julian Winkler , Kenji Homma , Jeffrey Michael Mendoza , Ramons A. Reba
CPC classification number: G10K11/16 , F02C7/24 , F05D2220/323 , F05D2260/96
Abstract: An acoustic attenuation structure for a gas turbine engine includes a periodic structure having a first unit cell, the first unit cell having a first central body and a first axial tube disposed on the first central body and a second axial tube disposed on the first central body, opposite the first axial tube, each of the first axial tube and the second axial tube being in fluid communication with one another through the first central body.
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