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公开(公告)号：US20230175589A1
公开(公告)日：2023-06-08
申请号：US17541593
申请日：2021-12-03
Applicant: Raytheon Technologies Corporation
Inventor： Brian P. Cigal , Christopher T. Anglin
IPC: F16J15/34
CPC classification number: F16J15/3452 , F16J15/3496
Abstract: An apparatus has: a first member; a shaft rotatable relative to the first member about an axis; and a seal system. The seal system has: a seal carried by the first member and having a seal face; a seal carrier; a seat carried by the shaft and having a seat face in sliding sealing engagement with the seal face; and one or more springs biasing the seal carrier relative to the first member so as to bias the seal face against the seat face. The seal carrier has: an axially-extending wall having an inner diameter (ID) surface; and a radially-extending wall having a first surface. The seal carrier axially-extending wall ID surface has a radially inwardly open groove having a first sidewall and a second sidewall and a base. A wave-form split ring contacts the first sidewall and biases the seal into engagement with the radial wall first surface.
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公开(公告)号：US20210324762A1
公开(公告)日：2021-10-21
申请号：US16849562
申请日：2020-04-15
Applicant: Raytheon Technologies Corporation
Inventor： Christopher T. Anglin , Kaleb Von Berg , Marios C. Soteriou , Graham B. Fulton, III , Shiling Zhang
Abstract: A gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a bearing compartment, a seal assembly configured to establish a seal of the bearing compartment. The seal assembly includes a seal plate. The gas turbine engine further includes a gutter configured to collect oil slung from the seal plate. The gutter extends only partially around the seal plate. A method is also disclosed.
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公开(公告)号：US11549436B2
公开(公告)日：2023-01-10
申请号：US16856304
申请日：2020-04-23
Applicant: Raytheon Technologies Corporation
Inventor： Christopher T. Anglin , Heriberto Rodriguez
Abstract: An assembly for a compartment of a gas turbine engine that includes a housing, a gear, and a baffle disposed about the gear. The baffle includes an upstream portion and a downstream portion. The upstream portion includes an upstream inner wall and an upstream outer wall separated from the gear. The upstream inner wall is positioned between the upstream outer wall and the gear. An upstream flow channel is formed between the upstream inner wall and the upstream outer wall. The downstream portion of the baffle includes a downstream inner wall and a downstream outer wall separated from the gear. The downstream inner wall is positioned between the downstream outer wall and the gear. A downstream flow channel is formed between the downstream outer wall and the downstream inner wall.
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公开(公告)号：US20210332775A1
公开(公告)日：2021-10-28
申请号：US16857661
申请日：2020-04-24
Applicant: Raytheon Technologies Corporation
Inventor： Yuk-Kwan Brian Yuen , Christopher T. Anglin , Matthew Nickerson , Daniel S. Rogers
Abstract: A fan assembly of a gas turbine engine includes a fan rotor including a fan rotor hub, and a plurality of fan blades extending radially outwardly from the fan rotor hub, and a fan case including an inner case portion and an outer case portion surrounding the plurality of fan blades. A plurality of struts extend between the inner case portion and the outer case portion. A bearing assembly is configured to support the fan rotor at the inner case portion. The bearing assembly includes a bearing inner race secured to the fan rotor, a bearing outer race secured to the inner case portion, and a plurality of bearing elements located radially between the bearing inner race and the bearing outer race.
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公开(公告)号：US20210332753A1
公开(公告)日：2021-10-28
申请号：US16856304
申请日：2020-04-23
Applicant: Raytheon Technologies Corporation
Inventor： Christopher T. Anglin , Heriberto Rodriguez
Abstract: An assembly for a compartment of a gas turbine engine that includes a housing, a gear, and a baffle disposed about the gear. The baffle includes an upstream portion and a downstream portion. The upstream portion includes an upstream inner wall and an upstream outer wall separated from the gear. The upstream inner wall is positioned between the upstream outer wall and the gear. An upstream flow channel is formed between the upstream inner wall and the upstream outer wall. The downstream portion of the baffle includes a downstream inner wall and a downstream outer wall separated from the gear. The downstream inner wall is positioned between the downstream outer wall and the gear. A downstream flow channel is formed between the downstream outer wall and the downstream inner wall.
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Patent Agency Ranking
公开(公告)号：US20200240471A1
公开(公告)日：2020-07-30
申请号：US16850497
申请日：2020-04-16
Applicant: Raytheon Technologies Corporation
Abstract: A seal assembly for a bearing compartment of a gas turbine engine includes a seal carrier, a seal element, a seal plate, and a trough. At least a portion of the seal element is within the seal carrier. The seal plate is in contact with the seal element and is configured to rotate relative to the seal element. The trough extends around the seal plate and comprises an annular channel positioned to capture oil slung from the seal plate.
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公开(公告)号：US11352979B2
公开(公告)日：2022-06-07
申请号：US16857661
申请日：2020-04-24
Applicant: Raytheon Technologies Corporation
Inventor： Yuk-Kwan Brian Yuen , Christopher T. Anglin , Matthew Nickerson , Daniel S. Rogers
Abstract: A fan assembly of a gas turbine engine includes a fan rotor including a fan rotor hub, and a plurality of fan blades extending radially outwardly from the fan rotor hub, and a fan case including an inner case portion and an outer case portion surrounding the plurality of fan blades. A plurality of struts extend between the inner case portion and the outer case portion. A bearing assembly is configured to support the fan rotor at the inner case portion. The bearing assembly includes a bearing inner race secured to the fan rotor, a bearing outer race secured to the inner case portion, and a plurality of bearing elements located radially between the bearing inner race and the bearing outer race.
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公开(公告)号：US10962060B2
公开(公告)日：2021-03-30
申请号：US16850497
申请日：2020-04-16
Applicant: Raytheon Technologies Corporation
Abstract: A seal assembly for a bearing compartment of a gas turbine engine includes a seal carrier, a seal element, a seal plate, and a trough. At least a portion of the seal element is within the seal carrier. The seal plate is in contact with the seal element and is configured to rotate relative to the seal element. The trough extends around the seal plate and comprises an annular channel positioned to capture oil slung from the seal plate.
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公开(公告)号：US11739845B2
公开(公告)日：2023-08-29
申请号：US17541593
申请日：2021-12-03
Applicant: Raytheon Technologies Corporation
Inventor： Brian P. Cigal , Christopher T. Anglin
IPC: F16J15/34
CPC classification number: F16J15/3452 , F16J15/3496
Abstract: An apparatus has: a first member; a shaft rotatable relative to the first member about an axis; and a seal system. The seal system has: a seal carried by the first member and having a seal face; a seal carrier; a seat carried by the shaft and having a seat face in sliding sealing engagement with the seal face; and one or more springs biasing the seal carrier relative to the first member so as to bias the seal face against the seat face. The seal carrier has: an axially-extending wall having an inner diameter (ID) surface; and a radially-extending wall having a first surface. The seal carrier axially-extending wall ID surface has a radially inwardly open groove having a first sidewall and a second sidewall and a base. A wave-form split ring contacts the first sidewall and biases the seal into engagement with the radial wall first surface.
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公开(公告)号：US11293307B2
公开(公告)日：2022-04-05
申请号：US16849562
申请日：2020-04-15
Applicant: Raytheon Technologies Corporation
Inventor： Christopher T. Anglin , Kaleb Von Berg , Marios C. Soteriou , Graham B. Fulton, III , Shiling Zhang
Abstract: A gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a bearing compartment, a seal assembly configured to establish a seal of the bearing compartment. The seal assembly includes a seal plate. The gas turbine engine further includes a gutter configured to collect oil slung from the seal plate. The gutter extends only partially around the seal plate. A method is also disclosed.
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