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公开(公告)号:US20160130963A1
公开(公告)日:2016-05-12
申请号:US14830636
申请日:2015-08-19
Applicant: United Technologies Corporation
Inventor: Ross Wilson , Michael G. McCaffrey , John R. Farris , Theodore W. Hall , John J. Korzendorfer , Elizabeth F. Vinson , Jeffrey Michael Jacques , Edwin Otero , John E. Paul
CPC classification number: F01D11/001 , F01D11/025 , F05D2240/55 , F05D2260/38 , F05D2260/96 , F16J15/44
Abstract: The present disclosure relates generally to a hydrostatic advanced low leakage seal having a shoe supported by at least two beams. An anti-vibration beam spacer is disposed in contact with two adjacent beams and operative to mitigate an externally induced vibratory response of the beams.
Abstract translation: 本公开总体上涉及一种具有由至少两个梁支撑的鞋的静水超前低泄漏密封件。 防振梁隔离件设置成与两个相邻的梁接触并且可操作以减轻外部感应的梁的振动响应。
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公开(公告)号:US10443450B2
公开(公告)日:2019-10-15
申请号:US14921533
申请日:2015-10-23
Applicant: United Technologies Corporation
Inventor: Ross Wilson , Michael G. McCaffrey , John R. Farris , Theodore W. Hall , John J. Korzendorfer , Elizabeth F. Vinson , Jeffrey Michael Jacques , John E. Paul , Alan W. Stoner , Edwin Otero
IPC: F01D25/28 , F16J15/16 , F01D5/22 , F01D5/24 , F01D5/26 , F01D5/28 , F01D9/02 , F01D9/04 , F01D11/00 , F01D11/12 , F01D25/24
Abstract: A seal support structure is provided for a circumferential seal. In one embodiment, the seal support structure includes an engine support structure, a seal support, and a shoulder joining the engine support and seal support. The shoulder offsets the engine support from the seal support, and the shoulder and the seal support structure are configured to dampen vibration for the circumferential seal. The seal support structure may employ one or more dampening elements or materials to interoperate with a seal support structure to dampen vibration to a seal system.
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公开(公告)号:US10436051B2
公开(公告)日:2019-10-08
申请号:US14921503
申请日:2015-10-23
Applicant: United Technologies Corporation
Inventor: Ross Wilson , Michael G. McCaffrey , John R. Farris , Theodore W. Hall , John J. Korzendorfer , Elizabeth F. Vinson , Jeffrey Michael Jacques , John E. Paul , Alan W. Stoner , Edwin Otero
Abstract: The present disclosure relates to sealing systems for gas turbine engines. In one embodiment, a seal support structure for a gas turbine engine includes a seal support configured to retain a circumferential seal and an engine support configured for mounting the seal support structure to a gas turbine engine mount. The engine support includes at least one channel configured to provide radial movement of the seal support structure and circumferential retention of the seal support. Another embodiment is directed to a sealing system including a circumferential seal and seal support structure configured to provide radial movement.
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公开(公告)号:US20180179959A1
公开(公告)日:2018-06-28
申请号:US15895058
申请日:2018-02-13
Applicant: United Technologies Corporation
Inventor: Nicholas Lefevre , John J. Korzendorfer , Peter Balawajder , Paul W. Palmer , Paul J. Colucci , Mahamoud Coulibaly
Abstract: A seal system for a gas turbine engine includes a cover plate with a radial flange; a seal carrier adjacent the cover plate; an outer compliant seal supported by the seal carrier; an inner compliant seal supported by the seal carrier, the inner compliant seal engaged with the radial flange; and a spring between the cover plate and the seal carrier.
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公开(公告)号:US10578026B2
公开(公告)日:2020-03-03
申请号:US15895058
申请日:2018-02-13
Applicant: United Technologies Corporation
Inventor: Nicholas Lefevre , John J. Korzendorfer , Peter Balawajder , Paul W. Palmer , Paul J. Colucci , Mahamoud Coulibaly
Abstract: A seal system for a gas turbine engine includes a cover plate with a radial flange; a seal carrier adjacent the cover plate; an outer compliant seal supported by the seal carrier; an inner compliant seal supported by the seal carrier, the inner compliant seal engaged with the radial flange; and a spring between the cover plate and the seal carrier.
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公开(公告)号:US20200025293A1
公开(公告)日:2020-01-23
申请号:US16243632
申请日:2019-01-09
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Michael G. McCaffrey , John R. Farris , Theodore W. Hall , John J. Korzendorfer , Elizabeth F. Vinson , Jeffrey Michael Jacques , John E. Paul , Ross Wilson , Edwin Otero , Alan W. Stoner
Abstract: A seal ring system is provided. The seal ring system comprises a segment defining a slot, a pedal along the slot, and an opening offset from the slot. A retention fastener may be disposed in the opening. A seal ring system is also provided comprising a first segment defining a first opening, a second segment defining a second opening, and a retention fastener extending through the first and second openings. The retention fastener configured to allow relative radial movement of the first segment and the second segment. A seal is further provided comprising a seal ring having a central axis, a petal extending radially inward with respect to the central axis of the seal ring, and a sealing disk axially proximate the seal ring. The sealing disk may have a seal shoe configured as a primary seal. The petal may extend toward the seal shoe.
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公开(公告)号:US20190331003A1
公开(公告)日:2019-10-31
申请号:US16455093
申请日:2019-06-27
Applicant: United Technologies Corporation
Inventor: Ross Wilson , Michael G. McCaffrey , John R. Farris , Theodore W. Hall , John J. Korzendorfer , Elizabeth F. Vinson , Jeffrey Michael Jacques , John E. Paul , Alan W. Stoner , Edwin Otero
IPC: F01D25/28 , F01D25/24 , F01D11/12 , F01D11/00 , F01D9/04 , F01D9/02 , F01D5/28 , F01D5/24 , F01D5/22 , F16J15/16 , F01D5/26
Abstract: A seal support structure is provided for a circumferential seal. In one embodiment, the seal support structure includes an engine support structure, a seal support, and a shoulder joining the engine support and seal support. The shoulder offsets the engine support from the seal support, and the shoulder and the seal support structure are configured to dampen vibration for the circumferential seal. The seal support structure may employ one or more dampening elements or materials to interoperate with a seal support structure to dampen vibration to a seal system.
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8.
公开(公告)号:US20140290213A1
公开(公告)日:2014-10-02
申请号:US14150385
申请日:2014-01-08
Applicant: United Technologies Corporation
Inventor: Nicholas Lefevre , John J. Korzendorfer , Peter Balawajder , Paul W. Palmer , Paul J. Colucci , Mahamoud Coulibaly
CPC classification number: F02C7/28 , F02K3/075 , F04D19/02 , F04D27/0215 , F04D29/083 , F05D2220/90 , Y02T50/672
Abstract: A seal system for a gas turbine engine includes an annular seal carrier and an annular compliant seal mounted around the annular seal carrier, the compliant seal includes a multiple of legs in cross-section.
Abstract translation: 用于燃气涡轮发动机的密封系统包括环形密封载体和围绕环形密封载体安装的环形柔性密封件,柔性密封件包括多个横截面的腿部。
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公开(公告)号:US11287045B2
公开(公告)日:2022-03-29
申请号:US16243632
申请日:2019-01-09
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Michael G. McCaffrey , John R. Farris , Theodore W. Hall , John J. Korzendorfer , Elizabeth F. Vinson , Jeffrey Michael Jacques , John E. Paul , Ross Wilson , Edwin Otero , Alan W. Stoner
Abstract: A seal ring system is provided. The seal ring system comprises a segment defining a slot, a pedal along the slot, and an opening offset from the slot. A retention fastener may be disposed in the opening. A seal ring system is also provided comprising a first segment defining a first opening, a second segment defining a second opening, and a retention fastener extending through the first and second openings. The retention fastener configured to allow relative radial movement of the first segment and the second segment. A seal is further provided comprising a seal ring having a central axis, a petal extending radially inward with respect to the central axis of the seal ring, and a sealing disk axially proximate the seal ring. The sealing disk may have a seal shoe configured as a primary seal. The petal may extend toward the seal shoe.
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公开(公告)号:US20160115804A1
公开(公告)日:2016-04-28
申请号:US14921503
申请日:2015-10-23
Applicant: United Technologies Corporation
Inventor: Ross Wilson , Michael G. McCaffrey , John R. Farris , Theodore W. Hall , John J. Korzendorfer , Elizabeth F. Vinson , Jeffrey Michael Jacques , John E. Paul , Alan W. Stoner , Edwin Otero
Abstract: The present disclosure relates to sealing systems for gas turbine engines. In one embodiment, a seal support structure for a gas turbine engine includes a seal support configured to retain a circumferential seal and an engine support configured for mounting the seal support structure to a gas turbine engine mount. The engine support includes at least one channel configured to provide radial movement of the seal support structure and circumferential retention of the seal support. Another embodiment is directed to a sealing system including a circumferential seal and seal support structure configured to provide radial movement.
Abstract translation: 本公开涉及燃气轮机发动机的密封系统。 在一个实施例中,用于燃气涡轮发动机的密封支撑结构包括构造成保持圆周密封件的密封支撑件和被构造用于将密封支撑结构安装到燃气涡轮发动机支架的发动机支撑件。 发动机支撑件包括至少一个通道,其构造成提供密封支撑结构的径向移动和密封支撑件的周向保持。 另一个实施例涉及一种包括周向密封和密封支撑结构的密封系统,该结构被配置为提供径向运动。
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