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公开(公告)号：US20190292941A1
公开(公告)日：2019-09-26
申请号：US15933537
申请日：2018-03-23
摘要： A gas turbine engine includes a cover, a support, and a sealing member. The cover has a cover housing and a cover arm extending from the cover housing between a first arm end connected to the cover housing and a second arm end having a cover end surface. The support has a support body, a first support arm extending between a first support arm first end connected to the support body and a first support arm second end. The cover arm extends into the first support arm. The sealing member at least partially extends across a gap defined between the cover end surface and the first support arm.
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公开(公告)号：US20190249719A1
公开(公告)日：2019-08-15
申请号：US15897660
申请日：2018-02-15
发明人： Armando Amador , Michael Gantt
CPC分类号： F16C43/065 , B23P15/003 , B25B27/06 , F16C19/26 , F16C43/04 , F16C43/06
摘要： A cylindrical roller bearing installation tool is provided. The cylindrical roller bearing has a plurality of rollers. The installation tool includes a ring-shaped body and a plurality of alignment projections. The ring-shaped body has a circumference and an inner bore. The plurality of alignment projections extend substantially axially outwardly from the body, and are distributed around the circumference of the ring-shaped body. Each alignment projection has at least one roller engagement surface. Each of the alignment projections is uniformly spaced around the circumference of the ring-shaped body.
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公开(公告)号：US20190249605A1
公开(公告)日：2019-08-15
申请号：US15893833
申请日：2018-02-12
发明人： Armando Amador , David Barger , Sean P. McGee
IPC分类号： F02C7/28 , F02C3/04 , F16J15/3288
CPC分类号： F02C7/28 , B64D27/10 , F01D25/183 , F02C3/04 , F02C7/06 , F04D29/102 , F04D29/644 , F05D2220/323 , F05D2240/55 , F05D2260/30 , F05D2260/38 , F05D2300/224 , F16F9/361 , F16J15/3288
摘要： A seal configuration for an aircraft engine includes a ring shaped sealing component defining an axis, a carrier disposed radially outward of the ring shaped sealing component and supporting the ring shaped sealing component, and a housing disposed at least partially about the carrier. The housing is maintained in a static position relative to the carrier via a bellows spring. At least one of the carrier and the housing include a plurality of rotation inhibiting features disposed in a balanced configuration about the at least one of the carrier and the housing. Each of the rotation inhibiting features including a finger extending from the housing and at least one interface feature corresponding to each finger, and being disposed on the carrier. The at least one interface feature comprises one of a notch protruding radially into the carrier and a tab protruding radially outward from the carrier.
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公开(公告)号：US10352456B2
公开(公告)日：2019-07-16
申请号：US15034756
申请日：2014-08-13
IPC分类号： F16J15/34
摘要： An annular seal plate for a shaft assembly in which the seal plate is disposed between and abuts a first adjacent element that rotates with the shaft and seal plate and a second adjacent element that does not rotate with the shaft. The annular seal plate includes an axial scoop defining an annular lubricant collection area disposed radially outwardly from an oil supply orifice that is in fluid communication with a source of pressurized lubricant supplied through the first adjacent element. Lubricant flows through the oil supply orifice and collects in the collection area. An oil passage places the collection area in fluid communication with a lateral surface facing and abutting the second adjacent element to provide lubricant to the interface between the annular seal plate and the second adjacent element.
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公开(公告)号：US11199263B2
公开(公告)日：2021-12-14
申请号：US16361689
申请日：2019-03-22
发明人： Armando Amador , Ernest Boratgis
IPC分类号： F16J15/3276 , F01D11/00 , F16J15/24 , F16J15/34
摘要： A contacting seal for a gas turbine engine include a seal element rotationally fixed relative to an axis of rotation, and a seal seat configured to rotate circumferentially about an axis of rotation and contact the seal element at an interface surface of the seal seat. The seal seat includes an interface component including a seat wall including the interface surface and a seat cavity surface opposite the interface surface, such that a wall thickness of the interface component is defined therebetween. A cover component is secured to the interface component, the cover component including a cover cavity surface. The seat cavity surface and the cover cavity surface define a cooling cavity therebetween configured such that a flow of fluid therethrough cools the interface component via contact between the coolant and the seat cavity surface.
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公开(公告)号：US20210207532A1
公开(公告)日：2021-07-08
申请号：US16736281
申请日：2020-01-07
发明人： Armando Amador , Ernest Boratgis
摘要： A gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a shaft configured to rotate during operation of the gas turbine engine, and a squeeze film damper radially outside the shaft. The squeeze film damper includes a cavity including a film of lubricant axially between first and second cavity seals, and further includes a reservoir fluidly coupled to the cavity. A method is also disclosed.
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公开(公告)号：US10767510B2
公开(公告)日：2020-09-08
申请号：US16269071
申请日：2019-02-06
发明人： Armando Amador , Todd A. Davis , Jorn Axel Glahn
摘要： A seal seat includes an annular body and an extension. The annular body is disposed about a centerline axis. The extension is connected to and extends radially outward from the annular body. The extension includes first, second, and third portions. The first portion is connected to the annular body and is defined by axially opposed upstream and downstream wall faces. The first portion includes a fin connected to the upstream wall face. The second portion is connected to the first portion and extends substantially parallel to the annular body. The third portion is connected to the second portion and extends substantially parallel to the second portion.
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公开(公告)号：US10598020B2
公开(公告)日：2020-03-24
申请号：US15863452
申请日：2018-01-05
发明人： Armando Amador
摘要： A spanner nut for a bearing compartment of an engine with a bearing stack on a first shaft that rotates about an engine centerline includes a body, a piloting hook connected to the body, a first threaded portion, and a channel formed by the piloting hook. The piloting hook includes first and second extensions. The first extension is connected to and extends radially inward from the body. The second extension is connected to and extends in an axial direction from the first extension. The second extension includes a radially outward facing surface. The first threaded portion is configured to engage with a second threaded portion on the end of the first shaft. The channel is configured to receive the end of the first shaft. The piloting hook is configured to draw the second extension radially outward as the spanner nut is compressed.
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公开(公告)号：US11306657B2
公开(公告)日：2022-04-19
申请号：US16736281
申请日：2020-01-07
发明人： Armando Amador , Ernest Boratgis
IPC分类号： F02C7/06 , F01D9/06 , F01D25/16 , F01D25/18 , F01D25/20 , F01D25/22 , F16C27/04 , F16F15/023
摘要： A gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a shaft configured to rotate during operation of the gas turbine engine, and a squeeze film damper radially outside the shaft. The squeeze film damper includes a cavity including a film of lubricant axially between first and second cavity seals, and further includes a reservoir fluidly coupled to the cavity. A method is also disclosed.
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公开(公告)号：US11028717B2
公开(公告)日：2021-06-08
申请号：US15632628
申请日：2017-06-26
摘要： A bearing assembly according to an example of the present disclosure includes, among other things, a bearing situated in a bearing compartment, a seal assembly that defines the bearing compartment, at least one deflector between the bearing and the seal assembly that is rotatable about an axis, and a coalescer at least partially extending about the at least one deflector to define a fluid passage. A method of sealing is also disclosed.
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