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公开(公告)号:US20210102870A1
公开(公告)日:2021-04-08
申请号:US16696025
申请日:2019-11-26
Applicant: General Electric Company
Inventor: Deepak Trivedi , Grover Andrew Bennett, JR. , Sandeep Kumar , Manoj Kumar Koyithitta Meethal , David Mulford Shaddock , Andrew Crispin Graham , Stephen Paul Leclerc, JR.
IPC: G01M15/14
Abstract: An insertion apparatus for use with a rotary machine includes a body extending from an insertion end to a steering end and sized to fit within an annular cavity. The body has a first stiffness and curves along a circumference of the annular cavity as the insertion end travels through the annular cavity. The insertion apparatus also includes a stiffener coupled to the body and extending from the steering end to the insertion end. The stiffener has a second stiffness greater than the first stiffness. The insertion apparatus further includes at least one maintenance device coupled to the insertion end of the insertion apparatus and a displacement mechanism configured to adjust a position of the at least one maintenance device relative to the body.
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公开(公告)号:US20200308971A1
公开(公告)日:2020-10-01
申请号:US16369673
申请日:2019-03-29
Applicant: General Electric Company
Inventor: Deepak Trivedi , Uttara Vijay Kumar , Rahul Anil Bidkar
Abstract: A face seal assembly including a thermal fluid circuit, a turbomachine including the face seal assembly and a method of operating the turbomachine are disclosed. The face seal assembly includes a seal ring including a seal bearing face, at least one internal cavity including a cavity inlet and a cavity outlet. The face seal assembly further including a fluid inlet channel in fluid communication with the cavity inlet of the at least one internal cavity and a pressurized fluid and a fluid outlet port in fluid communication with the cavity outlet of the at least one internal cavity. The at least one internal cavity, the fluid inlet channel and the fluid outlet port define a thermal fluid circuit providing thermal management of the seal ring. In the turbomachine, the face seal assembly is disposed between a stationary component and a rotating component including a rotating component bearing face.
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公开(公告)号:US10788130B2
公开(公告)日:2020-09-29
申请号:US16736856
申请日:2020-01-08
Applicant: General Electric Company
Inventor: Deepak Trivedi , Christopher Edward Wolfe , Nathan EvanMcCurdy Gibson , Brian Joseph Prenger
Abstract: A seal assembly that includes a rotatable seal component, a non-rotatable seal component, and a plurality of pairs of flexures. The non-rotatable seal component is disposed facing the rotatable seal component. The plurality of pairs of flexures is spaced apart from each other along a circumferential direction of the seal assembly. Each pair of the plurality of pairs of flexures has a center line and includes a first flexure and a second flexure disposed in a stressed condition such that a portion of the first flexure and a portion of the second flexure are in contact with each other. Further, the first end of the first flexure is inclined at a first angle relative to the center line and a first end of the second flexure is inclined at a second angle relative to the center line. Also, first end of the first flexure and a first end of the second flexure are coupled to each other and to the non-rotatable seal component.
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公开(公告)号:US20200166142A1
公开(公告)日:2020-05-28
申请号:US16201564
申请日:2018-11-27
Applicant: General Electric Company
Inventor: Rahul Anil Bidkar , Christopher Edward Wolfe , Nathan Evan McCurdy Gibson , Rodrigo Rodriguez Erdmenger , Deepak Trivedi , Quang Tue Nguyen Tran
Abstract: A seal assembly for a rotary machine is positioned between a rotating component and a stationary component of the rotary machine. The seal assembly includes a seal bearing face that opposes the rotating component and a slide device. The slide device is positioned between different fluid pressure volumes in the rotary machine. The slide device axially moves toward the rotating component responsive to pressurization of the rotary machine. The slide device includes cross-over ports and the seal bearing face includes feed ports. The feed ports extend through the seal bearing face to form an aerostatic portion of a film bearing between the seal bearing face and the rotating component. The seal bearing face and/or the rotating component is a non-planar surface that, during rotating motion of the rotating component, forms an aerodynamic portion of the film bearing between the seal bearing face and the rotating component.
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公开(公告)号:US10563772B2
公开(公告)日:2020-02-18
申请号:US15810183
申请日:2017-11-13
Applicant: GENERAL ELECTRIC COMPANY
Inventor: Deepak Trivedi , Christopher Edward Wolfe , Nathan EvanMcCurdy Gibson , Brian Joseph Prenger
Abstract: A seal assembly, for example, a face seal assembly for a machine such as a turbomachine, and an associated method of operating the seal assembly in the machine are disclosed. The seal assembly includes a rotatable seal component, a non-rotatable seal component, and a plurality of pairs of flexures. The non-rotatable seal component is disposed facing the rotatable seal component. The plurality of pairs of flexures is spaced apart from each other along a circumferential direction of the seal assembly. Each pair of the plurality of pairs of flexures includes a first flexure and a second flexure disposed in a stressed condition such that a portion of the first flexure and a portion of the second flexure are in contact with each other. Further, an end of the first flexure and an end of the second flexure are coupled to each other and to the non-rotatable seal component.
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公开(公告)号:US20190383488A1
公开(公告)日:2019-12-19
申请号:US16012412
申请日:2018-06-19
Applicant: General Electric Company
Inventor: Jonathan Dwight Berry , Michael John Hughes , Russell Pierson DeForest , Kevin Weston McMahan , Victor John Morgan , Ibrahim Sezer , Neelesh Nandkumar Sarawate , Deepak Trivedi
Abstract: An integrated combustor nozzle includes an inner liner segment; an outer liner segment; and a panel extending radially between the inner and outer liner segments. The panel includes a forward end, an aft end, and a side walls extending axially from the forward end to the aft end. The aft end defines a turbine nozzle having a trailing edge circumferentially offset from the forward end. The inner liner segment has a pair of sealing surfaces, each of which defines a first continuous curve in the circumferential direction. The outer liner segment has a pair of sealing surfaces, each of which defines a second continuous curve in the circumferential direction. In some instances, the curves are monotonic in the circumferential direction. A segmented annular combustor including an array of such integrated combustor nozzles is also provided.
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公开(公告)号:US20180283128A1
公开(公告)日:2018-10-04
申请号:US15476422
申请日:2017-03-31
Applicant: GENERAL ELECTRIC COMPANY
Inventor: Deepak Trivedi , Kevin James Shufon , Walter John Smith , Charles Erklin Seeley , Brian Scott Baker
Abstract: A blind shear ram includes an upper carrier including an upper blade and a lower carrier including a lower blade. The upper carrier and the lower carrier are positionable in a first position in which the upper carrier and the lower carrier are spaced apart and a second position in which the upper carrier and the lower carrier seal a wellbore. The upper blade and the lower blade are configured to cut at least one pipe and at least one cable when the upper carrier and the lower carrier move between the first position and the second position. At least one of the upper blade and the lower blade includes a textured surface configured to induce friction between the at least one cable and the blade.
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公开(公告)号:US20180274322A1
公开(公告)日:2018-09-27
申请号:US15464437
申请日:2017-03-21
Applicant: General Electric Company
Inventor: Jamie Clay Gamble , Bodhayan Dev , Deepak Trivedi
CPC classification number: E21B33/063 , F16J15/022
Abstract: A seal for a blind shear ram is configured to extend between a first carrier and a second carrier of the blind shear ram. The seal includes a curved portion and an elastic layer extending through the curved portion. The elastic layer is configured to contact at least one of the first carrier and the second carrier to seal a wellbore when the first carrier and the second carrier are in a closed position. The elastic layer has a first elasticity. The seal also includes an anti-extrusion structure coupled to the elastic layer. The anti-extrusion structure extends through the curved portion. The anti-extrusion structure has a second elasticity less than the first elasticity. The anti-extrusion structure defines a plurality of slits to facilitate the anti-extrusion structure extending through the curved portion.
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公开(公告)号:US20180187673A1
公开(公告)日:2018-07-05
申请号:US15397514
申请日:2017-01-03
Applicant: General Electric Company
Inventor: Deepak Trivedi , Christopher Edward Wolfe , Brian Paul Reeves , Bodhayan Dev
CPC classification number: F04B47/08 , E21B43/121 , E21B43/128 , F04B2203/0903 , F15B1/02 , F15B11/10 , F15B15/1428 , F15B15/1447 , F15B15/22 , F15B2211/205 , F15B2211/212 , F15B2211/755
Abstract: An actuator for use with a fluid transfer device is provided. The actuator includes a piston cylinder having a longitudinal axis and defining a piston chamber having both a head end and a longitudinally opposite base end. The actuator further includes a piston disposed within the piston chamber. The piston movable between a first piston position proximate the piston chamber head end and a second piston position proximate the piston chamber base end. The piston includes a piston head end having a first indexing mechanism, a first piston seal, and at least one first feed hole. The piston further includes a base end longitudinally opposite the head end having a second indexing mechanism, a guide tooth, a second piston seal, and at least one second feed hole. The piston defines a plurality of channels that extends from proximate the first piston seal to proximate the second piston seal.
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公开(公告)号:US20170167219A1
公开(公告)日:2017-06-15
申请号:US14964639
申请日:2015-12-10
Applicant: General Electric Company
Inventor: Jifeng Wang , Deepak Trivedi , Bodhayan Dev , Aaron John Mashue
IPC: E21B33/06
CPC classification number: E21B33/062
Abstract: A variable ram for a blowout preventer is disclosed. The variable ram includes a ram block and a ram packer assembly disposed at least in part within the ram block. The ram packer assembly includes a plurality of inserts and a packer member. The plurality of inserts is configured to form an insert array, where the insert array includes a peripheral surface, and where the peripheral surface of the insert array is disposed facing an opening configured to receive a tubular member. The packer member is coupled to at least a portion of the plurality of inserts for providing a unitary structure to the ram packer assembly, where the packer member protrudes from the peripheral surface of the insert array into the opening to define a bore face of the variable ram, and where the packer member includes an elastomeric material.
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