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公开(公告)号：US11015527B2
公开(公告)日：2021-05-25
申请号：US15821157
申请日：2017-11-22
Applicant: United Technologies Corporation
Inventor： Kevin Duffy , Ronnie K. Kovacik , Keven G. Van Duyn , Jonathan F. Zimmitti , Richard J. Rubendall , Michael M. Davis , Joseph G. Colucci , Steven M. Danley , Christopher J. Zuck , Tina Rezvani
Abstract: Aspects of the disclosure are directed to a rotatable shaft, and a plurality of bearings coupled to the rotatable shaft, where the plurality of bearings include a first bearing, a second bearing, and a third bearing, where the first bearing defines an axial first bearing centerline, where the second bearing defines an axial second bearing centerline, where the third bearing defines an axial third bearing centerline, and where the axial second bearing centerline is radially offset from the axial first bearing centerline and the axial third bearing centerline.
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公开(公告)号：US10422243B2
公开(公告)日：2019-09-24
申请号：US15410049
申请日：2017-01-19
Applicant: United Technologies Corporation
Inventor： Gabriel L. Suciu , Hung Duong , Jonathan F. Zimmitti , William G. Sheridan , Michael E. McCune , Brian Merry
IPC: F01D15/12 , F02C7/268 , F01D5/06 , F01D15/10 , F01D25/20 , F16H3/30 , F02C7/277 , F02C7/32 , F02C7/36
Abstract: An exemplary gas turbine engine assembly includes a transmission coupling a starter generator assembly to a first set of gears. The transmission is transitionable between a first mode where the starter generator assembly is driven at a first speed relative to the second towershaft, and a second mode where the starter generator assembly is driven at a different, second speed relative to the second towershaft.
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公开(公告)号：US20160153287A1
公开(公告)日：2016-06-02
申请号：US14904003
申请日：2014-07-09
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： James T. Roach , Grant O. Cook , Lakshminarayan S. Bettagere , Jonathan F. Zimmitti , Majidullah Dehlavi , Shari L. Bugaj , Charles R. Watson , Brian D. Walter , Andrew G. Alarcon , Sarah M. Wall , Christopher J. Hertel , Octavio Martin , Thomas J. Robertson , Aaron Beaudry , Jeffrey J. Scalia , Joseph J. Wassel , Joe Ott , Barry Barnett , Glenn Levasseur
CPC classification number: F01D25/005 , B64D29/00 , B64D2045/009 , C23C18/1641 , C23C18/31 , C25D1/00 , C25D5/56 , C25D7/00 , F01D5/282 , F01D5/3092 , F01D9/041 , F01D25/24 , F01D25/30 , F02C7/04 , F02K1/54 , F04D29/023 , F04D29/321 , F04D29/322 , F04D29/522 , F04D29/542 , F05D2220/32 , F05D2230/31 , F05D2230/90 , F05D2240/00 , F05D2240/12 , F05D2240/30 , F05D2240/60 , F05D2250/283 , F05D2260/96 , F05D2300/10 , F05D2300/40 , F05D2300/43 , F05D2300/603 , F16C3/02 , Y02T50/672 , Y02T50/673
Abstract: Plated polymeric gas turbine engine parts and methods for fabricating lightweight plated polymeric gas turbine engine parts are disclosed. The parts include a polymeric substrate plated with one or more metal layers. The polymeric material of the polymeric substrate may be structurally reinforced with materials that may include carbon, metal, or glass. The polymeric substrate may also include a plurality of layers to form a composite layup structure.
Abstract translation: 公开了用于制造轻质电镀聚合物燃气涡轮发动机部件的电镀聚合物燃气涡轮发动机部件和方法。 这些部件包括镀有一个或多个金属层的聚合物基材。 聚合物基材的聚合材料可以用可以包括碳，金属或玻璃的材料在结构上加强。 聚合物基底还可以包括多个层以形成复合铺层结构。
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公开(公告)号：US11619237B2
公开(公告)日：2023-04-04
申请号：US16791298
申请日：2020-02-14
Applicant: United Technologies Corporation
Inventor： Pantcho P. Stoyanov , Jonathan F. Zimmitti , Nasr A. Shuaib
Abstract: A seal assembly includes a housing at least partially defining a seal opening and at least partially surrounding a rotatable shaft. A carbon seal is located at least partially in the seal opening and includes a sealing surface. The rotatable shaft includes a radially facing surface that has a carbide based coating and a diamond-like carbon coating in engagement with the sealing surface on the carbon seal.
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公开(公告)号：US20210123357A1
公开(公告)日：2021-04-29
申请号：US16666890
申请日：2019-10-29
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Masayoshi Sonokawa , Jonathan F. Zimmitti , Nasr A. Shuaib
Abstract: A seal housing may comprise an aft flange, an outer diameter (OD) ring and a stopper. The stopper may extend radially inward from a radially inner surface of OD ring. The stopper may be configured to interface with a monobloc carbon seal. The stopper may comprise a circumferential stopping portion and an axial stopping portion. There may be a plurality of the stopper.
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Patent Agency Ranking
公开(公告)号：US10526976B2
公开(公告)日：2020-01-07
申请号：US15498764
申请日：2017-04-27
Applicant: United Technologies Corporation
Inventor： Gabriel L. Suciu , Hung Duong , Jonathan F. Zimmitti , William G. Sheridan , Michael E. McCune , Brian Merry
IPC: F02C7/36
Abstract: A gas turbine engine comprises a high speed spool and a low speed spool. A low speed power takeoff is driven by the low speed spool and a high speed power takeoff is driven by the high speed spool. The low speed power takeoff drives a plurality of low speed driven accessories about low speed spool drive axes and the high speed power takeoff drives a plurality of high speed driven accessories about high speed spool drive axes. The low speed spool drive axes are generally tangential to an envelope defined about a center axis of the engine, and the high speed spool drive axes are generally tangential to an envelope defined about the center.
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公开(公告)号：US20190153946A1
公开(公告)日：2019-05-23
申请号：US15821157
申请日：2017-11-22
Applicant: United Technologies Corporation
Inventor： Kevin Duffy , Ronnie K. Kovacik , Keven G. Van Duyn , Jonathan F. Zimmitti , Richard J. Rubendall , Michael M. Davis , Joseph G. Colucci , Steven M. Danley , Christopher J. Zuck , Tina Rezvani
Abstract: Aspects of the disclosure are directed to a rotatable shaft, and a plurality of bearings coupled to the rotatable shaft, where the plurality of bearings include a first bearing, a second bearing, and a third bearing, where the first bearing defines an axial first bearing centerline, where the second bearing defines an axial second bearing centerline, where the third bearing defines an axial third bearing centerline, and where the axial second bearing centerline is radially offset from the axial first bearing centerline and the axial third bearing centerline.
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公开(公告)号：US20180202368A1
公开(公告)日：2018-07-19
申请号：US15410113
申请日：2017-01-19
Applicant: United Technologies Corporation
Inventor： Gabriel L. Suciu , Hung Duong , Jonathan F. Zimmitti , William G. Sheridan , Michael E. McCune , Brian Merry
IPC: F02C7/32 , F02C3/06 , F02C7/18 , F02C7/36 , F02C7/268 , F01D15/10 , F01D15/12 , F01D25/12 , F16H1/22 , H02K7/116 , H02K7/18
CPC classification number: F02C7/32 , F01D15/10 , F01D15/12 , F01D25/12 , F02C3/06 , F02C7/185 , F02C7/268 , F02C7/275 , F02C7/36 , F05D2220/32 , F05D2260/4031 , F05D2260/85 , F16H1/222 , H02K7/116 , H02K7/1823
Abstract: An exemplary gas turbine engine assembly includes a first spool having a first turbine operatively mounted to a first turbine shaft, and a second spool having a second turbine operatively mounted to a second turbine shaft. The first and second turbines are mounted for rotation about a common rotational axis within an engine static structure. The first and second turbine shafts are coaxial with one another. First and second towershafts are respectively coupled to the first and second turbine shafts. An accessory drive gearbox has a set of gears. A compressor is driven by the first towershaft. The engine assembly further includes a starter generator assembly, and a transmission coupling the starter generator assembly to the first set of gears. The transmission is transitionable between a first mode where the starter generator assembly is driven at a first speed relative to the second towershaft, and a second mode where the starter generator assembly is driven at a different, second speed relative to the second towershaft.
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公开(公告)号：US20180202367A1
公开(公告)日：2018-07-19
申请号：US15409974
申请日：2017-01-19
Applicant: United Technologies Corporation
Inventor： Gabriel L. Suciu , Hung Duong , Jonathan F. Zimmitti , William G. Sheridan , Michael E. McCune , Brian Merry
IPC: F02C7/32 , F02C7/277 , F02C7/22 , F01D15/10 , F01D15/08 , F01D15/12 , F01D5/06 , F01D25/20 , F01D25/16
CPC classification number: F02C7/32 , F01D5/06 , F01D15/08 , F01D15/10 , F01D15/12 , F01D25/16 , F01D25/20 , F02C7/22 , F02C7/277 , F02C7/36 , F05D2220/32 , F05D2220/50 , F05D2240/60 , F05D2260/4031
Abstract: A gas turbine engine assembly includes a turbine section having first and second turbines mounted for rotation about a common rotational axis within an engine static structure, first and second turbine shafts coaxial with one another and to which the first and second turbines are respectively operatively mounted, first and second towershafts respectively coupled to the first and second turbine shafts, an accessory drive gearbox mounted to the engine static structure, the accessory drive gearbox including a first gear train and a second gear train, the first towershaft extending into a housing and coupled to the first gear train, the second towershaft extending into the housing and coupled to the second gear train, a hydraulic pump, a transmission coupling the hydraulic pump to the first gear train, the transmission transitionable between a first mode where the hydraulic pump is driven at a first speed relative to the first towershaft, a second mode where the hydraulic pump is driven at a different, second speed relative to the first towershaft, and a third mode where the hydraulic pump is driven at a different, third speed relative to the first towershaft.
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公开(公告)号：US20160230601A1
公开(公告)日：2016-08-11
申请号：US14617178
申请日：2015-02-09
Applicant: United Technologies Corporation
Inventor： Lakshminarayan S. Bettagere , Keven Van Duyn , Mark R. Sondeen , Jonathan F. Zimmitti
CPC classification number: F01D25/28 , F02C7/32 , F02M26/67 , F05D2230/642 , F05D2250/241 , F05D2260/30 , F05D2260/37 , Y02T50/675
Abstract: An exemplary gearbox assembly includes a shear bracket connectable to a flange of a housing structure, and a support pin extending along a longitudinal axis, the support pin supporting the shear bracket relative to a turbomachine, the shear bracket moveable axially relative to the support pin.
Abstract translation: 示例性的齿轮箱组件包括可连接到壳体结构的凸缘的剪切支架和沿着纵向轴线延伸的支撑销，所述支撑销相对于涡轮机支撑剪切支架，所述剪切支架可相对于支撑销轴向移动。
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