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公开(公告)号：US20170167299A1
公开(公告)日：2017-06-15
申请号：US14964806
申请日：2015-12-10
Applicant: General Electric Company
IPC: F01D25/28
CPC classification number: F01D25/285 , B66F3/36 , B66F7/28 , F01D9/023 , F05D2230/68 , F05D2230/70 , F05D2230/72 , F05D2260/02 , F23R3/46 , F23R2900/00017 , F23R2900/00019
Abstract: A combustor assembly lift system comprises a track that extends in at least a longitudinal direction, a lift arm moveably engaged with the track such that it can traverse along the track in at least the longitudinal direction, and a combustor assembly engagement frame connected to the lift arm, wherein the combustor assembly engagement frame is configured to temporarily secure to at least a portion of a combustor assembly.
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公开(公告)号：US10408091B2
公开(公告)日：2019-09-10
申请号：US15476224
申请日：2017-03-31
Applicant: General Electric Company
Inventor： Sandra Beverly Kolvick , Daryl Paul Capriotti , Ansley Michelle Heard , Rachel Kate King , Travis Edwin Lipstein , Maithri Muddasani , Tewodros Fiseha Wondimu
Abstract: Mounting apparatuses for turbine airfoils of turbine systems are disclosed. The mounting apparatuses may include a body portion configured to be at least partially positioned between a first airfoil and a second airfoil of the turbine system, and an adjustable, first retention component formed on a first side of the body portion. The adjustable, first retention component may be configured to contact a portion of a suction side of the first airfoil of the turbine system. The mounting apparatuses may also include a second retention component formed on a second side of the body portion, opposite the first side. The second retention component may be configured to contact a portion of a pressure side of the second airfoil of the turbine system.
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公开(公告)号：US20190338677A1
公开(公告)日：2019-11-07
申请号：US16516847
申请日：2019-07-19
Applicant: General Electric Company
Inventor： Sandra Beverly Kolvick , Daryl Paul Capriotti , Ansley Michelle Heard , Rachel Kate King , Travis Edwin Lipstein , Maithri Muddasani , Tewodros Fiseha Wondimu
Abstract: Mounting apparatuses for turbine airfoils of turbine systems are disclosed. The mounting apparatuses may include a body portion configured to be at least partially positioned between a first airfoil and a second airfoil of the turbine system, and an adjustable, first retention component formed on a first side of the body portion. The adjustable, first retention component may be configured to contact a portion of a suction side of the first airfoil of the turbine system. The mounting apparatuses may also include a second retention component formed on a second side of the body portion, opposite the first side. The second retention component may be configured to contact a portion of a pressure side of the second airfoil of the turbine system.
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Patent Agency Ranking
公开(公告)号：US20180283214A1
公开(公告)日：2018-10-04
申请号：US15476224
申请日：2017-03-31
Applicant: General Electric Company
Inventor： Sandra Beverly Kolvick , Daryl Paul Capriotti , Ansley Michelle Heard , Rachel Kate King , Travis Edwin Lipstein , Maithri Muddasani , Tewodros Fiseha Wondimu
CPC classification number: F01D25/28 , B25B5/065 , B25B5/14 , F01D5/147 , F05D2220/32 , F05D2240/90 , F05D2260/30
Abstract: Mounting apparatuses for turbine airfoils of turbine systems are disclosed. The mounting apparatuses may include a body portion configured to be at least partially positioned between a first airfoil and a second airfoil of the turbine system, and an adjustable, first retention component formed on a first side of the body portion. The adjustable, first retention component may be configured to contact a portion of a suction side of the first airfoil of the turbine system. The mounting apparatuses may also include a second retention component formed on a second side of the body portion, opposite the first side. The second retention component may be configured to contact a portion of a pressure side of the second airfoil of the turbine system.
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公开(公告)号：US10934893B2
公开(公告)日：2021-03-02
申请号：US15779317
申请日：2015-12-31
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Sandra Beverly Kolvick , Jeffrey Scott LeBegue , Ansley Michelle Heard , Jesse Ellis Barton , Paul Robert Fernandez , Adrian Adam Klejc
Abstract: A combustor assembly lift system (200) comprises an exterior lift frame (220) comprising a base portion (222) and an arm portion (224), wherein the arm portion extends away from a base portion to form an interior, and, an interior combustor assembly engagement frame (240) at least partially disposed in the interior of the exterior lift frame and configured to temporarily secure to at least a portion of a combustor assembly. The interior combustor assembly engagement frame is connected to the base portion of the exterior lift frame.
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6.发明申请公开(公告)号：US20170167298A1
公开(公告)日：2017-06-15
申请号：US14964792
申请日：2015-12-10
Applicant: General Electric Company
Inventor： Sandra Beverly Kolvick , Ansley Michelle Heard , Thomas Alan Mogle, II , Michael Leon Helton , Jason Dean Lorge, SR. , Lonnie Wood
IPC: F01D25/28
CPC classification number: F01D25/285 , B66C1/62 , F23R3/60 , F23R2900/00017 , F23R2900/00019
Abstract: A combustor assembly lift system comprises a lift arm comprising a first portion connected to a second portion, and a combustor assembly engagement frame connected to the lift arm, wherein the combustor assembly engagement frame is configured to temporarily secure to at least a portion of a combustor assembly.
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公开(公告)号：US10920620B2
公开(公告)日：2021-02-16
申请号：US16516847
申请日：2019-07-19
Applicant: General Electric Company
Inventor： Sandra Beverly Kolvick , Daryl Paul Capriotti , Ansley Michelle Heard , Rachel Kate King , Travis Edwin Lipstein , Maithri Muddasani , Tewodros Fiseha Wondimu
Abstract: Mounting apparatuses for turbine airfoils of turbine systems are disclosed. The mounting apparatuses may include a body portion configured to be at least partially positioned between a first airfoil and a second airfoil of the turbine system, and an adjustable, first retention component formed on a first side of the body portion. The adjustable, first retention component may be configured to contact a portion of a suction side of the first airfoil of the turbine system. The mounting apparatuses may also include a second retention component formed on a second side of the body portion, opposite the first side. The second retention component may be configured to contact a portion of a pressure side of the second airfoil of the turbine system.
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公开(公告)号：US10208627B2
公开(公告)日：2019-02-19
申请号：US14964806
申请日：2015-12-10
Applicant: General Electric Company
Abstract: A combustor assembly lift system comprises a track that extends in at least a longitudinal direction, a lift arm moveably engaged with the track such that it can traverse along the track in at least the longitudinal direction, and a combustor assembly engagement frame connected to the lift arm, wherein the combustor assembly engagement frame is configured to temporarily secure to at least a portion of a combustor assembly.
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