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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：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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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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