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公开(公告)号:US10576533B2
公开(公告)日:2020-03-03
申请号:US15895316
申请日:2018-02-13
Applicant: General Electric Company
Inventor: Magdalena Gaca , Adrian Adam Klejc , Mateusz Dolecki
Abstract: A staking tool is disclosed. The staking tool may include a main body, at least one punch disposed within the main body, and an actuator in mechanical communication with the at least one punch. The actuator may be configured to drive the at least one punch from a first position to a second position.
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公开(公告)号:US10533751B2
公开(公告)日:2020-01-14
申请号:US15882082
申请日:2018-01-29
Applicant: General Electric Company
Inventor: Sandra Beverly Kolvick , Adrien Francis Bigotte , Adrian Adam Klejc , Bernard Finbar Shannon
Abstract: Various embodiments include apparatuses for performing maintenance on a gas turbine (GT) combustion can, along with related methods. One apparatus can include: a mounting plate having at least two fasteners extending therethrough, the mounting plate configured to engage a fixed combustion chamber in the GT; a can adjustment bar configured to engage the can combustor, the can adjustment bar including a set of apertures extending therethrough; a set of guide pins extending through the set of apertures in the can adjustment bar and coupled with the mounting plate, the set of guide pins connecting the mounting plate with the can adjustment bar; and an adjustment member extending between the can adjustment bar and the mounting plate, the adjustment member configured to modify a position of the can adjustment bar relative to the mounting plate.
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公开(公告)号:US20180142560A1
公开(公告)日:2018-05-24
申请号:US15806479
申请日:2017-11-08
Applicant: General Electric Company
Inventor: Hubert Karol Wojtowicz , Adrian Adam Klejc , Sandra Beverly Kolvick
CPC classification number: F01D5/3007 , B23P19/02 , F01D5/005 , F01D5/225 , F01D25/285 , F05D2230/60 , F05D2230/68 , F05D2230/70 , F05D2240/30
Abstract: Embodiments of the present disclosure relate to the installation or removal of turbine blades at a turbine blade base thereof. An apparatus according to the present disclosure can include: an operative head configured to engage an axial sidewall of a turbine blade base; and a mount removably coupled to a portion of a turbomachine assembly by a coupler, wherein the operative head is slidably coupled to the mount such that the operative selectively engages the axial sidewall of the turbine blade base, and wherein the operative head is shaped to impart an axial and a circumferential force against the turbine blade base.
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