摘要:
Embodiments of the present disclosure relate generally to an apparatus and method for treating a rotatable component (4). An apparatus according to the present disclosure can include: a sliding engagement member (6) configured to slidably engage a portion of a rotating component (4) that is temporarily stationary; and a tool engaging member (8) for positioning a machining tool (10) relative to the rotating component (4) to machine a surface of the rotating component (10), wherein the tool engaging member (8) is rotatable to one of a plurality of angles relative to the sliding engagement member (6).
摘要:
A system (40) for modifying a slot (24) in a rotor (18) includes a drill (42), a clamp (80) connected to the drill (42) and configured to engage with an interior surface of the slot (24), and means for supporting the drill (42) from a stationary platform adjacent to the rotor (18). A method for modifying a slot (24) in a rotor (18) includes connecting a coupling (100) to a stationary platform adjacent to the rotor (18), connecting a drill (42) to the coupling (100), and locating the drill (42) proximate to the slot (24). The method further includes inserting a clamp (80) into the slot (24), engaging the clamp (80) with an interior surface of the slot (24), and operating the drill (42) to create a cavity in the slot (24).
摘要:
A turbomachine rotor blade milling machine system (40) includes a fixture (44) having a body (58) including first and second opposing surfaces (60, 62) and a slot (96). The fixture (44) is configured and disposed to connect with first and second rotor blade sections mounted in a rotor wheel (16). A mounting system (106) includes at least one mounting element (108, 109) coupled to one of the first and second opposing surfaces (60, 62) of the body (58) at the slot (96). A milling machine (48) is coupled to the one of the first and second opposing surfaces (60, 62) through the at least one mounting element (108, 109). The milling machine (48) includes a cutter (147) and is configured and disposed to form an opening extending axially through a dovetail portion of a third rotor blade section arranged between the first and second rotor blade sections.
摘要:
Various embodiments include alignment apparatuses and associated methods for use on a turbine (e.g., a gas turbine). In various particular embodiments, an apparatus to for aligning an unfixed inlet guide vane (IGV) 12 adjacent a fixed IGV 8 in a gas turbine for. In some cases the apparatus includes: a first wedge member 6 for interfacing with the fixed IGV 8; a second wedge member 10 movably coupled with the first wedge member 6, the second wedge member 10 for interfacing with the unfixed IGV 12; and an adjustment apparatus 32 coupled to the first wedge member 6 and the second wedge member 10, the adjustment apparatus 32 for modifying a position of the second wedge member 10 relative to the first wedge member 6 to actuate movement of the unfixed IGV 12 relative to the fixed IGV 8.
摘要:
Various embodiments include alignment apparatuses and associated methods for use on a turbine (e.g., a gas turbine). In various particular embodiments, an apparatus to for aligning an unfixed inlet guide vane (IGV) 12 adjacent a fixed IGV 8 in a gas turbine for. In some cases the apparatus includes: a first wedge member 6 for interfacing with the fixed IGV 8; a second wedge member 10 movably coupled with the first wedge member 6, the second wedge member 10 for interfacing with the unfixed IGV 12; and an adjustment apparatus 32 coupled to the first wedge member 6 and the second wedge member 10, the adjustment apparatus 32 for modifying a position of the second wedge member 10 relative to the first wedge member 6 to actuate movement of the unfixed IGV 12 relative to the fixed IGV 8.
摘要:
Embodiments of the present disclosure relate generally to an apparatus and method for treating a rotatable component (4). An apparatus according to the present disclosure can include: a sliding engagement member (6) configured to slidably engage a portion of a rotating component (4) that is temporarily stationary; and a tool engaging member (8) for positioning a machining tool (10) relative to the rotating component (4) to machine a surface of the rotating component (10), wherein the tool engaging member (8) is rotatable to one of a plurality of angles relative to the sliding engagement member (6).
摘要:
A system (40) for modifying a slot (24) in a rotor (18) includes a base (44) having a vertical axis (46). a drill (42) is slidingly connected to the base (44) along the vertical axis (46), and a clamp (80) is connected to the base (44) and configured to engage with an interior surface of the slot (24). a method for modifying a slot (24) in a rotor (18) includes locating a drill (42) proximate to the slot (24) and inserting a clamp (80) into the slot (24), wherein the clamp (80) is slidingly connected to the drill (42). the method further includes engaging the clamp (80) with an interior surface of the slot (24) and operating the drill (42) to create a cavity (28) in the slot (24).
摘要:
A system for heating a stator segment includes a first frame member 46, a plurality of arms 50 extending radially from the first frame member 46, and a heater 44 releasably connected to each arm 50. The system further includes a biasing element 64 for biasing each heater away from the first frame member 46.
摘要:
A turbomachine rotor blade milling machine system (40) includes a fixture (44) having a body (58) including first and second opposing surfaces (60, 62) and a slot (96). The fixture (44) is configured and disposed to connect with first and second rotor blade sections mounted in a rotor wheel (16). A mounting system (106) includes at least one mounting element (108, 109) coupled to one of the first and second opposing surfaces (60, 62) of the body (58) at the slot (96). A milling machine (48) is coupled to the one of the first and second opposing surfaces (60, 62) through the at least one mounting element (108, 109). The milling machine (48) includes a cutter (147) and is configured and disposed to form an opening extending axially through a dovetail portion of a third rotor blade section arranged between the first and second rotor blade sections.