摘要:
An apparatus (2) for aligning an end of a transition piece (TP) (4) with an outlet (6) of a combustor component (8) is disclosed. The apparatus (2) includes: a mount (10) configured to attach to the combustor component (8) proximate the outlet (6); a hinge component (16) pivotably connected to the mount (10), the hinge component (16) having an axis of motion substantially perpendicular with a primary axis of the combustor component (8); a dummy transition piece component (18) fixedly attached to the hinge component (16) for pivoting with the hinge component; and an adjustment apparatus (32) having a first end (34) fixedly attached to the dummy TP (18), and a second end (38) with an actuatable adjustment member (40) for modifying a position of the dummy TP (18).
摘要:
A method and system adapted for removing one or more shells from an assembly of multiple annular shells (14, 16, 18, 20), for example, turbine shells of a gas turbine engine (10). The method includes removing an upper shell (14, 18) positioned in an upper position relative to a lower shell (16, 20) of the assembly of multiple annular shells, and then positioning and securing a counterweight (22) in the upper position and securing the counterweight (22) to the lower shell as a replacement for the upper shell in the upper position. The counterweight (22) and the lower shell (16, 20) are then rotated in unison until the lower shell is in the upper position and the counterweight (22) is in a lower position previously occupied by the lower shell. Thereafter, the lower shell (16, 20) can be removed from the assembly.
摘要:
A system for lifting a first casing section (12) relative to a second casing section (14) is disclosed. The system may generally include a guide member (60) configured to be coupled to the second casing section (14) so as to generally extend lengthwise in a lift direction (36) of the first casing section (12) and a sleeve member (62) configured to be coupled to the first casing section (12). The sleeve member (62) may be movably disposed on the guide member (60) such that the sleeve member (62) is displaced along a length (64) of the guide member (60) as the first casing section (12) is lifted in the lift direction (36).
摘要:
A system for lifting a first casing section (12) relative to a second casing section (14) is disclosed. The system may generally include a guide member (60) configured to be coupled to the second casing section (14) so as to generally extend lengthwise in a lift direction (36) of the first casing section (12) and a sleeve member (62) configured to be coupled to the first casing section (12). The sleeve member (62) may be movably disposed on the guide member (60) such that the sleeve member (62) is displaced along a length (64) of the guide member (60) as the first casing section (12) is lifted in the lift direction (36).
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:
Methods for moving a starting motor 20 or a torque converter 22 within an auxiliary compartment 10 of a gas turbine are provided. A removal apparatus 24, which includes a lifting fixture 300 attached to a beam 110 pivotally mounted on a mast 104, is secured within the auxiliary compartment 10. To move the starting motor 20, a plurality of lifting hooks 316 on the lifting fixture 300 are attached to the starting motor 20, and the lifting fixture 300 and the starting motor 20 are hoisted. To move the torque converter 22, a pair of lifting lugs 308 on the lifting fixture 300 is attached to the torque converter 22, and the lifting fixture 300 and the torque converter 22 are hoisted. Methods are also generally provided for securing a removal apparatus 24 within an auxiliary compartment 10 of a gas turbine.
摘要:
A method and a machining kit (40) for machining a bore hole (24) into a shroud block (22) are disclosed. The method includes designating a location (42) of the bore hole (24) on an exterior surface (44) of the shroud block (22), positioning the shroud block (22) in a machining device (60), securing the shroud block (22) in the machining device (60), and machining the bore hole (24) in the shroud block (22). The machining device (60) includes a locating tool (82), a machining tool (84), a platform (62), a securing device (64), and a radial support (66). The radial support (66) is configured to mate with a radial exterior surface (48) of the shroud block (22) such that a machining axis (72) of the machining device (60) may be aligned with a radial axis (70) of the shroud block (22) during positioning.