초록 ▼

A stator vane stage in a split-case, variable geometry axial flow compressor includes two 180-degree spoke-like arrays of stator vanes on upper and lower case halves of the compressor case and a pair of unitary, 180-degree arc shroud ring segments. Each stator vane has a pivot shaft at one end rotat

A stator vane stage in a split-case, variable geometry axial flow compressor includes two 180-degree spoke-like arrays of stator vanes on upper and lower case halves of the compressor case and a pair of unitary, 180-degree arc shroud ring segments. Each stator vane has a pivot shaft at one end rotatably supported in a radial bore in the corresponding case half by a bushing and a cylindrical vane button at the other end. Each shroud ring segment has a corresponding plurality of cylindrical vane button sockets in an outer surface thereof which rotatably receives a corresponding vane button. The spoke-like array of the stator vanes rigidly positions the shroud ring segments relative to the compressor case. To assemble the shroud ring segments to the stator vanes, the shroud ring segments are first resiliently squeezed radially inward while the vane buttons are sequentially inserted into the corresponding vane button sockets and then released to spring back to their true 180-degree arc shapes in which they are captured on the stator vanes.

대표청구항 ▼

A method of making an annular stage of variable geometry stator vanes on a case of an axial flow compressor, said case being split in a horizontal center-plane thereof a first case half and a second case abutting in said horizontal center-plane at respective longitudinal edges thereof and each of sa

A method of making an annular stage of variable geometry stator vanes on a case of an axial flow compressor, said case being split in a horizontal center-plane thereof a first case half and a second case abutting in said horizontal center-plane at respective longitudinal edges thereof and each of said stator vanes having a pivot shaft at one end and a vane button at the other end, said method comprising the steps of: forming on each of said first and said second case halves a 180-degree array of a plurality of radial bores in a plane perpendicular to a longitudinal axis of said compressor case, inserting each of said vane pivot shafts loosely into a respective one of said radial bores, forming a first unitary 180-degree arc shroud ring segment having a first planar end and a second planar end and a plurality of vane button sockets in an outer surface thereof equal in number to the number of said stator vanes in said 180-degree array on said first case half, forming a second unitary 180-degree arc shroud ring segment having a first planar end and a second planar end and a plurality of vane button sockets in an outer surface thereof equal in number to the number of said stator vanes in said 180-degree array on said second case half, maintaining each of said first and said second shroud segments in a pinched condition achieved by resiliently deflecting said first and said second planar ends toward each other, fitting said first shroud ring segment on said 180-degree array of stator vanes on said first case half by inserting said vane buttons thereof into respective ones of said vane button sockets on said first shroud ring segment, fitting said second shroud ring segment on said 180-degree array of stator vanes on said second case half by inserting said vane buttons thereof into respective ones of said vane button sockets on said second shroud ring segment, releasing each of said first and said second shroud ring segments from said pinched condition, inserting a bushing between each of said stator vane pivot shafts and the corresponding one of said radial bores to rotatably mount each of said stator vanes on respective ones of said first and said second case halves, and joining said first and said second case halves at said longitudinal edges thereof. In a split-case axial flow compressor having a case including a first case half having a pair of longitudinal edges and a second case half having a pair of longitudinal edges abutting respective ones of said longitudinal edges of said first case half in a horizontal center-plane of said case, a stator vane stage comprising means defining a plurality of radial bores in each of said first and said second case halves in a plane perpendicular to a longitudinal axis of said case and arrayed symmetrically between said longitudinal edges of the corresponding ones of said first and said second case halves, a plurality of stator vanes each having a pivot shaft at a first end thereof loosely received in a respective one of said radial bores in said upper and said lower case halves and a cylindrical vane button at a second end thereof, a plurality of bushings interposed between each of said stator vane pivot shafts and the corresponding one of said radial bores whereby each of said stator vanes is supported on a corresponding one of said first and said second case halves for rotation about a radial axis of said case, a first unitary 180-degree arc shroud ring segment having an outer surface with a plurality of cylindrical bores therein symmetrically spaced between a pair of planar ends of said first shroud ring segment and rotatably receiving a corresponding one of said vane buttons on said stator vanes on said first case half, and a second unitary 180-degree arc shroud ring segment having an outer surface with a plurality of cylindrical bores therein symmetrically spaced between a pair of planar ends of said second shroud ring segment and rotatably receiving a corresponding one of said vane buttons on said stator vanes on said second case half.