Variable stator and shroud assembly

Claim 2

A variable stator assembly for a gas turbine engine, said variable stator assembly comprising: a plurality of generally radially aligned variable stator blades, each said blade including opposed radially inner and radially outer ends and opposed upstream and downstream edges, said stator blades being adjustably mounted in the engine to rotate about an axis extending between the opposed inner and outer ends; a winglet fixedly mounted to at least one of said inner and outer ends of each said stator blade and moveable therewith relative to the engine, said winglet extending upstream beyond the upstream edge of said stator blade; and at least one shroud fixedly mounted to the engine, said shroud including a downstream edge spaced slightly from the upstream edge of each said stator blade at a location intermediate said inner and outer ends of each said stator blade, the downstream edge of said shroud being configured such that portions of said shroud are disposed intermediate adjacent stator blades, whereby said winglets and said shroud channelize the flow of gases through said variable stator assembly.

Claim 3

As assembly as in claim 1 wherein each said stator blade includes an inner winglet fixedly secured to the inner end of said stator blade and an outer winglet fixedly secured to the outer end of each said blade.

Claim 4

An assembly as in claim 2 wherein said at least one shroud comprises an inner shroud disposed substantially adjacent to said inner winglets and an outer shroud disposed substantially adjacent said outer winglets.

Claim 5

An assembly as in claim 3 wherein the inner and outer shrouds include portions disposed substantially parallel to the respective inner and outer winglets.

Claim 6

An assembly as in claim 4 wherein the downstream edge of each said shroud is disposed further downstream than the upstream edges of said winglets for each adjustable position of said stator blade, such that the inner and outer shrouds are disposed in overlapping relationship with the respective inner and outer winglets.

Claim 7

An assembly as in claim 1 wherein each said stator blade is generally rectangular in shape.

Claim 8

An assembly as in claim 1 wherein each said stator blade is generally trapezoidal in shape.

Claim 9

A variable stator assembly for a gas turbine engine, said engine comprising a generally annular flow path for combustion gases, said variable stator assembly comprising: a plurality of generally radially extending variable stator blades disposed in said flow path of said engine, each said blade including opposed upstream and downstream edges extending in generally radial directions relative to said engine, each said stator blade further including opposed radially inner and radially outer ends, each said stator blade being mounted in said flow path for controlled rotatable movement about an axis extending in a generally radial direction relative to the engine; inner and outer winglets fixedly mounted to the respective inner and outer ends of each said stator blade and moveable therewith relative to the engine, each said winglet including an upstream edge disposed further upstream in the engine than the upstream edge of the associated variable stator blade, the inner and outer winglets being spaced from the inner and outer walls of the flow path thereby defining generally annular inner and outer gaps therebetween; inner and outer shrouds fixedly mounted to the inner and outer walls respectively, said inner and outer shrouds each including downstream portions disposed substantially parallel and adjacent to portions of the respective inner and outer winglets, said downstream portions of said inner and outer shrouds being disposed intermediate the inner and outer winglets.

Claim 10

A variable stator assembly for a gas turbine engine, said engine comprising a generally annular flow path for combustion gases, said variable stator assembly comprising: a plurality of generally radially extending variable stator blades disposed in said flow path of said engine, each said blade including opposed upstream and downstream edges extending in generally radial directions relative to said engine, each said stator blade further including opposed radially inner and radially outer ends, each said stator blade being mounted in said flow path for controlled rotatable movement about an axis extending in a generally radial direction relative to the engine; inner and outer winglets fixedly mounted to the respective inner and outer ends of each said stator blade and moveable therewith relative to the engine, each said winglet including an upstream edge disposed further upstream in the engine than the upstream edge of the associated variable stator blade, the inner and outer winglets being spaced from the inner and outer walls of the flow path thereby defining generally annular inner and outer gaps therebetween; inner and outer shrouds fixedly mounted to the inner and outer walls respectively, said inner and outer shrouds each including downstream portions disposed substantially parallel and adjacent to portions of the respective inner and outer winglets, said downstream portions of said inner and outer shrouds being disposed intermediate the inner and outer winglets.

Claim 11

An assembly as in claim 8 wherein said inner and outer shrouds each include a downstream edge, said downstream edges being configured to be spaced slightly from the upstream edge of each said variable stator blade throughout the full range of movement for said variable stator blades.

Claim 12

An assembly as in claim 9 wherein the downstream portions of said inner and outer shrouds are configured to extend into the portion of the flow path intermediate adjacent ones of said variable stator blades.

Claim 13

An assembly as in claim 8 further comprising means for adjustably moving each of said variable stator blades.

Claim 14

An assembly as in claim 8 wherein the respective downstream edges of said inner and outer shrouds are of generally scalloped configuration.

Claim 15

An assembly as in claim 12 wherein the scalloped configuration of the respective downstream edges of said inner and outer shrouds defines points extending into the flow path between adjacent said variable stator blades.

Claim 16

As assembly as in claim 13 wherein a portion of the downstream edges of said inner and outer shrouds adjacent the points formed thereon is aligned generally parallel to a direction of flow of the combustion gases for a selected alignment of said variable stator blades.