초록 ▼

The present invention relates to an improved system for installing a vane in a gas turbine. The system includes a receptor pocket positioned within a first support structure and a boot attached to a first or inner end of a vane for insertion into the receptor pocket. In a first embodiment of the pre

The present invention relates to an improved system for installing a vane in a gas turbine. The system includes a receptor pocket positioned within a first support structure and a boot attached to a first or inner end of a vane for insertion into the receptor pocket. In a first embodiment of the present invention, the receptor pocket is formed by machining it into the support structure. In a second embodiment of the present invention, the receptor pocket is formed by an insert which is installed into the support structure. In accordance with the present invention, the inner end of the vane having the boot is first inserted into the receptor pocket. After insertion has been completed, the vane is rotated until an outer base is brought into position against an outer support structure. The outer end of the vane is then secured to the outer support structure using studs and nuts.

대표청구항 ▼

1. A system for installing a vane in a gas turbine comprising: a receptor pocket machined into an annular ring portion of an inner casing; and a boot molded to a first end of said vane for insertion into said receptor pocket. 2. A system according to claim 1, wherein said boot is formed from a

1. A system for installing a vane in a gas turbine comprising: a receptor pocket machined into an annular ring portion of an inner casing; and a boot molded to a first end of said vane for insertion into said receptor pocket. 2. A system according to claim 1, wherein said boot is formed from a flexible dampening material. 3. A system according to claim 1, wherein said boot is formed from silicone rubber and is contoured to fit said receptor pocket. 4. A system according to claim 1, wherein said receptor pocket has a curved configuration and said boot has a curvature which matches said curved configuration. 5. A system according to claim 4, wherein said receptor pocket machined into said annular ring portion is open-ended and wherein said boot has a depth greater than a depth of the receptor pocket. 6. A system according to claim 1, wherein a second end of said vane is secured to a second support structure by a pair of bolts. 7. A system for installing a vane in a gas turbine engine comprising: a receptor pocket positioned within a first support structure; a boot attached to a first end of said vane for insertion into said receptor pocket; said first support structure having an opening; said receptor pocket being formed by an insert installed in said opening; said boot on said vane fitting into said insert; and retention devices for retaining said insert within said opening. 8. A system according to claim 7, wherein each said retention device is positioned between a side wall of said opening and a side wall of said insert. 9. A vane for use in a gas turbine comprising: an airfoil structure having a first end and a second end; a boot surrounding said first end of the airfoil structure; and said boot being molded to said airfoil structure. 10. A vane according to claim 9, wherein said boot is formed from a flexible material. 11. A vane according to claim 9, wherein said boot is formed from silicone rubber. 12. A vane according to claim 9, further comprising an outer base adjacent an outer end of said airfoil and said outer base including a platform and a sleeve. 13. A method of installing a vane into a gas turbine comprising the steps of: providing an inner support structure having an opening machined therein; providing a vane having a boot attached to an inner end; attaching said vane to said support structure by positioning said boot in said opening; inserting an insert cup into said opening prior to said attaching step; said attaching step comprising inserting said boot into said insert cup; rotating said vane after said attaching step and securing an outer end of said vane to an outer support structure; and said outer end securing step comprising securing said outer end of said vane to said outer support structure using threaded studs and nuts.