초록 ▼

A retainer for securing the outer air seal assembly of a turbine rotor stage in a locked position. The outer air seal is suspended from the turbine casing over the rotor stage and is locked to the casing by annular segmented locking keys. A series of circumferentially spaced seats are located upon t

A retainer for securing the outer air seal assembly of a turbine rotor stage in a locked position. The outer air seal is suspended from the turbine casing over the rotor stage and is locked to the casing by annular segmented locking keys. A series of circumferentially spaced seats are located upon the front face of the locking key segments with the outer surfaces of the seats describing a circle approximating a first diameter. A split ring retainer is slidably carried in a radially disposed groove and is arranged to secure the key segments in a locked position. A series of lugs extend inwardly from the inside wall of the ring. The lugs are circumferentially spaced about the ring with the inner surface of the lugs approximating a circle having a second diameter that is less that of the first diameter approximated by the seats. The lugs are spaced so that each lug can be seated upon a seat to flex the ring outwardly in a radial direction and thus secure the key segment in a locking position.

대표청구항 ▼

What is claimed is: 1. A split retaining ring for preventing axial movement of a series of locking key segments for securing the outer air seal assembly of a turbine rotor stage to the turbine casing when the keys are in a locking position, said split ring retainer including: an annular body that i

What is claimed is: 1. A split retaining ring for preventing axial movement of a series of locking key segments for securing the outer air seal assembly of a turbine rotor stage to the turbine casing when the keys are in a locking position, said split ring retainer including: an annular body that is slidably contained within a radially disposed groove in the turbine casing, said annular body having a split therein whereby the body can be flexed radially in an outward direction within said groove, said body being arranged to engage a series of locking key segments to prevent axial movement of said key segments; a series of circumferentially spaced raised lugs located upon the inside wall of said annular body, said lugs having inner surfaces that approximates a circle having a first diameter; and said lugs being adapted to mount upon a series of circumferentially spaced seats, said seats having outer surfaces that approximate a circle having a second diameter that is greater than said first diameter whereby the retaining ring is flexed outwardly in a radial direction when mounted upon said seats. 2. The split ring retainer of claim 1 that further includes inclined means associated with each of the lugs for guiding the lugs into seating engagement with the seats as the ring is rotated within said groove. 3. The split ring retainer of claim 2, wherein said ring further includes a detent mechanism for locking the ring in place when the lugs are mounted upon the seats to prevent further rotation of the ring. 4. The split ring retainer of claim 3, wherein said detent means is diametrically opposed with relation to the split in said retaining ring. 5. The split ring retainer of claim 4 wherein the ring body further includes areas of reduced thickness on either side of said detent mechanism. 6. The split ring retainer for claim 2, wherein said inclined means further includes an inclined ramp located on either side of each lug. 7. The split ring of claim 1, wherein said seats are mounted upon the key segments. 8. A method of retaining an outer air seal of a turbine rotor stage to the turbine casing, said method including the steps of: mounting a series of circumferentially spaced seats upon movable locking segments that are arranged to retain the outer air seal of a rotor stage in engagement with the turbine casing when said key segments are placed in a locked position, the outer surfaces of said seats approximating a circle having a first diameter; providing a retaining ring having a body of a given thickness, said body having a split therein wherein said ring can be flexed outwardly; slidably containing said body in a radially disposed groove in the turbine casing so as to prevent axial movement of said locking key when in the locking position; locating a series of lugs upon the inside wall of the ring body so that the lugs extend inwardly in a radial direction, said lugs having inner surfaces that approximate a circle that has a second diameter that is less than said first diameter; and circumferentially spacing said lugs so that the inner surface of each lug can be mounted upon the outer surface of a rib to flex the ring outwardly in a radial direction. 9. The method of claim 8 that further includes the step of positioning inclined ramps on either side of said lugs and rotating said ring within said groove to guide the seats over said ramps onto said lugs. 10. The method of claim 9 that includes the further step of locating a detent upon said ring which is diametrically opposed to said split in the ring and snap fitting the detent to a keeper on one of said key segments when said lugs are mounted upon said seats to prevent further rotation of said ring. 11. The method of claim 10 that includes the further step of providing areas of reduced thickness in said ring on either side of said detent.