The present application relates generally to a replaceable staking insert for the retention of a wheel attachment and more particularly relates to a replaceable staking insert for a blade mounted on a compressor rotor or other type of rotating turbine component.
Gas turbine systems generally include a compressor rotor having a number of stages. Air flowing into the compressor is compressed at each stage. Each stage includes a number of rotor buckets or blades mounted to a rim of a rotor wheel or a disk in a spaced relationship. A typical compressor rotor may have dozens of rotor blades mounted thereon.
Generally described, each blade may have a dovetailed portion that interlocks with a dovetail region of the rim to secure the blade to the rotor. The blade dovetails may be secured to the rotor via a process called “staking”. Specifically, the rotor blade is placed within the rim slot and then “staked” into place by deforming the metal material around the blade dovetail with a tool similar to a nail punch. This process is then repeated for each rotor blade for each rotor assembly stage. Staking provides an economical and mechanically secured means of securing a blade or other attachment to the rotor or other type of wheel slot.
In an inspection or an overhaul process, the rotor blades may be removed from the rotor wheel and the original “stakes” may be ground out. There are a finite number of attachments due to a limited number of viable staking locations about the rotor wheel. As such, the rotor wheel generally must be replaced once these staking locations have been consumed even if the rotor wheel is otherwise still in operational condition.
There is a desire therefore for improved methods and devices for securing a blade or other type of wheel attachment to a rotor or other type of wheel without destroying the rotor or the wheel or limiting its part life. These improved methods and devices should provide for simple but secure attachment of the blade or other component to the wheel in a fast and efficient manner.
The present application thus describes a rotating assembly. The rotating assembly may include a wheel, a slot positioned about the wheel with the slot having a staking recess positioned therein, a wheel attachment positioned within the slot, and a staking insert positioned within the staking recess. The staking recess axially retains the staking insert and the wheel attachment radially retains the staking insert.
The application further describes a rotor assembly. The rotor assembly may include a rotor, a number of axial slots positioned about a rim of the rotor with the axial slots each having one or more staking recesses positioned therein, a blade positioned within each of the axial slots, and a staking insert positioned within each of the staking recesses.
The application further describes a staking tool assembly for use about a wheel with rim having a number of axial slots. The staking tool assembly may include a staking tool and a staking tool guide positioned axially about the rim and the axial slots of the wheel.
These and other features of the present application will become apparent to one of ordinary skill in the art upon review of the following detailed description when taken in conjunction with the several drawings and the appended claims.
Referring now to the drawings, in which like numerals refer to like elements throughout the several views,
Each end 160, 170 of the axial slot 120 may have an insert recess 180 formed therein. The insert recess 180 may include an insert base 190 that has a stepped down shape from the base 130 of the axial slot 120. The insert recess 180 also may have a pair of concave insert sidewalls 200 that define an axial opening 210. Other shapes may be used herein. The shape and dimensions of the insert recess 180 may vary with the geometry of the axial slot 120 and the rotor assembly 100 as a whole.
The rotor assembly 100 also includes a number of rotor buckets or blades 220. Any number of blades 220 may be used herein. Each axial slot 120 may have a blade 220 mounted therein. Each blade 220 may include a root 230 with an airfoil 240 extending therefrom. The root 230 may have a substantial dovetail-like shape that conforms to the dovetail-like shape of the axial slot 120. Specifically, the root 230 may include a base 250 and a pair of convex sidewall 260. The root 230 may extend the length of the axial slot 120 from the first end 160 to the second end 170 of the base 130 or the root 230 may extend for a portion of the length and one or more spacers (not shown) also may be used to fill the length of the axial slot 120.
The rotor assembly 100 further may include a staking insert 270. The staking insert 270 may be inserted in each of the insert recesses 180 of the axial slots 120. The staking insert 270 may be sized to cooperate with the insert recess 180 and may have a staking insert base 280 and a pair of convex sidewalls 290. Other shapes may be used herein. The staking insert 270 may be made out of alloy steel, nickel, or other types of substantially heat resistant and/or corrosion resistant materials. The staking insert 270 may be axially retained within the sidewalls 200 of the insert recess 180. Other types of complementary shapes and retaining means may be used herein.
In use, the staking inserts 270 may be inserted within the insert recesses 180 of the axial slots 120. Each axial slot 120 may have two (2) insert recesses 180 such that two (2) staking inserts 270 may be used for each blade 220. As described above, the staking insert 270 may be retained axially via the shape of the insert recess 180. A blade 220 then may be slid into each axial slot 120. The root 230 of the blade 220 retains the staking insert 270 radially.
As is shown in
The staking tool assembly 300 may include a staking tool guide 340. As is shown in
The base 370 also may be used to position other types of equipment about the axial slot 120 or otherwise. For example, a drilling/milling apparatus may be mounted thereon to provide for machining of the axial slot 120 or otherwise. In this case, multiple bases 370 may be used such that both adjoining axial slots 120 may be used. Other types of equipment may be mounted herein.
The use of the staking tool guides 340, 400 thus provide for the proper location of the staking tool 310 for controlled staking locations and consistently reproducible results. The staking inserts 270 may be quickly inserted and staked for efficient construction or repair.
Although the use of the rotor assembly 100 has been described herein with the use of the rotor 105, the present invention may be applicable to any type of rotating assembly. Other potential applications include rotating buckets of gas turbines, rotating buckets/blades of steam turbines, or the retention of any device that is mechanically attached to a rotating wheel or disk with an axial slot or dovetail arrangement.
It should be apparent that the foregoing relates only to the preferred embodiments of the present application and that numerous changes and modifications may be made herein by one of ordinary skill in the art without departing from the general spirit and scope of the invention as defined by the following claims and the equivalents thereof.
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59113207 | Jun 1984 | JP |
Number | Date | Country | |
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20090077795 A1 | Mar 2009 | US |