US2013094969A1PendingUtilityA1
System for sealing a shaft
Assignee: AMARAL SERGIO DANIEL MARQUESPriority: Oct 17, 2011Filed: Oct 17, 2011Published: Apr 18, 2013
Est. expiryOct 17, 2031(~5.3 yrs left)· nominal 20-yr term from priority
F01D 11/006
40
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Claims
Abstract
An embodiment of the present invention takes the form of a seal that may substantially reduce cross-shank leakage between components mounted on a shaft. Embodiments of the seal may be connected to a wide variety of rotatable components including, but not limited to, compressor blades, turbine buckets, or the like.
Claims
exact text as granted — not AI-modifiedWhat is claimed is:
1 . A system comprising:
a rotatable component comprising:
an airfoil portion comprising a first end, an opposite second end, and suction and pressure surfaces located between the first end and the opposite second end;
a shank portion comprising a mount and a slot, wherein the slot is positioned near a wall and is adjacent a downstream edge of the airfoil portion;
a platform portion that connects the airfoil portion to the shank portion;
a seal comprising:
an arm portion; and
a hook portion;
wherein the arm and hook portions are shaped to mate with the slot such that the slot restrains the movement of the seal;
wherein the seal is sized to substantially prevent a cooling flow from leaking through a shank pocket.
2 . The system of claim 1 , wherein the rotatable component is located in a turbine section of an air-ingesting turbomachine.
3 . The system of claim 1 , wherein the rotatable component is located in a compressor section of an air-ingesting turbomachine.
4 . The system of claim 1 , wherein the seal is maintained in the slot by a pressure difference between the shank pocket and a purge flow associated with an aft end of the rotatable component.
5 . The system of claim 1 , wherein the width of the seal comprises a range of from about 0.2 inches to about 1.0 inch.
6 . The system of claim 1 , wherein a length of the seal comprises a range of from about 2.0 inches to about 10.0 inches.
7 . The system of claim 1 , wherein a thickness of the seal comprises a range of from about 0.1 inches to about 0.5 inches.
8 . The system of claim 1 , wherein a shape of the hook portion includes: an arc portion, a polygon, or combinations thereof.
9 . The system of claim 8 , wherein a diameter of the arc portion comprises a range of from about 0.2 inches to about 1.0 inch.
10 . A system comprising:
a gas turbine comprising: a compressor section and a turbine section; a turbine bucket installed in the turbine section, wherein the turbine bucket comprises:
an airfoil comprising a tip, a base, and suction and pressure surfaces that connected the tip and the base;
a shank comprising a mount and a slot, wherein the slot is positioned near a surface that is adjacent an edge of the airfoil, and an end of the slot is adjacent to a top portion of the mount;
a platform portion that connects the airfoil to the shank;
a seal comprising:
an arm; and
a hook;
wherein the arm and hook are sized to allow insertion into the slot such that the slot secures the movement of the seal;
wherein the seal has a width that substantially prevents a cooling flow from leaking through a shank pocket, which is formed between the shank portion of the rotatable component and an another shank portion of an adjacent rotatable component.
11 . The system of claim 10 , wherein the seal is maintained in the slot by a pressure difference between the shank pocket and a purge flow associated with the turbine bucket.
12 . The system of claim 10 , wherein the width of the seal comprises a range of from about 0.2 inches to about 1.0 inch.
13 . The system of claim 10 , wherein a length of the seal extends from the platform to the mount.
14 . The system of claim 10 , wherein the length of the seal comprises a range of from about 2.0 inches to about 10.0 inches.
15 . The system of claim 10 , wherein a thickness of the seal comprises a range of from about 0.1 inches to about 0.5 inches.
16 . The system of claim 10 , wherein a shape of the hook portion includes: an arc portion, a polygon, or combinations thereof.
17 . The system of claim 16 , wherein a diameter of the arc portion comprises a range of from about 0.2 inches to about 1.0 inch.Cited by (0)
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