Combination for sealing a gap between turbomachine blades and for reducing vibrations of the turbomachine blades
US-2019128120-A1 · May 2, 2019 · US
US11566526B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11566526-B2 |
| Application number | US-201917284560-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 25, 2019 |
| Priority date | Nov 1, 2018 |
| Publication date | Jan 31, 2023 |
| Grant date | Jan 31, 2023 |
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A vibration damping device according to an embodiment is a vibration damping device for a blade of a rotating machine, which includes at least one housing configured to be containable in a cavity formed under a platform of the blade, and to be detachable from the blade, and an attenuation material disposed in a vibration damping space formed inside the housing.
Opening claim text (preview).
The invention claimed is: 1. A vibration damping device for a blade of a rotating machine, the device comprising: at least one housing configured to be containable in a cavity formed under a platform of the blade, and to be detachable from the blade; and an attenuation material disposed in a vibration damping space formed inside the housing, wherein the housing includes at least one wall member disposed in the vibration damping space, wherein the wall member divides the vibration damping space into a plurality of regions which include a pair of regions facing each other across the wall member and communicating with each other, wherein the attenuation material is configured to be movable between the pair of regions, and wherein, in the vibration damping space, a minimum gap portion, where a distance between the at least one wall member and an inner wall surface of the housing defining the vibration damping space is minimum, is formed at a position farther away from an airfoil part of the blade than a center position of the housing in a thickness direction of the blade. 2. A rotating machine, comprising: a blade which includes a platform and an airfoil part erected on the platform; and the vibration damping device according to claim 1 mounted on the blade, under the platform. 3. A vibration damping device for a blade of a rotating machine, the device comprising: at least one housing configured to be containable in a cavity formed under a platform of the blade, and to be detachable from the blade; and an attenuation material disposed in a vibration damping space formed inside the housing, wherein the housing includes at least one wall member disposed in the vibration damping space, wherein the wall member divides the vibration damping space into a plurality of regions which include a pair of regions facing each other across the wall member and communicating with each other, and wherein the attenuation material is configured to be movable between the pair of regions, wherein, in the vibration damping space, a minimum gap portion, where a distance between the at least one wall member and an inner wall surface of the housing defining the vibration damping space is minimum, is formed, and wherein the wall member has an inclined surface inclined with respect to the inner wall surface such that the distance between the wall member and the inner wall surface increases with distance from the minimum gap portion. 4. A vibration damping device for a blade of a rotating machine, the device comprising: at least one housing configured to be containable in a cavity formed under a platform of the blade, and to be detachable from the blade; and an attenuation material disposed in a vibration damping space formed inside the housing, wherein the housing includes at least one wall member disposed in the vibration damping space, wherein the wall member divides the vibration damping space into a plurality of regions which include a pair of regions facing each other across the wall member and communicating with each other, wherein the attenuation material is configured to be movable between the pair of regions, and wherein the wall member includes: an axial wall portion extending along a chordwise direction of the blade; and a circumferential wall portion extending along a thickness direction of the blade.
for counteracting blade vibration · CPC title
for aircraft propulsion, e.g. jet engines · CPC title
Platforms for stationary or moving blades · CPC title
Preventing, counteracting or reducing vibration or noise · CPC title
for preventing blade vibration (means on blade-carrying members or blades F01D5/00) · CPC title
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