Vibration damping device for blade of rotating machine and rotating machine including the same

US11566526B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11566526-B2
Application numberUS-201917284560-A
CountryUS
Kind codeB2
Filing dateJul 25, 2019
Priority dateNov 1, 2018
Publication dateJan 31, 2023
Grant dateJan 31, 2023

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

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.

First claim

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.

Assignees

Inventors

Classifications

  • F01D5/16Primary

    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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What does patent US11566526B2 cover?
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.
Who is the assignee on this patent?
Mitsubishi Heavy Ind Aero Engines Ltd
What technology area does this patent fall under?
Primary CPC classification F01D5/16. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Jan 31 2023 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 10 related publications on this page (citations in our corpus or others sharing the same primary CPC).