IP Library › Granted Patent US 11,566,526
Granted Patent B2
US 11,566,526 · App. 17/284,560 · Granted Jan 31, 2023

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

Inventors: Toshio Watanabe (Tokyo, JP); Kentaro Akimoto (Komaki, JP)
Assignee: MITSUBISHI HEAVY INDUSTRIES AERO ENGINES, LTD.
F01D5/16F01D5/18F01D25/06F05D2220/323F05D2240/80F05D2260/96
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 11,566,526
App. No.
17/284,560
Granted
Jan 31, 2023
Kind
B2
Abstract

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.

Claims (27)

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.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 12, 2021
From: WATANABE, TOSHIO; AKIMOTO, KENTARO
To: MITSUBISHI HEAVY INDUSTRIES AERO ENGINES, LTD.
Reel/Frame 055890/0434 →
Priority Claims (1)
JP JP2018-206239 · Nov 1, 2018 · national
Continuity (1)
Related Publication 20210317744A1 · Oct 14, 2021