US4268223A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Vibration supression for turbine blades
Assignee: BBC Brown Boveri AG Switzerland
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Filing: 1978-09-14
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Granted: 1981-05-19
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Expires: 1998-09-14
Abstract
Abstract A method and apparatus for suppressing vibration in turbine blading and the like is disclosed. A damping tube is inserted through an aperture in each of a plurality of turbine blades. By expanding the damping tube after it is inserted in the blades the tube is firmly secured to each blade. A wire may be inserted through the damping tube and is secured by crimping the expanded tube portions. The tube may be divided into circumferential segments with each tube being widened for example by means of a center punch at an end portion which extends through the final blade of each segment.
Inventors
- 👤 Emil Anner
- 👤 Harry Brunner
- 👤 Hans J. Meister
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-08 06:40
CPC Classifications
F; F01; F01D; F01D5/00; F01D5/12; F01D5/22; F01D5/24; Y; Y10; Y10S; Y10S416/00; Y10S416/50
Claims Analysis
Total Claims: 4
Claim 1
Independent Claim
219 words
In a turbine or compressor of the type having stator and rotor members formed with adjacent radial blades arranged in a row about a central axis of the turbine or compressor, a vibration suppressed blade arrangement comprising: a damping tube including a plurality of curved damping tube segments which extend through a plurality of blades arranged in a blade ring; at least two adjacent blades having apertures therein, the damping tube extending through and being both closely and directly received by said apertures and having a thickness adjacent said apertures that is greater than the size of said apertures to securely position the damping tube with respect to said blades, each of the damping tube segments including enlarged end portions which are provided in close proximity to a respective one of the apertures of one of the blades, said enlarged end portions being wider than the size of the respective one of the apertures to securely position the tube segment with respect to the one blade; and a wire extending through the damping tube, the wire including a plurality of wire segments, each wire segment extending through a corresponding one of said curved damping tube segments along a longitudinal axis of the damping tube, the wire being secured to the damping tube intermediate adjacent blades of the blade ring.
Claim 2
Dependent Claim
219 words
In a turbine or compressor of the type having stator and rotor members formed with adjacent radial blades arranged in a row about a central axis of the turbine or compressor, a vibration suppressed blade arrangement comprising: a damping tube including a plurality of curved damping tube segments which extend through a plurality of blades arranged in a blade ring; at least two adjacent blades having apertures therein, the damping tube extending through and being both closely and directly received by said apertures and having a thickness adjacent said apertures that is greater than the size of said apertures to securely position the damping tube with respect to said blades, each of the damping tube segments including enlarged end portions which are provided in close proximity to a respective one of the apertures of one of the blades, said enlarged end portions being wider than the size of the respective one of the apertures to securely position the tube segment with respect to the one blade; and a wire extending through the damping tube, the wire including a plurality of wire segments, each wire segment extending through a corresponding one of said curved damping tube segments along a longitudinal axis of the damping tube, the wire being secured to the damping tube intermediate adjacent blades of the blade ring.
Claim 3
Dependent Claim
51 words
The arrangement according to claim 1 wherein said damping tube is secured to the wire by crimps provided in the damping tube between adjacent blades of the blade ring and further wherein the wire is closely received within the damping tube at the apertures of the at least two adjacent blades.
Claim 4
Dependent Claim
26 words
The arrangement according to claim 1 wherein the damping tube has a diameter between adjacent blades which is substantially greater than the diameter of the wire.
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1984-05-18 | 1984-11-17 | 1985-05-19 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1988-05-18 | 1988-11-17 | 1989-05-19 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1992-05-18 | 1992-11-17 | 1993-05-19 | $7700.00 | Window Closed / Lapsed |