Patent US4460314A successfully refreshed from Google Patents.
US4460314A
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US
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Vibration damped rotor blades for turbomachines
Assignee: Rolls Royce PLC
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Filing: 1981-12-04
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Granted: 1984-07-17
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Expires: 2001-12-04
Abstract
Abstract A blade for a turbomachine having an aerofoil portion and a root portion. The blade is provided with a vibration damper for damping a predetermined vibration of the blade. The damper comprises a closed chamber 14 within the aerofoil portion 13 adjacent the tip of the blade, and liquid 15 within the chamber 14. The volume of liquid 15 is less than the volume of the chamber 14. The chamber 14 is shaped, positioned, and aligned relative to the blade, so that in use the liquid 15 is constrained to form a column which oscillates in the chamber 14 in radial directions and in the same directions as the vibration to be damped. The volume, mass, and viscosity of the liquid are all chosen in relation to the frequency vibration (W B ) of the vibration to be damped and the rotor speed (W E ) so that, in use, the length (L) of the column of liquid is such that ##EQU1## where R=the blade tip radius. In this way the liquid 15 is caused to oscillate, under centrifugal loads, at a natural frequency which matches, or is close to, the resonant frequency of the vibration to be damped.
Inventors
- 👤 John R. D. Fuller, deceased
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-28 18:09
CPC Classifications
F; F01; F01D; F01D5/00; F01D5/12; F01D5/26; F16; F16F; F16F15/00; F16F15/10; F16F15/16; Y; Y10; Y10S; Y10S416/00; Y10S416/50
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
226 words
A blade for a turbomachine having an airfoil portion and a root portion, the blade being provided with a vibration damper for damping a predetermined vibration of the blade, the damper comprising a closed chamber "U"-shaped in cross section within the airfoil portion adjacent the tip of the blade, and a material within the chamber which, at least in use, is a liquid, the volume of liquid being less than the volume of the chamber, the chamber having a concave surface that faces toward the root portion and extends in a direction along the length of the airfoil portion to define a "U"-shaped path along which the liquid is constrained to oscillate, and the chamber being shaped, positioned, dimensioned and aligned relative to the blade so that the liquid forms a column which oscillates in the chamber in radial directions and the volume, mass and viscosity of the liquid being chosen in relation to the frequency (W B ) of the vibration to be damped, and the rotor speed (W E ) so that, in use, the length (L) of the column of liquid is such that ##EQU18## where R=the blade tip radius, thereby to cause the liquid to oscillate in a "U"-shaped path under centrifugal loads, at a natural frequency which matches, or is close to, the resonant frequency of the vibration to be damped.
Claim 2
Dependent Claim
226 words
A blade for a turbomachine having an airfoil portion and a root portion, the blade being provided with a vibration damper for damping a predetermined vibration of the blade, the damper comprising a closed chamber "U"-shaped in cross section within the airfoil portion adjacent the tip of the blade, and a material within the chamber which, at least in use, is a liquid, the volume of liquid being less than the volume of the chamber, the chamber having a concave surface that faces toward the root portion and extends in a direction along the length of the airfoil portion to define a "U"-shaped path along which the liquid is constrained to oscillate, and the chamber being shaped, positioned, dimensioned and aligned relative to the blade so that the liquid forms a column which oscillates in the chamber in radial directions and the volume, mass and viscosity of the liquid being chosen in relation to the frequency (W B ) of the vibration to be damped, and the rotor speed (W E ) so that, in use, the length (L) of the column of liquid is such that ##EQU18## where R=the blade tip radius, thereby to cause the liquid to oscillate in a "U"-shaped path under centrifugal loads, at a natural frequency which matches, or is close to, the resonant frequency of the vibration to be damped.
Claim 3
Dependent Claim
47 words
A blade according to claim 1 wherein the chamber is shaped to define two radially extending limbs interconnected at their ends nearest to the tip of the blade, so that in use centrifugal forces on the liquid cause it to oscillate from one limb to the other.
Claim 4
Dependent Claim
38 words
A blade according to claim 1 wherein the chamber is defined by the gap between a concave wall which is spaced from, and faces, a convex wall, and in use the concave wall faces towards the root portion.
Claim 5
Dependent Claim
13 words
A blade according to claim 1 wherein the liquid is a liquid metal.
Claim 6
Dependent Claim
31 words
A blade according to claim 1 wherein the liquid comprises a material which when not in use is non-liquid but in use is liquid at the operating temperature of the blade.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1987-07-17 | 1988-01-16 | 1988-07-17 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1991-07-17 | 1992-01-16 | 1992-07-17 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1995-07-17 | 1996-01-16 | 1996-07-17 | $7700.00 | Window Closed / Lapsed |