US4621979A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Fan rotor blades of turbofan engines
Assignee: RTX Corp
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Filing: 1979-11-30
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Granted: 1986-11-11
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Expires: 1999-11-30
Abstract
Abstract The present invention provides improvements to fan rotor blades of turbofan gas turbine engines. Increased low cycle fatigue life is sought, and a specific object is to obtain a more nearly uniform chordwise distribution of maximum stress levels across the root sections of fan blades. In one effective embodiment incorporating concepts of the present invention the root section of a fan blade is contoured to an arcuate geometry which approximates the contour of the airfoil cross section at the inner wall of the working medium flowpath. Further contour specifications for reducing local stress levels are discussed.
Inventors
- 👤 Robert H. Zipps
- 👤 Chester H. Rynaski
- 👤 Graham B. Fulton
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-07 19:14
CPC Classifications
F; F01; F01D; F01D5/00; F01D5/30; F01D5/3007; F01D11/00; F01D11/005; F01D11/006; F01D11/008; F01D5/12; F01D5/14; F01D5/141; Y; Y02; Y02T; Y02T50/00; Y02T50/60
Claims Analysis
Total Claims: 5
Claim 1
Independent Claim
112 words
A fan blade of the type extending outwardly from a rotor disk across the annular flowpath for working medium gases in the fan section of a turbofan engine, including: an airfoil section having an arcuate cross section contour at the inner wall of the working medium flowpath; and a root section having an upstream end and a downstream end wherein the root section is formed to an arcuate contour which approximates the arcuate contour of the airfoil cross section at the inner wall of the working medium flowpath projected onto the root section, and wherein the root section is convergently tapered from the downstream end toward the upstream end of the blade.
Claim 2
Dependent Claim
112 words
A fan blade of the type extending outwardly from a rotor disk across the annular flowpath for working medium gases in the fan section of a turbofan engine, including: an airfoil section having an arcuate cross section contour at the inner wall of the working medium flowpath; and a root section having an upstream end and a downstream end wherein the root section is formed to an arcuate contour which approximates the arcuate contour of the airfoil cross section at the inner wall of the working medium flowpath projected onto the root section, and wherein the root section is convergently tapered from the downstream end toward the upstream end of the blade.
Claim 3
Dependent Claim
103 words
The fan blade according to claim 1 wherein the fan blade has a suction side and a pressure side and wherein the projected airfoil cross section has a non-circular arc, mean line L A and wherein the root section has a circular arc mean line L R the non-circular arc mean line L A of the projected airfoil cross section being offset to the suction side of the blade from the circular arc mean line L R at the upstream end of the blade and being essentially coextensive with the circular arc mean line L R at the downstream end of the blade.
Claim 4
Dependent Claim
43 words
The fan blade according to claim 2 wherein the circular arc mean line L R has a radius R R which is scribed from a point P R laterally of the blade between the upstream end and the downstream end of the blade.
Claim 5
Dependent Claim
98 words
The fan blade according to claim 3 which includes at least one arcuate tooth at the suction side of the blade and at least one arcuate tooth at the pressure side of the blade, the teeth extending to approximately equal radii R A and R B , respectively from points P A and P B , respectively which lie on a line X at equal distances from the point P R wherein the line X extends through the point P R and the intersection of the root mean line L R with the downstream edge of the blade.
References Cited (Backward Citations)
US1041269A
Cited
US1719415A
Cited
US1793468A
Cited
DE587923C
Cited
FR1143952A
Cited
US3986793A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1989-11-10 | 1990-05-12 | 1990-11-11 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1993-11-10 | 1994-05-12 | 1994-11-11 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1997-11-10 | 1998-05-12 | 1998-11-11 | $7700.00 | Window Closed / Lapsed |