← Back to Patent Explorer
US5102298A Expired / Lapsed US ⏱️ 0.0 years remaining

Axial flow turbine

Assignee: Alstom SA
•
Filing: 1990-08-23
•
Granted: 1992-04-07
•
Expires: 2010-08-23
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract An axial flow turbine, whose outlet rotor blades (12) are followed by a diffuser (13), has first means (8) within the retardation zone of the diffuser for swirl removal from the swirling flow. A row with adjustable guide vanes (11) is arranged between these first means for swirl removal in the form of aerodynamic ribs and the outlet rotor blades. These guide vanes (11) have a straight mean camber line with a symmetrical aerofoil section, are conically shaped in the radial direction and are twisted. In addition to a substantial improvement in the pressure recovery over a wide load range, this measure also permits the vortex usually occurring between the rotor blades and the aerodynamic ribs to be prevented.

Inventors

  • 👤 Franz Kreitmeier

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-05 06:38
CPC Classifications
F; F01; F01D; F01D17/00; F01D17/10; F01D17/12; F01D17/14; F01D17/16; F01D17/162; F01D25/00; F01D25/30

Claims Analysis

Total Claims: 10
Claim 1
Independent Claim 79 words
Axial flow turbine comprising: a plurality of rotor blades include a set of outlet rotor blades from which a swirling gas flow may be discharged, a diffuser following said outlet rotor blades in a gas flow direction, means for swirl removal from the swirling flow, said swirl removal means being provided with a retardation zone of the diffuser, and at least one row of adjustable guide vanes arranged between the means for swirl removal and the outlet rotor blades.
Claim 2
Dependent Claim 79 words
Axial flow turbine comprising: a plurality of rotor blades include a set of outlet rotor blades from which a swirling gas flow may be discharged, a diffuser following said outlet rotor blades in a gas flow direction, means for swirl removal from the swirling flow, said swirl removal means being provided with a retardation zone of the diffuser, and at least one row of adjustable guide vanes arranged between the means for swirl removal and the outlet rotor blades.
Claim 3
Dependent Claim 23 words
Axial flow turbine as claimed in claim 1, wherein the guide vanes have a straight mean camber line with a symmetrical aerofoil section.
Claim 4
Dependent Claim 19 words
Axial flow turbine as claimed in claim 2, wherein the guide vanes are conically shaped in the radial direction.
Claim 5
Dependent Claim 14 words
Axial flow turbine as claimed in claim 2, wherein the guide vanes are twisted.
Claim 6
Dependent Claim 29 words
Axial flow turbine as claimed in claim 1, wherein the pitch/chord ratio of the guide vanes is between 0.5 and 1 in the center section of the flow duct.
Claim 7
Dependent Claim 55 words
Axial flow turbine as claimed in claim 1, wherein the means for swirl removal within the diffuser are aerodynamic ribs which are arranged evenly around the periphery and which have a straight mean camber line, a symmetrical aerofoil section and a pitch/chord ratio between 0.5 and 1 in the center section of the flow duct.
Claim 8
Dependent Claim 19 words
Axial flow turbine as claimed in claim 6, wherein the aerodynamic ribs are conically shaped in the radial direction.
Claim 9
Dependent Claim 41 words
Method of operating an axial flow turbine as claimed in claim 1, wherein the guide vanes are adjusted as a function of operating parameters in such a way that the shaft power assumes the maximum possible value at each operating condition.
Claim 10
Dependent Claim 49 words
Method of operating an axial flow turbine as claimed in claim 1, wherein the guide vanes are adjusted as a function of operating parameters in such a way that the pressure between the outlet rotor blades and the guide vanes assumes the lowest possible value at each operating condition.

References Cited (Backward Citations)

US2682363A Cited
US2674845A Cited
US2815770A Cited
US3447741A Cited
US3652184A Cited
US4116584A Cited
US4398865A Cited
GB2047820A Cited
US4802821A Cited
EP0265633B1 Cited
US4950129A Cited
US4995786A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1995-04-07 1995-10-07 1996-04-07 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1999-04-07 1999-10-07 2000-04-07 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2003-04-07 2003-10-07 2004-04-07 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag