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US5277549A Expired / Lapsed US ⏱️ 0.0 years remaining

Controlled reaction L-2R steam turbine blade

Assignee: Siemens Energy Inc
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Filing: 1992-03-16
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Granted: 1994-01-11
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Expires: 2012-03-16
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Abstract

Abstract A high performance steam turbine blade is provided in which the geometry of the blade airfoil is configured to minimize energy loss through the row of blades and control the radial distribution of the degree of reaction. The velocity of the steam over the blade surface is minimized to reduce friction losses, rapid deceleration of the steam velocity as it expands toward the trailing edge is avoided to prevent boundary layer separation and the reaction distribution is adjusted so that a relatively high reaction occurs at the base of the airfoil, thereby reducing secondary flow, and a relatively low reaction occurs at tip of the airfoil, thereby minimizing tip leakage. Specifically, the radial reaction distribution is such that in the hub region at least 20% of the stage pressure drop occurs in the blade row and in the tip region less than 50% of the stage pressure drop occurs in the blade row.

Inventors

  • 👤 Shun Chen
  • 👤 Jurek Ferleger

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-08 06:45
CPC Classifications
F; F01; F01D; F01D5/00; F01D5/12; F01D5/14; F01D5/141

Claims Analysis

Total Claims: 10
Claim 1
Independent Claim 330 words
A steam turbine comprising: a) a stationary cylinder for containing a steam flow, and a rotor enclosed by said cylinder; b) a stage disposed within said cylinder and having means for at least partially expanding said steam flow, whereby said steam flow undergoes a stage pressure drop as it expands through said stage, said stage having a row of vanes and a row of blades, said row of blades having a tip region and a hub region; c) said row of vanes having means for causing said steam to undergo a first portion of said stage pressure drop as said steam flows through said row of vanes; and d) said row of blades having (i) means for causing said steam to undergo a second portion of said stage pressure drop as said steam flows through said row of blades, and (ii) means for controlling the radial distribution of said second portion of said stage pressure drop so that said second portion is greater than 20% of said stage pressure drop in said hub region and less than 50% of said stage pressure drop in said tip region, e) said pressure drop radial distribution control means comprising(i) each of said blades having an airfoil portion having a base section, a mid-height section, a 25% height section between said base and mid-height sections, a 75% height section between said mid-height section and said tip region, and each of said airfoil portions being defined by the following parameters having approximately the values indicated below, all angles being expressed in degrees: ______________________________________ 75%- Parameter 25% Height Mid-Height Height ______________________________________ Pitch/Chord Ratio 0.6 0.7 0.8 Pitch/Width Ratio 0.7 0.9 1.3 Stagger Angle 25 41 54 Max Thickness/Chord Ratio 0.3 0.2 0.1 Metal Turning Angle 106 84 62 Exit Opening (mm) 21 21 22 Exit Opening Angle 33 31 30 Inlet Metal Angle 55 78 102 Inlet Included Angle 42 51 40 Exit Metal Angle 20 19 17 Suction Surface 16 15 14 Turning Angle ______________________________________
Claim 2
Dependent Claim 330 words
A steam turbine comprising: a) a stationary cylinder for containing a steam flow, and a rotor enclosed by said cylinder; b) a stage disposed within said cylinder and having means for at least partially expanding said steam flow, whereby said steam flow undergoes a stage pressure drop as it expands through said stage, said stage having a row of vanes and a row of blades, said row of blades having a tip region and a hub region; c) said row of vanes having means for causing said steam to undergo a first portion of said stage pressure drop as said steam flows through said row of vanes; and d) said row of blades having (i) means for causing said steam to undergo a second portion of said stage pressure drop as said steam flows through said row of blades, and (ii) means for controlling the radial distribution of said second portion of said stage pressure drop so that said second portion is greater than 20% of said stage pressure drop in said hub region and less than 50% of said stage pressure drop in said tip region, e) said pressure drop radial distribution control means comprising(i) each of said blades having an airfoil portion having a base section, a mid-height section, a 25% height section between said base and mid-height sections, a 75% height section between said mid-height section and said tip region, and each of said airfoil portions being defined by the following parameters having approximately the values indicated below, all angles being expressed in degrees: ______________________________________ 75%- Parameter 25% Height Mid-Height Height ______________________________________ Pitch/Chord Ratio 0.6 0.7 0.8 Pitch/Width Ratio 0.7 0.9 1.3 Stagger Angle 25 41 54 Max Thickness/Chord Ratio 0.3 0.2 0.1 Metal Turning Angle 106 84 62 Exit Opening (mm) 21 21 22 Exit Opening Angle 33 31 30 Inlet Metal Angle 55 78 102 Inlet Included Angle 42 51 40 Exit Metal Angle 20 19 17 Suction Surface 16 15 14 Turning Angle ______________________________________
Claim 3
Dependent Claim 91 words
The steam turbine according to claim 1, wherein each of said airfoil portions is further defined by the following parameters having approximately the values indicated below, all angles being expressed in degrees: ______________________________________ Parameter Base Tip ______________________________________ Pitch/Chord Ratio 0.5 0.8 Pitch/Width Ratio 0.5 2.0 Stagger Angle 17 67 Max Thickness/Chord Ratio 0.3 0.1 Metal Turning Angle 116 36 Exit Opening (mm) 21 19 Exit Opening Angle 33 23 Inlet Metal Angle 43 129 Inlet Included Angle 30 33 Exit Metal Angle 21 15 Suction Surface 16 9 Turning Angle ______________________________________
Claim 4
Dependent Claim 140 words
In a steam turbine, a row of blades comprising an airfoil for each blade, each of said airfoils having a base section, a mid-height section, a tip section, a 25% height section between said base and mid-height sections, a 75% height section between said mid-height and tip sections, and defined by the following parameters having approximately the values indicated below, all angles being expressed in degrees: ______________________________________ Mid- Parameter 25% Height Height 75%- Height ______________________________________ Pitch/Chord Ratio 0.6 0.7 0.8 Pitch/Width Ratio 0.7 0.9 1.3 Stagger Angle 25 41 54 Max Thickness/Chord Ratio 0.3 0.2 0.1 Metal Turning Angle 106 84 62 Exit Opening (mm) 21 21 22 Exit Opening Angle 33 31 30 Inlet Metal Angle 55 78 102 Inlet Included Angle 42 51 40 Exit Metal Angle 20 19 17 Suction Surface 16 15 14 Turning Angle ______________________________________
Claim 5
Dependent Claim 140 words
In a steam turbine, a row of blades comprising an airfoil for each blade, each of said airfoils having a base section, a mid-height section, a tip section, a 25% height section between said base and mid-height sections, a 75% height section between said mid-height and tip sections, and defined by the following parameters having approximately the values indicated below, all angles being expressed in degrees: ______________________________________ Mid- Parameter 25% Height Height 75%- Height ______________________________________ Pitch/Chord Ratio 0.6 0.7 0.8 Pitch/Width Ratio 0.7 0.9 1.3 Stagger Angle 25 41 54 Max Thickness/Chord Ratio 0.3 0.2 0.1 Metal Turning Angle 106 84 62 Exit Opening (mm) 21 21 22 Exit Opening Angle 33 31 30 Inlet Metal Angle 55 78 102 Inlet Included Angle 42 51 40 Exit Metal Angle 20 19 17 Suction Surface 16 15 14 Turning Angle ______________________________________
Claim 6
Dependent Claim 86 words
The row of blade airfoils according to claim 3, further defined by the following parameters having approximately the values indicated below, all angles being expressed in degrees: ______________________________________ Parameter Base Tip ______________________________________ Pitch/Chord Ratio 0.5 0.8 Pitch/Width Ratio 0.5 2.0 Stagger Angle 17 67 Max Thickness/Chord Ratio 0.3 0.1 Metal Turning Angle 116 36 Exit Opening (mm) 21 19 Exit Opening Angle 33 23 Inlet Metal Angle 43 129 Inlet Included Angle 30 33 Exit Metal Angle 21 15 Suction Surface 16 9 Turning Angle ______________________________________
Claim 7
Dependent Claim 33 words
The row of blade airfoils according to claim 4, further defined by a gauging parameter, said gauging parameter varying from approximately 0.4 at said base portion to approximately 0.3 at said tip portion.
Claim 8
Dependent Claim 22 words
The row of blade airfoils according to claim 4, wherein each of said airfoils has a shroud formed on said tip portion.
Claim 9
Dependent Claim 249 words
In a steam turbine having a stage having a row of stationary vanes and a row of rotating blades, (iii) a tip region, and (iv) a hub region, a method of at least partially expanding a flow of steam across said stage, whereby said steam undergoes a stage pressure drop, comprising the steps of: a) causing said steam flow to undergo a first portion of said stage pressure drop by flowing through said row of vanes; and b) causing said steam flow to undergo a second portion of said stage pressure drop by the step of flowing said steam through a row of blade airfoils having a base portion and a mid-height portion, and defined by the following parameters having approximately the values indicated below, all angles being expressed in degrees: ______________________________________ Parameter Base Mid Tip ______________________________________ Pitch/Chord Ratio 0.5 0.7 0.8 Pitch/Width Ratio 0.6 0.9 2.0 Stagger Angle 17 41 67 Max Thickness/Chord Ratio 0.3 0.2 0.1 Metal Turning Angle 116 84 36 Exit Opening (mm) 21 21 19 Exit Opening Angle 33 31 23 Inlet Metal Angle 43 78 129 Inlet Included Angle 30 51 33 Exit Metal Angle 21 19 15 Suction Surface 16 15 9 Turning Angle ______________________________________ so as to control the radial distribution of said second portion of said stage pressure drop so that said second portion is greater than 20% of said stage pressure drop in said hub portion and less than 50% of said stage pressure drop in said tip region.
Claim 10
Dependent Claim 249 words
In a steam turbine having a stage having a row of stationary vanes and a row of rotating blades, (iii) a tip region, and (iv) a hub region, a method of at least partially expanding a flow of steam across said stage, whereby said steam undergoes a stage pressure drop, comprising the steps of: a) causing said steam flow to undergo a first portion of said stage pressure drop by flowing through said row of vanes; and b) causing said steam flow to undergo a second portion of said stage pressure drop by the step of flowing said steam through a row of blade airfoils having a base portion and a mid-height portion, and defined by the following parameters having approximately the values indicated below, all angles being expressed in degrees: ______________________________________ Parameter Base Mid Tip ______________________________________ Pitch/Chord Ratio 0.5 0.7 0.8 Pitch/Width Ratio 0.6 0.9 2.0 Stagger Angle 17 41 67 Max Thickness/Chord Ratio 0.3 0.2 0.1 Metal Turning Angle 116 84 36 Exit Opening (mm) 21 21 19 Exit Opening Angle 33 31 23 Inlet Metal Angle 43 78 129 Inlet Included Angle 30 51 33 Exit Metal Angle 21 19 15 Suction Surface 16 15 9 Turning Angle ______________________________________ so as to control the radial distribution of said second portion of said stage pressure drop so that said second portion is greater than 20% of said stage pressure drop in said hub portion and less than 50% of said stage pressure drop in said tip region.

References Cited (Backward Citations)

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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) 1997-01-10 1997-07-12 1998-01-11 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 2001-01-10 2001-07-12 2002-01-11 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2005-01-10 2005-07-12 2006-01-11 $7700.00 Window Closed / Lapsed

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