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.