NON UNIFORM VANE SPACING
First Claim
1. A gas turbine engine ring or circular row of non-uniformally spaced vanes comprising:
- first group and second groups including all the vanes in the ring or circular row,only one first group and only one second group of adjacent vanes,unequal first and second spacing between the adjacent vanes in the first and second groups respectively, andthe first spacing greater than the second spacing.
1 Assignment
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Accused Products
Abstract
A circular row of non-uniformally spaced vanes includes only one first group and only one second group of adjacent vanes, unequal first and second spacing between adjacent vanes in the first and second groups, and first spacing greater than second spacing. An embodiment with second group including only three adjacent vanes. Second spacing may be about 25%-35% smaller than a nominal uniform spacing used as a design parameter for designing spacing of the non-uniformly spaced stator vanes. Circular row may be sectored. A gas turbine engine section may include one or more rings or circular rows of fixed and/or variable non-uniformally spaced vanes. Method for designing non-uniform vane spacing for circular row includes determining nominal uniform spacing and forming first spacing and second spacing from nominal uniform spacing of vanes.
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Citations
20 Claims
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1. A gas turbine engine ring or circular row of non-uniformally spaced vanes comprising:
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first group and second groups including all the vanes in the ring or circular row, only one first group and only one second group of adjacent vanes, unequal first and second spacing between the adjacent vanes in the first and second groups respectively, and the first spacing greater than the second spacing. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10)
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11. A gas turbine engine assembly comprising:
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a gas turbine engine section including one or more rings or circular rows of fixed and/or variable non-uniformally spaced vanes, first group and second groups including all the vanes in each of the one or more rings or circular rows, only one first group and only one second group of adjacent vanes in each of the one or more rings or circular rows, unequal first and second spacing between the adjacent vanes in the first and second groups respectively, and the first spacing greater than the second spacing. - View Dependent Claims (12, 13, 14, 15, 16, 17)
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18. A method for designing non-uniform vane spacing for a ring or circular row of non-uniformally spaced gas turbine engine vanes, the method comprising:
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determining a 360 degree nominal uniform spacing S pattern, spreading apart one interim pair of the nominal uniformally spaced apart vanes and moving the remaining vanes closer together wherein the remaining vanes are all evenly spaced at a first spacing creating one big gap or an interim large spacing between the interim pair, and inserting an additional vane in the one big gap or interim large spacing forming two adjacent equal narrow gaps or spaces having second spacings smaller than the first spacing. - View Dependent Claims (19, 20)
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Specification