Low lump mass combustor wall with quench aperture(s)
First Claim
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1. An assembly for a turbine engine, comprising:
- a combustor wall including a first layer vertically connected with a second layer;
a first portion of the first layer overlapping and vertically spaced from the second layer by a cavity; and
a second portion of the first layer vertically inline with an adjacent portion of the second layer, and at least partially forming a quench aperture vertically through the combustor wall;
wherein a vertical thickness of the first portion is equal to a vertical thickness of the second portion; and
wherein the combustor wall extends circumferentially about and axially along a centerline, and the first portion is located axially forward of the second portion.
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Abstract
An assembly is provided for a turbine engine. This turbine engine assembly includes a combustor wall including a first layer vertically connected with a second layer. A first portion of the first layer overlaps and is vertically spaced from the second layer by a cavity. A second portion of the first layer is substantially vertically inline with an adjacent portion of the second layer. The second portion of the first layer at least partially forms a quench aperture vertically through the combustor wall.
27 Citations
13 Claims
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1. An assembly for a turbine engine, comprising:
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a combustor wall including a first layer vertically connected with a second layer; a first portion of the first layer overlapping and vertically spaced from the second layer by a cavity; and a second portion of the first layer vertically inline with an adjacent portion of the second layer, and at least partially forming a quench aperture vertically through the combustor wall; wherein a vertical thickness of the first portion is equal to a vertical thickness of the second portion; and wherein the combustor wall extends circumferentially about and axially along a centerline, and the first portion is located axially forward of the second portion. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11)
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12. An assembly for a turbine engine, comprising:
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a combustor wall including a first layer vertically connected with a second layer; a first portion of the first layer overlapping and vertically spaced from the second layer by a cavity; and a second portion of the first layer vertically inline with an adjacent portion of the second layer, and at least partially forming a quench aperture vertically through the combustor wall; wherein a vertical thickness of the first portion is equal to a vertical thickness of the second portion; and wherein the combustor wall extends circumferentially about and axially along a centerline, and the first portion is located axially aft of the second portion.
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13. An assembly for a turbine engine, comprising:
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a combustor wall including a first layer vertically connected with a second layer; a first portion of the first layer overlapping and vertically spaced from the second layer by a cavity; and a second portion of the first layer vertically inline with an adjacent portion of the second layer, and at least partially forming a quench aperture vertically through the combustor wall; wherein a vertical thickness of the first portion is equal to a vertical thickness of the second portion; and wherein a third portion of the first layer overlaps and is vertically spaced from the second layer by the cavity or another cavity, and the second portion is between the first portion and the third portion.
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Specification