Shielded combustor

Claim 2

A combustor having a combustion zone comprising: a shell including a capture slot, said slot extending in a substantially circumferential direction and having an opening facing in a radial direction; an arcuate liner having a lip, said lip being disposed in said slot for supporting said liner at one end in said shell, and a shield portion disposed between said shell and the combustion zone; and said lip being loosely disposed in said slot to permit movement of said lip in said slot for accommodating a radial component of differential thermal expansion between said shell and said liner.

Claim 3

A combustor according to claim 1 wherein said liner comprises an annular ring.

Claim 4

A combustor according to claim 1 wherein said liner comprises a plurality of liner segments disposed in circumferential alignment in said slot.

Claim 5

A combustor according to claim 1 wherein said shell and said liner comprise dissimilar materials, said liner material being suitable for withstanding higher temperatures than said shell material.

Claim 6

A combustor according to claim 4 wherein said liner material comprises ceramic.

Claim 7

A combustor according to claim 4 wherein said liner material comprises carbon-carbon.

Claim 8

A combustor according to claim 1 wherein said lip is disposed on an upstream end of said liner.

Claim 9

A combustor according to claim 1 wherein said shell comprises an outer shell and said opening faces radially inwardly; and said liner comprises an outer liner and said lip is inclined in a generally radially outward direction.

Claim 10

A combustor according to claim 1 wherein said shell comprises an inner shell and said opening faces radially outwardly; and said liner comprises an inner liner and said lip is inclined in a generally radially inward direction.

Claim 11

A combustor according to claim 1 further including a plurality of axially spaced capture slots disposed in said shell, and wherein said liner comprises a plurality of liner sections disposed in respective ones of said slots, each of said liner sections having a lip and shield portion.

Claim 12

A combustor according to claim 10 wherein a shield portion of a first liner section is spaced radially from and overlaps a lip of an adjacent second liner section for shielding said lip and said slot from combustion gases.

Claim 13

A combustor according to claim 11 wherein one of said first and second liner sections includes three bosses disposed to bear on the other thereof and effective for centering at least one of said first and second liner sections in said combustor.

Claim 14

A combustor according to claim 10 further including a plurality of cooling air apertures disposed in said shell and being effective for directing cooling air to impinge against an outer surface of said liner and to flow over an inner surface of an adjacent downstream one of said liners.

Claim 15

A combustor according to claim 13 wherein one of said liners includes a dilution aperture effective for receiving and directing a portion of said impingement air to dilute combustion gases in said combustor.

Claim 16

A combustor according to claim 1 wherein said slot is generally U-shaped and includes an apex.

Claim 17

A combustor according to claim 15 wherein said slot is defined by complementary ends of adjacent first and second shell sections fixedly attached to each other at said apex.

Claim 18

A combustor according to claim 16 wherein said slot includes a first radially directed wall integral with a downstream end of said first shell section, a second radially directed wall integral with an upstream end of said second shell section, a first bend at a radially outer end of said first radially directed wall, a second bend at a radially outer end of said second radially directed wall, said first and second bends being effective to place first and second mating surfaces in mutual abutment.

Claim 19

A combustor according to claim 17 further including a weld bead joining a portion of said first and second mating surfaces.

Claim 20

A combustor according to claim 18 wherein said portion is a radially outermost portion whereby said weld bead is removable to permit access to a liner supported in said slot.

Claim 21

A combustor according to claim 17 wherein said first radially directed wall has a first radial dimension effective to substantially align an inner surface of said first shell section with an inner surface of a liner supported in said slot, said second radially directed wall has a second radial dimension smaller than said first radial dimension for defining an air flow channel.

Claim 22

A combustor for a gas turbine engine comprising: a dome; an outer shell having at least first and second shell sections; a first radially directed capture slot at a junction of said dome and said first second shell section; a second radially directed capture slot at a junction of said first and second shell sections; a first liner section inside said shell; including a first radially directed lip on an upstream end thereof captured in said first radially directed capture slot and effective to retain said first liner section in said combustor spaced inward of said first shell section to form a first flow channel; at least a second liner section inside said shell; including a second radially directed lip on an upstream end thereof captured in said second radially directed capture slot and effective to retain said second liner section in said combustor spaced inward of said second shell section; and means for admitting a flow of air through said first shell section into said flow channel; said first and second lips being loosely disposed in said first and second slots, respectively, to permit movement of said lips in said slots for accommodating a radial component of differential thermal expansion between said shell and said first and second liner sections; and a downstream end of said first liner section being spaced radially inward from and overlapping an upstream end of said second liner section to permit sheet-type film cooling airflow from said flow channel along an inner surface of said second liner section, said overlapping and said airflow being effective to shield said second radially directed capture slot from temperature in a combustion zone of said combustor.

Claim 23

A combustor for a gas turbine engine comprising: a dome; an outer shell having at least first and second shell sections; a first radially directed capture slot at a junction of said dome and said first second shell section; a second radially directed capture slot at a junction of said first and second shell sections; a first liner section inside said shell; including a first radially directed lip on an upstream end thereof captured in said first radially directed capture slot and effective to retain said first liner section in said combustor spaced inward of said first shell section to form a first flow channel; at least a second liner section inside said shell; including a second radially directed lip on an upstream end thereof captured in said second radially directed capture slot and effective to retain said second liner section in said combustor spaced inward of said second shell section; and means for admitting a flow of air through said first shell section into said flow channel; said first and second lips being loosely disposed in said first and second slots, respectively, to permit movement of said lips in said slots for accommodating a radial component of differential thermal expansion between said shell and said first and second liner sections; and a downstream end of said first liner section being spaced radially inward from and overlapping an upstream end of said second liner section to permit sheet-type film cooling airflow from said flow channel along an inner surface of said second liner section, said overlapping and said airflow being effective to shield said second radially directed capture slot from temperature in a combustion zone of said combustor.

Claim 24

For a combustor including a shell having a capture slot for receiving and loosely supporting from one end a liner to permit movement of said liner in said slot for accommodating a radial component of differential thermal expansion between said shell and said liner, an arcuate liner comprising a lip and a shield portion, said lip being inclined substantially perpendicularly to said shield portion.

Claim 25

For a combustor including a shell having a capture slot for receiving and loosely supporting from one end a liner to permit movement of said liner in said slot for accommodating a radial component of differential thermal expansion between said shell and said liner, an arcuate liner comprising a lip and a shield portion, said lip being inclined substantially perpendicularly to said shield portion.

Claim 26

A liner according to claim 22 comprising a material dissimilar to that of the shell, said liner material being suitable for withstanding higher temperatures than the shell material.

Claim 27

A liner according to claim 23 wherein said liner material comprises ceramic.

Claim 28

A liner according to claim 23 wherein said liner material comprises carbon-carbon.

Claim 31

A combustor according to claim 1 wherein said capture slot and said lip both extend in a substantially radial only direction.

Claim 32

A combustor according to claim 21 wherein said first and second capture slots and said first and second lips extend in a substantially radial only direction.