Combustors with quench inserts
AssigneeHoneywell International Inc.
InventorsNagaraja S. Rudrapatna, Philip Smalley, Lowell Frye, William Landram
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AssigneeHoneywell International Inc.
InventorsNagaraja S. Rudrapatna, Philip Smalley, Lowell Frye, William Landram
Estimating the term…
A combustor for a turbine engine is provided. The combustor includes a first liner and a second liner forming a combustion chamber with the first liner, the combustion chamber configured to receive an air-fuel mixture for combustion therein. The first liner defining an air admission hole for directing a first jet of pressurized air into the combustion chamber, and the air admission hole may have a non-circular shape. The combustor further includes an insert positioned within the air admission hole to guide the first jet through the air admission hole and into the combustion chamber.
A combustor for a turbine engine, comprising:
A method for installing an insert in an air admission hole of a combustor liner, the insert including a body portion, a shoulder, and an inlet portion and the combustor liner having a liner wall with a first side and a second side, the method comprising the steps of:
Dependencies are inferred from the claim text.