Turbine nozzles and methods of manufacturing the same
AssigneeHoneywell International Inc.
InventorsBradley Reed Tucker, Mark C. Morris, Jason Smoke, Daniel Ryan
Life of this patent
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AssigneeHoneywell International Inc.
InventorsBradley Reed Tucker, Mark C. Morris, Jason Smoke, Daniel Ryan
Estimating the term…
Turbine nozzles and methods of manufacturing the turbine nozzles are provided. In an embodiment, by way of example only, a turbine nozzle includes a first ring, a vane, and a first joint. The first ring comprises a single unitary component and having a first opening and including a first metal alloy. The vane includes a first end disposed in the first opening and includes a second metal alloy. The first joint is formed in the first opening between the first ring and the vane and includes a first braze layer and an oxide layer. The first braze layer is disposed adjacent to the oxide layer, and the first braze layer and the oxide layer are disposed between the first ring and the vane.
A turbine nozzle, comprising:
A method of manufacturing a turbine nozzle, the method comprising the steps of:
A method of manufacturing a turbine nozzle, the method comprising the steps of:
Dependencies are inferred from the claim text.