Containment system for gas turbine engine
AssigneeHoneywell International Inc.
InventorsYathiraj Kasal, Reha Gomuc, Abhay Naik, Donald G. Godfrey
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AssigneeHoneywell International Inc.
InventorsYathiraj Kasal, Reha Gomuc, Abhay Naik, Donald G. Godfrey
Estimating the term…
A containment system for a gas turbine engine includes an outer containment ring having a first projection that extends radially inward and an inner containment ring having at least a second projection that extends radially outward toward the outer containment ring. The second projection is offset and spaced apart from the first projection to define a chamber in a first state. The containment system includes a lattice defined within the chamber that spans the chamber, and the lattice is integrally formed with each of the outer containment ring and the inner containment ring. A density of the lattice varies in at least one of an axial direction and a radial direction. The second projection is configured to interlock with the first projection in a second state.
A containment system for a gas turbine engine, comprising:
A containment system for a gas turbine engine, comprising:
A gas turbine engine, comprising:
Dependencies are inferred from the claim text.