Seal with a shim base and a honeycomb structure having a number of cavities are formed in a gas turbine engine
A technology of gas turbines and seals, which is applied in the directions of engine seals, engine components, gas turbine devices, etc., and can solve problems such as extrusion and deformation
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[0033] Described below are examples of seals (and individual components of the seals) that may be used to form a seal between components in a gas turbine engine. Methods of making and using the seal are also disclosed. The seal may include a gasket base and a honeycomb structure having a plurality of cavities therein formed as a single unitary structure with the gasket base. For example, a gasket base and a honeycomb structure with adjacent cavities can be formed as a single monolithic structure using additive manufacturing. Exemplary additive manufacturing processes may include 3D printing, among others. Direct metal laser melting (DMLM) is one exemplary manufacturing technique that may be used to manufacture the seal. Powder fusion welding (sometimes referred to as laser metal deposition) is another exemplary fabrication technique that may be used to form the cavity. Binder jetting is another exemplary fabrication technique that may be used to form the cavity. The seal m...
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