Composite filled gas turbine engine blade with gas film damper

Details Composite filled gas turbine engine blade with gas film damper Composite filled gas turbine engine blade with gas film damper

2007-10-09

2007-10-09

Look, Edward K. (Department: 3745)

Fluid reaction surfaces (i.e., impellers)

Specific blade structure

Laminated, embedded member or encased material

C416S500000

Reexamination Certificate

active

11131570

ABSTRACT:
A gas turbine engine blade comprises a housing, a composite core located within the housing, and a gas damper located within the housing for damping vibration of the blade.

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