7 Patents
- US120719022024Method and System for Determining Aircraft Engine Inlet Total Pressure
PRATT & WHITNEY CANADA Corp.
0 cites - US120250602024Method and System for Operating an Engine to Prevent High Power Engine Surges
PRATT & WHITNEY CANADA Corp.
0 cites - 0 cites
- US118595612024Method and System for Determining Aircraft Engine Inlet Total Pressure
PRATT & WHITNEY CANADA Corp.
0 cites - US117396992023Method of Controlling the Geometrical Configuration of a Variable Geometry Element in a Gas Turbine Engine Compressor Stage
PRATT & WHITNEY CANADA Corp.
0 cites - 0 cites
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