4 Patents
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- US120250262024Geometric Approach to Stress Reduced Intra-flow Path Shrouds for Tuning Modal Responses in Ram Air Turbine Rotors
Honeywell International Inc.
0 cites - US117677602023Geometric Approach to Stress Reduced Intra-flow Path Shrouds for Tuning Modal Responses in Ram Air Turbine Rotors
Honeywell International Inc.
0 cites - 0 cites