2 Patents
- 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