4. F - Mech Eng,Light,Heat,Weapons
  5. 02
  6. C

Aspi Rustom Wadia

F - Mech Eng,Light,Heat,Weapons – 02 – C

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Inventor

Country: United States Of America

Airfoil leading edge end wall vortex reducing plasma

F - Mech Eng,Light,Heat,Weapons – 02 – C
Patent

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Compressor and gas turbine engine with a plasma actuator

F - Mech Eng,Light,Heat,Weapons – 04 – D
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Compressor and gas turbine engine with a plasma actuator

F - Mech Eng,Light,Heat,Weapons – 04 – D
Patent

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Compressor blade tip clearance control system with a plasma...

F - Mech Eng,Light,Heat,Weapons – 01 – D
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Curved platform turbine blade

F - Mech Eng,Light,Heat,Weapons – 01 – D
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Profile ID: LFCA-PAI-P-1276726

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