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

Donald Lee Gardner

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

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Country: United States Of America

Aircraft gas turbine engine blade tip clearance control

F - Mech Eng,Light,Heat,Weapons – 01 – D
Patent

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Gas turbine engine case counterflow thermal control

F - Mech Eng,Light,Heat,Weapons – 02 – C
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Integrated nacelle assembly

F - Mech Eng,Light,Heat,Weapons – 02 – C
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Profile ID: LFCA-PAI-P-1428853

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