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Inventor: Gardner; Donald Lee
Address: West Chester, OH
No. of patents: 1
Patents:
| Patent Number |
Title Of Patent |
Date Issued |
| 8126628 |
Aircraft gas turbine engine blade tip clearance control |
February 28, 2012 |
| A method and system adjusts blade tip clearance between rotating aircraft gas turbine engine blade tips and a surrounding shroud in anticipation of and before an engine command that changes an engine rotational speed. The method may include determining when to begin adjusting the tip cle |
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