Resources Contact Us Home
Gardner; Donald Lee
West Chester, OH
No. of 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

  Recently Added Patents
Optimized delivery of web application code
Organic elelectroluminescent display
Apparatus and method for storing event information for an HVAC system
Process for manufacturing a self-sealing composition
Pear-shaped convertible reading glasses
Manipulation of an alternative respiratory pathway in photo-autotrophs
Low temperature pressure chamber unit, magnetic resonance device with a low temperature pressure chamber unit, and an attachment method to attach at least one add-on unit to an external housin
  Randomly Featured Patents
Exhaust silencer device for internal combustion engine
Seating product with sinuous spring assemblies
Ballpoint pen
Method and system for vehicular guidance using a crop image
Phase changeable memory devices and methods of forming the same in which an upper electrode includes a tip that extends toward a lower electrode
Method and apparatus for distributed signaling for uplink rate control
Local area network cable test instrument
Blow out preventer handling system
Method for manufacturing opaque rib structures for display panels
Read head preamplifier with thermal asperity transient control