US Patent Application No: 2001/0008,070

Number of patents in Portfolio can not be more than 2000

Air impingement cooling system


See full text


Loading Importance Indicators... loading....


See full text

Where gas turbine engine structure eg combustion equipment, is to be air impingement cooled, the surface which receives the air jets is so shaped as to produce boundary layer separation zones 34, 38 and 44 in the cooling air, as it spreads across the surface. Mixing of the boundary layer with the remainder of the air flow results, followed by the reestablishment of the boundary layer. The new boundary layer is cooler than the original layer and so provides more effective cooling.

Loading the Abstract Image... loading....

First Claim

See full text

all claims..

Related Publications

Loading Related Publications... loading....

Patent Owner(s)

Patent OwnerAddressTotal Patents

International Classification(s)

  • [Classification Symbol]
  • [Patents Count]


Inventor Name Address # of filed Patents Total Citations
Dailey, Geoffrey M Derby, GB 24 69
Son, Changmin Derby, GB 10 8

Patent Citation Ranking

Forward Cite Landscape

  • No Forward Cites to Display