Gas turbine clearance control gas flow device

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

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

F01D 11/08 (2006.01) F01D 11/24 (2006.01) F01D 25/14 (2006.01)

Patent

CA 2209297

The primary component is a gas mixer (8), placed in the gas flow before the part (3) to be heated or cooled, which consists in a succession of chambers (12, 14, 15) fitted with communicating or outlet orifices (16, 17, 18) in increasing numbers to equalize the gas flow rate and temperature. Application to gas turbines.

L'élément primordial est un mélangeur (8) des gaz, qui est disposé sur l'écoulement des gaz avant la pièce (3) à échauffer ou refroidir, et qui consiste en une succession de chambres (12, 14, 15) munies d'orifices de communication ou de sortie (16, 17, 18) toujours plus nombreux pour uniformiser l'écoulement des gaz en débit et température. Application aux turbomachines.

LandOfFree

Say what you really think

Search LandOfFree.com for Canadian inventors and patents. Rate them and share your experience with other people.

Rating

Gas turbine clearance control gas flow device does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Gas turbine clearance control gas flow device, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Gas turbine clearance control gas flow device will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFCA-PAI-O-1566732

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.