High temperature - low temperature rotor for turbines

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

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

26/150, 170/84

F01D 5/28 (2006.01) B23K 9/028 (2006.01) B23K 9/23 (2006.01) B23K 33/00 (2006.01) B23P 15/04 (2006.01) F01D 5/06 (2006.01)

Patent

CA 2030989

Abstract A turbine rotor is formed from two rotor segments that are composed of different low allay steels, one a high temperature alloy and the other a low temperature alloy. The rotor segments have cavities in confronting faces that form an annular flange at the outer surface, with the segments welded together across the flange. A clad layer is first welded an one of the flanges and a filler material welds the clad layer to the other flange to form a composite turbine rotor.

LandOfFree

Say what you really think

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

Rating

High temperature - low temperature rotor for turbines does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with High temperature - low temperature rotor for turbines, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and High temperature - low temperature rotor for turbines will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFCA-PAI-O-1347773

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