Radially removable turbine vanes

Details Radially removable turbine vanes Radially removable turbine vanes

F - Mech Eng,Light,Heat,Weapons

01

D

170/66

F01D 9/00 (2006.01) F01D 9/04 (2006.01)

Patent

CA 1071107

C-2756 D-326 RADIALLY REMOVABLE TURBINE VANES Abstract of the Disclosure A gas turbine engine has a turbine vane case, an outer combustion case and inner vane case along with an air seal located in circumferential surrounding relationship to a circumferential row of stator vanes defining a turbine nozzle assembly upstream of a high pressure turbine stage. Individual stator vanes can be replaced without removing the high pressure turbine stage by configuring an index vane to be removably secured to an inner support band by means of a spring loaded pin and configuring each of the remaining vanes in the vane row to have a side slotted base secured to the inner band and removable therefrom by rotation of each of the individual vanes in a direction opposite to the tangential gas load thereon.

283729

Affiliated with

Also associated with

Rating

Radially removable turbine vanes does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Radially removable turbine vanes, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Radially removable turbine vanes will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-887721