Hollow turbine blade tip closure

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

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

170/71

F01D 5/18 (2006.01)

Patent

CA 1073818

HOLLOW TURBINE BLADE TIP CLOSURE ABSTRACT OF THE INVENTION An arrangement for closing selective areas of the tip portion of a hollow turbine blade having internal serpen- tine coolant passages is provided by radially extended wall portions at the tip of the blade along at least two sides of the outer ends of each two adjacent internal passages to be closed at the tip, retaining grooves provided in the facing surfaces of the extended wall portions, cover means overlie the outer ends of the selected adjacent passages and have opposite lateral edges received in the retaining grooves, and bond means secure the cover means along the lateral edges to the wall portions. The cover plate means preferably takes the form of two or more separable plates which can be inde- pendently inserted into the retaining grooves from an area on the tip portion of the blade which does not have the radially extended walls with retaining grooves therein.

282430

LandOfFree

Say what you really think

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

Rating

Hollow turbine blade tip closure does not yet have a rating. At this time, there are no reviews or comments for this patent.

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

Rate now

     

Profile ID: LFCA-PAI-O-713679

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