Bayoneted anti-rotation turbine seals
An assembly for connecting a coverplate and a rotor includes a first rotor for use in a rotating engine; a first cover mounted to the first rotor, wherein the rotor and the cover create a space there between, the space for having cooling air therein; and a lock assembly for preventing the cover from rotating circumferentially or moving axially away from the rotor if mounted to the to the rotor wherein the cover is sealed against the rotor.
1. An assembly for connecting a cover to a rotor, said assembly comprising:
a first rotor for use in a rotating engine;
a cover mounted to said first rotor;
a second rotor for use in the rotating engine; and
a lock preventing said cover from rotating circumferentially and moving axially away from said first rotor when mounted to said first rotor, wherein said lock performs another function other than preventing said cover from rotating circumferentially and moving axially away from said first rotor, wherein said lock comprises:
a first tab mounted to said first rotor;
a second tab mounted to said cover, wherein said second tab is axially aligned with said first tab; and
a tooth preventing said first tab and said second tab from being unaligned with each other, said tooth projecting from said second rotor.
2. The assembly of claim 1 wherein said first tab is axially aft said second tab.
3. The assembly of claim 1 wherein said second tab is axially aft said first tab.
4. The assembly of claim 1 wherein said cover has a reinforced area adjacent said second tab, said reinforced area for minimizing torque effects on said cover.
5. The assembly of claim 1 wherein said cover is urged against said first rotor when said first tab is disposed behind said second tab.
6. The assembly of claim 1 wherein said cover has a gap between adjacent teeth thereof, said gap angling axially forward and radially inwardly from an aft surface of said cover.
7. The assembly of claim 1 wherein the first rotor holds a plurality of first rotor blades and wherein the second rotor holds a plurality of second rotor blades.
8. An assembly for connecting a cover and a rotor, said assembly comprising:
a rotor for use in a rotating gas turbine engine;
a cover mounted to said rotor, wherein said rotor and said cover create a space there-between, said space for having cooling air therein; and
a lock assembly for preventing said cover from rotating circumferentially and moving axially away from said rotor when mounted to said to said rotor, wherein said cover is sealed against said rotor, and wherein said lock assembly comprises:
a first tab mounted to said rotor;
a second tab mounted to said cover, wherein said second tab is axially aligned with said first tab; and
a tooth preventing said first tab and said second tab from being unaligned with each other, wherein said tooth is attached to a sleeve.
9. The assembly of claim 8 wherein the cover is urged against said rotor when said first tab is disposed behind said second tab.
10. The assembly of claim 8 wherein said sleeve includes a plurality of sprockets extending axially forward from an end of said sleeve, and wherein said tooth is provided by one of said sprockets.
11. A method of assembling a cover and a rotor comprising the steps of:
providing a first rotor for use in a rotating gas turbine engine, said first rotor having a plurality of first tabs mounted thereto, said first tabs having a first gap disposed between each adjacent first tab;
providing a cover having a plurality of second tabs mounted thereto, said second tabs having a second gap disposed between each adjacent second tab;
maneuvering one of (1) said first tabs through said second gaps and (2) said second tabs through said first gaps;
rotating said cover to align said first tabs and said second tabs axially; and
filling at least one of said first gap and said second gap with one of (1) a tooth projecting from a sleeve and (2) a tooth projecting from a second rotor.
12. The method of claim 11 further comprising:
filling at least one of said first gap and said second gap such that said first tabs may not rotate circumferentially relative to said second tabs.
13. The method of claim 11 further comprising:
filling at least one of said first gap and said second gap such that said first tabs may not rotate circumferentially relative to said second tabs nor may said cover move axially away from said rotor.
14. The method of claim 11 wherein said sleeve includes a plurality of sprockets extending axially forward from an end of said sleeve, and wherein said tooth is provided by one of said sprockets.