Interstage seal arrangement for airfoil stages of turbine engine

Power plants – Reaction motor – Interrelated reaction motors

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

2988921, 4151744, 60268, F02K 302

Patent

active

051972816

ABSTRACT:
A gas turbine engine has outer and inner counterrotatable annular turbine rotors and pluralities of turbine blades disposed in alternating rows and mounted on and extending between the respective rotors. An interstage seal arrangement for the engine is composed of a sequence of alternating inner and outer seals. Each outer seal is disposed between an interior side of the outer rotor and outer ends of the blades in one plurality thereof being spaced radially inward at their outer ends from the outer rotor and being mounted at their inner ends to the exterior side of the inner rotor. Each inner seal is disposed between the exterior side of the inner rotor and inner ends of the blades in another plurality thereof being spaced radially outward at their inner ends from the inner rotor and being mounted at their outer ends to the interior side of the outer rotor. Each inner seal is composed of an annular honeycomb component attached to the blade inner ends and a plurality of annular seal elements or teeth mounted on the exterior side of the inner rotor and projecting radially outwardly therefrom for sealably interfacing with the honeycomb component concurrently as the outer and inner rotors counterrotate relative to one another.

REFERENCES:
patent: 2907595 (1959-10-01), Benson
patent: 2963307 (1960-12-01), Bobo
patent: 3262635 (1966-07-01), Simuland
patent: 3501089 (1970-03-01), Alford
patent: 3529905 (1970-09-01), Meginnis
patent: 3537713 (1970-11-01), Matthews
patent: 3603599 (1971-09-01), Laird
patent: 3836156 (1974-09-01), Dunthorne
patent: 3846899 (1974-11-01), Gross
patent: 4543039 (1985-09-01), Ruis
patent: 4623298 (1986-11-01), Hallinger et al.
patent: 4767267 (1988-08-01), Salt
patent: 4867639 (1989-09-01), Strangman
patent: 4979755 (1990-12-01), Lebreton
patent: 5010729 (1991-04-01), Adamson

LandOfFree

Say what you really think

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

Rating

Interstage seal arrangement for airfoil stages of turbine engine does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Interstage seal arrangement for airfoil stages of turbine engine, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Interstage seal arrangement for airfoil stages of turbine engine will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-1273561

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