Composite seal for turbomachinery

Rotary kinetic fluid motors or pumps – Bearing – seal – or liner between runner portion and static part – Erodable or permanently deformable

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

415200, F01D 1108

Patent

active

041358511

ABSTRACT:
A gas path seal suitable for use with a turbine engine or compressor is provided. A shroud wearable or abradable by the abrasion of the rotor blades of the turbine or compressor shrouds the rotor blades. A compliant backing surrounds the shroud. The backing may be made of corrugated sheets or the like with adjacent layers having off-set corrugations, with axes of the folds parallel to the rotor axis. The sheets may be bonded together at points of contact by brazing, welding or the like. In another embodiment a compliant material is covered with a thin ductile layer. A mounting fixture surrounds the backing.

REFERENCES:
patent: 2477852 (1949-08-01), Bacon
patent: 2994124 (1961-08-01), Denny et al.
patent: 3423070 (1969-01-01), Corrigan
patent: 4063742 (1977-12-01), Watkins, Jr.

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

Composite seal for turbomachinery does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Composite seal for turbomachinery, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Composite seal for turbomachinery will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-2270957

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