Integral inner and outer shrouds and vanes

Rotary kinetic fluid motors or pumps – Bearing – seal – or liner between runner portion and static part – Between axial flow runner and vane or vane diaphragm structure

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

415200, 4152101, F01D 904

Patent

active

054824338

ABSTRACT:
The inner shroud of the vane of a vane assembly for the compressor section of a gas turbine engine is fabricate from a composite material preferably imide resin reinforced with carbon fibers and is formed into an open ended box-like member segment supporting no less than two vanes or airfoils. The segments are interlocked by a necked down edge adapted to slip into the open end of the adjacent inner shroud of the stator vane that serve to seal the gas path and provide damping. Rub strips are integrally formed on the bottom surface of the inner shroud.

REFERENCES:
patent: 2868439 (1959-01-01), Hampshire et al.
patent: 2917276 (1959-12-01), Klompas et al.
patent: 3069135 (1962-12-01), Welsh
patent: 3079128 (1963-02-01), Burge
patent: 3118593 (1964-01-01), Robinson et al.
patent: 3275294 (1966-09-01), Allen et al.
patent: 3393862 (1968-07-01), Harrison
patent: 3588267 (1971-06-01), Wilkinson et al.
patent: 4655682 (1987-04-01), Kunz et al.

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

Integral inner and outer shrouds and 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 Integral inner and outer shrouds and vanes, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Integral inner and outer shrouds and vanes will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-1299206

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