Gas turbine engine casing

Rotary kinetic fluid motors or pumps – Working fluid passage or distributing means associated with... – Passage or casing attached removable liner or wear member

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

415 9, 415108, 415217, 415219R, 416 2, 602261, F04D 2940

Patent

active

044250800

ABSTRACT:
A containment ring for a gas turbine engine consists of a substantially rigid inner cylinder around the periphery of which is wound layers of fibrous material, a plurality of axially extending strips are located upon the outermost curved surface of the layers of fibrous material and are secured thereto by self-tapping screws.

REFERENCES:
patent: 2999667 (1961-09-01), Morley
patent: 3004700 (1961-10-01), Warren
patent: 3542152 (1970-11-01), Adamson
patent: 3936219 (1976-02-01), Holmes
patent: 3974313 (1976-08-01), James
patent: 4038118 (1977-07-01), James
patent: 4377370 (1983-03-01), Porcelli

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

Gas turbine engine casing does not yet have a rating. At this time, there are no reviews or comments for this patent.

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

Rate now

     

Profile ID: LFUS-PAI-O-451751

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