Compressor disk assembly

Fluid reaction surfaces (i.e. – impellers) – Rotor having flow confining or deflecting web – shroud or... – Axially extending shroud ring or casing

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

416193A, 416500, F01D 516

Patent

active

051082616

ABSTRACT:
A lightweight, integrally bladed rotor has airfoils (18) and a full hoop blade platform (26), a support ring (28) is inside and spaced from the platform, with radial webs (30) extending from the support ring to the platform. Each web is a radial extension (32) of an airfoil. A radially extending shear plate (36) is secured to the platform and the ring.

REFERENCES:
patent: 3871791 (1975-03-01), Guy et al.
patent: 4019832 (1977-04-01), Salemme et al.
patent: 4062638 (1977-12-01), Hall, Jr.
patent: 4355957 (1982-10-01), Sifford et al.
patent: 4505642 (1985-03-01), Hill
patent: 4568247 (1986-02-01), Jones et al.
patent: 4595340 (1986-06-01), Klassen et al.
patent: 4784572 (1988-11-01), Novotny et al.
patent: 4784573 (1988-11-01), Ress, Jr.
patent: 4872812 (1989-10-01), Hendley et al.
patent: 4917574 (1990-04-01), Dodd 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

Compressor disk assembly does not yet have a rating. At this time, there are no reviews or comments for this patent.

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

Rate now

     

Profile ID: LFUS-PAI-O-1243611

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