High temperature turbine engine structure

Metal working – Method of mechanical manufacture – Impeller making

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

295251, B23P 1500

Patent

active

052790312

ABSTRACT:
A high temperature ceramic/metallic turbine engine includes a metallic housing which journals a rotor member of the turbine engine. A ceramic disk-like shroud portion of the engine is supported on the metallic housing portion and maintains a close running clearance with the rotor member. A ceramic spacer assembly maintains the close running clearance of the shroud portion and rotor member despite differential thermal movements between the shroud portion and metallic housing portion.

REFERENCES:
patent: B563412 (1976-02-01), Booher
patent: 808627 (1906-01-01), Booth
patent: 845121 (1907-02-01), Reniff
patent: 1370474 (1921-03-01), Newsom
patent: 1407548 (1922-02-01), Knouff
patent: 1750770 (1930-03-01), Austin
patent: 2429936 (1947-10-01), Kenney
patent: 2538396 (1951-01-01), Sutin
patent: 2590175 (1952-03-01), Hajdu
patent: 3031049 (1962-04-01), Somville
patent: 3112547 (1963-12-01), Poe
patent: 3208035 (1965-09-01), Horvath et al.
patent: 3316861 (1967-05-01), Dailey
patent: 3835615 (1974-09-01), King, Jr.
patent: 3857649 (1974-12-01), Schaller
patent: 4122605 (1978-10-01), Hirabayashi et al.
patent: 4312599 (1982-01-01), Davolia
patent: 4391434 (1983-07-01), LaBate
patent: 4540304 (1985-09-01), Pavelka et al.
patent: 4834569 (1989-05-01), Foote et al.
patent: 4861211 (1989-08-01), Dunsmore
patent: 4925364 (1990-05-01), Das
patent: 4943013 (1990-07-01), Kapala et al.
patent: 4975014 (1990-12-01), Rutin et al.
patent: 5011353 (1991-04-01), Boyd
Ceramic Design Methodology and the Agt101 Tech. Paper Mar. 1985 by Gary L. Boyd et al.
Automotive Gas Turbine Ceramic Component Testing Tech. Paper by Gary L. Boyd.
DOE/NASA/0167-82/4 "Advanced GAs Turbine (AGT) Powertrain System Development For Automotive Applications" p. 39.
DOE/NASA/0167-6 "Advanced Gas Turbine (AGT) Technology Development" p. 46.
DOE/NASA/0167-8 "Advanced Gas Turbine (AGT) Technology Development" p. 30.
DOE/NASA/0167-10 "Advanced Gas Turbine (AGT) Technology Development Project" pp. 15, 16, 25, 38, 100.
DOE/NASA/0167-9 "Advanced Gas Turbine (AGT) Technology Development" pp. 29, 60, 62.
DOE/NASA/0167-12 "Advanced Gas Turbine (AGT) Technology Development Project" pp. 207, 252, 253.

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

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

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

Rate now

     

Profile ID: LFUS-PAI-O-1129527

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