Ceramic duct system for turbine engine

Details Ceramic duct system for turbine engine Ceramic duct system for turbine engine

1980-10-22

1983-02-15

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

Multiple fluid-operated motors

60 39512, F02C 310

Patent

active

043733263

ABSTRACT:
A gas turbine engine has a metal engine block which houses interconnected ceramic duct components defining the gas flow path between a combustor and turbine stages of a two spool gas turbine engine. The ceramic duct components are coupled to the engine block by support cages that accommodate thermal expansion of the duct components to prevent excessive stress levels within the ceramic components throughout a wide range of turbine engine operating conditions.

REFERENCES:
patent: 2428830 (1947-10-01), Birmann
patent: 2663141 (1953-12-01), Hage
patent: 2715814 (1955-08-01), Barr
patent: 4118927 (1978-10-01), Kronogard
patent: 4286430 (1981-09-01), Smith

Affiliated with

Also associated with

Rating

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

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

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-1794423