Power plants – Internal combustion engine with treatment or handling of... – Material from exhaust structure fed to engine intake
Patent
1974-11-26
1976-08-17
Croyle, Carlton R.
Power plants
Internal combustion engine with treatment or handling of...
Material from exhaust structure fed to engine intake
181 3311B, F02K 100, F01N 700
Patent
active
039746496
ABSTRACT:
An exhaust duct for a thrust jet engine, such as a rocket or gas turbine, which an acoustic and/or thermal protection lining is situated coaxially within a support element of the duct and is deformable radially relative to the support member, and preferably also adapted for relieving axial differential expansion stresses between the lining and the support element.
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Camboulives Andre Alphonse Mederic Leon
LE Maout Theophile Francois
Rejzner Jacques Serge
Vandenbroucke Roger Alfred Jules
Croyle Carlton R.
Ross Thomas I.
Societe Nationale d'Etude et de Construction de Moteurs d'Aviati
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