Power plants – Internal combustion engine with treatment or handling of... – Material from exhaust structure fed to engine intake
Patent
1977-04-14
1979-04-24
Garrett, Robert E.
Power plants
Internal combustion engine with treatment or handling of...
Material from exhaust structure fed to engine intake
60200A, 60263, 23926515, F02K 904
Patent
active
041505409
ABSTRACT:
An improved rocket nozzle system having a closure insulator located adjacent the combustion chamber of a rocket engine. The closure insulator has formed as an integral part thereof a plurality of nozzles. Each of the nozzles has incorporated therein a throat insert of pyrolized graphite cloth laminate and a consumable washer. The entire closure insulator assembly including nozzles is transfer molded as one piece into a steel housing. The housing is mounted on the combustion chamber thereby providing an effective nozzle system which is reliably operable under high temperature operation.
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patent: 3052090 (1962-09-01), Herzog
patent: 3133411 (1964-05-01), McCorkle
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patent: 3372548 (1968-03-01), Mathis et al.
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patent: 3694883 (1972-10-01), Olcott
patent: 3771726 (1973-11-01), Mikeska
"Mark's Handbook", 7th Edit., 1967, McGraw-Hill; pp. 6-182, 6-205.
"Rubber Technology", 2nd Edit., 1973, Van Nostrand; pp. 368, 369, 381.
Dolgonas Gene
Krayenbuhl Harold A.
Rogers Charles J.
Erlich Jacob N.
Garrett Robert E.
Rusz Joseph E.
The United States of America as represented by the Secretary of
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