Two-dimensional plug nozzle

Power plants – Reaction motor – Air passage bypasses combustion chamber

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F02K 306

Patent

active

042902622

ABSTRACT:
The ducting extending a substantial axial length of a gas turbine engine is faired to transition the annular flows of the core engine and fan to a rectangular separate flow in a pair of two-dimensional exhaust nozzles so as to control each flow individually. Each flow is judiciously located to achieve noise control and infrared suppression.

REFERENCES:
patent: 2679726 (1954-06-01), Moncrieff
patent: 3103102 (1963-09-01), Sargent
patent: 3137131 (1964-06-01), Tyler
patent: 3340689 (1967-09-01), Kueng
patent: 3393518 (1968-07-01), Bridge
patent: 3433244 (1969-03-01), Gardiner
patent: 3659422 (1972-05-01), Hope

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