Power plants – Reaction motor – With thrust direction modifying means
Patent
1990-12-14
1992-10-13
Bertsch, Richard A.
Power plants
Reaction motor
With thrust direction modifying means
60228, 60271, 23926519, F02K 100
Patent
active
051540509
ABSTRACT:
A thrust vectoring exhaust nozzle structure for an engine, such as a ramjet, rocket or turbojet, which generates thrust by expulsion of gaseous fuel combustion products along a thrust axis is described which comprises a generally axisymmetric housing defined along a central thrust axis including a wall structure defining an exhaust duct, and an axially spaced radially inwardly convergent portion, throat and radically outwardly divergent portion, and at least one airfoil disposed on the wall structure of the divergent portion and mounted for rotation about an axis substantially perpendicular to the thrust axis.
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patent: 2694898 (1954-11-01), Stauff
patent: 3201937 (1965-08-01), McKee
patent: 3229457 (1966-01-01), Rowe et al.
patent: 3371491 (1968-03-01), Pinter
patent: 3486698 (1969-12-01), Cologna
patent: 3743184 (1973-07-01), Mancus
Franke Milton E.
Friddell Jerold H.
Herup Eric J.
Bertsch Richard A.
Kocharov Michael I.
Scearce Bobby D.
Singer Donald J.
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