|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/225 ; 60/244 ; 137/015.1|
|발명자 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 5 인용 특허 : 7|
A combined ramjet and rocket engine, operates as a ramjet in atmosphere, and a rocket engine in space is provided with a rectilinear duct. The engine has interior of the rectilinear duct paired and hinged rectilinear baffles which move from one of the duct walls. These hinged rectilinear baffles move into and out of the planar duct wall and define both the constriction of the Venturi for the ramjet engine configuration or the closure of the duct for the rocket engine configuration. The hinged rectilinear baffles are given leading and trailing wall surfac...
[ What is claimed is:] [1.] A combination ramjet and rocket engine comprising:a rectilinear duct defined by upper and lower parallel walls and left and right parallel walls, the rectilinear duct having an intake, an outlet, and a combustion chamber between the intake and the outlet;at least a forward rectilinear baffle and rear rectilinear baffle, the forward rectilinear baffle and the rear rectilinear baffle each having first and second sides with parallel edges adjacent the left and right parallel walls of the rectilinear duct respectively, each forwar...