公开(公告)号：US3334847A

公开(公告)日：1967-08-08

申请号：US51435965

申请日：1965-12-16

Applicant: SAAB AB

Inventor： EVERT AXENBORG CARL

IPC: B64D25/02 ,  B64D25/06 ,  B64D25/10

CPC classification number: B64D25/06 ,  B64D25/02 ,  B64D25/10

公开(公告)号：DE1756716A1

公开(公告)日：1970-08-13

申请号：DE1756716

申请日：1968-07-02

Applicant: SAAB AB

Inventor： EVERT AXENBORG CARL ,  THEODOR MENNBORG HANS JOERGEN ,  HENRIK WEDIN STEN

IPC: F02K9/84 ,  B64D25/10

Abstract: For adjustment of the direction of its thrust vector, an ejection seat rocket motor is mounted on the ejectable frame element for bodily angular motion, or has an adjustable gas deflector. The seat element, heightwise adjustable on the frame element, has a motion transmitting connection with the rocket motor whereby the thrust vector is maintained in desired relation to the center of gravity of the seat/occupant mass in every position of seat adjustment. At high speeds an airspeed responsive member transiently engages, during ejection, a sensing member associated with said connection, modifying the thrust vector adjustment.