| 摘要 |
PROBLEM TO BE SOLVED: To provide a thrust deflecting device excellent in the responsiveness and the revolving performance and having no risk to impair the accelerating performance. SOLUTION: The thrust deflecting device is composed of a nozzle part 12 coupled with a flying object to generate a revolving force by deflecting the axial direction from the airframe axis direction and changing the combustion gas jetting direction, moving plates 19 arranged at the constant pitch phase angle in the circumferential direction of the neighbourhood where the nozzle part is coupled, making fore-and-aft motions along the side face of a combustor 14, moving the nozzle part of the specific phase to the front or the rear, and deflecting the axial direction from the airframe axis direction, an actuator 16 to move the moving plates to the front and the rear, and injection holes 21 and 22 bored perpendicularly to the airframe axis direction in the moving plates and the side faces of combustor and put in communication when the nozzle part is deflected so that the combustion gas is jetted for generation of a sideways force in the lateral direction.
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