Abstract: A first jet tab and a second jet tab are symmetrically arranged with respect to a symmetry plane and have a symmetrical shape with respect to the symmetry plane, and are symmetrically driven with respect to the symmetry plane by a driving section. A distance between a tip of the first jet tab and a first rotation axis is larger than a distance between the first rotation axis and the symmetry plane. A distance between a tip section of the second jet tab and a second rotation axis is larger than a distance between the second rotation axis and the symmetry plane.

Abstract: The thrust vectoring apparatus has a nozzle, a jet tab arranged behind the nozzle, a rotation shaft 30 connected to the jet tab, and a gas seal member arranged on an outer circumferential surface of the rotation shaft. The rotation shaft is connected to the jet tab, and has the protrusion in the redial direction out of the rotation shaft on the rear side of the gas seal member. The protrusion restrains that the combustion gas exhausted from the nozzle flows toward the gas seal member.

Abstract: A thrust vectoring device (101) equipped with: a shroud (102) having an opening; a nozzle (104) for spraying gas through the opening in the shroud (102), and provided in the interior of the shroud (102); a rotational drive shaft (140) positioned in parallel to the central axis (S104) of the shroud (102), and passing through one surface of the shroud (102); and a jet tab vectoring body (130) facing one surface of the shroud (102), and provided on one section of the rotational drive shaft (140) outside the shroud (102). Furthermore, a pressure adjustment part (110) is provided in the thrust vectoring device (101) so as to face the flow of the gas (151) directed toward the rotational drive shaft (140), and positioned on the one surface of the shroud (102) and/or the surface of the jet tab vectoring body (130) facing the one surface of the shroud (102).

Abstract: A first jet tab and a second jet tab are symmetrically arranged with respect to a first symmetry plane and have a symmetrical shape with respect to the first symmetry plane, and are symmetrically driven with respect to the first symmetry plane by a driving section. A distance between a tip sensation of the first jet tab and a first rotation axis is larger than a distance between the first rotation axis and the first symmetry plane. A distance between a tip section of the second jet tab and a second rotation axis is larger than a distance between the second rotation axis and the first symmetry plane.

Abstract: The thrust vectoring apparatus has a nozzle, a jet tab arranged behind the nozzle, a rotation shaft 30 connected to the jet tab, and a gas seal member arranged on an outer circumferential surface of the rotation shaft. The rotation shaft is connected to the jet tab, and has the protrusion in the redial direction out of the rotation shaft on the rear side of the gas seal member. The protrusion restrains that the combustion gas exhausted from the nozzle flows toward the gas seal member.