The invention discloses a gas flow regulation device for a rotary spray
pipe value of a
solid rocket-
ramjet engine. Each of a first fixed part and a rotating part is provided with one central hole andtwo arc-shaped holes in the axial direction; the front end of a transmission shell and an axial outlet section of a rear sealing head shell of a
combustion chamber form a dynamic sealing structure; the
tail end of the transmission shell and the head end of a spray
pipe shell form a dynamic sealing structure; an outer ring of a thrust self-aligning
roller bearing is mounted and fixed to the interior of a shell hole in the head end of the spray
pipe shell; and the inner ring of the thrust self-aligning
roller bearing is fixed to a shaft neck of the
tail end of the transmission shell in a matched manner. A driving motor drives a driven gear to rotate to determine a corresponding angle of a
transmission ratio, and finally, drives the rotating part to rotate at a corresponding angle relative to the first fixed part, so that the two arc-shaped holes of the rotating part and the fixed part are staggered and sheltered in the axial direction, thereby changing the effective outlet circulation area of the gas of the
combustion chamber and realizing gas flow regulation with determined accuracy. The gas flow regulation device for the rotary spray pipe value of the
solid rocket-
ramjet engine isbetter in transmission mechanism
thermal protection, more compact in structure and has higher work reliability, and can realize higher-precision and larger-range gas flow regulation.