초록 ▼

A method and apparatus for producing a thrust force from an annular axial stream of gaseous products fed to a nozzle with a supercritical pressure drop and acceleration to subsonic speed. In the nozzle, the direction of the subsonic annular stream is changed from axial to radial and the radial strea

A method and apparatus for producing a thrust force from an annular axial stream of gaseous products fed to a nozzle with a supercritical pressure drop and acceleration to subsonic speed. In the nozzle, the direction of the subsonic annular stream is changed from axial to radial and the radial stream is divided into a plurality of opposing jets which collide in a braking zone and change direction back to axial for discharge into the ambient atmosphere. A change in thrust intensity (modulus) is effected by changing the flow rate of the radial jets and/or the flow rate of the axial stream discharged into the ambient atmosphere. Adjustment of the angle of the thrust vector is effected by changing the angle of discharge of the axial stream into the ambient atmosphere. The nozzle comprises a housing, a central body with a flat base in the housing, and a casing surrounding the central body and having an end face with profiled outlet edges forming together with the flat base of the central body a radial channel with a critical cross section and an axial outlet. The casing is axially adjustable and the central body is angularly movable to adjust the flat base from a position perpendicular to the longitudinal axis of the nozzle to an angular position relative thereto.

대표청구항 ▼

A process for producing thrust, comprising the steps of: forming an annular stream with an axially directed velocity vector from gaseous combustion products incoming with a supercritical pressure drop; accelerating said gaseous combustion products in the annular stream to a subsonic speed; convertin

A process for producing thrust, comprising the steps of: forming an annular stream with an axially directed velocity vector from gaseous combustion products incoming with a supercritical pressure drop; accelerating said gaseous combustion products in the annular stream to a subsonic speed; converting said axial annular stream of said gaseous combustion products into radial jets by changing the direction of movement of said gaseous combustion products from axial to radial with opposing velocity vectors of said radial jets; accelerating said gaseous combustion products as radial jets to supersonic speed; adjusting the thrust modulus by changing the flow rate of said radial jets of said gaseous combustion products; colliding said opposing radial jets, resulting in their braking and a change of the direction of the velocity vector of said gaseous combustion products from radial to axial to form an outflowing axial stream; adjusting the thrust modulus by changing the flow rate of said outflowing axial stream; changing the direction of the thrust vector by changing the direction of the velocity vector of said outflowing axial stream by deflecting it from the axial direction during the discharge into the ambient medium.