METHOD OF CONTROL OF THRUST VECTOR OF AIRCRAFT CRUISE ENGINES Russian patent published in 1998 - IPC

Abstract RU 2122510 C1

FIELD: aviation. SUBSTANCE: thrust vector is regulated in direction deflecting the engine nozzles by means of drives receiving signals relative to preset magnitudes of nozzle positions, thus creating the longitudinal moment. Nozzles turn around axes which are inclined relative to horizontal plane of aircraft. At similar deflection of nozzles control of aircraft is ensured at simultaneous creation of longitudinal and lateral moments. At different angles of deflection of nozzles, yawing moment is created with no change in fuel delivery and consequently with no reduction in total thrust. EFFECT: enhanced efficiency.

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RU 2 122 510 C1

Authors

Simonov M.P.

Dates

1998-11-27—Published

1998-03-24—Filed