| 摘要 |
A thrust vectoring, thrust reversing and lift augmentation system is provided for jet aircraft in a compact package to optimize the several controlled flight regimes of the aircraft. Thus, the pilot can selectively direct and control the exhaust gases of each engine to give maximum forward thrust, boundary layer control and/or jet flap lift augmentation or he can select some combination of vectored thrust with lift augmentation. Additionally, when desired a thrust reversing position can be selected to minimize ground roll after landing of the aircraft.
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