ENGINE AND THRUST CONTROL OF AIRCRAFT IN NO DWELL ZONE

Aircraft, engine electronic controller systems, and methods for controlling thrust in a no dwell zone are provided. An aircraft includes a first engine that includes a first compressor fan rotating ata first speed and a second engine that includes a second compressor fan rotating at a second speed. First and second engine electronic controllers receive engine thrust commands and are in communication with the first and second engines, respectively. When the engine thrust commands correspond to an engine response within a no dwell zone, the first engine electronic controller directs the first engine to have the first speed at or below a compressor fan speed lower boundary and the second engine electronic controller directs the second engine to have the second speed at or above the compressor fan speed upper boundary to produce an overall average thrust within the no dwell zone. 提供了航空器、发动机电子控制器系统和用于控制在非驻留区中的推力的方法。在一个示例中，航空器包括第一发动机和第二发动机，第一发动机包括以第一速度旋转的第一压缩机风扇，第二发动机包括以第二速度旋转的第二压缩机风扇。第一和第二发动机电子控制器接收发动机推力命令并分别与第一和第