The invention discloses a mechanically distributed propulsion driveline and architecture, and relates to an aircraft with an integrated boundary layer suction propulsion device having a mechanically distributed propulsion system. The mechanically distributed propulsion system may include an engine for generating mechanical drive power, a driveshaft, a direction reversal transmission, and a propeller fan. The drive shaft may be operably coupled to an engine to receive mechanical drive power. The direction reversal transmission may have a first rotational shaft operably coupled to the drive shaft to receive mechanical drive power and a second rotational shaft, the direction reversal transmission configured to divert the mechanical drive power received at the first rotational shaft from a first direction to a second direction facing at the second rotational shaft. A propeller fan may be coupled to the second rotating shaft to convert the mechanical drive power into thrust.
本申请公开机械分布式推进传动系和架构,涉及一种具有集成式边界层吸入推进装置的航空器,其具有机械分布式推进系统。该机械分布式推进系统可包括用于产生机械驱动动力的发动机、驱动轴、方向反转传动装置和推进器风扇。驱动轴可被可操作地耦接到发动机以接收机械驱动动力。方向反转传动装置可具有第一旋转轴和第二旋转轴,第一旋转轴可操作地耦接到驱动轴以接收机械驱动动力,该方向反转传动装置被配置成将在第一旋转轴处接收的机械驱动动力从第一方向转向成在第二旋转轴处面向第二方向。推进器风扇可耦接到第二旋转轴,以将机械驱动动力转换成推力。
Mechanically distributed propulsion driveline and architecture
机械分布式推进传动系和架构
2023-11-28
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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