The invention belongs to the field of wing body fusion layout aircraft power devices and control methods thereof, and particularly relates to a wing body fusion layout aircraft power device and a control method thereof. A built-in engine is arranged on the inner side of the rear portion of an aircraft body, and an external engine is arranged on the outer side of the rear portion of an aircraft; the built-in engine and the external engine jointly provide thrust for takeoff of the aircraft, only the external engine provides thrust for cruising of the aircraft during cruising of the aircraft, takeoff performance of the aircraft can be improved on the premise that the weight of the aircraft is not remarkably increased, and cruising resistance of the aircraft is guaranteed through the design of an air inlet channel, an air outlet channel, an air inlet cover and an air outlet cover of the built-in engine. The increase of the cruise resistance of the aircraft is avoided, so that the condition that the cruise performance and take-off performance of the aircraft are not coordinated with each other in the wing body fusion layout can be well balanced.
本申请属于翼身融合布局飞机动力装置及其操控方法领域,具体涉及一种翼身融合布局飞机动力装置及其操控方法,在机体后部内侧设置内置发动机,在飞机后部外侧布置外置发动机,在飞机起飞时,以内置发动机、外置发动机共同为飞机起飞提供推力,在飞机巡航时,仅外置发动机为飞机巡航提供推力,可在不显著增加飞机重量的前提下,改善飞机起飞性能,且通过内置发动机进气道、排气道、进气口盖、排气口盖的设计,保证飞机巡航阻力,避免飞机巡航阻力的增加,以此能够很好的平衡翼身融合布局飞机巡航性能、起飞性能不协调的情况。
Aircraft power device with wing body fusion layout and control method of aircraft power device
一种翼身融合布局飞机动力装置及其操控方法
2025-01-14
Patent
Electronic Resource
Chinese
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