Structure for enhancing vortex surfing, wing and aircraft
A vortex, surfing technology, applied in the direction of air flow, aircraft parts, aircraft control, etc. that flows through the surface of the aircraft, it can solve the problems of increasing the additional lift of the rear aircraft, unable to actively control, etc., to achieve more additional lift, good effect, reduce The effect of fuel consumption
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Embodiment 1
[0050] Such as Figure 1-9b , a structure for strengthening vortex surfing according to the present invention, including a jet device, the jet device includes a nozzle hole 103, the nozzle hole 103 is arranged on the wingtip 11, and the jet device can open and close the nozzle hole 103, the nozzle hole 103 is used for spraying airflow.
[0051] The wing tip 11 refers to the winglet at the wing tip of the aircraft's wing. The jet device can be an existing jet, such as a small jet engine, etc., which can provide jet airflow to the nozzle hole 103 on the wingtip 11 . The number and size of the nozzle holes 103 are all determined according to actual conditions. Adopting the structure of strengthening vortex surfing described in this embodiment, by setting the nozzle hole 103 of the jet device on the wingtip 11, and opening and closing the nozzle hole 103 on the wing tip 11 through the jet device, the jet on the wingtip 11 can be actively controlled. The nozzle hole 103 sprays t...
Embodiment 2
[0068] This embodiment provides a wing for enhanced vortex surfing, which includes a wing body 1 , the wing body 1 includes a wingtip 11 , and the structure for enhancing vortex surfing described in Embodiment 1.
[0069] Adopt the wing that strengthens the vortex surfing described in this embodiment, be used on the aircraft, be arranged on the wingtip 11 of the described strengthened vortex surfing wing of the aircraft by the spray hole 103 of the jet device, and be active by the jet device Control the jet airflow of the nozzle hole 103 on the wingtip 11 to actively control the vortex ring volume of the front aircraft, thereby increasing the additional lift to the rear aircraft and reducing the fuel consumption of the rear aircraft, so as to reduce the overall fuel consumption of the formation aircraft.
Embodiment 3
[0071] This embodiment provides an aircraft with enhanced vortex surfing, including the wing with enhanced vortex surfing described in Embodiment 2. Generally, the wings for strengthening vortex surfing described in Embodiment 2 are arranged in pairs on the aircraft.
[0072]The aircraft adopting the enhanced vortex surfing of the present invention, by setting the nozzle hole 103 of the jet device on the wingtip 11 of the wing of the aircraft, and actively controlling the jet flow from the nozzle hole 103 on the wing tip 11 through the jet device, To actively control the vortex ring volume of the front aircraft, thereby increasing the additional lift to the rear aircraft and reducing the fuel consumption of the rear aircraft, so as to reduce the overall fuel consumption of the formation aircraft.
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