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Driving flow control system and method of ship tail flight deck flow field

An active flow control and flight deck technology, applied in the field of aerodynamics, can solve problems such as inability to achieve a good control effect, and achieve the effects of reducing instability, ensuring safety, and simple system structure

Active Publication Date: 2017-06-13
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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AI Technical Summary

Problems solved by technology

The study adopts the method of adding curved deflectors on the top of the hangar for control, and a good improvement effect has been achieved under the design condition of 0° wind direction, but for the more common non-design condition of strong wind direction when the ship is sailing, This method of passive flow control cannot achieve a good control effect

Method used

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  • Driving flow control system and method of ship tail flight deck flow field
  • Driving flow control system and method of ship tail flight deck flow field
  • Driving flow control system and method of ship tail flight deck flow field

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Embodiment Construction

[0042] The present invention will be described in further detail below in conjunction with the accompanying drawings.

[0043] figure 1 It is a schematic diagram of the suction force received by the shipboard helicopter when it lands on the ship. figure 2 It is a schematic diagram of the pitching moment of the shipboard helicopter when it lands on the ship. image 3 It is a schematic diagram of the rolling moment of the shipborne helicopter when it lands on the ship. As shown in the figure, when the aircraft lands, after the air flows through the stern hangar, a complex vortex structure and low-pressure area will be formed above the deck, accompanied by unsteady flow states such as upwash, downwash and side wash, causing helicopter When landing, the torque is unbalanced, which will cause a helicopter safety accident in severe cases.

[0044]A kind of active flow control method of the flight deck flow field at the stern of the present invention is characterized in that the ...

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Abstract

The invention discloses a driving flow control method of a ship tail flight deck flow field. The driving flow control method of the ship tail flight deck flow field is characterized in that the wind speed and the wind angle of a ship are detected by a wind speed and direction sensor; when a ship-based helicopter takes off or lands, a flow control actuating element is driven by a control unit to generate a control airflow according to the detected wind speed and wind angle, a flow state of a main flow is changed, the ranged of a vortex region is reduced, a high upwash airflow or a downwash airflow is restrained to form, a rolling moment and a yawing moment of the ship-based helicopter during ship landing are weakened, and a flow field structure above a ship tail flight deck is improved. The driving flow control method of the ship tail flight deck flow field is applied to ship types such as a marine surveillance ship with a hangar and a destroyer, a complex flow field above a deck can be controlled, and uniformity of the flow field is improved.

Description

technical field [0001] The invention belongs to the technical field of aerodynamics, and relates to a method for improving the flow field of a flight deck at the stern of a ship, in particular to an active flow control system and a method for the flow field of the flight deck at the stern of a ship. Background technique [0002] The shipborne helicopter will be affected by complex sea conditions and high-speed navigation of the ship on the aft flight deck, and the airflow will form a complex flow structure on the aft flight deck of the ship, including the severe low-pressure separation area and the ship's sides on both sides of the deck. Upwash, downwash, etc. These complex flow structures have caused great difficulty in maneuvering the helicopter to land, and may even cause a crash. Due to the instability of the flow field on the flight deck at the tail of the ship, landing a shipborne helicopter has become one of the most difficult flying techniques to master. Even the mo...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B63G11/00B64F1/00
CPCB63G11/00B64F1/00
Inventor 顾蕴松郑越洋王翰墨孙之骏王逸斌
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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