An aircraft jet airfoil system belongs to the technical field of aircrafts. The invention provides an air jet airfoil system of an aircraft, which comprises an air compression device and an air jet airfoil, and is characterized in that the air jet airfoil is provided with an airfoil air jet port on the airfoil of the aircraft or a control surface air jet port on the control surface of the airfoil, and the airfoil air jet port or the control surface air jet port can jet air compressed by the air compression device. The control force of the airfoil of the aircraft can be enhanced, so that the attitude control capability of the aircraft is improved, and the aircraft can still realize stable control of the flight attitude when flying at a low speed.

    飞行器喷气翼面系统属于飞行器技术领域。本发明提供了飞行器喷气翼面系统,包括空气压缩装置和喷气翼面,其特征在于,所述喷气翼面是在飞行器的翼面上有翼面喷气口或者在翼面的舵面上有舵面喷气口,所述翼面喷气口或者舵面喷气口能够喷射空气压缩装置压缩的空气。本发明可以增强飞行器翼面的操控力,进而提高飞行器的姿态控制能力,使飞行器在低速飞行时仍能实现飞行姿态的稳定控制。


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    Title :

    Aircraft jet airfoil system


    Additional title:

    飞行器喷气翼面系统


    Contributors:
    LIU KAI (author) / ZHENG PEIYING (author)

    Publication date :

    2024-08-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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