Combined synthetic jet type circulation control system and method

The invention relates to a combined synthetic jet type circulation control system and method. The system comprises a wing upper surface and a wing lower surface, a fluid chamber is arranged between the wing upper surface and the wing lower surface, a vibrating membrane is arranged in the fluid chamb...

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Bibliographic Details
Main Authors GUO ZHENG, SHAO SHUAI, LU YAFEI, GUO BIN, JIA GAOWEI, HOU ZHONGXI, GAO XIANZHONG
Format Patent
LanguageChinese
English
Published 11.06.2024
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Summary:The invention relates to a combined synthetic jet type circulation control system and method. The system comprises a wing upper surface and a wing lower surface, a fluid chamber is arranged between the wing upper surface and the wing lower surface, a vibrating membrane is arranged in the fluid chamber, a driving assembly is further arranged in the fluid chamber, and one side of the driving assembly is in sliding fit with the rear edge of the wing; jet outlets are formed between the driving assembly and the wing upper surface and between the driving assembly and the wing lower surface, and concave cavities corresponding to the jet outlets are formed in the sides, close to the driving assembly, of the wing rear edges; the driving assembly drives the rear edges of the wings to slide along the contact surfaces, so that the concave cavities and the corresponding jet outlets are opened, communicated or relatively blocked. The driving assembly is in sliding fit with the trailing edge of the wing to control the trail
Bibliography:Application Number: CN202410176487