The invention relates to a pivoting wing (12) for an aircraft (13), characterized in that the pivoting wing is configured as a sub-airfoil-pivoting wing, said sub-airfoil-pivoting wing being formed by combining the sub-airfoils (1) when the individual sub-airfoils (1) are pivoted together.
一种用于飞行器(13)的枢转机翼(12),其特征在于,所述枢转机翼构造为子翼型‑枢转机翼,其中,所述子翼型‑枢转机翼在各个子翼型(1)枢转在一起时由这些子翼型(1)合并而成。
Pivoting wing as sub-airfoil-pivoting wing with pivotable sub-airfoil
带有可枢转的子翼型的作为子翼型-枢转机翼的枢转机翼
2025-03-07
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
Wing flap pivoting torsional connection
Emerald Group Publishing | 2001
PIVOTING SYSTEM, PIVOTING ASSEMBLY, PIVOTING MODULE AND SEAT COMPRISING THE PIVOTING SYSTEM
European Patent Office | 2021
|