| 摘要 |
An aircraft nacelle includes an air intake, connected to a means of propulsion, which defines a longitudinal direction, an outer wall, an inner duct including an annular flange connected, by means of connecting elements, to the means of propulsion, and a forward frame and a rear frame which connects the outer wall and the inner duct. The rear frame includes a first ring and a second ring, in longitudinal planes. The rings include a first connection to the outer wall. The first ring includes a second connection with the annular flange. The second ring includes a third connection with the inner duct. The third connection is remote from the second connection. |
