| 摘要 |
The invention relates to an effort recovery structure (101) of a connecting strut for attaching a turboreactor to the wing system of an aircraft. Said structure comprises a first lateral block (102) and a second lateral block (103) to be attached to the wing system of the aircraft, and a spigot fastener to be attached to the turboreactor, said lateral blocks (102, 103) surrounding an essentially long central plate (104) following the main axis (105) of the structure (101). The central plate (104) is connected to the spigot fastener and is produced from a metal or an alloy that can resist a temperature of at least 1000°C over a period of at least 15 minutes, such as to recover the static and dynamic efforts generated by the turboreactor according to the main axis (105). The invention also relates to a connecting strut for attaching a turboreactor to a wing system of an aircraft, comprising such a primary structure (101). |
