| 摘要 |
The invention relates to a device for the detachable attachment of loads, especially of missiles and containers to aircraft which is designed such that the large loads which occur during a flight at the interface between the missile and a T-lug are absorbed in an optimum manner and are introduced into the structure of the load, by distribution of the forces and moments. Exemplary embodiments are explained and are clarified in the Figures of the drawing. <IMAGE> |
