CFRP fuselage frame fixed to vertical tail

The invention relates to a CFRP fuselage frame fixed to a vertical tail. A securing assembly for securing a vertical tail assembly to an aircraft includes a first lug member secured to the vertical tail assembly. The fixation assembly further includes a first U-joint member. The first U-joint member includes a first end of the first U-joint member joined to the first lug member. The second end of the first U-joint member is secured to a first fuselage frame made of composite material with a first fastener extending through the second end and the first fuselage frame in a first direction transverse to the first fuselage frame. 本申请涉及一种固定至垂直尾翼的CFRP机身框架。一种用于将垂直尾翼组件固定至飞机的固定组件包括固定至垂直尾翼组件的第一凸耳构件。固定组件进一步包括第一U形接头构件。第一U形接头构件包括接合至第一凸耳构件的第一U形接头构件的第一端部。第一U形接头构件的第二端部利用第一紧固件固定至由复合材料构成的第一机身框架，第一紧固件在横向于第一机身框架的第一方向上延伸穿过第二端部和第一机身框架。