Joining system and method for joining stringer to fuselage skin
Joining system and method for joining stringer to fuselage skin
- Neue Suche nach: AUTRY BYRON J
- Neue Suche nach: WIENTHES PAUL G
- Neue Suche nach: KNUTSON SAMUEL J
- Neue Suche nach: HICKMAN GREGORY
- Neue Suche nach: ARNOLD ALICE R
- Neue Suche nach: AUTRY BYRON J
- Neue Suche nach: WIENTHES PAUL G
- Neue Suche nach: KNUTSON SAMUEL J
- Neue Suche nach: HICKMAN GREGORY
- Neue Suche nach: ARNOLD ALICE R
A joining system and method of joining a stringer to a fuselage skin. The joining system includes a retention clip assembly configured to retain the fuselage skin. The stringer is temporarily attached to the fuselage skin. The joint system includes an upper beam assembly including an upper beam and a lower beam assembly. The lower beam assembly includes a lower beam and at least one lower heating element. A retention clip assembly is coupled to the upper beam assembly. A retention clip assembly is coupled to the underbeam assembly. The upper beam is movable relative to the lower beam to clamp together at least one of the plurality of stringers and the fuselage skin prior to and during welding.
一种将桁条接合到机身蒙皮的接合系统和方法，接合系统包括构造为保持机身蒙皮的保持夹具组件。桁条暂时附接到机身蒙皮。该接合系统包括上梁组件和下梁组件，该上梁组件包括上梁。下梁组件包括下梁和至少一个下加热元件。保持夹具组件联接到上梁组件。保持夹具组件联接到下梁组件。上梁能相对于下梁移动，以在焊接之前和期间将多个桁条中的至少一个桁条和机身蒙皮夹持在一起。
Dokumentinformationen
Joining system and method for joining stringer to fuselage skin
将桁条接合到机身蒙皮的接合系统和方法
2023-04-18
Patent
Elektronische Ressource
Chinesisch
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