An example method of mounting a first component to a second component includes receiving at least a fastening assembly within an aperture established in the first component, the fastening assembly coupled to the second component via a linking member, positioning a felt metal material between the fastening assembly and the first component, securing the fastening assembly, and compressing the felt metal material during the securing.
METHOD AND APPARATUS FOR ATTACHING COMPONENTS HAVING DISSIMILAR RATES OF THERMAL EXPANSION
2018-12-06
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge / F16B DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES , Vorrichtungen zum Befestigen oder Sichern von Konstruktionselementen oder Maschinenteilen, z.B. Nägel, Bolzen, Schrauben, Sprengringe, Klemmen, Klammern oder Keile |
Method and apparatus for attaching components having dissimilar rates of thermal expansion
Europäisches Patentamt | 2020
|Method and apparatus for attaching components having dissimilar rates of thermal expansion
Europäisches Patentamt | 2018
|Method and apparatus for attaching components having dissimilar rates of thermal expansion
Europäisches Patentamt | 2018
|Transition joint and method for attaching dissimilar metal tubes
Europäisches Patentamt | 2017
|Apparatus for attaching aircraft wing structural components
Europäisches Patentamt | 2022
|