A casing structure interposed between the engine and the nacelle of an aircraft, the casing structure including a shroud surrounding the engine and including a plurality of sectors; at least one radial arm providing the connection to the nacelle; and a plurality of fasteners for securing the plurality of shroud sectors to one another or to the at least one radial arm; the plurality of fasteners including a plurality of connection tabs, each provided with two parallel series of holes for receiving two respective series of headed bolts, a first series passing through a corresponding set of orifices of one shroud sector, and a second series passing through a corresponding set of orifices of an adjacent shroud sector or an adjacent radial arm.
Casing structure with connection tabs
07.05.2019
Patent
Elektronische Ressource
Englisch
Modular unmanned aerial vehicle connection system having insertable tabs
Europäisches Patentamt | 2024
|Emerald Group Publishing | 1947
|Engineering Index Backfile | 1948
|Emerald Group Publishing | 1947
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