A joint for an aircraft assembly

A joint to be assembled for an aircraft assembly is provided. The joint has a first joint part including a spigot and a second joint part including a housing and a floating socket in an interior of the housing, wherein the second joint part is arranged to receive the spigot in the floating socket. T...

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Bibliographische Detailangaben
Hauptverfasser:	JULIEN LAVERNE, ANDREW MCMAHON, OLIVER MARKS, JOERG SCHWICKERT, SAIF RAFIQUE, UMBERTO POLIMENO, RAUL-JOSE GOMEZ VIZCAINO, JOHN HOBDAY, ANDREW HENSTRIDGE, ABISHEK RAMESH
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION BLASTING COSMONAUTICS DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS ORMACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS,CLIPS, WEDGES, JOINTS OR JOINTING ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HELICOPTERS LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	A joint to be assembled for an aircraft assembly is provided. The joint has a first joint part including a spigot and a second joint part including a housing and a floating socket in an interior of the housing, wherein the second joint part is arranged to receive the spigot in the floating socket. The joint is configured to receive a curable medium, such as curable resin, in the interior to contact between the housing and the floating socket. 本申请涉及一种用于飞行器组件的待组装接合件。该接合件具有包括插头的第一接合部分。该接合件还具有带有壳体的第二接合部分。在壳体的内部有浮动插座。第二接合部分将插头接纳在浮动插座中。接合件布置成在内部中接纳可固化介质、比如可固化树脂，以在壳体与浮动插座之间产生接触。