FASTENER BRACKET, FASTENER KIT, AIRCRA.. STRUCTURE AND METHODS

Disclosed is a fastener bracket 10, 102 103, 104, 105, 106, 107, 108 configured to be installed on a holding structure 1. The fastener bracket is formed as a single piece comprising a plate portion 11, 112, 115 and at least two pins 12, 122, 123, 124, 125, 127 protruding in parallel from a first sur...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser: Vichniakov, Alexei
Format: Patent
Sprache:eng ; fre ; ger
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Zusammenfassung:Disclosed is a fastener bracket 10, 102 103, 104, 105, 106, 107, 108 configured to be installed on a holding structure 1. The fastener bracket is formed as a single piece comprising a plate portion 11, 112, 115 and at least two pins 12, 122, 123, 124, 125, 127 protruding in parallel from a first surface S of the plate portion 11, 112, 115. The at least two pins 12, 122, 123, 124, 125, 127 are at least partially made of a remouldable material.Further disclosed is a fastener kit 1002, 1003, 1004, 1005, 1007 comprising such fastener bracket 10, 102 103, 104, 105, 106, 107 and at least one counter component 202, 204, 205, 206, 208, 303, 507. Moreover, an aircraft structure 1000 comprising at least one fastener bracket or even fastener kit is disclosed, as are an installation method of installing a fastener bracket, and a fastening method of fastening an object to a holding structure 1 of an aircraft structure 1000.