Systems and methods for use in covering a portion of a fastener protruding from a surface

A cap (250) for use in covering a portion (212) of a fastener (210) protruding from a surface (206) is provided. The portion (212) includes threads. The cap (250) includes an interior (252), a base (258) that at least partially delimits the interior (252), a threaded receptacle (292) on the interior...

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Bibliographic Details
Main Authors Rawdon, Blaine Knight, Cameron, Michael Scott
Format Patent
LanguageEnglish
French
German
Published 14.06.2017
Subjects
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN 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
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS
HEATING
LIGHTING
MECHANICAL ENGINEERING
PARACHUTES
PERFORMING OPERATIONS
THERMAL INSULATION IN GENERAL
TRANSPORTING
WEAPONS
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Summary:A cap (250) for use in covering a portion (212) of a fastener (210) protruding from a surface (206) is provided. The portion (212) includes threads. The cap (250) includes an interior (252), a base (258) that at least partially delimits the interior (252), a threaded receptacle (292) on the interior (252) configured to threadably engage the portion (212) of the fastener (210), and a seal (260) coupled to the base (258) to engage the surface (206).
Bibliography:Application Number: EP20140185995