FIELD: machine building.
SUBSTANCE: group of the inventions relates to devices of mounting of power plant in the aircraft. The cap is designed with a possibility of prevention of arcing at flowing of lightning current through the fastening element. The cap (27) is made fixable with providing of closing of a part of the fastening element (15) connecting the upper plating (3) of the aircraft with a stringer (11), placed from the interior of the upper plating (3), and the named part appears from the stringer (11). The external surface (33) of the cap passing into internal space of the upper plating (3), is curvilinear. The cap is made from conductive material. The fastening structure uses the cap. The aircraft comprises the fastening construction.
EFFECT: group of inventions is aimed at improvement of safety.
4 cl, 3 dwg
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RU2660096C2 |
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STRUCTURAL MATERIAL FOR MAKING STRUCTURAL ELEMENTS, FUEL TANK, MAIN WING AND AIRCRAFT | 2013 |
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RU2605716C2 |
FUEL TANK, MAIN WINGS, AIRCRAFT BODY, FLYING VEHICLE AND VEHICLE | 2014 |
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FUEL TANK, MAIN WINGS, AIR FRAME, AIRCRAFT AND VEHICLE | 2014 |
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RU2628291C2 |
FUEL TANK, MAIN WING, AIRCRAFT FUSELAGE, AIRCRAFT AND MOVING BODY | 2013 |
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RU2581104C1 |
APPARATUS AND METHODS FOR JOINING AIRCRAFT COMPOSITE STRUCTURES | 2014 |
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RU2666593C2 |
AIRCRAFT FUEL TANK | 2010 |
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STRUCTURE MADE OF COMPOSITE MATERIALS, AIRCRAFT MAIN WING AND BODY CONTAINING SAID STRUCTURE | 2010 |
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RU2518927C2 |
FASTENING SYSTEMS, ENSURING PROTECTION AGAINST ELECTROMAGNETIC EFFECTS | 2014 |
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RU2592958C2 |
Authors
Dates
2014-10-20—Published
2011-03-22—Filed