MX2015014572A - Tapa inyectable. - Google Patents
Tapa inyectable.Info
- Publication number
- MX2015014572A MX2015014572A MX2015014572A MX2015014572A MX2015014572A MX 2015014572 A MX2015014572 A MX 2015014572A MX 2015014572 A MX2015014572 A MX 2015014572A MX 2015014572 A MX2015014572 A MX 2015014572A MX 2015014572 A MX2015014572 A MX 2015014572A
- Authority
- MX
- Mexico
- Prior art keywords
- cap
- annular
- cap member
- sealing material
- cavity
- Prior art date
Links
- 239000003566 sealing material Substances 0.000 abstract 4
- 238000007789 sealing Methods 0.000 abstract 3
- 238000004891 communication Methods 0.000 abstract 1
- 239000012530 fluid Substances 0.000 abstract 1
- 238000002347 injection Methods 0.000 abstract 1
- 239000007924 injection Substances 0.000 abstract 1
- 238000000034 method Methods 0.000 abstract 1
- 238000010943 off-gassing Methods 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B33/00—Features common to bolt and nut
- F16B33/004—Sealing; Insulation
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/02—Lightning protectors; Static dischargers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B37/00—Nuts or like thread-engaging members
- F16B37/14—Cap nuts; Nut caps or bolt caps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B11/00—Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding
- F16B11/006—Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding by gluing
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Gasket Seals (AREA)
- Closures For Containers (AREA)
Abstract
La presente invención propone una tapa (100) para formar una cavidad sellada (12) sellada alrededor de un extremo de un sujetador (2-4) para así contener eventos de desgasificación o de chispa en caso de un impacto de rayo en el sujetador (2-4). La invención también propone una junta que comprende tal tapa (100), y un estuche de partes y un método para instalar tal tapa (100). La tapa (100) de conformidad con la invención comprende un miembro (10) interno de tapa que tiene un base (11) anular que termina en un borde (18), el cual rodea una abertura dentro de la cavidad (12) de aire para encerrar un extremo del sujetador (2,4), y un miembro (20) externo de tapa que tiene un faldón anular o reborde (40) que se extiende en forma radial hacia afuera lejos de la base (11) anular, el faldón anular o reborde (40) y la base (11) anular entre ellos define una cavidad (34a-c) anular de sellado. La tapa (100) también comprende una entrada (44) de material sellador que comprende una abertura (22) en el miembro (20) externo de tapa que está en comunicación de fluidos con la cavidad (34a-c) anular de sellado, la abertura (32) está dispuesta para interconectarse con el dispositivo (80) de inyección de material sellador para proporcionar un flujo de material (81) de sellado curable desde la entrada (44) de material sellador dentro de la cavidad (34a-c) anular de sellado. El miembro (20) externo de tapa tiene una superficie interna formada con una primera característica de cierre (95, 96) y el miembro (10) interno de tapa tiene una superficie externa formada con una segunda característica (97) de cierre que forma una junta de ajuste a presión con una primera característica (95, 96) de cierre.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB201307134A GB201307134D0 (en) | 2013-04-19 | 2013-04-19 | Injectable nut cap |
GB201316990A GB201316990D0 (en) | 2013-09-25 | 2013-09-25 | Injectable cap |
PCT/GB2014/051192 WO2014170672A1 (en) | 2013-04-19 | 2014-04-16 | Injectable cap |
Publications (2)
Publication Number | Publication Date |
---|---|
MX2015014572A true MX2015014572A (es) | 2016-12-16 |
MX367717B MX367717B (es) | 2019-09-03 |
Family
ID=50543230
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
MX2015014572A MX367717B (es) | 2013-04-19 | 2014-04-16 | Tapa inyectable. |
Country Status (7)
Country | Link |
---|---|
US (1) | US9829030B2 (es) |
EP (1) | EP2986509B1 (es) |
JP (1) | JP6302046B2 (es) |
CN (1) | CN105121287B (es) |
CA (1) | CA2908919C (es) |
MX (1) | MX367717B (es) |
WO (1) | WO2014170672A1 (es) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20160044495A (ko) * | 2013-08-21 | 2016-04-25 | 에어버스 오퍼레이션즈 리미티드 | 주입식 밀봉재를 구비하는 캡 |
GB2535518A (en) * | 2015-02-20 | 2016-08-24 | Airbus Operations Ltd | Cap with injected sealant |
GB2535519A (en) | 2015-02-20 | 2016-08-24 | Airbus Operations Ltd | Two part cap |
US11161156B2 (en) * | 2015-10-27 | 2021-11-02 | Hamilton Sundstrand Corporation | Powder monitoring |
US9937746B2 (en) * | 2016-05-03 | 2018-04-10 | Maclean Fogg Company | Capped wheel fastener and method of assembly |
EP3392418B1 (de) * | 2017-04-19 | 2020-04-29 | Geberit International AG | Befestigungssystem |
GB2568069A (en) * | 2017-11-03 | 2019-05-08 | Airbus Operations Ltd | A nut cap |
GB2572377A (en) * | 2018-03-28 | 2019-10-02 | Airbus Operations Ltd | Cap with sealant flow path |
DE202018104479U1 (de) * | 2018-08-03 | 2018-08-21 | Fairchild Fasteners Europe - Camloc Gmbh | Einsatz zur Verbindung eines elektrischen Anschlusses mit einer Wand sowie Schutzkappe für einen Einsatz |
US11022164B2 (en) * | 2018-09-11 | 2021-06-01 | The Boeing Company | Double shell fastener caps |
GB2579229A (en) | 2018-11-26 | 2020-06-17 | Airbus Operations Ltd | Spark containment cap |
US10982704B2 (en) * | 2019-01-03 | 2021-04-20 | The Boeing Company | EME protection cap system with screw sealant mechanism |
GB2582631A (en) * | 2019-03-28 | 2020-09-30 | Airbus Operations Ltd | A joint for an aircraft assembly |
GB2598373A (en) * | 2020-08-28 | 2022-03-02 | Airbus Operations Ltd | Spark containment cap |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2710113A (en) | 1952-01-23 | 1955-06-07 | Gen Dynamics Corp | Seal construction |
US4755904A (en) * | 1986-06-06 | 1988-07-05 | The Boeing Company | Lightning protection system for conductive composite material structure |
FR2626629B1 (fr) | 1988-01-29 | 1990-03-09 | Aerospatiale | Procede et dispositif de fixation d'elements de structures d'aeronefs protegees contre la foudre, et outil pour la mise en oeuvre de ce procede |
US4905931A (en) | 1988-02-18 | 1990-03-06 | The Boeing Company | Arc suppression around fasteners |
JPH02102910A (ja) * | 1988-10-13 | 1990-04-16 | Dainippon Toryo Co Ltd | ボルト・ナットの防食方法及び保護キャップ |
JPH0439313U (es) * | 1990-07-27 | 1992-04-03 | ||
US5419666A (en) | 1993-09-27 | 1995-05-30 | Best; Don A. | Protective waterproof cover assembly for covering a fastener |
JP3023464U (ja) * | 1995-10-04 | 1996-04-16 | 株式会社ビッグウエスト | ナットキャップ |
DE102005030817B4 (de) | 2005-07-01 | 2008-07-24 | Radolid Thiel Gmbh | Schutzkappe für Schraubverbindungen sowie Verfahren zur Herstellung von Schutzkappen für Schraubverbindungen |
JP5055178B2 (ja) * | 2008-03-24 | 2012-10-24 | 三菱重工業株式会社 | 航空機組立品 |
JP5610758B2 (ja) | 2009-04-02 | 2014-10-22 | 三菱航空機株式会社 | 耐雷ファスナ、キャップ、耐雷ファスナの取り付け方法、航空機 |
EP2673193B1 (en) | 2011-02-10 | 2018-07-11 | Airbus Operations Limited | Cap for forming sealed cavity around fastener |
US8388293B2 (en) | 2011-02-28 | 2013-03-05 | Physical Systems, Inc. | Insulated and sealed cap for a fastener component |
JP5611097B2 (ja) * | 2011-03-30 | 2014-10-22 | 三菱航空機株式会社 | 耐雷防爆用ファスナ |
US9400007B2 (en) | 2012-05-31 | 2016-07-26 | Airbus Operations Limited | Injectable nut cap |
-
2014
- 2014-04-16 JP JP2016508238A patent/JP6302046B2/ja not_active Expired - Fee Related
- 2014-04-16 CA CA2908919A patent/CA2908919C/en not_active Expired - Fee Related
- 2014-04-16 MX MX2015014572A patent/MX367717B/es active IP Right Grant
- 2014-04-16 EP EP14718700.9A patent/EP2986509B1/en active Active
- 2014-04-16 CN CN201480021835.3A patent/CN105121287B/zh active Active
- 2014-04-16 WO PCT/GB2014/051192 patent/WO2014170672A1/en active Application Filing
- 2014-04-16 US US14/785,197 patent/US9829030B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
CA2908919C (en) | 2019-11-26 |
CN105121287A (zh) | 2015-12-02 |
EP2986509A1 (en) | 2016-02-24 |
MX367717B (es) | 2019-09-03 |
JP6302046B2 (ja) | 2018-03-28 |
US9829030B2 (en) | 2017-11-28 |
JP2016517941A (ja) | 2016-06-20 |
EP2986509B1 (en) | 2018-05-30 |
CA2908919A1 (en) | 2014-10-23 |
WO2014170672A1 (en) | 2014-10-23 |
US20160069376A1 (en) | 2016-03-10 |
CN105121287B (zh) | 2017-05-24 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG | Grant or registration |