JP6637694B2 - ハットストリンガ終端部取付け具とその作製方法 - Google Patents
ハットストリンガ終端部取付け具とその作製方法 Download PDFInfo
- Publication number
- JP6637694B2 JP6637694B2 JP2015160295A JP2015160295A JP6637694B2 JP 6637694 B2 JP6637694 B2 JP 6637694B2 JP 2015160295 A JP2015160295 A JP 2015160295A JP 2015160295 A JP2015160295 A JP 2015160295A JP 6637694 B2 JP6637694 B2 JP 6637694B2
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- Prior art keywords
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- hat stringer
- openings
- coupled
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Links
- 238000004519 manufacturing process Methods 0.000 title claims description 4
- 230000002093 peripheral effect Effects 0.000 claims description 39
- 230000000295 complement effect Effects 0.000 claims description 29
- 239000012530 fluid Substances 0.000 claims description 29
- 238000004891 communication Methods 0.000 claims description 26
- 238000010168 coupling process Methods 0.000 claims description 26
- 238000000034 method Methods 0.000 claims description 26
- 230000008878 coupling Effects 0.000 claims description 24
- 238000005859 coupling reaction Methods 0.000 claims description 24
- 239000002828 fuel tank Substances 0.000 description 18
- 238000009423 ventilation Methods 0.000 description 11
- 235000012149 noodles Nutrition 0.000 description 9
- 238000005452 bending Methods 0.000 description 5
- 239000000853 adhesive Substances 0.000 description 4
- 230000001070 adhesive effect Effects 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 230000006870 function Effects 0.000 description 3
- 230000008569 process Effects 0.000 description 3
- 239000012812 sealant material Substances 0.000 description 3
- 230000002411 adverse Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000005304 joining Methods 0.000 description 2
- 239000004918 carbon fiber reinforced polymer Substances 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 230000032798 delamination Effects 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 210000003437 trachea Anatomy 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
- 238000013022 venting Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/18—Spars; Ribs; Stringers
- B64C3/182—Stringers, longerons
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/34—Tanks constructed integrally with wings, e.g. for fuel or water
-
- 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
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/005—Accessories not provided for in the groups B64D37/02 - B64D37/28
-
- 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
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/02—Tanks
- B64D37/04—Arrangement thereof in or on aircraft
-
- 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
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/02—Tanks
- B64D37/06—Constructional adaptations thereof
- B64D37/10—Constructional adaptations thereof to facilitate fuel pressurisation
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Connection Of Plates (AREA)
- Moulding By Coating Moulds (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US14/464,098 | 2014-08-20 | ||
| US14/464,098 US9399510B2 (en) | 2014-08-20 | 2014-08-20 | Hat stringer closeout fitting and method of making same |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2016043923A JP2016043923A (ja) | 2016-04-04 |
| JP2016043923A5 JP2016043923A5 (enExample) | 2018-10-04 |
| JP6637694B2 true JP6637694B2 (ja) | 2020-01-29 |
Family
ID=53540629
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2015160295A Active JP6637694B2 (ja) | 2014-08-20 | 2015-08-17 | ハットストリンガ終端部取付け具とその作製方法 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US9399510B2 (enExample) |
| EP (1) | EP2987720B1 (enExample) |
| JP (1) | JP6637694B2 (enExample) |
| CN (1) | CN105383682B (enExample) |
| CA (1) | CA2891878C (enExample) |
Families Citing this family (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| USD799690S1 (en) * | 2014-12-22 | 2017-10-10 | Ebara Corporation | Inner cylinder for exhaust gas treatment apparatus |
| CA171066S (en) * | 2015-10-20 | 2017-01-09 | Kimura Kohki Co | Air-conditioning outlet |
| CA168044S (en) * | 2015-10-20 | 2017-01-09 | Kimura Kohki Co | Air-conditioning outlet |
| JP1560177S (enExample) * | 2015-10-20 | 2016-10-03 | ||
| JP1560175S (enExample) * | 2015-10-20 | 2016-10-03 | ||
| CA171067S (en) * | 2015-10-20 | 2017-01-09 | Kimura Kohki Co | Air-conditioning outlet |
| WO2018211234A1 (en) * | 2017-05-18 | 2018-11-22 | Bae Systems Plc | Door assembly for a vehicle |
| EP3403917A1 (en) * | 2017-05-18 | 2018-11-21 | BAE SYSTEMS plc | Door assembly for a vehicle |
| GB2575103A (en) | 2018-06-29 | 2020-01-01 | Airbus Operations Ltd | Method of manufacturing duct stringer |
| GB2575105A (en) * | 2018-06-29 | 2020-01-01 | Airbus Operations Ltd | A duct stringer |
| GB2575102A (en) * | 2018-06-29 | 2020-01-01 | Airbus Operations Ltd | Duct stringer with bulkhead |
| GB2575106B (en) * | 2018-06-29 | 2020-09-02 | Airbus Operations Ltd | A duct stringer |
| GB2575280A (en) * | 2018-07-04 | 2020-01-08 | Airbus Operations Ltd | A Connector |
| CN109911176A (zh) * | 2019-03-20 | 2019-06-21 | 成都飞机工业(集团)有限责任公司 | 一种机翼整体油箱区柔性连接干燥导管结构 |
| US11794874B2 (en) | 2019-10-23 | 2023-10-24 | The Boeing Company | Low impact hat stringer fluid dam |
| GB2590477A (en) * | 2019-12-19 | 2021-06-30 | Airbus Operations Ltd | Duct stringer assembly with bulkhead |
| US11554876B2 (en) * | 2020-03-19 | 2023-01-17 | The Boeing Company | Single piece vent dam |
| DE102021101438B3 (de) * | 2021-01-22 | 2022-01-13 | Airbus Defence and Space GmbH | Verbinder für ein strukturintegriertes Leitungssystem |
| US11718384B2 (en) | 2021-07-30 | 2023-08-08 | The Boeing Company | Hat-stringer assemblies for an aircraft and methods of forming same |
| US11597495B2 (en) | 2021-07-30 | 2023-03-07 | The Boeing Company | Vented hat stringers and methods of forming the same |
Family Cites Families (70)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3878356A (en) * | 1973-09-27 | 1975-04-15 | Cleveland E Roye | Diffusion band riveting method |
| US4645244A (en) * | 1984-02-15 | 1987-02-24 | Edwin Curtis | Aircraft duct gimbaled joint |
| US4802642A (en) * | 1986-10-14 | 1989-02-07 | The Boeing Company | Control of laminar flow in fluids by means of acoustic energy |
| JPH0367222U (enExample) * | 1989-10-25 | 1991-07-01 | ||
| US5263747A (en) * | 1992-02-13 | 1993-11-23 | Titeflex Corporation | Means for and methods of attaching metal hoses to end fittings |
| US5370427A (en) * | 1994-01-10 | 1994-12-06 | General Electric Company | Expansion joint for fluid piping with rotation prevention member |
| DE29823586U1 (de) * | 1998-05-29 | 1999-11-18 | IWK Regler und Kompensatoren GmbH, 76297 Stutensee | Flexibles Leitungselement |
| US6458309B1 (en) * | 1998-06-01 | 2002-10-01 | Rohr, Inc. | Method for fabricating an advanced composite aerostructure article having an integral co-cured fly away hollow mandrel |
| JP4010817B2 (ja) * | 2002-01-30 | 2007-11-21 | 本田技研工業株式会社 | 車両の車体フレーム構造 |
| US6814382B2 (en) * | 2002-03-04 | 2004-11-09 | Nishikawa Rubber Co., Ltd. | Car door structure and noise insulation sheet |
| US7040666B2 (en) * | 2003-06-06 | 2006-05-09 | General Electric Company | Full port externally gimballed joint |
| US7325771B2 (en) * | 2004-09-23 | 2008-02-05 | The Boeing Company | Splice joints for composite aircraft fuselages and other structures |
| US7387277B2 (en) * | 2004-12-29 | 2008-06-17 | The Boeing Company | Aircraft wing composed of composite and metal panels |
| US7377598B2 (en) * | 2005-01-10 | 2008-05-27 | American Axle & Manufacturing, Inc. | Axle housing assembly and method |
| USD551336S1 (en) * | 2006-05-08 | 2007-09-18 | Eastern Sheet Metal, Inc. | Duct and seal assembly |
| US7871040B2 (en) * | 2006-11-10 | 2011-01-18 | The Boeing Company | Composite aircraft structures with hat stiffeners |
| US7635106B2 (en) * | 2006-11-30 | 2009-12-22 | The Boeing Company | Composite shear tie |
| US20080169641A1 (en) * | 2007-01-16 | 2008-07-17 | Santa Cruz Cathy D | Inline irrigation pipe adapter fitting and method of installation |
| US20080302912A1 (en) * | 2007-06-08 | 2008-12-11 | The Boeing Company | Bladderless Mold Line Conformal Hat Stringer |
| US8043554B2 (en) * | 2007-06-08 | 2011-10-25 | The Boeing Company | Manufacturing process using bladderless mold line conformal hat stringer |
| DE102007029500B4 (de) * | 2007-06-25 | 2013-02-14 | Airbus Operations Gmbh | Verfahren zum Koppeln von Versteifungsprofilelementen sowie Strukturbauteil |
| US7686387B2 (en) * | 2007-08-28 | 2010-03-30 | Ford Global Technologies, Llc | Reinforcing sleeve for a tubular beam |
| US7828246B2 (en) * | 2007-09-14 | 2010-11-09 | Spectrum Aeronautical, Llc | Wing with sectioned tubular members |
| FR2922517B1 (fr) | 2007-10-18 | 2010-04-23 | Airbus France | Avion comportant des jonctions d'arrets de raidisseurs et procede de fabrication d'un tel avion |
| US7879276B2 (en) * | 2007-11-08 | 2011-02-01 | The Boeing Company | Foam stiffened hollow composite stringer |
| US8292214B2 (en) * | 2008-01-18 | 2012-10-23 | The Boeing Company | Vibration damping for wing-to-body aircraft fairing |
| EP2099077A1 (en) * | 2008-03-06 | 2009-09-09 | Inventux Technologies AG | Module for converting solar radiation into electricity |
| US20090266936A1 (en) * | 2008-04-29 | 2009-10-29 | Fernando Ferreira Fernandez | Aircraft fuselage structural components and methods of making same |
| US8465613B2 (en) * | 2011-08-24 | 2013-06-18 | The Boeing Company | Method and apparatus for fabricating variable gauge, contoured composite stiffeners |
| US8293051B2 (en) * | 2008-12-10 | 2012-10-23 | The Boeing Company | Method for producing composite laminates using a collapsible mandrel |
| US9296187B2 (en) * | 2008-12-10 | 2016-03-29 | The Boeing Company | Bagging process and mandrel for fabrication of elongated composite structure |
| US8074694B2 (en) * | 2009-05-28 | 2011-12-13 | The Boeing Company | Stringer transition method |
| US8617687B2 (en) * | 2009-08-03 | 2013-12-31 | The Boeing Company | Multi-functional aircraft structures |
| JP5515510B2 (ja) * | 2009-08-21 | 2014-06-11 | 日産自動車株式会社 | 車体構造 |
| DE102009029575B4 (de) * | 2009-09-18 | 2011-06-22 | Airbus Operations GmbH, 21129 | Verfahren zur Versteifung eines Faserverbundbauteils und Anordnung zur Herstellung eines versteiften Faserverbundteils |
| US8167245B1 (en) * | 2009-11-03 | 2012-05-01 | The Boeing Company | Fuel barrier |
| US9010689B1 (en) * | 2010-01-04 | 2015-04-21 | The Boeing Company | Fluid dynamic vent dam |
| US20130118624A1 (en) * | 2010-03-29 | 2013-05-16 | Hamilton Sundstrand Corporation | Sealed flapper diverter valve |
| US8408493B2 (en) * | 2010-05-19 | 2013-04-02 | The Boeing Company | Composite stringer end trim |
| FR2963273B1 (fr) * | 2010-07-29 | 2014-01-03 | Airbus Operations Sas | Procede de fabrication d'un panneau raidi en materiau composite |
| GB201012730D0 (en) * | 2010-07-29 | 2010-09-15 | Airbus Operations Ltd | A refuel valve assembly and method for refuelling an aircraft |
| CA2806330C (en) * | 2010-08-13 | 2017-01-03 | Hexcel Corporation | Machinable composite material |
| TW201234041A (en) * | 2010-09-18 | 2012-08-16 | Tonta Electro Optical Co Ltd | Optical device for coupling to a camera lens to form a visual observation system |
| GB201101435D0 (en) | 2011-01-27 | 2011-03-16 | Airbus Uk Ltd | Stringer for an aircraft wing and method of forming thereof |
| US8864181B2 (en) * | 2011-02-16 | 2014-10-21 | Sensus Spectrum, Llc | Split-ring gland pipe coupling with corrugated armor |
| US8777158B2 (en) * | 2011-03-25 | 2014-07-15 | The Boeing Company | Joint sealing system |
| ES2400129B1 (es) * | 2011-05-30 | 2014-06-18 | Airbus Operations, S.L. | Método de fabricación de larguerillos con forma de "t" con un ángulo diferente de 90� entre el alma y el pie |
| US9108497B2 (en) * | 2011-06-13 | 2015-08-18 | Albert W. Harrison, III | Structural enclosure for packaging power electronics for vehicle battery modules and methods of servicing and manufacturing vehicles using same |
| FR2976916B1 (fr) * | 2011-06-27 | 2013-07-26 | Airbus Operations Sas | Dispositif et procede d'assemblage de deux troncons de fuselage d'aeronef |
| US8998299B2 (en) * | 2011-09-09 | 2015-04-07 | Bae Systems Land & Armaments, L.P. | Armored vehicle with bolt-on bottom |
| JP6100461B2 (ja) * | 2011-12-27 | 2017-03-22 | 三菱航空機株式会社 | ベント部材、航空機の主翼 |
| GB201204231D0 (en) * | 2012-03-09 | 2012-04-25 | Airbus Uk Ltd | Space frame structure |
| GB2515953A (en) * | 2012-03-27 | 2015-01-07 | Brian Lewis | Interchangeable axle suspension spacer slider system and method of making same |
| US9144948B2 (en) * | 2012-04-04 | 2015-09-29 | The Boeing Company | Hat stiffeners with canted webs |
| US9381704B2 (en) * | 2012-06-08 | 2016-07-05 | The Boeing Company | Non-vented bladder system for curing composite parts |
| US8758879B2 (en) * | 2012-06-24 | 2014-06-24 | The Boeing Company | Composite hat stiffener, composite hat-stiffened pressure webs, and methods of making the same |
| US10309235B2 (en) * | 2012-08-27 | 2019-06-04 | United Technologies Corporation | Shiplap cantilevered stator |
| US9517594B2 (en) * | 2012-10-04 | 2016-12-13 | The Boeing Company | Composite structure having a stabilizing element |
| GB201217801D0 (en) * | 2012-10-05 | 2012-11-14 | Airbus Operations Ltd | An aircraft structure |
| US9278763B2 (en) * | 2013-01-15 | 2016-03-08 | The Boeing Company | Method and system for identifying fastener placement zones |
| JP6093192B2 (ja) * | 2013-01-25 | 2017-03-08 | 三菱航空機株式会社 | 航空機の機体用パネル、航空機の翼 |
| US20140272312A1 (en) * | 2013-03-13 | 2014-09-18 | Gulfstream Aerospace Corporation | Aircraft component and method of making an aircraft component |
| US9758251B2 (en) * | 2013-03-15 | 2017-09-12 | United Airlines, Inc. | Aircraft emergency escape slide container and method of changing an aircraft emergency escape slide |
| US9096324B2 (en) * | 2013-03-19 | 2015-08-04 | The Boeing Company | Joint assembly to form a sealed flow conduit |
| US9169948B2 (en) * | 2013-05-13 | 2015-10-27 | David Jay Buttars | Support structures for electrical and plumbing systems |
| US10479475B2 (en) * | 2013-08-09 | 2019-11-19 | The Boeing Company | Composite stringer beam joint structure of an aircraft |
| GB2517954B (en) * | 2013-09-05 | 2018-07-04 | Airbus Operations Ltd | Repair of a damaged composite aircraft wing |
| US9434422B2 (en) * | 2014-03-04 | 2016-09-06 | Ford Global Technologies, Llc | Geometric/mechanical isolation of aluminum to steel joining at trim edges for corrosion protection |
| DE102014204087A1 (de) * | 2014-03-06 | 2015-09-10 | Airbus Operations Gmbh | Halter zur Anbindung eines Bauteils an eine Komponente eines Luft- oder Raumfahrzeugs, Anordnung, Luft- oder Raumfahrzeug, sowie Verfahren |
| US9399509B2 (en) * | 2014-04-10 | 2016-07-26 | The Boeing Company | Vent stringer fitting |
-
2014
- 2014-08-20 US US14/464,098 patent/US9399510B2/en active Active
-
2015
- 2015-05-19 CA CA2891878A patent/CA2891878C/en active Active
- 2015-07-06 EP EP15175417.3A patent/EP2987720B1/en active Active
- 2015-08-17 JP JP2015160295A patent/JP6637694B2/ja active Active
- 2015-08-20 CN CN201510516343.8A patent/CN105383682B/zh active Active
Also Published As
| Publication number | Publication date |
|---|---|
| US9399510B2 (en) | 2016-07-26 |
| EP2987720B1 (en) | 2019-11-06 |
| CA2891878C (en) | 2017-06-27 |
| CA2891878A1 (en) | 2016-02-20 |
| EP2987720A1 (en) | 2016-02-24 |
| JP2016043923A (ja) | 2016-04-04 |
| CN105383682A (zh) | 2016-03-09 |
| CN105383682B (zh) | 2018-03-30 |
| US20160052617A1 (en) | 2016-02-25 |
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