FR3000018B1 - Raidisseur de fuselage d'aeronef, son procede de fabrication, et fuselage d'aeronef equipe d'un tel raidisseur - Google Patents
Raidisseur de fuselage d'aeronef, son procede de fabrication, et fuselage d'aeronef equipe d'un tel raidisseurInfo
- Publication number
- FR3000018B1 FR3000018B1 FR1262649A FR1262649A FR3000018B1 FR 3000018 B1 FR3000018 B1 FR 3000018B1 FR 1262649 A FR1262649 A FR 1262649A FR 1262649 A FR1262649 A FR 1262649A FR 3000018 B1 FR3000018 B1 FR 3000018B1
- Authority
- FR
- France
- Prior art keywords
- stiffener
- aircraft fuselage
- manufacturing
- aircraft
- fuselage equipped
- 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.)
- Expired - Fee Related
Links
- 239000003351 stiffener Substances 0.000 title 2
- 238000004519 manufacturing process Methods 0.000 title 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D5/00—Bending sheet metal along straight lines, e.g. to form simple curves
- B21D5/16—Folding; Pleating
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D53/00—Making other particular articles
- B21D53/92—Making other particular articles other parts for aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/061—Frames
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/12—Construction or attachment of skin panels
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Moulding By Coating Moulds (AREA)
- Shaping Metal By Deep-Drawing, Or The Like (AREA)
- Connection Of Plates (AREA)
- Body Structure For Vehicles (AREA)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1262649A FR3000018B1 (fr) | 2012-12-21 | 2012-12-21 | Raidisseur de fuselage d'aeronef, son procede de fabrication, et fuselage d'aeronef equipe d'un tel raidisseur |
CN201380066896.7A CN105073577B (zh) | 2012-12-21 | 2013-12-20 | 用于飞行器机身的加强件、用于制造飞行器机身的加强件的方法以及装有这种加强件的飞行器机身 |
PCT/FR2013/053232 WO2014096741A1 (fr) | 2012-12-21 | 2013-12-20 | Raidisseur de fuselage d'aeronef, son procede de fabrication, et fuselage d'aeronef equipe d'un tel raidisseur |
US14/652,118 US9708050B2 (en) | 2012-12-21 | 2013-12-20 | Stiffener for an aircraft fuselage, method for manufacturing same, and aircraft fuselage equipped with such a stiffener |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1262649A FR3000018B1 (fr) | 2012-12-21 | 2012-12-21 | Raidisseur de fuselage d'aeronef, son procede de fabrication, et fuselage d'aeronef equipe d'un tel raidisseur |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3000018A1 FR3000018A1 (fr) | 2014-06-27 |
FR3000018B1 true FR3000018B1 (fr) | 2016-12-09 |
Family
ID=48289243
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1262649A Expired - Fee Related FR3000018B1 (fr) | 2012-12-21 | 2012-12-21 | Raidisseur de fuselage d'aeronef, son procede de fabrication, et fuselage d'aeronef equipe d'un tel raidisseur |
Country Status (4)
Country | Link |
---|---|
US (1) | US9708050B2 (fr) |
CN (1) | CN105073577B (fr) |
FR (1) | FR3000018B1 (fr) |
WO (1) | WO2014096741A1 (fr) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
USD777014S1 (en) * | 2014-08-12 | 2017-01-24 | Servi-Sure, LLC | Integrated stiffener |
GB2571911A (en) * | 2017-12-21 | 2019-09-18 | Airbus Operations Gmbh | A Stiffener for an Aircraft Assembly |
US11414213B2 (en) * | 2020-02-10 | 2022-08-16 | The Boeing Company | Low cost, high performance, multi-head drill and fill machine |
US11766828B2 (en) * | 2020-07-15 | 2023-09-26 | Spirit Aerosystems, Inc. | Method of manufacturing folded structure with additive features |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR531501A (fr) * | 1916-08-31 | 1922-01-16 | Zeppelin Werk Lindau G M B H | élément portant de construction |
US1357073A (en) * | 1920-01-09 | 1920-10-26 | Mooney Dermot Joseph | Metal construction |
US3698224A (en) | 1970-11-16 | 1972-10-17 | Siderurgica Occidental C A | Process for the production of steel structural shapes |
US4635882A (en) * | 1980-11-14 | 1987-01-13 | The Boeing Company | Method and apparatus for reducing low to mid frequency interior noise |
DE3401189A1 (de) * | 1983-01-25 | 1984-07-26 | Westland PLC, Yeovil, Somerset | Verbund-hubschrauberrumpf |
US5307601A (en) * | 1992-02-06 | 1994-05-03 | Mccracken Robert G | Beam member for use in concrete forming apparatus |
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 |
JP4526698B2 (ja) * | 2000-12-22 | 2010-08-18 | 富士重工業株式会社 | 複合材成形品及びその製造方法 |
US9359061B2 (en) * | 2005-10-31 | 2016-06-07 | The Boeing Company | Compliant stiffener for aircraft fuselage |
GB0611875D0 (en) * | 2006-06-15 | 2006-07-26 | Airbus Uk Ltd | A stringer for an aircraft wing and a method of forming thereof |
NL2000232C2 (nl) * | 2006-09-12 | 2008-03-13 | Gtm Consulting B V | Huidpaneel voor een vliegtuigromp. |
GB2441753B (en) * | 2006-09-12 | 2009-02-11 | Gkn Aerospace Services Ltd | Rib post |
FR2922516B1 (fr) * | 2007-10-18 | 2010-04-16 | Airbus France | Eclissage de raidisseurs en omega au niveau d'une jonction circonferentielle d'un fuselage d'avion |
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 |
ES2352941B1 (es) * | 2008-05-16 | 2012-01-25 | Airbus Operations, S.L. | Estructura integrada de aeronave en material compuesto |
US8074694B2 (en) * | 2009-05-28 | 2011-12-13 | The Boeing Company | Stringer transition method |
ES2382765B1 (es) * | 2009-06-29 | 2013-05-03 | Airbus Operations, S.L. | Diseño de cuadernas de aeronave |
EP2404824B1 (fr) * | 2010-07-08 | 2015-09-09 | Airbus Opérations SAS | Structure d'aeronef et Procédé de réalisation d'une telle structure |
-
2012
- 2012-12-21 FR FR1262649A patent/FR3000018B1/fr not_active Expired - Fee Related
-
2013
- 2013-12-20 US US14/652,118 patent/US9708050B2/en active Active
- 2013-12-20 CN CN201380066896.7A patent/CN105073577B/zh not_active Expired - Fee Related
- 2013-12-20 WO PCT/FR2013/053232 patent/WO2014096741A1/fr active Application Filing
Also Published As
Publication number | Publication date |
---|---|
CN105073577B (zh) | 2017-12-26 |
FR3000018A1 (fr) | 2014-06-27 |
CN105073577A (zh) | 2015-11-18 |
US9708050B2 (en) | 2017-07-18 |
US20150321742A1 (en) | 2015-11-12 |
WO2014096741A1 (fr) | 2014-06-26 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 4 |
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PLFP | Fee payment |
Year of fee payment: 5 |
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PLFP | Fee payment |
Year of fee payment: 6 |
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PLFP | Fee payment |
Year of fee payment: 8 |
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PLFP | Fee payment |
Year of fee payment: 9 |
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PLFP | Fee payment |
Year of fee payment: 10 |
|
ST | Notification of lapse |
Effective date: 20230808 |