FR2984274B1 - Poutre securisee, en particulier cadre fort de fuselage, ainsi que fuselage d'aeronef equipe de tels cadres - Google Patents

Poutre securisee, en particulier cadre fort de fuselage, ainsi que fuselage d'aeronef equipe de tels cadres

Info

Publication number
FR2984274B1
FR2984274B1 FR1161666A FR1161666A FR2984274B1 FR 2984274 B1 FR2984274 B1 FR 2984274B1 FR 1161666 A FR1161666 A FR 1161666A FR 1161666 A FR1161666 A FR 1161666A FR 2984274 B1 FR2984274 B1 FR 2984274B1
Authority
FR
France
Prior art keywords
frames
well
fuselage
strong
frame
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.)
Active
Application number
FR1161666A
Other languages
English (en)
Other versions
FR2984274A1 (fr
Inventor
Julien Guillemaut
Guillaume Gallant
Jerome Colmagro
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR1161666A priority Critical patent/FR2984274B1/fr
Priority to US13/714,789 priority patent/US20130157017A1/en
Priority to CN2012105989919A priority patent/CN103158855A/zh
Publication of FR2984274A1 publication Critical patent/FR2984274A1/fr
Application granted granted Critical
Publication of FR2984274B1 publication Critical patent/FR2984274B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • B64C1/062—Frames specially adapted to absorb crash loads
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24479—Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness
    • Y10T428/24612—Composite web or sheet
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24628—Nonplanar uniform thickness material
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/249921—Web or sheet containing structurally defined element or component
    • Y10T428/249923—Including interlaminar mechanical fastener

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
FR1161666A 2011-12-15 2011-12-15 Poutre securisee, en particulier cadre fort de fuselage, ainsi que fuselage d'aeronef equipe de tels cadres Active FR2984274B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1161666A FR2984274B1 (fr) 2011-12-15 2011-12-15 Poutre securisee, en particulier cadre fort de fuselage, ainsi que fuselage d'aeronef equipe de tels cadres
US13/714,789 US20130157017A1 (en) 2011-12-15 2012-12-14 Secure beam, in particular strong frame of fuselage, and aircraft fuselage provided with such frames
CN2012105989919A CN103158855A (zh) 2011-12-15 2012-12-15 安全梁、尤其是坚固的机身框架以及设有这种框架的飞机机身

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1161666A FR2984274B1 (fr) 2011-12-15 2011-12-15 Poutre securisee, en particulier cadre fort de fuselage, ainsi que fuselage d'aeronef equipe de tels cadres

Publications (2)

Publication Number Publication Date
FR2984274A1 FR2984274A1 (fr) 2013-06-21
FR2984274B1 true FR2984274B1 (fr) 2014-06-27

Family

ID=45809177

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1161666A Active FR2984274B1 (fr) 2011-12-15 2011-12-15 Poutre securisee, en particulier cadre fort de fuselage, ainsi que fuselage d'aeronef equipe de tels cadres

Country Status (3)

Country Link
US (1) US20130157017A1 (fr)
CN (1) CN103158855A (fr)
FR (1) FR2984274B1 (fr)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102014103438A1 (de) * 2013-07-16 2015-01-22 Airbus Operations Gmbh Spritzgussverfahren zur Herstellung eines Primärstrukturverbindungselements
EP3119577A1 (fr) * 2014-03-17 2017-01-25 GTM-Advanced Products B.V. Élément de raccordement de structure primaire pour aéronef et procédé de fabrication de l'élément de raccordement
US10295438B2 (en) * 2016-06-24 2019-05-21 The Boeing Company Modeling and analysis of leading edge ribs of an aircraft wing
CA3132276A1 (fr) 2019-03-01 2020-09-10 Pratt & Whitney Canada Corp. Configurations de systeme de refroidissement pour un aeronef ayant un systeme de propulsion hybride-electrique
US11628942B2 (en) 2019-03-01 2023-04-18 Pratt & Whitney Canada Corp. Torque ripple control for an aircraft power train
US11574548B2 (en) 2019-04-25 2023-02-07 Pratt & Whitney Canada Corp. Aircraft degraded operation ceiling increase using electric power boost
US11912422B2 (en) 2019-08-26 2024-02-27 Hamilton Sundstrand Corporation Hybrid electric aircraft and powerplant arrangements
US11667391B2 (en) 2019-08-26 2023-06-06 Pratt & Whitney Canada Corp. Dual engine hybrid-electric aircraft
US11738881B2 (en) 2019-10-21 2023-08-29 Hamilton Sundstrand Corporation Auxiliary power unit systems
US11319051B2 (en) * 2020-01-03 2022-05-03 The Boeing Company Stiffened composite ribs

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4702205A (en) * 1984-03-06 1987-10-27 David Constant V External combustion vane engine with conformable vanes
US5102723A (en) * 1989-11-13 1992-04-07 Pepin John N Structural sandwich panel with energy-absorbing material pierced by rigid rods
US5688426A (en) * 1995-06-07 1997-11-18 The Boeing Company Hybrid metal webbed composite beam
US6375120B1 (en) * 1997-07-14 2002-04-23 Jason M. Wolnek Method and apparatus for building a metal/composite hybrid airplane component
US6743504B1 (en) * 2001-03-01 2004-06-01 Rohr, Inc. Co-cured composite structures and method of making them
JP2004025946A (ja) * 2002-06-24 2004-01-29 Honda Motor Co Ltd 航空機の翼構造
US7325771B2 (en) * 2004-09-23 2008-02-05 The Boeing Company Splice joints for composite aircraft fuselages and other structures
DE102007029337B4 (de) * 2007-06-26 2010-07-22 Airbus Deutschland Gmbh Korrosionsfeste Verbindung zwischen einem ersten Bauteil und einem zweiten Bauteil
US8540833B2 (en) * 2008-05-16 2013-09-24 The Boeing Company Reinforced stiffeners and method for making the same
DE102008044229A1 (de) * 2008-12-01 2010-06-10 Airbus Deutschland Gmbh Schalenbauteil für ein Luft- oder Raumfahrzeug
DE102009021369A1 (de) * 2009-05-12 2010-11-18 Airbus Operations Gmbh Verfahren zur Herstellung eines Flugzeugrumpfes und Flugzeugrumpf
DE102010042970A1 (de) * 2010-05-12 2011-11-17 Airbus Operations Gmbh Strukturbauteil mit verbesserter Leitfähigkeit und mechanischer Festigkeit sowie Verfahren zu dessen Herstellung

Also Published As

Publication number Publication date
FR2984274A1 (fr) 2013-06-21
CN103158855A (zh) 2013-06-19
US20130157017A1 (en) 2013-06-20

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