FI20075172A0 - Bågelement och kompositfläns för luftfartyg - Google Patents

Bågelement och kompositfläns för luftfartyg

Info

Publication number
FI20075172A0
FI20075172A0 FI20075172A FI20075172A FI20075172A0 FI 20075172 A0 FI20075172 A0 FI 20075172A0 FI 20075172 A FI20075172 A FI 20075172A FI 20075172 A FI20075172 A FI 20075172A FI 20075172 A0 FI20075172 A0 FI 20075172A0
Authority
FI
Finland
Prior art keywords
aircraft
composite flange
arc elements
arc
elements
Prior art date
Application number
FI20075172A
Other languages
English (en)
Finnish (fi)
Other versions
FI119979B (sv
FI20075172A (sv
Inventor
Lauri Halme
Juha Halme
Original Assignee
Patria Aerostructures Oy
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 Patria Aerostructures Oy filed Critical Patria Aerostructures Oy
Priority to FI20075172A priority Critical patent/FI119979B/sv
Publication of FI20075172A0 publication Critical patent/FI20075172A0/sv
Priority to US12/074,857 priority patent/US7967248B2/en
Priority to EP08152587.5A priority patent/EP1970303A3/en
Publication of FI20075172A publication Critical patent/FI20075172A/sv
Application granted granted Critical
Publication of FI119979B publication Critical patent/FI119979B/sv

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • B64C3/187—Ribs
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • 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
    • F16B2200/00—Constructional details of connections not covered for in other groups of this subclass
    • F16B2200/50—Flanged connections
    • 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
    • Y10T403/00—Joints and connections
    • Y10T403/51—Joints and connections including spaced, diverse connections

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Connection Of Plates (AREA)
FI20075172A 2007-03-12 2007-03-12 Bågelement och kompositfläns för luftfartyg FI119979B (sv)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FI20075172A FI119979B (sv) 2007-03-12 2007-03-12 Bågelement och kompositfläns för luftfartyg
US12/074,857 US7967248B2 (en) 2007-03-12 2008-03-06 Rib element and composite flange for aircraft
EP08152587.5A EP1970303A3 (en) 2007-03-12 2008-03-11 Rib element and composite flange for aircraft

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FI20075172A FI119979B (sv) 2007-03-12 2007-03-12 Bågelement och kompositfläns för luftfartyg
FI20075172 2007-03-12

Publications (3)

Publication Number Publication Date
FI20075172A0 true FI20075172A0 (sv) 2007-03-12
FI20075172A FI20075172A (sv) 2008-09-13
FI119979B FI119979B (sv) 2009-05-29

Family

ID=37930083

Family Applications (1)

Application Number Title Priority Date Filing Date
FI20075172A FI119979B (sv) 2007-03-12 2007-03-12 Bågelement och kompositfläns för luftfartyg

Country Status (3)

Country Link
US (1) US7967248B2 (sv)
EP (1) EP1970303A3 (sv)
FI (1) FI119979B (sv)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0606079D0 (en) * 2006-03-27 2006-05-03 Airbus Uk Ltd Aircraft component
GB0611875D0 (en) * 2006-06-15 2006-07-26 Airbus Uk Ltd A stringer for an aircraft wing and a method of forming thereof
FR2903732B1 (fr) * 2006-07-12 2008-09-12 Airbus France Sas Entree d'air pour turbomoteur d'aeronef.
DE102008002117B4 (de) * 2008-05-30 2013-10-31 Airbus Operations Gmbh Verbund und Struktur
ES2372828B1 (es) * 2008-12-17 2012-12-13 Airbus Operations, S.L. Costilla-herraje.
US8679616B2 (en) * 2010-12-14 2014-03-25 The Boeing Company Skew-angle radius filler
FR2975970B1 (fr) * 2011-05-30 2013-05-17 Aircelle Sa Ensemble pour une nacelle d'aeronef
US8535042B1 (en) 2012-09-14 2013-09-17 General Electric Company Apparatus for manufacturing a flanged component and methods of manufacturing the same
US9149997B2 (en) 2012-09-14 2015-10-06 United Technologies Composite flange from braided preform
US20140119904A1 (en) 2012-11-01 2014-05-01 United Technologies Corporation In-situ pressure enhanced processing of composite articles
GB2528078B (en) * 2014-07-08 2020-07-29 Airbus Operations Ltd Structure
GB2528076B (en) * 2014-07-08 2020-07-29 Airbus Operations Ltd Rib foot
US10196126B2 (en) 2015-04-07 2019-02-05 The Boeing Company Rib structure and method of forming thereof
GB201522327D0 (en) * 2015-12-17 2016-02-03 Airbus Operations Ltd Wing structure
US10196937B2 (en) 2015-12-30 2019-02-05 General Electric Company Method and system for improving structural characteristics of composite component corners
GB2575102A (en) * 2018-06-29 2020-01-01 Airbus Operations Ltd Duct stringer with bulkhead
US11180238B2 (en) * 2018-11-19 2021-11-23 The Boeing Company Shear ties for aircraft wing
US20200331616A1 (en) * 2019-04-19 2020-10-22 Goodrich Corporation Bonded structural rib for heated aircraft leading edge
CN114233732B (zh) * 2021-12-15 2024-02-27 北京机科国创轻量化科学研究院有限公司 一种胶粘式复合材料连接件及利用其连接复合板材的方法

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1363569A (en) * 1920-07-08 1920-12-28 Adoniram J Cook Metal aeroplane
US1796654A (en) * 1927-11-07 1931-03-17 Hermann Otto Metallic aeroplane wing
US2140558A (en) * 1938-06-03 1938-12-20 Schmidt Karl Airplane fabric attachment
US2427853A (en) * 1944-02-23 1947-09-23 Curtiss Wright Corp Aircraft construction
US2397447A (en) * 1944-10-19 1946-03-26 Budd Edward G Mfg Co Metallic structure
US2567124A (en) * 1946-05-10 1951-09-04 Curtiss Wright Corp Airfoil construction
US5233129A (en) * 1992-10-15 1993-08-03 At&T Bell Laboratories Seismic network bay frame
ES2168027B1 (es) * 1998-12-18 2003-10-01 Airbus Espana Sl Un procedimiento de union a traccion-compresion de caracter desmontable y/o fijo para aplicar a materiales compuestos.
US6190484B1 (en) * 1999-02-19 2001-02-20 Kari Appa Monolithic composite wing manufacturing process
GB0022589D0 (en) * 2000-09-14 2000-11-01 Bae Systems Plc Composite joints
JP4574086B2 (ja) * 2001-09-03 2010-11-04 富士重工業株式会社 複合材翼の製造方法および複合材翼
GB0609166D0 (en) * 2006-05-09 2006-06-21 Airbus Uk Ltd Apparatus for and method of inhibiting delamination
US7735600B2 (en) * 2006-12-08 2010-06-15 The Boeing Corporation Monolithic acoustically-treated engine nacelle inlet panels

Also Published As

Publication number Publication date
US7967248B2 (en) 2011-06-28
FI119979B (sv) 2009-05-29
US20080223987A1 (en) 2008-09-18
EP1970303A3 (en) 2015-11-18
EP1970303A2 (en) 2008-09-17
FI20075172A (sv) 2008-09-13

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