BRPI0907670A2 - conjunto de estrutura de aeronave - Google Patents

conjunto de estrutura de aeronave

Info

Publication number
BRPI0907670A2
BRPI0907670A2 BRPI0907670A BRPI0907670A BRPI0907670A2 BR PI0907670 A2 BRPI0907670 A2 BR PI0907670A2 BR PI0907670 A BRPI0907670 A BR PI0907670A BR PI0907670 A BRPI0907670 A BR PI0907670A BR PI0907670 A2 BRPI0907670 A2 BR PI0907670A2
Authority
BR
Brazil
Prior art keywords
aircraft structure
structure set
aircraft
Prior art date
Application number
BRPI0907670A
Other languages
English (en)
Inventor
José Antonio Estancano Ercilla
Original Assignee
Forplan Metales S A
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 Forplan Metales S A filed Critical Forplan Metales S A
Publication of BRPI0907670A2 publication Critical patent/BRPI0907670A2/pt
Publication of BRPI0907670B1 publication Critical patent/BRPI0907670B1/pt

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
    • B64C1/12—Construction or attachment of skin panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
    • 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
    • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/0004—Joining sheets, plates or panels in abutting relationship
    • F16B5/0032—Joining sheets, plates or panels in abutting relationship by moving the sheets, plates, or panels or the interlocking key parallel to the abutting edge
    • F16B5/0052—Joining sheets, plates or panels in abutting relationship by moving the sheets, plates, or panels or the interlocking key parallel to the abutting edge the interlocking key acting as a dovetail-type key
    • 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
    • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/07—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of multiple interengaging protrusions on the surfaces, e.g. hooks, coils

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Connection Of Plates (AREA)
  • Laminated Bodies (AREA)
BRPI0907670 2008-04-30 2009-04-20 conjunto de estrutura de aeronave BRPI0907670B1 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ES200801266A ES2355998B1 (es) 2008-04-30 2008-04-30 Sistema de unión entre revestimientos y elementos estructurales que los soportan.
PCT/ES2009/000212 WO2009133222A1 (es) 2008-04-30 2009-04-20 Sistema de unión entre revestimientos y elementos estructurales que los soportan

Publications (2)

Publication Number Publication Date
BRPI0907670A2 true BRPI0907670A2 (pt) 2016-11-29
BRPI0907670B1 BRPI0907670B1 (pt) 2019-12-03

Family

ID=41254795

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0907670 BRPI0907670B1 (pt) 2008-04-30 2009-04-20 conjunto de estrutura de aeronave

Country Status (12)

Country Link
US (1) US20110168842A1 (pt)
EP (1) EP2281745B1 (pt)
JP (1) JP2011518722A (pt)
CN (1) CN102046465B (pt)
BR (1) BRPI0907670B1 (pt)
CA (1) CA2723316C (pt)
ES (2) ES2355998B1 (pt)
HU (1) HUE031521T2 (pt)
PL (1) PL2281745T3 (pt)
PT (1) PT2281745T (pt)
RU (1) RU2490165C2 (pt)
WO (1) WO2009133222A1 (pt)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2371951B1 (es) * 2009-03-25 2012-11-21 Airbus Operations, S.L. Disposición de junta de elementos estructurales de un material compuesto.
CN102561168A (zh) * 2011-12-27 2012-07-11 东南大学 竹胶板梁结构
US8961059B2 (en) * 2012-09-06 2015-02-24 The Boeing Company Self-locking joints for panel structures and methods of fabricating the same
CN104131961B (zh) * 2014-08-19 2016-08-17 东莞瑞柯电子科技股份有限公司 带有可拆卸多功能启动电源的便携式空压机
US11554561B2 (en) * 2019-10-21 2023-01-17 The Boeing Company Integrally stiffened bonded panel with machined pockets and methods of manufacture

Family Cites Families (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB548572A (en) * 1941-06-19 1942-10-15 Alfred Elliott Improvements relating to members consisting of a frame covered with sheet metal
FR966996A (fr) * 1948-05-24 1950-10-23 Const Aero Navales Dispositif d'assemblage entre deux éléments d'un ensemble à surfaces unies
US3185267A (en) * 1952-07-26 1965-05-25 Pavlecka John Interlocked panel structure
US3037590A (en) * 1952-12-26 1962-06-05 Pavlecka John Interlocked panel structure
GB841923A (en) * 1957-03-01 1960-07-20 Contraves Ag Improvements in and relating to assemblies of structural elements
US2959383A (en) * 1957-12-26 1960-11-08 Pavlecka John Airfoil structure
US2959384A (en) * 1958-01-09 1960-11-08 Pavlecka John Airfoil structure
US2999658A (en) * 1958-07-16 1961-09-12 Pavlecka John Airfoil structure
US3004645A (en) * 1959-08-27 1961-10-17 Jr George E Moul Aerodynamic surface attaching structure
US3002717A (en) * 1960-01-12 1961-10-03 Pavlecka John Airfoil structure
US3160245A (en) * 1960-05-26 1964-12-08 Pavlecka John Interlocked panel structure
US3276377A (en) * 1964-11-03 1966-10-04 Jack B Bell Fin locking device
US3304677A (en) * 1964-11-30 1967-02-21 Pavlecka John Interlocked panel structure
US3296759A (en) * 1964-12-07 1967-01-10 Pavlecka John Interlocked hollow panel structure
FR2258775A7 (en) * 1974-01-23 1975-08-18 Manigand Jean Jacques Assembly device for joining panels - has separate mortise and tenon pieces fixed to adjacent panels
JPS57100279A (en) * 1980-12-15 1982-06-22 Nippon Aluminium Mfg Heat insulating mold material
JPS61119461A (ja) * 1985-01-30 1986-06-06 株式会社日立製作所 車両用内装材の支持構造
JPS6254863U (pt) * 1985-09-27 1987-04-04
JPH0644757Y2 (ja) * 1990-01-31 1994-11-16 池田物産株式会社 車両の成形天井取付構造
JPH10280556A (ja) * 1997-04-03 1998-10-20 Sunstar Eng Inc 建築物における木材の結合部強化方法
US6464170B2 (en) * 2001-03-07 2002-10-15 Lockheed Martin Corporation Aircraft and aircraft manufacturing method
JP3978361B2 (ja) * 2002-04-03 2007-09-19 株式会社アイ．エヌ．ジー 建築・土木構造用継手
GB2393927A (en) * 2002-10-09 2004-04-14 Bae Systems Plc A method of assembling components
US6871822B2 (en) * 2003-04-18 2005-03-29 The Boeing Company Apparatus and methods of attaching panels to support structures
RU33926U1 (ru) * 2003-07-31 2003-11-20 Вайнштейн Леонид Леонидович Устройство для крепления панелей пола самолета
RU2263829C2 (ru) * 2004-01-13 2005-11-10 Кузнецова Елна Юрьевна Узел соединения плоских деталей
JP2006009441A (ja) * 2004-06-28 2006-01-12 Kenichi Horio 木造建築物
US7247002B2 (en) * 2004-12-02 2007-07-24 Siemens Power Generation, Inc. Lamellate CMC structure with interlock to metallic support structure
US7578468B2 (en) * 2004-12-20 2009-08-25 Sikorsky Aircraft Corporation Acoustic absorption system for an aircraft airframe
NZ540706A (en) * 2005-06-13 2007-09-28 Cameron Grant Jones Fin for surfing apparatus
DE102005038856A1 (de) * 2005-08-17 2007-02-22 Airbus Deutschland Gmbh Kontinuierlicher Rumpfanschluss
DE102007004554B4 (de) * 2007-01-30 2015-08-27 Airbus Operations Gmbh Schiene zur Positionierung und Arretierung von Bauteilen und eines dazugehörigen Fittings

Also Published As

Publication number Publication date
ES2355998B1 (es) 2012-02-27
EP2281745B1 (en) 2016-10-05
WO2009133222A1 (es) 2009-11-05
RU2010148870A (ru) 2012-06-10
US20110168842A1 (en) 2011-07-14
PT2281745T (pt) 2017-01-13
EP2281745A4 (en) 2015-08-19
CA2723316C (en) 2013-06-04
PL2281745T3 (pl) 2017-08-31
CN102046465B (zh) 2013-10-16
JP2011518722A (ja) 2011-06-30
CN102046465A (zh) 2011-05-04
ES2355998A1 (es) 2011-04-04
HUE031521T2 (en) 2017-07-28
RU2490165C2 (ru) 2013-08-20
ES2611462T3 (es) 2017-05-09
BRPI0907670B1 (pt) 2019-12-03
CA2723316A1 (en) 2009-11-05
EP2281745A1 (en) 2011-02-09

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06T Formal requirements before examination [chapter 6.20 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 10 (DEZ) ANOS CONTADOS A PARTIR DE 03/12/2019, OBSERVADAS AS CONDICOES LEGAIS. (CO) 10 (DEZ) ANOS CONTADOS A PARTIR DE 03/12/2019, OBSERVADAS AS CONDICOES LEGAIS