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IT1392320B1 - Bordo d'attacco per ali ed impennaggi di aeromobili - Google Patents

Bordo d'attacco per ali ed impennaggi di aeromobili

Info

Publication number
IT1392320B1
IT1392320B1 ITTO2008A000912A ITTO20080912A IT1392320B1 IT 1392320 B1 IT1392320 B1 IT 1392320B1 IT TO2008A000912 A ITTO2008A000912 A IT TO2008A000912A IT TO20080912 A ITTO20080912 A IT TO20080912A IT 1392320 B1 IT1392320 B1 IT 1392320B1
Authority
IT
Italy
Prior art keywords
layer
wings
aircraft makes
attack edge
securely fixed
Prior art date
Application number
ITTO2008A000912A
Other languages
English (en)
Inventor
Luigi Capasso
Giovanni Sagnella
Massimo Ricco
Marco Fassero
Salvatore Russo
Original Assignee
Alenia Aeronautica Spa
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 Alenia Aeronautica Spa filed Critical Alenia Aeronautica Spa
Priority to ITTO2008A000912A priority Critical patent/IT1392320B1/it
Priority to JP2009263592A priority patent/JP5424830B2/ja
Priority to AT09177579T priority patent/ATE532626T1/de
Priority to ES09177579T priority patent/ES2376089T3/es
Priority to EP09177579A priority patent/EP2196309B1/en
Priority to US12/634,402 priority patent/US8245972B2/en
Publication of ITTO20080912A1 publication Critical patent/ITTO20080912A1/it
Application granted granted Critical
Publication of IT1392320B1 publication Critical patent/IT1392320B1/it

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/28Leading or trailing edges attached to primary structures, e.g. forming fixed slots
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00Layered products comprising a layer of metal
    • B32B15/14Layered products comprising a layer of metal next to a fibrous or filamentary layer
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00Layered products comprising a layer of metal
    • B32B15/20Layered products comprising a layer of metal comprising aluminium or copper
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/02Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/10Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
    • B32B3/12Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04Interconnection of layers
    • B32B7/12Interconnection of layers using interposed adhesives or interposed materials with bonding properties
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2250/00Layers arrangement
    • B32B2250/044 layers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10Inorganic fibres
    • B32B2262/101Glass fibres
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2605/00Vehicles
    • B32B2605/18Aircraft
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24149Honeycomb-like

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
  • Transition And Organic Metals Composition Catalysts For Addition Polymerization (AREA)
  • Window Of Vehicle (AREA)
  • Confectionery (AREA)
  • Vibration Dampers (AREA)
ITTO2008A000912A 2008-12-09 2008-12-09 Bordo d'attacco per ali ed impennaggi di aeromobili IT1392320B1 (it)

Priority Applications (6)

Application Number Priority Date Filing Date Title
ITTO2008A000912A IT1392320B1 (it) 2008-12-09 2008-12-09 Bordo d'attacco per ali ed impennaggi di aeromobili
JP2009263592A JP5424830B2 (ja) 2008-12-09 2009-11-19 航空機の翼及び尾部の前縁
AT09177579T ATE532626T1 (de) 2008-12-09 2009-12-01 Flügel- und leitwerkvorderkante
ES09177579T ES2376089T3 (es) 2008-12-09 2009-12-01 Borde de ataque para empenajes y alas de aeronave.
EP09177579A EP2196309B1 (en) 2008-12-09 2009-12-01 Leading edge for aircraft wings and empennages
US12/634,402 US8245972B2 (en) 2008-12-09 2009-12-09 Leading edge for aircraft wings and empennages

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ITTO2008A000912A IT1392320B1 (it) 2008-12-09 2008-12-09 Bordo d'attacco per ali ed impennaggi di aeromobili

Publications (2)

Publication Number Publication Date
ITTO20080912A1 ITTO20080912A1 (it) 2010-06-10
IT1392320B1 true IT1392320B1 (it) 2012-02-24

Family

ID=40908394

Family Applications (1)

Application Number Title Priority Date Filing Date
ITTO2008A000912A IT1392320B1 (it) 2008-12-09 2008-12-09 Bordo d'attacco per ali ed impennaggi di aeromobili

Country Status (6)

Country Link
US (1) US8245972B2 (it)
EP (1) EP2196309B1 (it)
JP (1) JP5424830B2 (it)
AT (1) ATE532626T1 (it)
ES (1) ES2376089T3 (it)
IT (1) IT1392320B1 (it)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101269553B (zh) * 2008-05-09 2010-12-08 大连交通大学 镁合金蜂窝板及其生产工艺
ITMI20080886A1 (it) * 2008-05-15 2009-11-16 Alenia Aermacchi Spa Giunto per indurre elevate cadute di temperatura tra parti collegate su un velivolo
CN102030102B (zh) * 2010-11-18 2013-05-08 西北工业大学 一种抗鸟撞飞机平尾前缘
KR101347369B1 (ko) * 2011-09-02 2014-01-07 삼성중공업 주식회사 풍력터빈용 블레이드 및 이를 갖춘 풍력터빈
US9434466B2 (en) 2011-11-30 2016-09-06 Airbus Sas Component having a box structure for an airplane airfoil
GB201120707D0 (en) * 2011-12-01 2012-01-11 Airbus Operations Ltd Leading edge structure
US9708030B1 (en) * 2011-12-08 2017-07-18 The Boeing Company Impact-energy tolerant method and structures
US8968437B2 (en) * 2012-05-02 2015-03-03 Michael J Kline Jet engine with deflector
FR2993857B1 (fr) * 2012-07-26 2015-03-27 Airbus Operations Sas Dispositif de protection d'une structure de longeron avant d'un caisson central d'aile d'aeronef et d'au moins un equipement situe dans ladite aile
CN103057690A (zh) * 2012-12-21 2013-04-24 中国商用飞机有限责任公司 一种飞机翼面前缘结构
CN104002977B (zh) * 2014-05-06 2017-01-18 嘉兴美盾航空材料有限公司 防鸟撞挡板及其制备工艺
US9896190B1 (en) * 2014-05-07 2018-02-20 The Boeing Company Wing leading edge architecture suitable for laminar flow
US9592898B1 (en) 2014-10-22 2017-03-14 Allen L. Davies, Jr. Airframe
CN105048102B (zh) * 2015-06-10 2018-01-19 湖北三江航天江北机械工程有限公司 锥桶形防热罩内壁粘接吸波贴片和铝箔的方法
US11274653B2 (en) 2016-09-27 2022-03-15 Siemens Gamesa Renewable Energy A/S Protective cover system
ES2822933T3 (es) * 2016-11-04 2021-05-05 Airbus Operations Sl Estructura de panel para una aeronave y procedimiento de fabricación de la misma
US10556701B2 (en) * 2017-04-14 2020-02-11 Rohr, Inc. Bird-strike energy absorbing net
FR3070369B1 (fr) * 2017-08-30 2019-08-23 Airbus Operations Procede de fabrication d'un panneau d'un bord d'attaque d'aeronef permettant d'obtenir un ecoulement laminaire etendu, bord d'attaque comprenant au moins un panneau obtenu a partir dudit procede
DE102017128497A1 (de) 2017-11-30 2019-06-06 Airbus Operations Gmbh Vorderkantenanordnung für einen Strömungskörper eines Fahrzeugs

Family Cites Families (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL89352C (it) * 1957-02-20 1900-01-01
US3097982A (en) * 1960-06-06 1963-07-16 Eugene M Stoner Method of fabricating airfoils
GB1120381A (en) * 1964-07-07 1968-07-17 Handley Page Ltd Improvements in or relating to the manufacture of aerodynamic structures
US3490983A (en) * 1965-05-17 1970-01-20 Hitco Fiber reinforced structures and methods of making the same
US4411380A (en) * 1981-06-30 1983-10-25 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Metal matrix composite structural panel construction
US4599255A (en) * 1981-12-28 1986-07-08 The Boeing Company Composite structures having conductive surfaces
US4542056A (en) * 1983-08-26 1985-09-17 The Boeing Company Composite structure having conductive surfaces
WO1985001489A1 (en) * 1983-09-29 1985-04-11 The Boeing Company High strength to weight horizontal and vertical aircraft stabilizer
FR2616409B1 (fr) * 1987-06-09 1989-09-15 Aerospatiale Pale en materiaux composites et son procede de fabrication
DE3816582A1 (de) * 1988-05-15 1989-11-23 Messerschmitt Boelkow Blohm Verfahren zur herstellung eines einbauelementes und einbauelement
US4879152A (en) * 1989-02-15 1989-11-07 Green Patrick H Composite panel structure
US5106668A (en) * 1989-06-07 1992-04-21 Hexcel Corporation Multi-layer honeycomb structure
US5123814A (en) * 1990-07-27 1992-06-23 The Marley Cooling Tower Company Industrial cooling tower fan blade having abrasion resistant leading edge
US5567500A (en) * 1991-08-07 1996-10-22 Speciality Cellular Products Company Composite honeycomb core structure comprising cell walls constructed of at least three unidirectional fiber layers or at least two unidirectional fiber layers and a random fiber layer
US5445861A (en) * 1992-09-04 1995-08-29 The Boeing Company Lightweight honeycomb panel structure
US5344280A (en) * 1993-05-05 1994-09-06 General Electric Company Impact resistant fan case liner
JPH07165197A (ja) * 1993-12-14 1995-06-27 Nec Corp 衛星用ハニカムパネル
US5604010A (en) * 1996-01-11 1997-02-18 Hartz; Dale E. Composite honeycomb sandwich structure
US5685940A (en) * 1996-03-20 1997-11-11 The Boeing Company Adhering tiedown plies in composite construction
US5789060A (en) * 1996-07-29 1998-08-04 Specialty Cellular Products Company Heat conduction honeycomb core
US6180206B1 (en) * 1997-09-19 2001-01-30 The Boeing Company Composite honeycomb sandwich panel for fixed leading edges
US6612217B1 (en) * 1998-06-02 2003-09-02 Sri International Penetration resistant fabric structures and materials
US6568310B2 (en) * 2001-10-25 2003-05-27 Timothy W. Morgan Lightweight armored panels and doors
US20050175813A1 (en) * 2004-02-10 2005-08-11 Wingert A. L. Aluminum-fiber laminate
US7988809B2 (en) * 2004-09-01 2011-08-02 Hexcel Corporation Aircraft floor and interior panels using edge coated honeycomb
JP2007170328A (ja) * 2005-12-26 2007-07-05 Toray Ind Inc 風力発電用風車翼およびその製造方法
US7628358B2 (en) * 2006-10-26 2009-12-08 The Boeing Company Wing panel structure
US7866605B2 (en) * 2007-04-24 2011-01-11 The Boeing Company Energy absorbing impact band and method

Also Published As

Publication number Publication date
ITTO20080912A1 (it) 2010-06-10
JP5424830B2 (ja) 2014-02-26
EP2196309A1 (en) 2010-06-16
US8245972B2 (en) 2012-08-21
ES2376089T3 (es) 2012-03-08
US20100140405A1 (en) 2010-06-10
EP2196309B1 (en) 2011-11-09
ATE532626T1 (de) 2011-11-15
JP2010137850A (ja) 2010-06-24

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