IT1392320B1 - Bordo d'attacco per ali ed impennaggi di aeromobili - Google Patents
Bordo d'attacco per ali ed impennaggi di aeromobiliInfo
- 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
Links
- 239000002184 metal Substances 0.000 abstract 2
- 239000011152 fibreglass Substances 0.000 abstract 1
- 239000011888 foil Substances 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/28—Leading or trailing edges attached to primary structures, e.g. forming fixed slots
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/14—Layered products comprising a layer of metal next to a fibrous or filamentary layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/20—Layered products comprising a layer of metal comprising aluminium or copper
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered 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
- B32B3/02—Layered 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered 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
- B32B3/10—Layered 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
- B32B3/12—Layered 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B7/00—Layered 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
- B32B7/04—Interconnection of layers
- B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2250/00—Layers arrangement
- B32B2250/04—4 layers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/101—Glass fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2605/00—Vehicles
- B32B2605/18—Aircraft
-
- 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.]
- Y10T428/24149—Honeycomb-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)
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)
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)
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 |
-
2008
- 2008-12-09 IT ITTO2008A000912A patent/IT1392320B1/it active
-
2009
- 2009-11-19 JP JP2009263592A patent/JP5424830B2/ja not_active Expired - Fee Related
- 2009-12-01 AT AT09177579T patent/ATE532626T1/de active
- 2009-12-01 EP EP09177579A patent/EP2196309B1/en active Active
- 2009-12-01 ES ES09177579T patent/ES2376089T3/es active Active
- 2009-12-09 US US12/634,402 patent/US8245972B2/en not_active Expired - Fee Related
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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