FR3003233B1 - Panneau de voilure pour aeronef - Google Patents
Panneau de voilure pour aeronefInfo
- Publication number
- FR3003233B1 FR3003233B1 FR1352381A FR1352381A FR3003233B1 FR 3003233 B1 FR3003233 B1 FR 3003233B1 FR 1352381 A FR1352381 A FR 1352381A FR 1352381 A FR1352381 A FR 1352381A FR 3003233 B1 FR3003233 B1 FR 3003233B1
- Authority
- FR
- France
- Prior art keywords
- aircraft
- panel
- 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
Links
Classifications
-
- 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
-
- 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
- B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B15/08—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
-
- 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
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/06—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B27/08—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
-
- 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
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/18—Layered products comprising a layer of synthetic resin characterised by the use of special additives
- B32B27/20—Layered products comprising a layer of synthetic resin characterised by the use of special additives using fillers, pigments, thixotroping agents
-
- 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
- B32B3/04—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 characterised by at least one layer folded at the edge, e.g. over another layer ; characterised by at least one layer enveloping or enclosing a material
-
- 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
- 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
- B32B3/26—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 particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
- B32B3/266—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 particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer characterised by an apertured layer, the apertures going through the whole thickness of the layer, e.g. expanded metal, perforated layer, slit layer regular cells B32B3/12
-
- 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
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/02—Mounting or supporting thereof
-
- 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
- B32B2262/106—Carbon fibres, e.g. graphite 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
-
- 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
- B32B3/06—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 for securing layers together; for attaching the product to another member, e.g. to a support, or to another product, e.g. groove/tongue, interlocking
-
- 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
- B32B3/18—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 an internal layer formed of separate pieces of material which are juxtaposed side-by-side
-
- 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
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/18—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by features of a layer of foamed material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/20—Integral or sandwich constructions
-
- 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
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/08—Stabilising surfaces mounted on, or supported by, wings
-
- 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
- Y10T428/16—Two dimensionally sectional layer
- Y10T428/163—Next to unitary web or sheet of equal or greater extent
-
- 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.]
- Y10T428/24008—Structurally defined web or sheet [e.g., overall dimension, etc.] including fastener for attaching to external surface
-
- 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.]
- Y10T428/24174—Structurally defined web or sheet [e.g., overall dimension, etc.] including sheet or component perpendicular to plane of 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.]
- Y10T428/24273—Structurally defined web or sheet [e.g., overall dimension, etc.] including aperture
- Y10T428/24322—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
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249923—Including interlaminar mechanical fastener
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Connection Of Plates (AREA)
- Laminated Bodies (AREA)
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1352381A FR3003233B1 (fr) | 2013-03-18 | 2013-03-18 | Panneau de voilure pour aeronef |
| US14/197,945 US9415855B2 (en) | 2013-03-18 | 2014-03-05 | Wing panel for aircraft |
| CN201410101378.0A CN104058088B (zh) | 2013-03-18 | 2014-03-18 | 用于飞行器的翼板 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1352381A FR3003233B1 (fr) | 2013-03-18 | 2013-03-18 | Panneau de voilure pour aeronef |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR3003233A1 FR3003233A1 (fr) | 2014-09-19 |
| FR3003233B1 true FR3003233B1 (fr) | 2016-05-06 |
Family
ID=48613893
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR1352381A Active FR3003233B1 (fr) | 2013-03-18 | 2013-03-18 | Panneau de voilure pour aeronef |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US9415855B2 (fr) |
| CN (1) | CN104058088B (fr) |
| FR (1) | FR3003233B1 (fr) |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| AT517198B1 (de) * | 2015-04-24 | 2021-12-15 | Facc Ag | Steuerflächenelement für ein Flugzeug |
| FR3036373B1 (fr) * | 2015-05-21 | 2019-01-25 | Arianegroup Sas | Structure sandwich a prolongement formant une structure complementaire |
| US10179640B2 (en) * | 2016-08-24 | 2019-01-15 | The Boeing Company | Wing and method of manufacturing |
| US10773789B2 (en) * | 2017-07-07 | 2020-09-15 | The Boeing Company | Skin-panel interface of an aircraft |
| CN108099276B (zh) * | 2017-11-16 | 2020-12-01 | 中国航空工业集团公司西安飞机设计研究所 | 一种复合材料夹芯结构及其制造方法 |
| RU2687229C1 (ru) * | 2018-10-01 | 2019-05-07 | Михаил Борисович Жуков | Ребристая трехслойная панель |
Family Cites Families (48)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2327585A (en) * | 1939-08-04 | 1943-08-24 | Budd Edward G Mfg Co | Bolt spacer or reinforcing member |
| US2607447A (en) * | 1946-02-26 | 1952-08-19 | Us Plywood Corp | Fastener |
| US2585557A (en) * | 1946-04-19 | 1952-02-12 | Lockheed Aircraft Corp | Fastening means for structural sandwiches |
| US2484141A (en) * | 1947-01-09 | 1949-10-11 | United Aircraft Corp | Skin stressed laminated fiberglas rotor blade |
| US2961760A (en) * | 1956-03-26 | 1960-11-29 | Boeing Co | Structural sandwich spacer assemblies |
| US2967593A (en) * | 1958-01-29 | 1961-01-10 | Delron Company Inc | Structural spacer |
| US3020986A (en) * | 1958-08-18 | 1962-02-13 | Gen Dynamics Corp | Composite structural panel |
| US3137887A (en) * | 1962-06-15 | 1964-06-23 | Republic Aviat Corp | Bushing |
| US3193221A (en) * | 1962-11-13 | 1965-07-06 | Hiller Aircraft Company Inc | Aircraft landing gear strut structure |
| US3526072A (en) * | 1968-03-29 | 1970-09-01 | James R Campbell | Load distributing system for panels incorporating honeycomb core |
| US3716092A (en) * | 1970-04-14 | 1973-02-13 | Illinois Tool Works | Panel insert and method of installation |
| US3813186A (en) * | 1972-10-10 | 1974-05-28 | Textron Inc | Rotor blade shear reinforcement |
| US3987983A (en) * | 1974-12-20 | 1976-10-26 | The Boeing Company | Trailing edge flaps having spanwise aerodynamic slot opening and closing mechanism |
| US4000870A (en) * | 1975-09-08 | 1977-01-04 | Western Gear Corporation | Modular system for quick conversion of aircraft passenger compartments to cargo baggage/compartments |
| US4211046A (en) * | 1977-08-15 | 1980-07-08 | Transco, Inc. | Acoustical panel mounting element |
| DE2840807C2 (de) * | 1978-09-20 | 1981-12-17 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Krafteinleitungselement für ein Sandwichbauteil |
| US5346367A (en) * | 1984-12-21 | 1994-09-13 | United Technologies Corporation | Advanced composite rotor blade |
| US5098043A (en) * | 1990-02-27 | 1992-03-24 | Grumman Aerospace Corporation | Integrated power hinge actuator |
| JPH05116267A (ja) * | 1991-04-22 | 1993-05-14 | Mitsubishi Electric Corp | インサート付サンドイツチ板の製造方法 |
| US5224670A (en) * | 1991-09-13 | 1993-07-06 | Grumman Aerospace Corporation | Composite focused load control surface |
| JPH05154956A (ja) * | 1991-12-05 | 1993-06-22 | Sekisui Chem Co Ltd | 板状複合体 |
| US5865397A (en) * | 1995-12-05 | 1999-02-02 | The Boeing Company | Method and apparatus for creating detail surfaces on composite aircraft structures |
| JPH09300501A (ja) * | 1996-05-15 | 1997-11-25 | Nippon Light Metal Co Ltd | ハニカムパネル |
| JPH1016098A (ja) * | 1996-07-08 | 1998-01-20 | Nippon Light Metal Co Ltd | ハニカムパネル |
| JP3732587B2 (ja) * | 1996-08-30 | 2006-01-05 | 株式会社アイ・エイチ・アイ・エアロスペース | 架台パネルの製造方法 |
| JPH10180914A (ja) * | 1996-12-25 | 1998-07-07 | Nippon Light Metal Co Ltd | ハニカムパネル |
| US6055790A (en) * | 1998-05-18 | 2000-05-02 | The United States Of America As Represented By The Secretary Of The Air Force | Thermal conductive insert for sandwich structures |
| BE1013181A5 (fr) * | 1999-12-17 | 2001-10-02 | Sonaca Sa | Jonction composite pour le montage d'au moins un organe exterieur sur un panneau sandwich, et panneau integrant au moins une telle jonction. |
| US6530191B2 (en) * | 2001-07-13 | 2003-03-11 | Carrier Corporation | Support panel for air handling unit |
| US7197852B2 (en) * | 2002-09-20 | 2007-04-03 | The Boeing Company | Internally stiffened composite panels and methods for their manufacture |
| DE502004009977D1 (de) * | 2003-09-08 | 2009-10-08 | Evonik Roehm Gmbh | Krafteinleitungsstelle in kernverbunden und verfahren zu ihrer herstellung mit in dickenrichtung des kernverbundes durchsetzenden armierungselementen |
| EP1533433A1 (fr) * | 2003-11-24 | 2005-05-25 | Aalborg Universitet | Panneau sandwich et procédé de sa fabrication |
| US8506743B2 (en) * | 2004-03-17 | 2013-08-13 | Airbus Deutschland Gmbh | Composite sandwich structure with integrated reinforcement area and method of producing the same |
| US7666493B2 (en) * | 2004-03-17 | 2010-02-23 | Airbus Deutschland Gmbh | Locally reinforced core structure for composite sandwich structure and method of producing the same |
| FR2891325B1 (fr) * | 2005-09-28 | 2007-10-26 | Airbus France Sas | Dispositif pour la fixation d'un panneau leger sur un support |
| JP4736795B2 (ja) * | 2005-12-26 | 2011-07-27 | トヨタ自動車株式会社 | 繊維強化プラスチック構造体 |
| FR2905739B1 (fr) * | 2006-09-08 | 2008-11-07 | Airbus France Sas | Assemblage de panneaux et procede de montage d'un assemblage de panneaux |
| GB0624208D0 (en) * | 2006-12-04 | 2007-01-10 | Airbus Uk Ltd | Composite structure |
| US8418962B2 (en) * | 2008-01-19 | 2013-04-16 | The Boeing Company | Distribution of point loads in honeycomb panels |
| GB0805963D0 (en) * | 2008-04-02 | 2008-05-07 | Airbus Uk Ltd | Aircraft structure |
| DE102008041788A1 (de) * | 2008-09-03 | 2010-03-11 | Airbus Deutschland Gmbh | Sandwichplatte mit integrierter Verstärkungsstruktur sowie Verfahren zu deren Herstellung |
| JP5195654B2 (ja) * | 2009-06-11 | 2013-05-08 | トヨタ自動車株式会社 | 取付部構造 |
| JP5532895B2 (ja) * | 2009-12-15 | 2014-06-25 | 横浜ゴム株式会社 | 航空機用の化粧室ユニット |
| DE102009058359A1 (de) * | 2009-12-15 | 2011-06-16 | Airbus Operations Gmbh | Krafteinleitungsbeschlag für Leichtbaukomponenten |
| GB201004757D0 (en) * | 2010-03-23 | 2010-05-05 | Airbus Operations Ltd | Joint |
| JP4865907B1 (ja) * | 2010-12-29 | 2012-02-01 | ジェイ・バス株式会社 | 組合せハニカムピース構造によるハニカムパネル |
| JPWO2013030960A1 (ja) * | 2011-08-30 | 2015-03-23 | 株式会社日立製作所 | 複合材への部品の締結構造 |
| WO2013030960A1 (fr) * | 2011-08-30 | 2013-03-07 | 株式会社日立製作所 | Structure d'assemblage d'une pièce avec un matériau composite |
-
2013
- 2013-03-18 FR FR1352381A patent/FR3003233B1/fr active Active
-
2014
- 2014-03-05 US US14/197,945 patent/US9415855B2/en active Active
- 2014-03-18 CN CN201410101378.0A patent/CN104058088B/zh active Active
Also Published As
| Publication number | Publication date |
|---|---|
| US9415855B2 (en) | 2016-08-16 |
| CN104058088A (zh) | 2014-09-24 |
| CN104058088B (zh) | 2017-01-18 |
| FR3003233A1 (fr) | 2014-09-19 |
| US20140272264A1 (en) | 2014-09-18 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB201314959D0 (en) | Panel for an aircraft | |
| CL2014000003S1 (es) | Automovil | |
| EP3090813C0 (fr) | Panneau | |
| GB201306247D0 (en) | Formwork Panel | |
| DK3016802T3 (da) | Flerlags panel | |
| UA29168S (uk) | Автомобіль | |
| DK3083173T3 (da) | Panel | |
| CL2014000155S1 (es) | Automovil | |
| GB201303507D0 (en) | Assays | |
| FR3004161B1 (fr) | Vitrage pour aeronef spatial | |
| FR3003233B1 (fr) | Panneau de voilure pour aeronef | |
| DK3071355T3 (da) | Spidsforsænker | |
| FR3001551B1 (fr) | Panneau imprime retro-eclaire | |
| DE102014109969A8 (de) | Armaturenbrettstruktur | |
| GB201323006D0 (en) | Panel | |
| FR2999636B1 (fr) | Serrure pour aeronef | |
| DE112013007456A5 (de) | Verbundplatte | |
| FR3014968B1 (fr) | Insert filete pour panneau sandwich | |
| FR3009279B1 (fr) | Ensemble propulsif pour aeronef | |
| FR3005697B1 (fr) | Ensemble propulsif pour aeronef | |
| FR3003539B1 (fr) | Structure anti-erosion pour aeronefs | |
| FR3005058B1 (fr) | Composition de pre-melange pour bitumes | |
| GB201323145D0 (en) | Panel craft | |
| FI10012U1 (fi) | Paneelirakenne | |
| UA28705S (uk) | Облицювальна панель |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PLFP | Fee payment |
Year of fee payment: 3 |
|
| PLFP | Fee payment |
Year of fee payment: 4 |
|
| PLFP | Fee payment |
Year of fee payment: 5 |
|
| PLFP | Fee payment |
Year of fee payment: 6 |
|
| PLFP | Fee payment |
Year of fee payment: 8 |
|
| PLFP | Fee payment |
Year of fee payment: 9 |
|
| PLFP | Fee payment |
Year of fee payment: 10 |
|
| PLFP | Fee payment |
Year of fee payment: 11 |
|
| PLFP | Fee payment |
Year of fee payment: 12 |
|
| PLFP | Fee payment |
Year of fee payment: 13 |