ATE524378T1 - Integral gedämpfte verbundflugzeugbodenplatten - Google Patents
Integral gedämpfte verbundflugzeugbodenplattenInfo
- Publication number
- ATE524378T1 ATE524378T1 AT06827499T AT06827499T ATE524378T1 AT E524378 T1 ATE524378 T1 AT E524378T1 AT 06827499 T AT06827499 T AT 06827499T AT 06827499 T AT06827499 T AT 06827499T AT E524378 T1 ATE524378 T1 AT E524378T1
- Authority
- AT
- Austria
- Prior art keywords
- integral
- aircraft floor
- core surface
- floor panels
- composite aircraft
- Prior art date
Links
- 239000002131 composite material Substances 0.000 title 1
- 238000013016 damping Methods 0.000 abstract 2
- 239000003822 epoxy resin Substances 0.000 abstract 2
- 239000000463 material Substances 0.000 abstract 2
- 229920000647 polyepoxide Polymers 0.000 abstract 2
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
- B64C1/18—Floors
-
- 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
- B32B27/38—Layered products comprising a layer of synthetic resin comprising epoxy resins
-
- 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
- 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
- B32B5/22—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/26—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
-
- 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
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/02—Composition of the impregnated, bonded or embedded layer
- B32B2260/021—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
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/02—Composition of the impregnated, bonded or embedded layer
- B32B2260/021—Fibrous or filamentary layer
- B32B2260/023—Two or more 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
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/04—Impregnation, embedding, or binder material
- B32B2260/046—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
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/02—Synthetic macromolecular fibres
- B32B2262/0261—Polyamide fibres
- B32B2262/0269—Aromatic polyamide 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
- 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
- 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
- B32B2307/00—Properties of the layers or laminate
- B32B2307/10—Properties of the layers or laminate having particular acoustical properties
- B32B2307/102—Insulating
-
- 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
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/54—Yield strength; Tensile strength
-
- 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
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/56—Damping, energy absorption
-
- 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
- B32B2419/00—Buildings or parts thereof
- B32B2419/04—Tiles for floors or walls
-
- 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
- B32B2605/003—Interior finishings
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Laminated Bodies (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US11/163,957 US7419031B2 (en) | 2005-11-04 | 2005-11-04 | Integrally damped composite aircraft floor panels |
| PCT/US2006/043076 WO2007056204A1 (en) | 2005-11-04 | 2006-11-02 | Integrally damped composite aircraft floor panels |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE524378T1 true ATE524378T1 (de) | 2011-09-15 |
Family
ID=37847082
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT06827499T ATE524378T1 (de) | 2005-11-04 | 2006-11-02 | Integral gedämpfte verbundflugzeugbodenplatten |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US7419031B2 (de) |
| EP (1) | EP1948503B1 (de) |
| AT (1) | ATE524378T1 (de) |
| WO (1) | WO2007056204A1 (de) |
Families Citing this family (38)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7837147B2 (en) | 2005-03-18 | 2010-11-23 | The Boeing Company | Systems and methods for reducing noise in aircraft fuselages and other structures |
| US9511571B2 (en) | 2007-01-23 | 2016-12-06 | The Boeing Company | Composite laminate having a damping interlayer and method of making the same |
| US8029642B2 (en) | 2007-07-27 | 2011-10-04 | The Boeing Company | Tape removal apparatus and process |
| JP2009062977A (ja) * | 2007-08-15 | 2009-03-26 | Rohr Inc | 線形音響ライナー |
| US8345269B2 (en) | 2007-09-22 | 2013-01-01 | The Boeing Company | Method and apparatus for measuring the width of composite tape |
| US7922856B2 (en) | 2008-01-02 | 2011-04-12 | The Boeing Company | Graphite tape supply and backing paper take-up apparatus |
| US8079443B2 (en) * | 2008-01-07 | 2011-12-20 | Pelzer Acoustic Products Gmbh | Aircraft trim panel with integrated adjustable acoustic properties |
| US8292214B2 (en) * | 2008-01-18 | 2012-10-23 | The Boeing Company | Vibration damping for wing-to-body aircraft fairing |
| US8056850B2 (en) * | 2008-01-18 | 2011-11-15 | The Boeing Company | Particle-filled wing-to-body fairing and method for reducing fairing vibrations |
| US8557074B2 (en) | 2008-02-27 | 2013-10-15 | The Boeing Company | Reduced complexity automatic fiber placement apparatus and method |
| US8986482B2 (en) * | 2008-07-08 | 2015-03-24 | The Boeing Company | Method and apparatus for producing composite structures |
| CA2748926C (en) * | 2009-01-06 | 2017-06-27 | Cytec Technology Corp. | Structural composite material with improved acoustic and vibrational damping properties |
| US8308101B2 (en) | 2009-03-09 | 2012-11-13 | The Boeing Company | Simplified fiber tensioning for automated fiber placement machines |
| US8454788B2 (en) * | 2009-03-13 | 2013-06-04 | The Boeing Company | Method and apparatus for placing short courses of composite tape |
| US8425710B2 (en) | 2009-03-13 | 2013-04-23 | The Boeing Company | Automated placement of vibration damping materials |
| US8127889B1 (en) * | 2009-09-15 | 2012-03-06 | The Boeing Company | Noise reduction system for structures |
| WO2011108677A1 (ja) * | 2010-03-04 | 2011-09-09 | Jx日鉱日石エネルギー株式会社 | 炭素繊維強化プラスチック成形体 |
| US8156710B1 (en) * | 2010-11-19 | 2012-04-17 | Advance Vinyl Floor Manufacturing Corp. | Method and apparatus for floor tiles and planks |
| US8808490B2 (en) | 2011-08-04 | 2014-08-19 | The Boeing Company | Methods for laminating composites |
| EP2596946B1 (de) | 2011-11-22 | 2014-03-19 | Eurocopter Deutschland GmbH | Luftfahrzeug mit Antirutsch- und Gasabdichtungs-Verbundboden |
| US8770343B2 (en) * | 2011-11-23 | 2014-07-08 | The Boeing Company | Noise reduction system for composite structures |
| EP2610052A1 (de) * | 2011-12-30 | 2013-07-03 | AGUSTAWESTLAND S.p.A. | Innere Verkleidungstafel eines Luftfahrzeugs, und mit solchen Tafeln ausgestattetes Luftfahrzeug |
| EP2674091A1 (de) | 2012-06-13 | 2013-12-18 | Nitto Europe N.V | Wabenbasierter Hochtemperatur-Strukturdämpfer |
| US8882089B2 (en) | 2012-08-17 | 2014-11-11 | Itt Manufacturing Enterprises Llc | Dual radius isolator |
| US9067374B2 (en) | 2012-11-30 | 2015-06-30 | The Boeing Company | Method and apparatus for applying film material to elongate members |
| US9676160B2 (en) | 2012-11-30 | 2017-06-13 | The Boeing Company | Holding system for elongate members |
| US8800245B1 (en) | 2013-03-27 | 2014-08-12 | Advancecd Vinyl Floor Manufacturing Corp. | Method and apparatus for floor tiles and planks |
| US9010053B1 (en) | 2014-01-28 | 2015-04-21 | Robert Jeffrey Kupferberg | High strength thermal barrier panel for an H.V.A.C. unit housing |
| US9725154B2 (en) * | 2014-05-13 | 2017-08-08 | The Boeing Company | Method and apparatus for reducing structural vibration and noise |
| US10160533B2 (en) * | 2014-09-23 | 2018-12-25 | The Boeing Company | Aircraft cabin pressure regulating subfloor |
| US9469985B1 (en) * | 2015-05-11 | 2016-10-18 | Hexcel Corporation | Acoustic structures with multiple degrees of freedom |
| US9741331B1 (en) | 2016-06-01 | 2017-08-22 | The Boeing Company | Sound-attenuating composite structure |
| US11043198B1 (en) * | 2017-05-31 | 2021-06-22 | Navy Island, Inc. | Acoustical panel subsurface layer |
| CN107804046B (zh) * | 2017-09-18 | 2019-11-12 | 航天材料及工艺研究所 | 一种复合材料消音降噪声衬及其制备方法 |
| US11052987B2 (en) * | 2018-05-30 | 2021-07-06 | The Boeing Company | Integrally damped composite aircraft floor panels |
| US11168485B2 (en) * | 2018-09-15 | 2021-11-09 | VBBT Corp. | Low cost emergency housing |
| US11459085B2 (en) * | 2019-04-30 | 2022-10-04 | Textron Innovations Inc. | Energy attenuation stabilizers and methods |
| FR3156751A1 (fr) * | 2023-12-14 | 2025-06-20 | Airbus Operations (S.A.S.) | Dispositif d’absorption d’énergie par compression, aéronef comprenant au moins un tel dispositif |
Family Cites Families (26)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3502171A (en) * | 1968-05-31 | 1970-03-24 | Boeing Co | Composite laminar structure for noise attenuation of fast moving gas streams,and method of making the same |
| US3977492A (en) * | 1975-01-09 | 1976-08-31 | Acon, Inc. | Acoustical material for use in association with noise generating machinery |
| US4111081A (en) * | 1976-01-02 | 1978-09-05 | The Boeing Company | Low non-linearity factor sound attenuating laminate |
| SE420750B (sv) * | 1978-11-17 | 1981-10-26 | Ingemanssons Ingenjorsbyra Ab | Ljudisolerande byggnadselement med stor styvhet |
| US4301890A (en) * | 1979-12-06 | 1981-11-24 | Lord Corporation | Sound-absorbing panel |
| US4416349A (en) * | 1981-09-30 | 1983-11-22 | The Boeing Company | Viscoelastically damped reinforced skin structures |
| US4425980A (en) * | 1981-12-14 | 1984-01-17 | The Boeing Company | Beam dampers for damping the vibrations of the skin of reinforced structures |
| US4641726A (en) * | 1983-04-20 | 1987-02-10 | Peabody Noise Control, Inc. | Composite structure and method of manufacturing it |
| JPS6112334A (ja) * | 1984-06-29 | 1986-01-20 | 川崎製鉄株式会社 | 複合型制振積層体 |
| US5151311A (en) * | 1987-11-02 | 1992-09-29 | Grumman Aerospace Corporation | Acoustic attenuating liner and method of making same |
| US5068001A (en) * | 1987-12-16 | 1991-11-26 | Reinhold Haussling | Method of making a sound absorbing laminate |
| GB8817669D0 (en) * | 1988-07-25 | 1988-09-01 | Short Brothers Ltd | Means for attenuating sound energy |
| GB9101355D0 (en) * | 1991-01-22 | 1991-03-06 | Short Brothers Plc | Noise attentuation panel |
| US5175401A (en) * | 1991-03-18 | 1992-12-29 | Grumman Aerospace Corporation | Segmented resistance acoustic attenuating liner |
| AU650769B2 (en) * | 1991-08-05 | 1994-06-30 | 3A Technology & Management Ltd. | Process for the production of a composite sheet comprising a cellular core and at least one outer layer |
| EP0606227B1 (de) | 1992-08-03 | 2000-01-26 | Supracor, Inc. | Perforierter wabenkörper |
| JPH06226891A (ja) | 1993-02-02 | 1994-08-16 | Kobe Steel Ltd | 制振ハニカムパネル |
| US5344280A (en) * | 1993-05-05 | 1994-09-06 | General Electric Company | Impact resistant fan case liner |
| US5904318A (en) * | 1996-12-18 | 1999-05-18 | Towfiq; Foad | Passive reduction of aircraft fuselage noise |
| US6110985A (en) * | 1998-10-30 | 2000-08-29 | Soundwich, Inc. | Constrained layer damping compositions |
| US6220388B1 (en) * | 2000-01-27 | 2001-04-24 | Strandtek International, Inc. | Acoustical insulation panel |
| FR2821788B1 (fr) * | 2001-03-09 | 2004-04-02 | Eads Airbus Sa | Procede de fabrication d'un panneau a couche resistive acoustique adaptee et panneau acoustique ainsi obtenu |
| US6913110B1 (en) * | 2002-08-05 | 2005-07-05 | Southern California Sound Image | Lightweight speaker enclosure |
| US6764754B1 (en) * | 2003-07-15 | 2004-07-20 | The Boeing Company | Composite material with improved damping characteristics and method of making same |
| US7484593B2 (en) * | 2004-12-02 | 2009-02-03 | The Boeing Company | Acoustic structure and method of manufacturing thereof |
| US7837147B2 (en) * | 2005-03-18 | 2010-11-23 | The Boeing Company | Systems and methods for reducing noise in aircraft fuselages and other structures |
-
2005
- 2005-11-04 US US11/163,957 patent/US7419031B2/en active Active
-
2006
- 2006-11-02 WO PCT/US2006/043076 patent/WO2007056204A1/en not_active Ceased
- 2006-11-02 EP EP06827499A patent/EP1948503B1/de active Active
- 2006-11-02 AT AT06827499T patent/ATE524378T1/de not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| EP1948503B1 (de) | 2011-09-14 |
| US7419031B2 (en) | 2008-09-02 |
| EP1948503A1 (de) | 2008-07-30 |
| US20070102239A1 (en) | 2007-05-10 |
| WO2007056204A1 (en) | 2007-05-18 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |