|
US2819032A
(en)
*
|
1953-10-20 |
1958-01-07 |
Douglas Aircraft Co Inc |
Aircraft fuselage having panel damping material
|
|
US3020986A
(en)
*
|
1958-08-18 |
1962-02-13 |
Gen Dynamics Corp |
Composite structural panel
|
|
US3088561A
(en)
*
|
1958-11-06 |
1963-05-07 |
Wright Barry Corp |
Damped structures
|
|
US3078969A
(en)
*
|
1959-06-15 |
1963-02-26 |
Lord Mfg Co |
Damped beam
|
|
US3078971A
(en)
*
|
1960-01-11 |
1963-02-26 |
Lord Mfg Co |
Damped beam
|
|
US3159249A
(en)
*
|
1960-01-27 |
1964-12-01 |
Univ Minnesota |
Damping means
|
|
US3160549A
(en)
*
|
1960-12-29 |
1964-12-08 |
Minnesota Mining & Mfg |
Vibration damping structures
|
|
US3193049A
(en)
*
|
1963-05-27 |
1965-07-06 |
Daubert Chemical Co |
Sound damping tape
|
|
US3832955A
(en)
*
|
1972-09-01 |
1974-09-03 |
Jered Prod Inc |
Reinforced plastic panel
|
|
SE420750B
(sv)
*
|
1978-11-17 |
1981-10-26 |
Ingemanssons Ingenjorsbyra Ab |
Ljudisolerande byggnadselement med stor styvhet
|
|
US4182495A
(en)
*
|
1978-12-04 |
1980-01-08 |
The United States Of America As Represented By The Secretary Of The Navy |
Graphite or carbon fiber composite structure, low temperature cure
|
|
GB2052388A
(en)
*
|
1979-06-02 |
1981-01-28 |
Nissan Motor |
Noise reducing cover for an internal combustion engine
|
|
US4828202A
(en)
*
|
1979-09-27 |
1989-05-09 |
The Boeing Company |
Method and apparatus for wideband vibration damping of reinforced skin structures
|
|
US4635882A
(en)
*
|
1980-11-14 |
1987-01-13 |
The Boeing Company |
Method and apparatus for reducing low to mid frequency interior noise
|
|
US4591402A
(en)
*
|
1981-06-22 |
1986-05-27 |
Ltv Aerospace And Defense Company |
Apparatus and method for manufacturing composite structures
|
|
US4428454A
(en)
*
|
1981-09-24 |
1984-01-31 |
Capaul Raymond W |
Acoustical panel construction
|
|
US4556439A
(en)
*
|
1981-09-25 |
1985-12-03 |
The Boeing Company |
Method of sealing and bonding laminated epoxy plates
|
|
US4463044A
(en)
*
|
1981-09-28 |
1984-07-31 |
The Boeing Company |
Composite panel of varied thickness
|
|
US4401495A
(en)
*
|
1981-09-28 |
1983-08-30 |
The Boeing Company |
Method of winding composite panels
|
|
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
|
|
US4553631A
(en)
*
|
1983-05-19 |
1985-11-19 |
United Mcgill Corporation |
Sound absorption method and apparatus
|
|
US4851501A
(en)
*
|
1983-06-17 |
1989-07-25 |
The Boeing Company |
Polyethersulfone prepregs, composites, and blends
|
|
US4477304A
(en)
*
|
1983-07-01 |
1984-10-16 |
International Business Machines Corporation |
Application tool
|
|
WO1985003032A1
(en)
*
|
1984-01-09 |
1985-07-18 |
The Boeing Company |
Composite material structure with integral fire protection
|
|
JPS6112334A
(ja)
*
|
1984-06-29 |
1986-01-20 |
川崎製鉄株式会社 |
複合型制振積層体
|
|
US4877471A
(en)
*
|
1984-08-24 |
1989-10-31 |
The Boeing Company |
Method and apparatus for delivering a resin-impregnated, multifilament band
|
|
US4608220A
(en)
*
|
1984-12-20 |
1986-08-26 |
The Boeing Company |
Method of forming composite material articles
|
|
US4966802A
(en)
*
|
1985-05-10 |
1990-10-30 |
The Boeing Company |
Composites made of fiber reinforced resin elements joined by adhesive
|
|
US4786343A
(en)
*
|
1985-05-10 |
1988-11-22 |
The Boeing Company |
Method of making delamination resistant composites
|
|
US4611687A
(en)
*
|
1985-07-23 |
1986-09-16 |
Nixon Michael T |
Three-function acoustical panel
|
|
JPS62111837U
(cg-RX-API-DMAC7.html)
*
|
1985-12-28 |
1987-07-16 |
|
|
|
US4699683A
(en)
*
|
1986-02-07 |
1987-10-13 |
The Boeing Company |
Multiroving fiber laminator
|
|
DE3614365A1
(de)
*
|
1986-04-28 |
1987-10-29 |
Messerschmitt Boelkow Blohm |
Vorrichtung zum ablegen eines vorimpraegnierten faserbandes
|
|
US4860851A
(en)
*
|
1987-01-27 |
1989-08-29 |
Raychem Corporation |
Dimensionally-recoverable damping article
|
|
US5151311A
(en)
*
|
1987-11-02 |
1992-09-29 |
Grumman Aerospace Corporation |
Acoustic attenuating liner and method of making same
|
|
JPH0673935B2
(ja)
*
|
1988-04-01 |
1994-09-21 |
ニチアス株式会社 |
制振材および制振材を用いた防音構造体
|
|
FR2632604B1
(fr)
*
|
1988-06-08 |
1991-07-12 |
Aerospatiale |
Cadre en materiau composite notamment pour fuselage d'aeronef, et son procede de fabrication
|
|
US5232073A
(en)
*
|
1988-12-09 |
1993-08-03 |
Trw Inc. |
Process for damping dynamic load
|
|
US5106668A
(en)
*
|
1989-06-07 |
1992-04-21 |
Hexcel Corporation |
Multi-layer honeycomb structure
|
|
JP2554063Y2
(ja)
*
|
1989-10-17 |
1997-11-12 |
財団法人日本航空機開発協会 |
胴体壁内装板
|
|
US5277958A
(en)
*
|
1990-01-02 |
1994-01-11 |
Tomkins Keith A |
Multiple-layer structures and joining method for honeycomb, foam and lightweight materials
|
|
DE4002087A1
(de)
*
|
1990-01-25 |
1991-08-08 |
Messerschmitt Boelkow Blohm |
Ablegen von faserbaendern auf doppelt gekruemmten koerpern oder flaechen
|
|
JPH04125136A
(ja)
*
|
1990-01-26 |
1992-04-24 |
Nec Corp |
繊維強化複合材料
|
|
US5087491A
(en)
*
|
1990-02-09 |
1992-02-11 |
The United States Of America As Represented By The Secretary Of The Navy |
Vibration-damping structural member
|
|
US5178717A
(en)
*
|
1991-03-06 |
1993-01-12 |
Rodriguez Peter A |
Adhesive applicator
|
|
JPH04341837A
(ja)
*
|
1991-05-17 |
1992-11-27 |
Ishikawajima Harima Heavy Ind Co Ltd |
Ｆｒｐ積層板
|
|
US5268055A
(en)
*
|
1991-10-31 |
1993-12-07 |
Bales John L |
Method for making perforated composite laminates
|
|
US5256223A
(en)
*
|
1991-12-31 |
1993-10-26 |
The Center For Innovative Technology |
Fiber enhancement of viscoelastic damping polymers
|
|
US5262232A
(en)
*
|
1992-01-22 |
1993-11-16 |
Minnesota Mining And Manufacturing Company |
Vibration damping constructions using acrylate-containing damping materials
|
|
US5445861A
(en)
*
|
1992-09-04 |
1995-08-29 |
The Boeing Company |
Lightweight honeycomb panel structure
|
|
US5308675A
(en)
*
|
1992-09-15 |
1994-05-03 |
The United States Of America As Represented By The Secretary Of The Navy |
Flexible high damping structure
|
|
US5744221A
(en)
*
|
1992-09-15 |
1998-04-28 |
The United States Of America As Represented By The Secretary Of The Navy |
Flexible high-damping composite structures and fabrication thereof
|
|
US5337288A
(en)
*
|
1992-09-30 |
1994-08-09 |
The United States Of America As Represented By The Secretary Of The Navy |
Acoustic and vibration attenuation composite material
|
|
US5354195A
(en)
*
|
1992-12-23 |
1994-10-11 |
United Technologies Corporation |
Composite molding apparatus for high pressure co-cure molding of lightweight honeycomb core composite articles having ramped surfaces utilizing low density, stabilized ramped honeycomb cores
|
|
US5916954A
(en)
*
|
1993-01-27 |
1999-06-29 |
Trw Inc. |
Fiber reinforced viscoelastic material composites for passive damping
|
|
US5368914A
(en)
*
|
1993-03-03 |
1994-11-29 |
The United States Of America As Represented By The Secretary Of The Navy |
Vibration-damping structural component
|
|
US5902755A
(en)
*
|
1993-05-03 |
1999-05-11 |
Tox-Wastech, Inc. |
High Strength composite materials
|
|
WO1994025180A1
(en)
*
|
1993-05-05 |
1994-11-10 |
Albany International Research Co. |
Composite sandwich element
|
|
US5507477A
(en)
*
|
1994-07-28 |
1996-04-16 |
Trw Inc. |
Composite damping structures and related method
|
|
US5622733A
(en)
*
|
1994-10-04 |
1997-04-22 |
Rockwell International Corporation |
Tooling for the fabrication of composite hollow crown-stiffened skins and panels
|
|
US5567499A
(en)
*
|
1995-01-03 |
1996-10-22 |
The Boeing Company |
Resin transfer molding in combination with honeycomb core
|
|
US5667866A
(en)
*
|
1995-05-02 |
1997-09-16 |
The Nordam Group, Inc. |
Multi-layered, unbalanced sandwich panel
|
|
US5710396A
(en)
*
|
1996-01-02 |
1998-01-20 |
Rogers; Lynn C. |
Energy-dissipating vibration damping structure
|
|
US5866272A
(en)
*
|
1996-01-11 |
1999-02-02 |
The Boeing Company |
Titanium-polymer hybrid laminates
|
|
US5700347A
(en)
*
|
1996-01-11 |
1997-12-23 |
The Boeing Company |
Thermoplastic multi-tape application head
|
|
US5604010A
(en)
*
|
1996-01-11 |
1997-02-18 |
Hartz; Dale E. |
Composite honeycomb sandwich structure
|
|
EP0820858B1
(en)
*
|
1996-07-22 |
2000-11-02 |
Hexcel Corporation |
Honeycomb core materials with particulate reinforcement
|
|
US5895013A
(en)
*
|
1996-10-02 |
1999-04-20 |
Mcdonnell Douglas Corp. |
Low frequency noise suppression system
|
|
US5904318A
(en)
*
|
1996-12-18 |
1999-05-18 |
Towfiq; Foad |
Passive reduction of aircraft fuselage noise
|
|
US5958556A
(en)
*
|
1996-12-19 |
1999-09-28 |
Minnesota Mining And Manufacturing Company |
Vibration damped and stiffened circuit articles
|
|
DE19653850C2
(de)
*
|
1996-12-21 |
1999-01-28 |
Daimler Benz Aerospace Airbus |
Wandelement
|
|
US6171705B1
(en)
*
|
1997-02-10 |
2001-01-09 |
Dofasco, Inc. |
Structural panel and method of manufacture
|
|
US5902535A
(en)
*
|
1997-07-30 |
1999-05-11 |
Mcdonnell Douglas Corporation |
Resin film infusion mold tooling and molding method
|
|
US7906191B2
(en)
*
|
1997-11-14 |
2011-03-15 |
William F. Pratt |
Wavy composite structures
|
|
US6453962B1
(en)
*
|
1997-11-14 |
2002-09-24 |
William F. Pratt |
Dual-axis method and machine for producing pre-preg
|
|
DE19804718C2
(de)
*
|
1998-02-06 |
2001-09-13 |
Eurocopter Deutschland |
Schall absorbierende Sandwichwand
|
|
US6458309B1
(en)
*
|
1998-06-01 |
2002-10-01 |
Rohr, Inc. |
Method for fabricating an advanced composite aerostructure article having an integral co-cured fly away hollow mandrel
|
|
US6177173B1
(en)
|
1998-07-01 |
2001-01-23 |
3M Innovative Properties Company |
Damped laminates having welded through holes and/or edges with decreased spring back and improved fastener force retention and, a method of making
|
|
US6110985A
(en)
*
|
1998-10-30 |
2000-08-29 |
Soundwich, Inc. |
Constrained layer damping compositions
|
|
DE19901965A1
(de)
*
|
1999-01-19 |
2000-07-20 |
Giesecke & Devrient Gmbh |
Tragbarer Datenträger mit ausbrechbarer Minichipkarte
|
|
GB9905145D0
(en)
*
|
1999-03-06 |
1999-04-28 |
Bolton Inst Higher Education |
Auxetic materials
|
|
US6510961B1
(en)
*
|
1999-04-14 |
2003-01-28 |
A&P Technology |
Integrally-reinforced braided tubular structure and method of producing the same
|
|
US6755998B1
(en)
*
|
1999-10-26 |
2004-06-29 |
Compsys, Inc. |
Composite panel adapted for point compressive loads and method for making same
|
|
BR9905840B1
(pt)
*
|
1999-12-14 |
2010-07-13 |
|
sistema dispersor de carga de unidades de craqueamento catalìtico fluido.
|
|
US6399199B1
(en)
*
|
1999-12-28 |
2002-06-04 |
Toray Industries Inc. |
Prepeg and carbon fiber reinforced composite materials
|
|
US6655633B1
(en)
*
|
2000-01-21 |
2003-12-02 |
W. Cullen Chapman, Jr. |
Tubular members integrated to form a structure
|
|
JP4526698B2
(ja)
*
|
2000-12-22 |
2010-08-18 |
富士重工業株式会社 |
複合材成形品及びその製造方法
|
|
US20050016671A1
(en)
*
|
2001-03-05 |
2005-01-27 |
Sharp Terrance M. |
Robotic tape applicator and method
|
|
US6497190B1
(en)
*
|
2001-05-29 |
2002-12-24 |
Compsys, Inc. |
Conformable composite structural member and method therefor
|
|
ATE509755T1
(de)
*
|
2001-08-02 |
2011-06-15 |
Ebert Composites Corp |
Verfahren zum crimpen der oberen und unteren endteile von in der z-achse orientierten fasern in die entsprechende obere und untere oberfläche eines verbundlaminats und verbundlaminat
|
|
US6659223B2
(en)
*
|
2001-10-05 |
2003-12-09 |
Collins & Aikman Products Co. |
Sound attenuating material for use within vehicles and methods of making same
|
|
TW561102B
(en)
*
|
2001-10-22 |
2003-11-11 |
Hrl Lab Llc |
Preparing composites by using resins
|
|
EP1336469A1
(en)
*
|
2002-02-19 |
2003-08-20 |
Alenia Aeronautica S.P.A. |
Methods of manufacturing a stiffening element for an aircraft skin panel and a skin panel provided with the stiffening element
|
|
GB2390999B
(en)
|
2002-07-19 |
2005-07-20 |
Oxford Magnet Tech |
Composite material for acoustic damping
|
|
US7419627B2
(en)
|
2002-09-13 |
2008-09-02 |
Northrop Grumman Corporation |
Co-cured vacuum-assisted resin transfer molding manufacturing method
|
|
US7197852B2
(en)
|
2002-09-20 |
2007-04-03 |
The Boeing Company |
Internally stiffened composite panels and methods for their manufacture
|
|
JP2004291408A
(ja)
*
|
2003-03-27 |
2004-10-21 |
Cci Corp |
制振性複合材料
|
|
GB2401346B
(en)
*
|
2003-05-07 |
2005-04-13 |
Oxford Magnet Tech |
A structural composite material for acoustic damping
|
|
US7213629B2
(en)
|
2003-05-14 |
2007-05-08 |
The Boeing Company |
Vacuum assisted ply placement shoe and method
|
|
US6764754B1
(en)
|
2003-07-15 |
2004-07-20 |
The Boeing Company |
Composite material with improved damping characteristics and method of making same
|
|
US7282107B2
(en)
*
|
2003-08-22 |
2007-10-16 |
The Boeing Company |
Multiple head automated composite laminating machine for the fabrication of large barrel section components
|
|
US7181891B2
(en)
|
2003-09-08 |
2007-02-27 |
Quiet Solution, Inc. |
Acoustical sound proofing material and methods for manufacturing same
|
|
USD533950S1
(en)
|
2004-02-26 |
2006-12-19 |
Dan-Pal |
Structural panel
|
|
US20050194210A1
(en)
*
|
2004-03-08 |
2005-09-08 |
The Boeing Company |
Apparatus and method for aircraft cabin noise attenuation via non-obstructive particle damping
|
|
US7083147B2
(en)
*
|
2004-03-11 |
2006-08-01 |
The Boeing Company |
Modularized insulation, systems, apparatus, and methods
|
|
JP2005262613A
(ja)
*
|
2004-03-18 |
2005-09-29 |
Toray Ind Inc |
Ｆｒｐ構造体用中間基材および該基材を用いたｆｒｐ構造体
|
|
US7040575B2
(en)
*
|
2004-03-29 |
2006-05-09 |
The Boeing Company |
Foam composite insulation for aircraft
|
|
US7527222B2
(en)
|
2004-04-06 |
2009-05-05 |
The Boeing Company |
Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections
|
|
US7134629B2
(en)
|
2004-04-06 |
2006-11-14 |
The Boeing Company |
Structural panels for use in aircraft fuselages and other structures
|
|
US7160621B2
(en)
|
2004-06-28 |
2007-01-09 |
General Electric Company |
Energy absorbing articles
|
|
US20060040096A1
(en)
*
|
2004-08-19 |
2006-02-23 |
Rajan Eadara |
Constrained layer, composite, acoustic damping material
|
|
US7325771B2
(en)
|
2004-09-23 |
2008-02-05 |
The Boeing Company |
Splice joints for composite aircraft fuselages and other structures
|
|
US7419031B2
(en)
|
2005-11-04 |
2008-09-02 |
The Boeing Company |
Integrally damped composite aircraft floor panels
|
|
US7503368B2
(en)
*
|
2004-11-24 |
2009-03-17 |
The Boeing Company |
Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections
|
|
US20060118244A1
(en)
*
|
2004-12-02 |
2006-06-08 |
The Boeing Company |
Device for laying tape materials for aerospace applications
|
|
US7578468B2
(en)
*
|
2004-12-20 |
2009-08-25 |
Sikorsky Aircraft Corporation |
Acoustic absorption system for an aircraft airframe
|
|
US7837147B2
(en)
|
2005-03-18 |
2010-11-23 |
The Boeing Company |
Systems and methods for reducing noise in aircraft fuselages and other structures
|
|
US7766063B2
(en)
|
2005-04-28 |
2010-08-03 |
The Boeing Company |
Machine assisted laminator and method
|
|
US7291373B2
(en)
|
2005-05-05 |
2007-11-06 |
Northrop Grumman Corporation |
Thermally insulated structure—full depth sandwich joint concept
|
|
DE102005028765B4
(de)
|
2005-06-22 |
2016-01-21 |
Airbus Operations Gmbh |
Verfahren zur Herstellung eines Verstärkungsprofils
|
|
US7681615B2
(en)
|
2005-08-04 |
2010-03-23 |
The Boeing Company |
Tow width adaptable placement head device and method
|
|
US20070069080A1
(en)
|
2005-09-28 |
2007-03-29 |
The Boeing Company |
Laminated passenger window with a vacuum layer for reduced noise transmission
|
|
ES2449515T3
(es)
|
2005-10-06 |
2014-03-20 |
Henkel Ag & Co. Kgaa |
Reducción de la transferencia de vibraciones
|
|
US10086921B2
(en)
|
2005-10-31 |
2018-10-02 |
The Boeing Company |
Aircraft having a forward-facing section that deflects elastically under impact loads
|
|
US9359061B2
(en)
|
2005-10-31 |
2016-06-07 |
The Boeing Company |
Compliant stiffener for aircraft fuselage
|
|
US20070125474A1
(en)
|
2005-12-05 |
2007-06-07 |
Huber Engineered Woods L.L.C. |
Handheld tape applicator and components thereof, and their methods of use
|
|
WO2007113345A1
(es)
|
2006-03-31 |
2007-10-11 |
Airbus España, S.L. |
Procedimiento de fabricacion de estructuras de material compuesto con un utillaje colapsable
|
|
CA2651742A1
(en)
|
2006-05-30 |
2007-12-06 |
Airbus Deutschland Gmbh |
Sandwich element for sound-absorbing inner cladding of transport means, especially for sound-absorbing inner cladding of aircraft fuselage cells
|
|
US7931240B2
(en)
|
2006-08-11 |
2011-04-26 |
Techno-Sciences, Inc. |
Cellular support structures used for controlled actuation of fluid contact surfaces
|
|
NL2000232C2
(nl)
|
2006-09-12 |
2008-03-13 |
Gtm Consulting B V |
Huidpaneel voor een vliegtuigromp.
|
|
US9511571B2
(en)
|
2007-01-23 |
2016-12-06 |
The Boeing Company |
Composite laminate having a damping interlayer and method of making the same
|
|
US8327743B2
(en)
|
2007-05-17 |
2012-12-11 |
The Boeing Company |
Mechanism and method for predetermined angular cutting of a plurality of ply strips
|
|
US8951923B2
(en)
|
2007-05-23 |
2015-02-10 |
The Boeing Company |
Hybrid composite structure having damped metallic fibers
|
|
US7798285B2
(en)
|
2008-11-14 |
2010-09-21 |
Rohr, Inc. |
Acoustic barrel for aircraft engine nacelle including crack and delamination stoppers
|
|
US8425710B2
(en)
|
2009-03-13 |
2013-04-23 |
The Boeing Company |
Automated placement of vibration damping materials
|