JPH0335105B2 - - Google Patents
Info
- Publication number
- JPH0335105B2 JPH0335105B2 JP56503067A JP50306781A JPH0335105B2 JP H0335105 B2 JPH0335105 B2 JP H0335105B2 JP 56503067 A JP56503067 A JP 56503067A JP 50306781 A JP50306781 A JP 50306781A JP H0335105 B2 JPH0335105 B2 JP H0335105B2
- Authority
- JP
- Japan
- Prior art keywords
- graphite
- reinforced
- layer
- kevlar
- fastening
- 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.)
- Expired - Lifetime
Links
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 40
- 229910002804 graphite Inorganic materials 0.000 description 40
- 239000010439 graphite Substances 0.000 description 40
- 229920000271 Kevlar® Polymers 0.000 description 19
- 239000004761 kevlar Substances 0.000 description 19
- 230000002787 reinforcement Effects 0.000 description 19
- 239000002131 composite material Substances 0.000 description 16
- 229920006231 aramid fiber Polymers 0.000 description 12
- 229910052782 aluminium Inorganic materials 0.000 description 6
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 6
- 239000000835 fiber Substances 0.000 description 6
- 230000007797 corrosion Effects 0.000 description 4
- 238000005260 corrosion Methods 0.000 description 4
- AZDRQVAHHNSJOQ-UHFFFAOYSA-N alumane Chemical group [AlH3] AZDRQVAHHNSJOQ-UHFFFAOYSA-N 0.000 description 3
- 239000004760 aramid Substances 0.000 description 3
- 229920003235 aromatic polyamide Polymers 0.000 description 3
- 230000003014 reinforcing effect Effects 0.000 description 3
- 239000003822 epoxy resin Substances 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 229920000647 polyepoxide Polymers 0.000 description 2
- 229920005989 resin Polymers 0.000 description 2
- 239000011347 resin Substances 0.000 description 2
- 239000004677 Nylon Substances 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229920001778 nylon Polymers 0.000 description 1
Classifications
-
- 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
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/06—Fibrous reinforcements only
- B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D24/00—Producing articles with hollow walls
- B29D24/002—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled
- B29D24/005—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled the structure having joined ribs, e.g. honeycomb
- B29D24/007—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled the structure having joined ribs, e.g. honeycomb and a chamfered edge
-
- 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
- B32B7/08—Interconnection of layers by mechanical means
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/46—Blades
- B64C27/473—Constructional features
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2277/00—Use of PA, i.e. polyamides, e.g. polyesteramides or derivatives thereof, as reinforcement
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2307/00—Use of elements other than metals as reinforcement
-
- 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
- B32B2305/00—Condition, form or state of the layers or laminate
- B32B2305/02—Cellular or porous
- B32B2305/024—Honeycomb
-
- 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
- B32B2307/70—Other properties
- B32B2307/718—Weight, e.g. weight per square meter
-
- 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
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/46—Blades
- B64C27/473—Constructional features
- B64C2027/4733—Rotor blades substantially made from particular materials
- B64C2027/4736—Rotor blades substantially made from particular materials from composite materials
-
- 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
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/902—High modulus filament or fiber
-
- 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
- Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
- Y10T156/10—Methods of surface bonding and/or assembly therefor
- Y10T156/1052—Methods of surface bonding and/or assembly therefor with cutting, punching, tearing or severing
- Y10T156/1059—Splitting sheet lamina in plane intermediate of faces
-
- 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
- Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
- Y10T156/10—Methods of surface bonding and/or assembly therefor
- Y10T156/1089—Methods of surface bonding and/or assembly therefor of discrete laminae to single face of additional lamina
-
- 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
- Y10T428/19—Sheets or webs edge spliced or joined
- Y10T428/192—Sheets or webs coplanar
- Y10T428/197—Sheets or webs coplanar with noncoplanar reinforcement
-
- 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
-
- 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
- Y10T428/24—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
- Y10T428/24331—Composite web or sheet including nonapertured component
-
- 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.]
- Y10T428/24479—Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness
-
- 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.]
- Y10T428/24777—Edge feature
-
- 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
- Y10T428/30—Self-sustaining carbon mass or layer with impregnant or other layer
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Aviation & Aerospace Engineering (AREA)
- Laminated Bodies (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/187,247 US4344995A (en) | 1980-09-15 | 1980-09-15 | Hybrid composite structures |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS57501368A JPS57501368A (en]) | 1982-08-05 |
JPH0335105B2 true JPH0335105B2 (en]) | 1991-05-27 |
Family
ID=22688195
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP56503067A Expired - Lifetime JPH0335105B2 (en]) | 1980-09-15 | 1981-09-08 |
Country Status (4)
Country | Link |
---|---|
US (1) | US4344995A (en]) |
EP (1) | EP0059735B1 (en]) |
JP (1) | JPH0335105B2 (en]) |
WO (1) | WO1982000974A1 (en]) |
Families Citing this family (63)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4662587A (en) * | 1981-09-30 | 1987-05-05 | The Boeing Company | Composite for aircraft wing and method of making |
US4565595A (en) * | 1981-09-30 | 1986-01-21 | The Boeing Company | Method of making composite aircraft wing |
DE3141869C2 (de) * | 1981-10-22 | 1984-02-02 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Fußbodenkonstruktion für den oberen Laderaum eines Luftfahrzeuges |
FR2533013B1 (fr) * | 1982-09-09 | 1986-05-30 | Alkan R & Cie | Procede d'implantation d'un renfort metallique dans une structure en materiau composite fibres-resine |
US4543040A (en) * | 1982-09-30 | 1985-09-24 | The Boeing Company | Helicopter rotor system |
US4557961A (en) * | 1983-05-27 | 1985-12-10 | The Boeing Company | Light-weight, fire-retardant structural panel |
DE3345576A1 (de) * | 1983-12-16 | 1985-06-27 | Ford-Werke AG, 5000 Köln | Sandwich-bauteil, insbesondere haube, klappe oder dergleichen fuer eine kraftfahrzeugkarosserie |
US4579475A (en) * | 1984-01-23 | 1986-04-01 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Optimized bolted joint |
US4699568A (en) * | 1984-06-25 | 1987-10-13 | Hartzell Propeller Inc. | Aircraft propeller with improved spinner assembly |
US4629358A (en) * | 1984-07-17 | 1986-12-16 | The United States Of America As Represented By The Secretary Of The Navy | Prefabricated panels for rapid runway repair and expedient airfield surfacing |
IT8422619U1 (it) * | 1984-07-18 | 1986-01-18 | T I R Service S N C Di Crepaldi Giulio & C | Brandina o lettino a struttura deformabile per cabine di veicoli industriali e simili, particolarmente adatta per ridurre i danni al conducente in caso di incidenti stradali. |
US4680216A (en) * | 1984-09-04 | 1987-07-14 | United Technologies Corporation | Method for stabilizing thick honeycomb core composite articles |
US4782864A (en) * | 1984-12-31 | 1988-11-08 | Edo Corporation | Three dimensional woven fabric connector |
US4674712A (en) * | 1985-01-22 | 1987-06-23 | The Boeing Company | Double-lobe fuselage composite airplane |
US4826106A (en) * | 1987-02-18 | 1989-05-02 | Grumman Aerospace Corporation | Advanced composite aircraft cowl |
US5122226A (en) * | 1987-08-12 | 1992-06-16 | United Technologies Corporation | Method of making hybrid composite structures of fiber reinforced glass and resin matrices |
US4910065A (en) * | 1987-10-15 | 1990-03-20 | The Boeing Company | Reinforced honeycomb core sandwich panels and method for making same |
US4895750A (en) * | 1988-03-28 | 1990-01-23 | General Dynamics Corp., Pomona Division | High-temperature tensile test specimen and methods of fabrication |
US5078843A (en) * | 1988-03-28 | 1992-01-07 | General Dynamics Corporation Air Defense Systems Division | Method for fabricating high-temperature tensile test specimens |
NL8801300A (nl) * | 1988-05-19 | 1989-12-18 | Halbertsma Deuren B V | Gevormde voorwerpen met een sandwichconstructie, alsmede werkwijze ter vervaardiging van deze voorwerpen. |
US5096526A (en) * | 1989-11-30 | 1992-03-17 | The Boeing Company | Core bonding and forming of thermoplastic laminates |
JPH06173772A (ja) | 1992-08-10 | 1994-06-21 | Boeing Co:The | 逆推進装置内壁およびそのサンドイッチ構造 |
US5820077A (en) * | 1995-09-26 | 1998-10-13 | Mcdonnell Douglas Technologies, Inc. | Aircraft radome and integral attaching structure |
US5895699A (en) * | 1996-03-15 | 1999-04-20 | The Boeing Company | Tiedown ply for reducing core crush in composite honeycomb sandwich structure |
US5795043A (en) * | 1996-11-01 | 1998-08-18 | The Protectoseal Company | Corrosion-resistant storage cabinet |
RU2116934C1 (ru) * | 1997-05-06 | 1998-08-10 | Акционерное общество "Центр перспективных разработок акционерного общества "Центральный научно-исследовательский институт специального машиностроения" | Нервюра из композиционных материалов (варианты) и устройство для изготовления ее плоской реберно-ячеистой структуры |
US6277463B1 (en) * | 1998-08-28 | 2001-08-21 | Mcdonnell Douglas Corporation | Composite member having increased resistance to delamination and method of making same |
US6505571B1 (en) | 2001-10-17 | 2003-01-14 | The United States Of America As Represented By The Secretary Of The Navy | Hybrid hull construction for marine vessels |
US6648273B2 (en) * | 2001-10-30 | 2003-11-18 | The Boeing Company | Light weight and high strength fuselage |
GB2407344B (en) * | 2003-10-22 | 2006-02-22 | Rolls Royce Plc | A liner for a gas turbine engine casing |
ES2277716B1 (es) * | 2004-12-31 | 2008-05-16 | Airbus España, S.L. | Tapa reforzada para ranuras en un contorno aerodinamico. |
ES2277715B1 (es) * | 2004-12-31 | 2008-05-16 | Airbus España, S.L. | Tapa reforzada para escotaduras en un contorno aerodinamico. |
US20060248854A1 (en) * | 2005-05-05 | 2006-11-09 | Bartley-Cho Jonathan D | Thermally insulated structure - tapered joint concept |
GB0526312D0 (en) * | 2005-12-23 | 2006-02-01 | Britax Premium Aircraft Interi | Composite panel |
US8709584B2 (en) * | 2006-01-31 | 2014-04-29 | Sikorsky Aircraft Corporation | Composite aircraft floor system |
US7628358B2 (en) * | 2006-10-26 | 2009-12-08 | The Boeing Company | Wing panel structure |
US7735600B2 (en) * | 2006-12-08 | 2010-06-15 | The Boeing Corporation | Monolithic acoustically-treated engine nacelle inlet panels |
DE102007003276B4 (de) * | 2007-01-23 | 2013-11-28 | Airbus Operations Gmbh | Luft- und Raumfahrzeug mit einem CFK-Bauteil und einem Metallbauteil, wobei das CFK-Bauteil und das Metallbauteil über wenigstens ein Verbindungselement mit einem Verbindungsabschnitt miteinander verbunden sind |
DE102007003277B4 (de) * | 2007-01-23 | 2012-08-02 | Airbus Operations Gmbh | Rumpf eines Luft- oder Raumfahrzeuges in CFK-Metall Hybridbauweise mit einem Metallrahmen |
US8292227B2 (en) * | 2008-07-12 | 2012-10-23 | The Boeing Company | Aircraft wings having continuously tailored structural strength |
US8402805B2 (en) * | 2008-07-12 | 2013-03-26 | The Boeing Company | Method and apparatus for forming a corrugated web having a continuously varying shape |
US20100040828A1 (en) * | 2008-08-15 | 2010-02-18 | Harper Engineering Co. | Latch cover |
FR2937303B1 (fr) | 2008-10-16 | 2011-01-14 | Airbus France | Plancher en materiau composite pour vehicule de transport et procede de fabrication d'un tel plancher |
DE102009013585B4 (de) * | 2009-03-17 | 2012-01-26 | Airbus Operations Gmbh | Rumpfzellenstruktur für ein Flugzeug in Hybridbauweise |
US8616621B2 (en) * | 2010-08-03 | 2013-12-31 | Harper Engineering Co. | Potted panel latch system |
US8333345B2 (en) * | 2010-08-26 | 2012-12-18 | The Boeing Company | Composite aircraft joint |
US8844873B2 (en) * | 2011-09-23 | 2014-09-30 | The Boeing Company | Stabilizer torque box assembly and method |
JP2016153166A (ja) * | 2013-06-28 | 2016-08-25 | 日産自動車株式会社 | 中空板 |
US9567778B2 (en) | 2013-10-16 | 2017-02-14 | Harper Engineering Company | Methods for installation of potted inserts having a latch mechanism |
US9925736B2 (en) * | 2013-12-13 | 2018-03-27 | Celltech Metals, Inc. | Sandwich structure |
WO2015148707A1 (en) | 2014-03-26 | 2015-10-01 | Celltech Metals Inc. | Container apparatus including sandwich structure |
US10710328B2 (en) | 2014-04-22 | 2020-07-14 | Celltech Metals, Inc. | Wheeled trailer sandwich structure including grooved outer sheet |
CA3148693C (en) | 2014-06-04 | 2023-08-15 | Sti Holdings, Inc. | Composite panel edge treatments and joints and cargo body having same |
US10144582B2 (en) | 2016-05-11 | 2018-12-04 | Celltech Metals, Inc. | Cargo container apparatus including a sandwich structure and a track |
US10814602B2 (en) * | 2016-09-14 | 2020-10-27 | The Boeing Company | Method of producing cored composite parts |
EP3636550B1 (en) * | 2017-06-07 | 2023-09-20 | IHI Corporation | Sound-absorbing panel and manufacturing method for same |
US10266098B1 (en) | 2017-12-21 | 2019-04-23 | Celltech Metals, Inc. | Cargo transportation system including a sandwich panel and a channel |
US10814581B2 (en) | 2018-07-03 | 2020-10-27 | STI Holdings, Iinc. | Composite sidewall and cargo body having same |
US11136072B2 (en) | 2018-08-07 | 2021-10-05 | Sti Holdings, Inc. | Cargo body with recessed logistics track |
US10507875B1 (en) | 2018-12-21 | 2019-12-17 | Celltech Metals Inc. | Trailer wall including logistics post |
US11097647B1 (en) | 2020-01-31 | 2021-08-24 | Sti Holdings, Inc. | Cargo body wall with logistics tracks |
CN113183493B (zh) * | 2021-04-13 | 2022-10-21 | 中国航空制造技术研究院 | 用于尾缘带泡沫结构的蜂窝夹层壁板成型工装及成型方法 |
US12060145B2 (en) * | 2022-03-02 | 2024-08-13 | The Boeing Company | Vehicle panel assembly and method of panel assembly |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2696451A (en) * | 1946-02-08 | 1954-12-07 | Lockheed Aircraft Corp | Plastic edge attachment |
US3145000A (en) * | 1963-05-29 | 1964-08-18 | William L Mackie | Light weight-high thermal resistant airfoil |
US3655818A (en) * | 1968-10-18 | 1972-04-11 | Minnesota Mining & Mfg | Particulate adhesive containing polyepoxides carboxylated butadiene-acrylonitrile copolymer and a urea derivative as a curing agent |
GB1406441A (en) * | 1972-03-13 | 1975-09-17 | Triplex Safety Glass Co | Laminated transparent assemblies |
US3919022A (en) * | 1974-02-21 | 1975-11-11 | Ppg Industries Inc | Window panel edge construction |
US4046933A (en) * | 1975-09-16 | 1977-09-06 | Ppg Industries, Inc. | Laminated window structure and its method of fabrication |
US4052523A (en) * | 1976-09-14 | 1977-10-04 | The United States Of America As Represented By The National Aeronautics And Space Administration | Composite sandwich lattice structure |
-
1980
- 1980-09-15 US US06/187,247 patent/US4344995A/en not_active Expired - Lifetime
-
1981
- 1981-09-08 EP EP81902555A patent/EP0059735B1/en not_active Expired
- 1981-09-08 JP JP56503067A patent/JPH0335105B2/ja not_active Expired - Lifetime
- 1981-09-08 WO PCT/US1981/001206 patent/WO1982000974A1/en active IP Right Grant
Also Published As
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US4344995A (en) | 1982-08-17 |
EP0059735A4 (en) | 1982-12-27 |
EP0059735A1 (en) | 1982-09-15 |
WO1982000974A1 (en) | 1982-04-01 |
EP0059735B1 (en) | 1985-02-13 |
JPS57501368A (en]) | 1982-08-05 |
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