CA2537945A1 - A resin infused transparent skin panel and method of making same - Google Patents

A resin infused transparent skin panel and method of making same Download PDF

Info

Publication number
CA2537945A1
CA2537945A1 CA002537945A CA2537945A CA2537945A1 CA 2537945 A1 CA2537945 A1 CA 2537945A1 CA 002537945 A CA002537945 A CA 002537945A CA 2537945 A CA2537945 A CA 2537945A CA 2537945 A1 CA2537945 A1 CA 2537945A1
Authority
CA
Canada
Prior art keywords
metal sheet
transparent
skin panel
resin
fiber reinforced
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.)
Granted
Application number
CA002537945A
Other languages
French (fr)
Other versions
CA2537945C (en
Inventor
Robert G. Albers
Paul S. Nordman
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Boeing Co
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of CA2537945A1 publication Critical patent/CA2537945A1/en
Application granted granted Critical
Publication of CA2537945C publication Critical patent/CA2537945C/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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
    • 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
    • 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
    • B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/02—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
    • B29C43/18—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles incorporating preformed parts or layers, e.g. compression moulding around inserts or for coating articles
    • 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
    • B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/02—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
    • B29C43/20—Making multilayered or multicoloured articles
    • B29C43/203—Making multilayered articles
    • 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
    • B29C70/088—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 and with one or more layers of non-plastics material or non-specified material, e.g. supports
    • 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
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/302—Details of the edges of fibre composites, e.g. edge finishing or means to avoid delamination
    • 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
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
    • B29C70/345—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using matched moulds
    • 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
    • B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
    • B29C70/86—Incorporated in coherent impregnated reinforcing layers, e.g. by winding
    • 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
    • B29C70/88—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced
    • B29C70/882—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced partly or totally electrically conductive, e.g. for EMI shielding
    • B29C70/885—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced partly or totally electrically conductive, e.g. for EMI shielding with incorporated metallic wires, nets, films or plates
    • 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 form; Layered products 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 form; Layered products 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 form; Layered products 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
    • 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
    • B32B5/28—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 impregnated with or embedded in a plastic substance
    • 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
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
    • B64C1/1476—Canopies; Windscreens or similar transparent elements
    • B64C1/1492—Structure and mounting of the transparent elements in the window or windscreen
    • 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
    • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • B29K2105/08—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
    • B29K2105/0854—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns in the form of a non-woven mat
    • 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
    • B29K2705/00—Use of metals, their alloys or their compounds, for preformed parts, e.g. for inserts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3076—Aircrafts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3076—Aircrafts
    • B29L2031/3082—Fuselages
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/778—Windows
    • 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
    • B32B2305/00—Condition, form or state of the layers or laminate
    • B32B2305/38—Meshes, lattices or nets
    • 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
    • B32B2307/40—Properties of the layers or laminate having particular optical properties
    • B32B2307/412—Transparent
    • 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
    • B32B2311/00—Metals, their alloys or their compounds
    • B32B2311/18—Titanium
    • 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
    • B32B2607/00—Walls, panels
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction
    • 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.]
    • Y10T428/24273—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
    • Y10T428/24339—Keyed
    • 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
    • Y10T428/24339—Keyed
    • Y10T428/24347—From both sides
    • 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.]
    • Y10T428/24355—Continuous and nonuniform or irregular surface on layer or component [e.g., roofing, etc.]
    • Y10T428/24364—Continuous and nonuniform or irregular surface on layer or component [e.g., roofing, etc.] with transparent or protective coating
    • 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

Abstract

A transparent skin panel for use in a mobile platform having a plurality of metal sheets (26). A fiber reinforced resin (36) at least partially surrounds the plurality of metal sheets (26). The fiber reinforced resin (36) is transparent. A cutout (32) is formed within each of the plurality of metal sheets (26), which is filled by the transparent resin (36) during the manufacturing process. The cutout (32) corresponds to a window (16) in the transparent skin panel (10). The transparent skin panel thus eliminates the need for a bulky and heavy frame structure that has traditionally been employed on aircraft, and which has heretofore limited the size of windows used on an aircraft. The present invention thus enables larger windows to be incorporated on aircraft without increasing the weight or cost associated with such windows.

Claims (19)

1. A transparent skin panel for use in a mobile platform comprising:
at least one metal sheet;
a fiber reinforced resin at least partially surrounding the at least one metal sheet, the fiber reinforced resin being transparent; and an opening defined in the at least one metal sheet, the transparent resin filling the opening forming a window in the transparent skin panel.
2. The transparent skin panel of claim 1, wherein at least one metal sheet includes a plurality of perforations formed therein, the perforations filled with the fiber reinforced resin.
3. The transparent skin panel of claim 1, wherein the metal sheet is comprised of aluminum.
4. The transparent skin panel of claim 1, wherein the metal sheet is comprised of titanium.
5. The transparent skin panel of claim 1, wherein the fiber reinforced resin fully covers the at least one metal sheet.
6. The transparent skin panel of claim 1, wherein the fiber reinforced resin includes a plurality of fiber mesh sheets one atop the other.
7. A method of forming a structural panel, comprising:
using at least one metal sheet to form a frame structure, wherein the frame structure defines an opening;
applying a generally transparent, fiber reinforced resin to the metal sheet to at least partially coat the metal sheet and fill the opening; and wherein the generally transparent, fiber reinforced resin forms a see through window.
8. The method of claim 7, wherein applying the generally transparent, fiber reinforced resin to the metal sheet comprises applying a generally transparent resin having a preform, the preform including a plurality of fibers.
9. The method of claim 8, wherein applying the generally transparent, fiber reinforced resin includes applying an aliphatic epoxy resin.
10. The method of claim 7, wherein using at least one metal sheet comprises using an aluminum sheet.
11. The method of claim 7, wherein applying a generally transparent, fiber reinforced resin comprises applying an aliphatic epoxy resin having a weave of fibers, wherein the fibers have an index of refraction matching an index of refraction of the resin.
12. The method of claim 7, wherein applying a generally transparent, fiber reinforced resin comprises applying an aliphatic epoxy resin.
13. A method of manufacturing a transparent skin panel comprising:
providing a mold;
providing a preform comprised of a plurality of fibers;
providing a metal sheet having a plurality of perforations formed therein;
inserting the preform and metal sheet into the mold such that the metal sheet and the preform are aligned one atop the other;
infusing a resin into the mold such that the resin flows through the perforations of the metal sheet and at least partially covers the metal sheet and the preform, the resin and preform of fibers being substantially transparent to form a see through window portion in the skin panel.
14. The method of manufacturing a transparent skin panel of claim 13, wherein the preform of fibers includes a weave of glass fibers.
15. The method of manufacturing a transparent skin panel of claim 13, wherein providing a preform, providing a metal sheet, and inserting the preform and the metal sheet into the mold are repeated to produce a series of layers of alternating preforms and metal sheets.
16. The method of manufacturing a transparent skin panel of claim 13, wherein the preform of fibers has an index of refraction matching an index of refraction of the resin.
17. The method of manufacturing a transparent skin panel of claim 13, wherein the resin comprises an aliphatic epoxy.
18. The method of manufacturing a transparent skin panel of claim 13, wherein the metal sheets are comprised of aluminum.
19. The method of manufacturing a transparent skin panel of claim 13, wherein the metal sheets are comprised of titanium.
CA2537945A 2003-09-04 2004-09-02 A resin infused transparent skin panel and method of making same Expired - Fee Related CA2537945C (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US10/655,257 2003-09-04
US10/655,257 US7300693B2 (en) 2003-09-04 2003-09-04 Resin infused transparent skin panel and method of making same
PCT/US2004/028549 WO2005056383A2 (en) 2003-09-04 2004-09-02 A resin infused transparent skin panel and method of making same

Publications (2)

Publication Number Publication Date
CA2537945A1 true CA2537945A1 (en) 2005-06-23
CA2537945C CA2537945C (en) 2010-11-23

Family

ID=34226094

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2537945A Expired - Fee Related CA2537945C (en) 2003-09-04 2004-09-02 A resin infused transparent skin panel and method of making same

Country Status (5)

Country Link
US (3) US7300693B2 (en)
EP (1) EP1663776B1 (en)
JP (1) JP4638434B2 (en)
CA (1) CA2537945C (en)
WO (1) WO2005056383A2 (en)

Families Citing this family (69)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9586699B1 (en) 1999-08-16 2017-03-07 Smart Drilling And Completion, Inc. Methods and apparatus for monitoring and fixing holes in composite aircraft
US7730680B2 (en) * 2001-03-14 2010-06-08 The Boeing Company Modular monolithic bulkhead panel
US9625361B1 (en) 2001-08-19 2017-04-18 Smart Drilling And Completion, Inc. Methods and apparatus to prevent failures of fiber-reinforced composite materials under compressive stresses caused by fluids and gases invading microfractures in the materials
US20050048260A1 (en) * 2003-08-27 2005-03-03 The Boeing Company Method and apparatus for fabricating a laminated fiber metal composite
US7300693B2 (en) * 2003-09-04 2007-11-27 The Boeing Company Resin infused transparent skin panel and method of making same
US8262823B2 (en) * 2003-09-04 2012-09-11 The Boeing Company Window skin panel and method of making same
US7661629B2 (en) * 2004-02-20 2010-02-16 The Boeing Company Systems and methods for destabilizing an airfoil vortex
DE05819580T1 (en) 2004-09-01 2008-04-24 Bell Helicopter Textron, Inc., Fort Worth Press-formed parts with an embedded conductor layer and manufacturing method therefor
US20070063393A1 (en) * 2005-09-22 2007-03-22 Nicolas Vernin Vacuum assisted resin transfer molding techniques with flow flooding chamber
US8491745B2 (en) 2007-02-03 2013-07-23 The Boeing Company Method and material efficient tooling for continuous compression molding
US8691137B2 (en) * 2009-03-04 2014-04-08 The Boeing Company Method of molding partus using a tool sleeve for mold die
US10449736B2 (en) 2006-02-02 2019-10-22 The Boeing Company Apparatus for fabricating thermoplastic composite parts
US10232532B1 (en) 2006-02-02 2019-03-19 The Boeing Company Method for fabricating tapered thermoplastic composite parts
US7807005B2 (en) * 2006-02-02 2010-10-05 The Boeing Company Fabrication process for thermoplastic composite parts
US8333858B2 (en) * 2006-02-02 2012-12-18 The Boeing Company Method for fabricating curved thermoplastic composite parts
US9102103B2 (en) * 2006-02-02 2015-08-11 The Boeing Company Thermoplastic composite parts having integrated metal fittings and method of making the same
DE102006025930B4 (en) * 2006-06-02 2008-09-11 Airbus Deutschland Gmbh Hull structure and method of making a hull structure
US8323436B2 (en) * 2007-03-28 2012-12-04 The United States Of America As Represented By The Secretary Of The Army Transparent, reinforced, composite fiber and articles made therefrom
US8449709B2 (en) * 2007-05-25 2013-05-28 The Boeing Company Method of fabricating fiber reinforced composite structure having stepped surface
ES2335837B1 (en) * 2007-06-29 2011-02-18 Airbus España, Sl. COVER FOR AIRCRAFT ACCESS MOUTH.
US8442804B2 (en) 2007-10-25 2013-05-14 The Boeing Company Method and apparatus for composite part data extraction
DE102008007545A1 (en) * 2008-02-05 2009-08-27 Airbus Deutschland Gmbh Load-bearing and damage tolerant laminate airplane window
US7963125B2 (en) * 2008-03-05 2011-06-21 The Boeing Company Glass fibers having improved strength
US7963126B2 (en) * 2008-03-05 2011-06-21 The Boeing Company Glass fibers having improved durability
US8370111B2 (en) * 2008-03-31 2013-02-05 The Boeing Company System and method for forming optimized perimeter surveillance
US8686854B2 (en) * 2008-03-31 2014-04-01 The Boeing Company System and method for forming optimized perimeter surveillance
US8997416B2 (en) 2008-07-15 2015-04-07 The Boeing Company Opaque fiber reinforcement of composites
US8210841B2 (en) * 2008-08-13 2012-07-03 University Of Delaware Apparatus and method for preform relaxation and flow control in liquid composite molding processes
WO2010039119A1 (en) * 2008-09-30 2010-04-08 Sikorsky Aircraft Corporation Pyrotechnic egress system
US8210953B1 (en) 2008-11-12 2012-07-03 Whitewater Composites Ltd. Translucent closed-molded fiber-reinforced plastic and method of making the same
NL2002289C2 (en) * 2008-12-04 2010-06-07 Gtm Holding B V Sandwich panel, support member for use in a sandwich panel and aircraft provided with such a sandwich panel.
EP2430251A4 (en) * 2009-05-13 2016-01-27 Hunter Douglas Ind Switzerland Structured-core laminate panels and methods of forming the same
WO2011022459A2 (en) * 2009-08-18 2011-02-24 University Of Delaware Computer controlled flow manipulation for vacuum infusion processes
MX2012003670A (en) * 2009-10-01 2012-06-27 Albany Eng Composites Inc Woven preform, composite, and method of making thereof.
EP2483045B1 (en) * 2009-10-01 2017-08-02 Albany Engineered Composites, Inc. Woven preform, composite, and method of making thereof
US8620627B2 (en) * 2009-10-13 2013-12-31 The Boeing Company Composite information display for a part
US10821653B2 (en) * 2010-02-24 2020-11-03 Alexander M. Rubin Continuous molding of thermoplastic laminates
US9434464B1 (en) 2010-07-15 2016-09-06 The Boeing Company Window exhibiting reduced sound transmission and method of making the same
US8652606B2 (en) 2010-08-17 2014-02-18 The Boeing Company Composite structures having composite-to-metal joints and method for making the same
US8993084B2 (en) 2010-08-17 2015-03-31 The Boeing Company Multi-layer metallic structure and composite-to-metal joint methods
US9522512B2 (en) 2010-08-17 2016-12-20 The Boeing Company Methods for making composite structures having composite-to-metal joints
US9079367B2 (en) 2010-08-25 2015-07-14 University Of Delaware Systems and methods for controlling permeability in vacuum infusion processes
EP2640919A4 (en) 2010-11-16 2018-01-10 The Nordam Group, Inc. Hybrid frame co-mold manufacture
FR2967644B1 (en) * 2010-11-19 2012-12-14 Airbus Operations Sas CABIN HALL WITH PROGRAMMED DEFORMATION, METHOD OF MANUFACTURING SUCH A DOOR AND AIRCRAFT INCORPORATING SUCH A HOBOT
JP5808111B2 (en) * 2011-02-04 2015-11-10 三菱重工業株式会社 Composite structure for aircraft, aircraft main wing and aircraft fuselage provided with the same
US20170088254A1 (en) * 2011-03-10 2017-03-30 RuiQing Hong Ultra-High-Pressure Fluid Injection Dynamic Orbit-Transfer System and Method
US8944381B2 (en) 2011-03-25 2015-02-03 The Boeing Company Aircraft window and installation method
TW201251558A (en) * 2011-06-14 2012-12-16 Compal Electronics Inc Method for manufacturing three-dimentional workpiece
US9097015B2 (en) 2011-10-12 2015-08-04 3Form, Llc Resin panels with embedded structured-cores and methods of making the same
EP2794395B1 (en) 2011-12-21 2018-10-10 Bombardier Inc. Drag neutral vehicle window
EP2730497B1 (en) * 2012-11-13 2017-04-19 Airbus Operations GmbH Aircraft window arrangement
US8973871B2 (en) * 2013-01-26 2015-03-10 The Boeing Company Box structures for carrying loads and methods of making the same
EP2974849B1 (en) * 2013-03-13 2018-07-04 Aisin Takaoka Co., Ltd. Composite structure of fiber-reinforced plastic sheet and metal sheet, and method for manufacturing same
DE102013012005B4 (en) * 2013-07-18 2022-05-05 Technische Universität München Process for manufacturing a component from a fiber composite material
US9383173B2 (en) * 2013-07-22 2016-07-05 The United States Of America As Represented By The Secretary Of The Army Transparent armor construction
CN104401478B (en) * 2014-11-27 2017-03-08 江西洪都航空工业集团有限责任公司 A kind of abdominal part big opening electromotor force-bearing quick release cabin door structure
DE102015101884B4 (en) 2015-02-10 2023-02-23 Deutsches Zentrum für Luft- und Raumfahrt e.V. Method for manufacturing a component from a fiber-plastic composite and device
DE102015110165B4 (en) * 2015-06-24 2017-03-02 Airbus Operations Gmbh Skin panel window unit for an aircraft
US10112695B2 (en) * 2015-08-20 2018-10-30 Georgian Aerospace Llc Receptacle, payload assembly and related methods for an aircraft
EP3159149A1 (en) * 2015-10-12 2017-04-26 C&D Zodiac, Inc. Aircraft panel assembly with reinforcement layers
EP3173331B1 (en) * 2015-11-30 2019-04-24 Airbus Operations GmbH Cover panel for a structural component
GB201522539D0 (en) * 2015-12-21 2016-02-03 Hexcel Composites Ltd Improvements in or relating to electrically conducting materials
ES2822933T3 (en) * 2016-11-04 2021-05-05 Airbus Operations Sl Panel structure for an aircraft and its manufacturing process
US10532539B2 (en) * 2017-01-12 2020-01-14 Ford Global Technologies, Llc Thermal and mechanical shock resistant laminated metal plate assembly
JP6584444B2 (en) * 2017-03-22 2019-10-02 アイシン高丘株式会社 Method for manufacturing composite structure
US11192333B2 (en) * 2018-10-25 2021-12-07 Honda Motor Co., Ltd. Embedded metal transition for joining fiber reinforced polymers and metallic structures
CN110014671A (en) * 2019-04-17 2019-07-16 中国科学院长春应用化学研究所 A kind of high light transmission impact resins-screw type nano-fiber composite film, preparation method and its application
NL2023482B1 (en) * 2019-07-11 2021-02-03 Dutch Thermoplastic Components B V Thermoplastic composite product
GB2609219A (en) * 2021-07-22 2023-02-01 Aston Martin Lagonda Ltd Method of manufacturing reinforced lightweight composites

Family Cites Families (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US690101A (en) * 1901-04-24 1901-12-31 Warren Earl Cooper Shaving-cup.
US3081205A (en) * 1959-06-15 1963-03-12 Pittsburgh Plate Glass Co Safety glass glazing unit
US5128678A (en) * 1963-07-17 1992-07-07 The Boeing Company Aircraft construction
US3584567A (en) * 1969-11-12 1971-06-15 Us Army Automatic shutter
NL8100088A (en) * 1981-01-09 1982-08-02 Tech Hogeschool Delft Afdeling LAMINATE OF METAL SHEETS AND CONNECTED WIRES, AND METHODS FOR MANUFACTURE THEREOF
JP2569577B2 (en) 1987-07-31 1997-01-08 日本電気株式会社 Line quality monitoring device
DE3876371T2 (en) * 1987-10-14 1993-05-13 Structural Laminates Co LAMINATE FROM METAL LAYERS AND FROM CONTINUOUS, FIBER REINFORCED, SYNTHETIC, THERMOPLASTIC MATERIAL AND METHOD FOR THE PRODUCTION THEREOF.
ATE78225T1 (en) * 1987-12-31 1992-08-15 Structural Laminates Co COMPOSITE LAMINATE OF METAL LAYERS AND PLASTIC LAYERS REINFORCED WITH CONTINUOUS THREADS.
US4964594A (en) * 1988-04-11 1990-10-23 Texstar, Inc. Blind fastener having special utility in the installation of transparencies in aircraft and the like
US5039566A (en) * 1988-06-27 1991-08-13 Mcdonnell Douglas Corporation Transparent composite material
US5160771A (en) * 1990-09-27 1992-11-03 Structural Laminates Company Joining metal-polymer-metal laminate sections
US5429326A (en) * 1992-07-09 1995-07-04 Structural Laminates Company Spliced laminate for aircraft fuselage
US5665450A (en) * 1992-08-21 1997-09-09 The Curators Of The University Of Missouri Optically transparent composite material and process for preparing same
US5951800A (en) * 1992-11-18 1999-09-14 Mcdonnell Douglas Corp. Fiber/metal laminate splice
US5547735A (en) * 1994-10-26 1996-08-20 Structural Laminates Company Impact resistant laminate
DE4443355A1 (en) 1994-12-06 1996-06-13 Roehm Gmbh Aircraft glazing with increased light stability, improved chemical stability and improved heat resistance
US5500272A (en) * 1995-01-11 1996-03-19 Northrop Grumman Corporation High efficiency load transfer in composite structure
US5958325A (en) * 1995-06-07 1999-09-28 Tpi Technology, Inc. Large composite structures and a method for production of large composite structures incorporating a resin distribution network
JPH1036139A (en) 1996-07-24 1998-02-10 Mitsubishi Heavy Ind Ltd Reinforced plate
DE19650416B4 (en) * 1996-12-05 2004-10-07 Airbus Deutschland Gmbh Window for an airplane with a pressurized cabin
US6082674A (en) * 1998-09-16 2000-07-04 Mcdonnel Douglas Corporation Aircraft window escuthcheon assembly
WO2000020275A2 (en) 1998-10-06 2000-04-13 Williams International Co., L.L.C. Aircraft window
TW476704B (en) * 2001-01-11 2002-02-21 Jing-Fa Ju Manufacturing method and structure of mass-producible fiber reinforced plastic plates
US6648273B2 (en) * 2001-10-30 2003-11-18 The Boeing Company Light weight and high strength fuselage
US6818306B2 (en) * 2002-09-27 2004-11-16 The Boeing Company Optically clear structural laminate
US6914781B2 (en) * 2003-04-25 2005-07-05 The Boeing Company Fixture and method for quick installation and removal of mobile platform electronic modules
US7189345B2 (en) * 2003-08-13 2007-03-13 The Boeing Company Method for vacuum assisted resin transfer molding
US20050048260A1 (en) * 2003-08-27 2005-03-03 The Boeing Company Method and apparatus for fabricating a laminated fiber metal composite
US7300693B2 (en) * 2003-09-04 2007-11-27 The Boeing Company Resin infused transparent skin panel and method of making same
US8262823B2 (en) * 2003-09-04 2012-09-11 The Boeing Company Window skin panel and method of making same
US6889938B1 (en) * 2003-10-21 2005-05-10 The Boeing Company Structural cockpit window and method of making same
US7028950B2 (en) * 2004-05-10 2006-04-18 The Boeing Company Load bearing window
DE102005010252A1 (en) * 2004-08-04 2006-03-16 Schierholt, Johannes, Dipl.-Ing. Transparent window pane material, for pressurized aircraft/submarines and the like, has outer layers of thin glass with inner layers of transparent fibers embedded in a transparent matrix

Also Published As

Publication number Publication date
US20070034743A1 (en) 2007-02-15
JP4638434B2 (en) 2011-02-23
WO2005056383A9 (en) 2005-08-11
US20050053765A1 (en) 2005-03-10
EP1663776A2 (en) 2006-06-07
CA2537945C (en) 2010-11-23
US7651756B2 (en) 2010-01-26
US20080131661A1 (en) 2008-06-05
US7968170B2 (en) 2011-06-28
JP2007504049A (en) 2007-03-01
WO2005056383A2 (en) 2005-06-23
US7300693B2 (en) 2007-11-27
EP1663776B1 (en) 2012-11-07
WO2005056383A3 (en) 2005-12-08

Similar Documents

Publication Publication Date Title
CA2537945A1 (en) A resin infused transparent skin panel and method of making same
US7790637B2 (en) Composite laminate having an improved cosmetic surface and method of making same
AU596122B2 (en) Coated optical fiber
AU2009202514B2 (en) Opaque fiber reinforcement of composites
WO2007140978A1 (en) Method for producing a glass pane
EP0945479A3 (en) Composite structural components containing thermotropic liquid crystalline polymer reinforcements for optical fiber cables
CN110494286A (en) With bending cover glass and display or the vehicle interior system of touch panel and forming method thereof
CN106660280A (en) A method of making frame components for spectacles and a component made by this method
EP2674294B1 (en) Bicomponent Fibers Containing Nano-Filaments For Use In Optically Transparent Composites
CN105258567A (en) Flexible stab-resistant material and preparation method thereof
CN101959815B (en) Glass fibers having improved strength
US20050051255A1 (en) Window skin panel and method of making same
CN106232537A (en) For the method forming optical fiber and prefabricated component
CN113514963B (en) Double-optical-film-layer color-changing lens and preparation method thereof
ITPD20120124A1 (en) PROCEDURE FOR REALIZING COMPONENTS OF FRAMES OF GLASSES AND COMPONENTS MADE WITH THIS PROCEDURE
CN102970837A (en) Rigid reinforced composite material and manufacturing method thereof
DE102012004635B4 (en) Display and / or control element for a motor vehicle with a three-dimensionally shaped glass body
DE102014226529A1 (en) CFRP-reinforced semi-transparent flat component, and a method for its production
JP4232537B2 (en) Laminated glass manufacturing method
CN211222379U (en) Window glass structure and vehicle comprising window glass structure
CA2362235A1 (en) Fibre reinforced composites and method of making same
CN216356843U (en) Take anti cell-phone shell of buckling of surrounding bone
CN2787558Y (en) Upright tube of bicycle front fork made of composite materials
JP2881026B2 (en) Method for producing sheet for molding fiber-reinforced resin
CN112389058A (en) Window glass structure, manufacturing method thereof and vehicle comprising window glass structure

Legal Events

Date Code Title Description
EEER Examination request
MKLA Lapsed

Effective date: 20220302

MKLA Lapsed

Effective date: 20200902