AU585055B2 – Improvements relating to the joining of aircraft skin panels of the sandwich type to frame elements
– Google Patents
AU585055B2 – Improvements relating to the joining of aircraft skin panels of the sandwich type to frame elements
– Google Patents
Improvements relating to the joining of aircraft skin panels of the sandwich type to frame elements
Info
Publication number
AU585055B2
AU585055B2
AU61763/86A
AU6176386A
AU585055B2
AU 585055 B2
AU585055 B2
AU 585055B2
AU 61763/86 A
AU61763/86 A
AU 61763/86A
AU 6176386 A
AU6176386 A
AU 6176386A
AU 585055 B2
AU585055 B2
AU 585055B2
Authority
AU
Australia
Prior art keywords
joining
frame elements
improvements relating
sandwich type
aircraft skin
Prior art date
1985-07-15
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.)
Ceased
Application number
AU61763/86A
Other versions
AU6176386A
(en
Inventor
Paul James Jonas
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.)
Beechcraft Corp
Original Assignee
Beech Aircraft Corp
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.)
1985-07-15
Filing date
1986-08-22
Publication date
1989-06-08
Family has litigation
First worldwide family litigation filed
litigation
Critical
https://patents.darts-ip.com/?family=25037085&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=AU585055(B2)
“Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
1986-08-22
Application filed by Beech Aircraft Corp
filed
Critical
Beech Aircraft Corp
1988-02-25
Publication of AU6176386A
publication
Critical
patent/AU6176386A/en
1989-06-08
Application granted
granted
Critical
1989-06-08
Publication of AU585055B2
publication
Critical
patent/AU585055B2/en
2006-08-22
Anticipated expiration
legal-status
Critical
Status
Ceased
legal-status
Critical
Current
Links
Espacenet
Global Dossier
Discuss
Classifications
D—TEXTILES; PAPER
D03—WEAVING
D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
D03D25/00—Woven fabrics not otherwise provided for
D03D25/005—Three-dimensional woven fabrics
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
B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
B29C65/50—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like
B29C65/5007—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like characterised by the structure of said adhesive tape, threads or the like
B29C65/5028—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like characterised by the structure of said adhesive tape, threads or the like being textile in woven or non-woven form
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
B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
B29C65/50—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like
B29C65/5064—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like of particular form, e.g. being C-shaped, T-shaped
B29C65/5071—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like of particular form, e.g. being C-shaped, T-shaped and being composed by one single element
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
B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
B29C65/50—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like
B29C65/5064—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like of particular form, e.g. being C-shaped, T-shaped
B29C65/5085—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like of particular form, e.g. being C-shaped, T-shaped and comprising grooves, e.g. being E-shaped, H-shaped
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
B29C66/00—General aspects of processes or apparatus for joining preformed parts
B29C66/01—General aspects dealing with the joint area or with the area to be joined
B29C66/05—Particular design of joint configurations
B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
B29C66/112—Single lapped joints
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
B29C66/00—General aspects of processes or apparatus for joining preformed parts
B29C66/01—General aspects dealing with the joint area or with the area to be joined
B29C66/05—Particular design of joint configurations
B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
B29C66/114—Single butt joints
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
B29C66/00—General aspects of processes or apparatus for joining preformed parts
B29C66/01—General aspects dealing with the joint area or with the area to be joined
B29C66/05—Particular design of joint configurations
B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
B29C66/114—Single butt joints
B29C66/1142—Single butt to butt joints
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
B29C66/00—General aspects of processes or apparatus for joining preformed parts
B29C66/01—General aspects dealing with the joint area or with the area to be joined
B29C66/05—Particular design of joint configurations
B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
B29C66/12—Joint cross-sections combining only two joint-segments; Tongue and groove joints; Tenon and mortise joints; Stepped joint cross-sections
B29C66/124—Tongue and groove joints
B29C66/1244—Tongue and groove joints characterised by the male part, i.e. the part comprising the tongue
B29C66/12443—Tongue and groove joints characterised by the male part, i.e. the part comprising the tongue having the tongue substantially in the middle
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
B29C66/00—General aspects of processes or apparatus for joining preformed parts
B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles
B29C66/43—Joining a relatively small portion of the surface of said articles
B29C66/432—Joining a relatively small portion of the surface of said articles for making tubular articles or closed loops, e.g. by joining several sheets ; for making hollow articles or hollow preforms
B29C66/4326—Joining a relatively small portion of the surface of said articles for making tubular articles or closed loops, e.g. by joining several sheets ; for making hollow articles or hollow preforms for making hollow articles or hollow-preforms, e.g. half-shells
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
B29C66/00—General aspects of processes or apparatus for joining preformed parts
B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles
B29C66/43—Joining a relatively small portion of the surface of said articles
B29C66/434—Joining substantially flat articles for forming corner connections, fork connections or cross connections
B29C66/4344—Joining substantially flat articles for forming fork connections, e.g. for making Y-shaped pieces
B29C66/43441—Joining substantially flat articles for forming fork connections, e.g. for making Y-shaped pieces with two right angles, e.g. for making T-shaped pieces, H-shaped pieces
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
B29C66/00—General aspects of processes or apparatus for joining preformed parts
B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles
B29C66/43—Joining a relatively small portion of the surface of said articles
B29C66/434—Joining substantially flat articles for forming corner connections, fork connections or cross connections
B29C66/4346—Joining substantially flat articles for forming cross connections, e.g. for making X-shaped pieces
B29C66/43461—Joining substantially flat articles for forming cross connections, e.g. for making X-shaped pieces with four right angles, e.g. for making +-shaped pieces
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
B29C66/00—General aspects of processes or apparatus for joining preformed parts
B29C66/50—General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
B29C66/51—Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
B29C66/54—Joining several hollow-preforms, e.g. half-shells, to form hollow articles, e.g. for making balls, containers; Joining several hollow-preforms, e.g. half-cylinders, to form tubular 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
B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
B29C70/22—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure
B29C70/222—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure the structure being shaped to form a three dimensional configuration
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
B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
B29C70/24—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least three directions forming a three dimensional structure
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
B29D24/004—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled the structure having vertical or oblique ribs
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
B29D99/00—Subject matter not provided for in other groups of this subclass
B29D99/0003—Producing profiled members, e.g. beams
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
B29D99/00—Subject matter not provided for in other groups of this subclass
B29D99/001—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
B29D99/0014—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with ridges or ribs, e.g. joined ribs
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
B64C3/00—Wings
B64C3/18—Spars; Ribs; Stringers
D—TEXTILES; PAPER
D03—WEAVING
D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
D03D11/00—Double or multi-ply fabrics not otherwise provided for
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
B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
B29C65/4805—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the type of adhesives
B29C65/483—Reactive adhesives, e.g. chemically curing adhesives
B29C65/4835—Heat curing adhesives
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
B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
B29C65/50—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like
B29C65/5007—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like characterised by the structure of said adhesive tape, threads or the like
B29C65/5035—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like characterised by the structure of said adhesive tape, threads or the like being in thread form, i.e. in the form of a single filament, e.g. in the form of a single coated filament
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
B29C66/00—General aspects of processes or apparatus for joining preformed parts
B29C66/01—General aspects dealing with the joint area or with the area to be joined
B29C66/05—Particular design of joint configurations
B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
B29C66/12—Joint cross-sections combining only two joint-segments; Tongue and groove joints; Tenon and mortise joints; Stepped joint cross-sections
B29C66/124—Tongue and groove joints
B29C66/1244—Tongue and groove joints characterised by the male part, i.e. the part comprising the tongue
B29C66/12441—Tongue and groove joints characterised by the male part, i.e. the part comprising the tongue being a single wall
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
B29C66/00—General aspects of processes or apparatus for joining preformed parts
B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
B29C66/729—Textile or other fibrous material made from plastics
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
B29L2024/00—Articles with hollow walls
B29L2024/006—Articles with hollow walls multi-channelled
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
B64—AIRCRAFT; AVIATION; COSMONAUTICS
B64C—AEROPLANES; HELICOPTERS
B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
B64C2001/0054—Fuselage structures substantially made from particular materials
B64C2001/0072—Fuselage structures 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
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.]
Y10T428/24149—Honeycomb-like
AU61763/86A
1985-07-15
1986-08-22
Improvements relating to the joining of aircraft skin panels of the sandwich type to frame elements
Ceased
AU585055B2
(en)
Applications Claiming Priority (1)
Application Number
Priority Date
Filing Date
Title
US06/754,951
US4671470A
(en)
1985-07-15
1985-07-15
Method for fastening aircraft frame elements to sandwich skin panels covering same using woven fiber connectors
Publications (2)
Publication Number
Publication Date
AU6176386A
AU6176386A
(en)
1988-02-25
AU585055B2
true
AU585055B2
(en)
1989-06-08
Family
ID=25037085
Family Applications (1)
Application Number
Title
Priority Date
Filing Date
AU61763/86A
Ceased
AU585055B2
(en)
1985-07-15
1986-08-22
Improvements relating to the joining of aircraft skin panels of the sandwich type to frame elements
Country Status (6)
Country
Link
US
(1)
US4671470A
(en)
EP
(1)
EP0257148B1
(en)
AU
(1)
AU585055B2
(en)
DE
(2)
DE3685586T2
(en)
FR
(1)
FR2603249B1
(en)
GB
(1)
GB2193698B
(en)
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1986-08-01
1989-11-24
Brochier Sa
MULTIDIMENSIONAL TEXTILE STRUCTURE FOR REINFORCING LAMINATE MATERIALS AND A WEAVING METHOD AND MATERIAL FOR OBTAINING SUCH A STRUCTURE
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1987-10-15
1990-03-20
The Boeing Company
Reinforced honeycomb core sandwich panels and method for making same
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1988-02-19
1993-11-11
Mitsubishi Heavy Ind Ltd
Textile structure for reinforcing structural elements, such as beams, from composite materials and processes for producing the same.
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1988-02-29
1995-10-04
三菱重工業株式会社
Three-dimensional fabric with irregular cross section
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1988-02-29
1994-09-06
Mitsubishi Jukogyo Kabushiki Kaisha
Profiled cross-section three dimensional woven fabric
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1990-01-02
1994-01-11
Tomkins Keith A
Multiple-layer structures and joining method for honeycomb, foam and lightweight materials
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1991-04-05
1997-07-08
The Boeing Company
Retort for achieving thermal uniformity in induction processing of organic matrix composites or metals
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1991-04-05
1998-09-15
The Boeing Company
Multilayer susceptors for achieving thermal uniformity in induction processing of organic matrix composites or metals
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1991-04-05
1998-08-11
The Boeing Company
Bonding using induction heating
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1991-04-05
1998-01-20
The Boeing Company
Internal tooling for induction heating
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1991-04-05
1998-03-03
The Boeing Company
Reinforced susceptor for induction or resistance welding of thermoplastic composites
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1991-04-05
2006-10-24
Th Boeing Company
Resistance welding of thermoplastics in aerospace structure
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1991-04-05
1997-04-29
The Boeing Company
Fixed coil induction heater for thermoplastic welding
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1991-10-18
1996-03-19
The Boeing Company
Tailored susceptors for induction welding of thermoplastic
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1992-02-11
1995-09-22
Aerospatiale
PROCESS FOR THE PRODUCTION OF A FIBER REINFORCEMENT FOR A COMPOSITE MATERIAL WITH NON-COPLANAR WALLS, AND A COMPOSITE PART COMPRISING SUCH A REINFORCEMENT.
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1994-05-21
2006-04-13
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1994-09-28
1998-01-20
The Boeing Company
Fluid tooling for thermoplastic welding
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1994-12-09
1997-08-26
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1995-01-03
1996-11-12
Lunden; C. David
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1995-06-06
2003-08-05
The Boeing Company
Method for alleviating residual tensile strain in thermoplastic welds
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1995-06-06
1998-01-06
The Boeing Company
Gap filling for thermoplastic welds
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1995-06-06
1998-02-10
The Boeing Company
Structural susceptor for thermoplastic welding
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(en)
*
1995-06-07
1998-05-26
The Boeing Company
Barbed susceptor for improviing pulloff strength in welded thermoplastic composite structures
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1995-06-07
1998-11-03
The Boeing Company
Welded aerospace structure using a hybrid metal webbed composite beam
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1995-06-29
1997-08-19
Hexcel-Fyfe Co., L.L.C.
Fabric reinforced beam and column connections
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1995-10-26
1998-06-02
The Boeing Company
Monitoring the bond line temperature in thermoplastic welds
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1995-11-06
1998-07-28
The Boeing Company
Self-steering system for guiding a moving induction coil during thermoplastic welding
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(en)
*
1996-06-06
1999-06-29
The Boeing Company
Susceptor integration into reinforced thermoplastic composites
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(en)
*
1996-07-29
1999-02-09
The Boeing Company
Post-weld annealing of thermoplastic welds
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1996-09-03
1999-05-11
Georgeson; Gary E.
Nondestructive evaluation of composite bonds, especially thermoplastic induction welds
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1996-10-07
1997-12-16
The Boeing Company
Apparatus and methods of providing corrosion resistant conductive path across non conductive joints or gaps
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1997-07-16
1998-08-20
Deutsch Zentr Luft & Raumfahrt
Structural element, e.g wing panel for aircraft
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1997-12-23
2001-09-04
The Boeing Company
Thermoplastic seam welds
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1998-09-22
2001-08-21
Elbert Rutan
Tensioned structural composite joint
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1998-10-05
2005-05-19
Deutsches Zentrum für Luft- und Raumfahrt e.V.
Structural element with large unidirectional stiffness
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1999-07-19
2003-02-04
Fuji Jukogyo Kabushiki Kaisha
Wing of composite material and method of fabricating the same
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2000-09-20
2004-06-01
Bally Ribbon Mills
Three-dimensional woven forms with integral bias fibers and bias weaving loom
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2001-01-16
2005-02-01
Lockheed Martin Corporation
System and method of forming structural assemblies with 3-D woven joint pre-forms
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2001-05-21
2009-04-21
Lockheed Martin Corporation
Embedded connector attached to a base panel
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2001-06-15
2004-03-30
Lockheed Martin Corporation
Three-dimensional weave architecture
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2001-08-23
2005-03-08
Lockheed Martin Corporation
Paste-bond clevis joint
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2001-08-28
2004-01-13
Lockheed Martin Corporation
Methods of hot-melt resin impregnation of 3-D, woven, textile preforms
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2001-09-12
2003-03-20
Lockheed Martin Corporation
Woven preform for structural joints
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2001-10-09
2004-11-23
Lockheed Martin Corporation
Co-bonded joint with Z-pins
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2001-10-16
2003-05-22
Bushey Richard D.
Floor grid system
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2001-12-21
2003-06-26
Sheahen Patrick D.
Low-cost method of assembling structures with 3-D woven connectors
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2002-05-23
2007-07-03
Rohr, Inc.
Structural element with rib-receiving member
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2002-07-19
2005-09-20
The Boeing Company
Apparatuses and methods for joining structural members, such as composite structural members
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2002-08-05
2004-02-05
Bersuch Larry R.
Z-pin closeout joint and method of assembly
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2002-09-13
2004-06-15
The Boeing Company
Composite assembly with integrated composite joints
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2002-09-20
2007-04-03
The Boeing Company
Internally stiffened composite panels and methods for their manufacture
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2003-04-18
2005-03-29
The Boeing Company
Apparatus and methods of attaching panels to support structures
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2004-04-30
2005-11-10
Indian Institute Of Technology, Bombay
Novel strength enhancing insert assemblies
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2004-12-02
2007-07-24
Siemens Power Generation, Inc.
Stacked lamellate assembly
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2005-04-07
2009-08-18
The Boeing Company
Composite-to-metal joint
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2005-11-03
2008-08-19
Albany Engineered Composites, Inc.
Corner fitting using fiber transfer
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2006-01-27
2009-10-09
Eurocopter France
IMPROVED COMPOSITE STRUCTURE FOR AIRCRAFT.
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2006-06-15
2011-02-15
The Boeing Company
Internal finger joint
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2006-06-19
2011-05-03
United Technologies Corporation
Repair of composite sandwich structures
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2006-07-05
2010-09-07
Lockheed Martin Corporation
System, method, and apparatus for three-dimensional woven metal preform structural joint
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2006-10-27
2009-03-20
Airbus France Sas
THREE DIMENSIONAL SURFACING WEAVING
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2006-11-02
2010-10-12
The Boeing Company
Mounting device for an aircraft
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2007-04-05
2013-07-23
The Boeing Company
Methods and systems for composite structural truss
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2007-04-05
2011-06-07
The Boeing Company
Methods and systems for composite structural truss
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2008-11-28
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Method for manufacturing an object from a sandwich structure with a reinforced angle and such an object.
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2007-05-31
2011-12-27
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Apparatus and methods for securing a first structural member and a second structural member to one another
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2007-06-28
2010-09-14
Airbus España S.L.
RIGIDIZED MULTILARGUERO TORSION DRAWER.
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2007-10-25
2012-08-07
The Boeing Company
Method to create bends in composite panels
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2007-10-25
2012-11-20
The Boeing Company
Method for forming bends in composite panels and composite panels made thereby
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2010-05-11
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Fiber architecture for Pi-preforms
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2008-06-30
2011-12-20
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Monolithic integrated structural panels especially useful for aircraft structures
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2008-12-07
2013-06-18
Norduyn Inc.
Modular utility cart
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2009-04-16
2011-12-27
United Technologies Corporation
Hybrid structure fan blade
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2009-04-16
2013-11-19
United Technologies Corporation
Hybrid structure airfoil
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2009-12-04
2015-03-31
The Boeing Company
Sandwich structure having arrestment feature and method of making the same
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2010-10-28
2010-12-08
Airbus Operations Ltd
Wing tip device attachment apparatus and method
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2010-12-28
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Bell Helicopter Textron Inc.
Multi-directional load joint system
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2011-05-20
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Rohr, Inc.
Reinforcement members for aircraft propulsion system components configured to address delamination of the inner fixed structure
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General Electric Company
Wind turbine blade shear web connection assembly
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2011-07-19
2013-03-12
General Electric Company
Wind turbine blade shear web connection assembly
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2011-10-13
2012-11-29
Airbus Operations Gmbh
Producing component for connecting structures at crossing regions of component, comprises depositing first and second fibers on base, connecting them along overlap region, in which first and second fibers overlaps, and pivoting the fibers
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2011-10-13
2013-04-18
Airbus Operations Gmbh
Method for producing a component for connecting structures, components and structural arrangements
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Airbus Operations Gmbh
Component, reinforcing member, structure assembly, aircraft or spacecraft and method
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2011-10-13
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Airbus Operations Gmbh
Structural assembly for e.g. aircraft, has fiber section having outer rib in which attachment point is formed so that load applied on attachment point formed in outer rib is transferred by another fiber section to support element
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Airbus Operations Sas
ANTI-SPEED AIRCRAFT FUSELAGE STRUCTURE ELEMENT
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2012-05-29
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Airbus Operations Sas
METHOD AND DEVICE FOR MAKING A SELF-RAIDI COMPOSITE PANEL
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2012-05-30
2016-05-31
The Boeing Company
Bonded composite airfoil
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2012-07-31
2016-08-17
東芝機械株式会社
Machine tool manufacturing method
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2012-12-19
2015-11-11
横浜ゴム株式会社
Connection structure for aircraft interior panels
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2013-03-13
2014-09-18
Gulfstream Aerospace Corporation
Aircraft component and method of making an aircraft component
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2013-03-27
2015-11-18
Airbus Operations GmbH
Composite reinforcement component, structural element, aircraft or spacecraft and method for producing a composite reinforcement component
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2016-11-29
General Electric Company
Method for installing a shear web insert within a segmented rotor blade assembly
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2013-09-04
2021-06-15
Biteam Ab
Method and means for weaving a 3d fabric, 3d fabric items thereof and their use
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三菱重工業株式会社
Joints and aircraft structures
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2013-10-11
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The Boeing Company
Bends in composite panels
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The Boeing Company
Corner tension fitting
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Vestas Wind Systems A/S
Manufacture of wind turbine blades
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2017-05-23
2020-02-25
General Electric Company
Joint assembly for a wind turbine rotor blade with flanged bushings
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2017-07-27
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General Electric Company
Injection method and device for connecting and repairing a shear web
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Textron Innovations Inc.
Tiltrotor aircraft wings having buckle zones
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2017-08-07
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General Electric Company
Joint assembly for a wind turbine rotor blade
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Northrop Grumman Systems Corporation
Aircraft full depth pi preform joints
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Caisson of wing detachable part
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Univ Delft Tech
Method for making a virgin joint between two separate structural hollow sections, and such a virgin joint
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2022-05-03
Airbus Operations Gmbh
Wing arrangement for an aircraft
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Airbus Operations Gmbh
Latching device for a wing arrangement for an aircraft
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Airbus Operations Gmbh
Wing arrangement for an aircraft and aircraft
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Airbus Operations GmbH
Arresting system for arresting a first aircraft component relative to a second aircraft component
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Airbus Operations Ltd
Aircraft assembly
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2023-10-24
Rtx Corporation
Multi-material vane for a gas turbine engine
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2023-02-07
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Multi-material vane for a gas turbine engine
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Also Published As
Publication number
Publication date
DE3685586D1
(en)
1992-07-09
GB2193698A
(en)
1988-02-17
GB2193698B
(en)
1990-09-26
FR2603249B1
(en)
1988-12-09
GB8620005D0
(en)
1986-09-24
EP0257148B1
(en)
1992-06-03
US4671470A
(en)
1987-06-09
FR2603249A1
(en)
1988-03-04
DE3685586T2
(en)
1993-01-21
DE8623542U1
(en)
1988-01-07
EP0257148A1
(en)
1988-03-02
AU6176386A
(en)
1988-02-25
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