GB860391A - A method of manufacturing aeroplane wings and tail units - Google Patents

A method of manufacturing aeroplane wings and tail units

Info

Publication number
GB860391A
GB860391A GB2304/58A GB230458A GB860391A GB 860391 A GB860391 A GB 860391A GB 2304/58 A GB2304/58 A GB 2304/58A GB 230458 A GB230458 A GB 230458A GB 860391 A GB860391 A GB 860391A
Authority
GB
United Kingdom
Prior art keywords
tail units
manufacturing
core
fischer
jan
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
Application number
GB2304/58A
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.)
BERNHARD SCHULZ WILMERT
Original Assignee
BERNHARD SCHULZ WILMERT
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 BERNHARD SCHULZ WILMERT filed Critical BERNHARD SCHULZ WILMERT
Publication of GB860391A publication Critical patent/GB860391A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/26Construction, shape, or attachment of separate skins, e.g. panels
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C44/00Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles
    • B29C44/02Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles for articles of definite length, i.e. discrete articles
    • B29C44/12Incorporating or moulding on preformed parts, e.g. inserts or reinforcements
    • B29C44/1228Joining preformed parts by the expanding material
    • B29C44/1242Joining preformed parts by the expanding material the preformed parts being concentric
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/68Shaping 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
    • B29C70/86Incorporated in coherent impregnated reinforcing layers, e.g. by winding
    • B29C70/865Incorporated in coherent impregnated reinforcing layers, e.g. by winding completely encapsulated
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29DPRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00Subject matter not provided for in other groups of this subclass
    • B29D99/0025Producing blades or the like, e.g. blades for turbines, propellers, or wings
    • B29D99/0028Producing blades or the like, e.g. blades for turbines, propellers, or wings hollow blades
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10Manufacturing or assembling aircraft, e.g. jigs therefor
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING 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
    • B29K2067/00Use of polyesters or derivatives thereof, as moulding material
    • B29K2067/06Unsaturated polyesters
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING 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
    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/04Condition, form or state of moulded material or of the material to be shaped cellular or porous
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING 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
    • B29K2309/00Use of inorganic materials not provided for in groups B29K2303/00 - B29K2307/00, as reinforcement
    • B29K2309/08Glass
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING 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
    • B29K2705/00Use of metals, their alloys or their compounds, for preformed parts, e.g. for inserts
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/40Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)
  • Toys (AREA)
  • Laminated Bodies (AREA)

Abstract

860,391. Moulding aerofoils. FISCHER, H. O., and SCHULZ-WILMERT, B., [trading as RHEIN - WEST - FLUG FISCHER & CO.]. Jan. 23, 1958 [Jan. 23, 1957], No. 2304/58. Class 87(2). [Also in Group XXXIII] A method of making aeroplane wing or tail units comprises forming a light metal core consisting of two interconnected hollow members 1, 2, inserting the core into a mould 12, 13 provided with a layer of plastic material 14 and filling the space between the layer 14 and the core 1, 2 with a foamed plastic material to mould the article. The lining may be glass fibre reinforced ployester resin.
GB2304/58A 1957-01-23 1958-01-23 A method of manufacturing aeroplane wings and tail units Expired GB860391A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DER20391A DE1059770B (en) 1957-01-23 1957-01-23 Process for the production of aircraft wings and tail surfaces

Publications (1)

Publication Number Publication Date
GB860391A true GB860391A (en) 1961-02-01

Family

ID=7400657

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2304/58A Expired GB860391A (en) 1957-01-23 1958-01-23 A method of manufacturing aeroplane wings and tail units

Country Status (2)

Country Link
DE (1) DE1059770B (en)
GB (1) GB860391A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3301926A (en) * 1964-04-08 1967-01-31 Gateway Erectors Inc Method of fabricating a self-braced concrete form
US3328496A (en) * 1963-11-26 1967-06-27 Gen Am Transport Methods of making heat-insulated railway tank car bodies
DE1290709B (en) * 1963-01-11 1969-03-13 Bellanca August Thomas Elongated, double-shell lightweight body with a foam material intermediate layer
US3790421A (en) * 1970-07-08 1974-02-05 Plexawood Inc Composite articles and methods of making the same
US4462778A (en) * 1981-02-19 1984-07-31 Mario Calcagni Extrusion head for extruding mouldings for roller blinds, frames, finish and the like
WO2015124761A1 (en) * 2014-02-24 2015-08-27 Marine Current Turbines Limited Foam-filled turbine blade and method of manufacture
EP2162350A4 (en) * 2007-06-21 2017-06-07 Sikorsky Aircraft Corporation Method of forming panels using an in-situ tape placement process and panels formed therefrom

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1290709B (en) * 1963-01-11 1969-03-13 Bellanca August Thomas Elongated, double-shell lightweight body with a foam material intermediate layer
US3328496A (en) * 1963-11-26 1967-06-27 Gen Am Transport Methods of making heat-insulated railway tank car bodies
US3301926A (en) * 1964-04-08 1967-01-31 Gateway Erectors Inc Method of fabricating a self-braced concrete form
US3790421A (en) * 1970-07-08 1974-02-05 Plexawood Inc Composite articles and methods of making the same
US4462778A (en) * 1981-02-19 1984-07-31 Mario Calcagni Extrusion head for extruding mouldings for roller blinds, frames, finish and the like
EP2162350A4 (en) * 2007-06-21 2017-06-07 Sikorsky Aircraft Corporation Method of forming panels using an in-situ tape placement process and panels formed therefrom
WO2015124761A1 (en) * 2014-02-24 2015-08-27 Marine Current Turbines Limited Foam-filled turbine blade and method of manufacture

Also Published As

Publication number Publication date
DE1059770B (en) 1959-06-18

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