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GB545090A - Improvements in and relating to the forming of tubular or like members from impregnated fibrous material - Google Patents

Improvements in and relating to the forming of tubular or like members from impregnated fibrous material

Info

Publication number
GB545090A
GB545090A GB1682740A GB1682740A GB545090A GB 545090 A GB545090 A GB 545090A GB 1682740 A GB1682740 A GB 1682740A GB 1682740 A GB1682740 A GB 1682740A GB 545090 A GB545090 A GB 545090A
Authority
GB
United Kingdom
Prior art keywords
corrugations
fabric
fibrous material
core
mould
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
GB1682740A
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.)
Boulton Paul Aircraft Ltd
Original Assignee
Boulton Paul Aircraft Ltd
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 Boulton Paul Aircraft Ltd filed Critical Boulton Paul Aircraft Ltd
Priority to GB1682740A priority Critical patent/GB545090A/en
Publication of GB545090A publication Critical patent/GB545090A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • B29D23/00Producing tubular articles
    • B29D23/001Pipes; Pipe joints
    • 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
    • B29C63/00Lining or sheathing, i.e. applying preformed layers or sheathings of plastics; Apparatus therefor
    • B29C63/0017Lining or sheathing, i.e. applying preformed layers or sheathings of plastics; Apparatus therefor characterised by the choice of the material
    • 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
    • B29C63/00Lining or sheathing, i.e. applying preformed layers or sheathings of plastics; Apparatus therefor
    • B29C63/26Lining or sheathing of internal surfaces
    • B29C63/28Lining or sheathing of internal surfaces applied by "rubber" bag or diaphragm

Landscapes

  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Mechanical Engineering (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
  • Storage Of Web-Like Or Filamentary Materials (AREA)

Abstract

545,090. Tubular members of fibrous material. BOULTON PAUL AIRCRAFT, Ltd., and N ORTH, J. D. Nov. 22, 1940, No. 16827. [Class 99 (ii)] [Also in Groups V and XXXIII] Tubes or other hollow members, such as aircraft fuselages, planes and control surfaces are composed of an outer smooth shell 6 and an inner liner 4 having corrugations of flattened form, both composed of impregnated fibrous material, the structure being formed by compression under heat between a core 2 and an outer mould 1, with interposed wedges 3, 5 as shown. The core 2 may consist of an inflated bag, or a tapered core pressed axially may be used, the outer mould being then correspondingly tapered. The material consists of thin layers of wood, paper, fabric, felt &c. impregnated with a thermo-setting plastic material such as a phenol-formaldehyde condensation product, or with a thermo-plastic material such as a polyvinyl ester or co-polymer of vinyl esters. When made of fabric the shell 6 may be formed by winding a length of fabric. The heating may be effected by steam tubes or electrical heating-elements in or surrounding the mould, or by inflating the bag with hot gas. In aerofoils, the corrugations may become smaller towards the trailing edge, which is rounded sufficiently to permit of the continuation of the corrugations.
GB1682740A 1940-11-22 1940-11-22 Improvements in and relating to the forming of tubular or like members from impregnated fibrous material Expired GB545090A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1682740A GB545090A (en) 1940-11-22 1940-11-22 Improvements in and relating to the forming of tubular or like members from impregnated fibrous material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1682740A GB545090A (en) 1940-11-22 1940-11-22 Improvements in and relating to the forming of tubular or like members from impregnated fibrous material

Publications (1)

Publication Number Publication Date
GB545090A true GB545090A (en) 1942-05-11

Family

ID=10084395

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1682740A Expired GB545090A (en) 1940-11-22 1940-11-22 Improvements in and relating to the forming of tubular or like members from impregnated fibrous material

Country Status (1)

Country Link
GB (1) GB545090A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2454719A (en) * 1943-11-11 1948-11-23 Studebaker Corp Method of making cored laminated plastic sheets
US2523524A (en) * 1947-08-15 1950-09-26 Alexander H Kerr & Co Inc Wall panel forming machine
US2608502A (en) * 1947-02-15 1952-08-26 Glenn L Martin Co Honeycomb structure and method of making same
US2639248A (en) * 1949-07-27 1953-05-19 Us Plywood Corp Dielectric material
DE1072875B (en) * 1957-03-25 1960-01-07 Aktiebolaget Sveaexport, Stockholm Method and machine for manufacturing a tubular body
GB2225742A (en) * 1988-12-09 1990-06-13 Westland Helicopters Moulding a fibre reinforced composite, into a hollow structure comprising outer and inner skins connected by ribs
GB2479875A (en) * 2010-04-27 2011-11-02 Warren Barratt Leigh Corrugated internal structural body component for an airfoil, eg a wind turbine blade

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2454719A (en) * 1943-11-11 1948-11-23 Studebaker Corp Method of making cored laminated plastic sheets
US2608502A (en) * 1947-02-15 1952-08-26 Glenn L Martin Co Honeycomb structure and method of making same
US2523524A (en) * 1947-08-15 1950-09-26 Alexander H Kerr & Co Inc Wall panel forming machine
US2639248A (en) * 1949-07-27 1953-05-19 Us Plywood Corp Dielectric material
DE1072875B (en) * 1957-03-25 1960-01-07 Aktiebolaget Sveaexport, Stockholm Method and machine for manufacturing a tubular body
GB2225742A (en) * 1988-12-09 1990-06-13 Westland Helicopters Moulding a fibre reinforced composite, into a hollow structure comprising outer and inner skins connected by ribs
GB2479875A (en) * 2010-04-27 2011-11-02 Warren Barratt Leigh Corrugated internal structural body component for an airfoil, eg a wind turbine blade

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