GB863115A - Improvements relating to aerofoils or sheet material impregnated with a synthetic resin and to methods of making such aerofoils - Google Patents

Improvements relating to aerofoils or sheet material impregnated with a synthetic resin and to methods of making such aerofoils

Info

Publication number
GB863115A
GB863115A GB23930/56A GB2393056A GB863115A GB 863115 A GB863115 A GB 863115A GB 23930/56 A GB23930/56 A GB 23930/56A GB 2393056 A GB2393056 A GB 2393056A GB 863115 A GB863115 A GB 863115A
Authority
GB
United Kingdom
Prior art keywords
along
aerofoils
apertured
skin
similarly
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
GB23930/56A
Inventor
James Brisbane Cameron
Kenneth Geoffrey Sherwood
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.)
Fairey Co Ltd
Original Assignee
Fairey Co 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 Fairey Co Ltd filed Critical Fairey Co Ltd
Priority to GB23930/56A priority Critical patent/GB863115A/en
Publication of GB863115A publication Critical patent/GB863115A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)

Abstract

863,115. Moulding resin-impregnated fabrics. FAIREY CO. Ltd. Aug. 2, 1957 [Aug. 2. 1956], No. 23930/56. Class 87(2). [Also in Group XXXIII] An aerofoil, e.g. an aircraft wing, is made hv folding a glass cloth sheet 12, Fig. 2, impregnated with uncured polyester resin adhesive into two halves along the line 13 about a greased wooden dowel pin fitted along the edge of a wooden strip 16, Fig. 4, of tapered section, and pressing the two halves together. A number of similar impregnated sheets 12 are superimposed over the first to form a laminated skin 11, and when the adhesive has set the dowel pin is removed to leave a hole 18 along the folded edge of the skin. A second skin 11 is similarly formed and is joined to the first along its edges, e.g. by resin adhesive, after interpoising apertured ribs 19 providing the desired aerofoil section. The wing may be connected to the fuselage by steel rods passing through the continuous holes 18, but preferably notches 22, Fig. 1, are cut at intervals to form hinge tabs 23 for co-operation with similarly apertured hinge tabs 24 (not shown) formed on the fuselage, and hinge pins passed through the two rows of apertured tabs. Similarly the hinge tabs may be used for joining together two wings. The invention is stated to be applicable also to the manufacture of helicopter rotor blades.
GB23930/56A 1956-08-02 1956-08-02 Improvements relating to aerofoils or sheet material impregnated with a synthetic resin and to methods of making such aerofoils Expired GB863115A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB23930/56A GB863115A (en) 1956-08-02 1956-08-02 Improvements relating to aerofoils or sheet material impregnated with a synthetic resin and to methods of making such aerofoils

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB23930/56A GB863115A (en) 1956-08-02 1956-08-02 Improvements relating to aerofoils or sheet material impregnated with a synthetic resin and to methods of making such aerofoils

Publications (1)

Publication Number Publication Date
GB863115A true GB863115A (en) 1961-03-15

Family

ID=10203604

Family Applications (1)

Application Number Title Priority Date Filing Date
GB23930/56A Expired GB863115A (en) 1956-08-02 1956-08-02 Improvements relating to aerofoils or sheet material impregnated with a synthetic resin and to methods of making such aerofoils

Country Status (1)

Country Link
GB (1) GB863115A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2304090A (en) * 1995-08-11 1997-03-12 Deutsche Forsch Luft Raumfahrt Load bearing structure, aircraft wing and wing attachment
CN101754571B (en) * 2008-12-10 2014-06-04 日本梅克特隆株式会社 Flexible multilayer wiring plate and its manufacturing method

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2304090A (en) * 1995-08-11 1997-03-12 Deutsche Forsch Luft Raumfahrt Load bearing structure, aircraft wing and wing attachment
US5924649A (en) * 1995-08-11 1999-07-20 Deutsch Forschungsanstalt Fur Luft-Und Raumfahrt E.V. Aircraft with supporting wings having members for taking up tensile and compressive forces
GB2304090B (en) * 1995-08-11 2000-02-16 Deutsche Forsch Luft Raumfahrt Load-bearing structures such as aircraft wings
CN101754571B (en) * 2008-12-10 2014-06-04 日本梅克特隆株式会社 Flexible multilayer wiring plate and its manufacturing method

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