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 aerofoilsInfo
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
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.
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)
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 |
-
1956
- 1956-08-02 GB GB23930/56A patent/GB863115A/en not_active Expired
Cited By (4)
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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