GB609313A - Improvements in or relating to aerofoil structures - Google Patents
Improvements in or relating to aerofoil structuresInfo
- Publication number
- GB609313A GB609313A GB24754/45A GB2475445A GB609313A GB 609313 A GB609313 A GB 609313A GB 24754/45 A GB24754/45 A GB 24754/45A GB 2475445 A GB2475445 A GB 2475445A GB 609313 A GB609313 A GB 609313A
- Authority
- GB
- United Kingdom
- Prior art keywords
- skin
- adhesive
- wing
- filling
- coated
- 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)
- Wind Motors (AREA)
Abstract
609,313. Aerofoil structures. BROADSMITH, N. E., BURGESS, D. G., GORDON, J. E., McMULLEN, P. L., PHILLIPS, L. N., QUINT, B. S. C., and WHITCUT, H. M. Sept. 24, 1945, Nos. 24754, 24756 and 24757. [Class 4] Aerofoil structures such as wings, ailerons, elevators and rudders have a fibrous filling comprising tubes extending between opposed surfaces formed by the skin. Individual tubes assembled together and bonded by glued joints along the lines of contact may form the filling. As shown in Fig. 4, the filling 23 of a wing may be a honeycomb structure of paper; sheets of paper are coated with spaced parallel strips of adhesive and assembled in stacks with the adhesive strips in staggered relation, the material being drawn out after setting of the adhesive to form a block. The adhesive may be a phenolic resinous bonding agent as described in Specification 609,315, [Group IV (a)] Blocks of filling are secured between ribs 21, 22 by adhesive and the skin 19, coated inside with glue, is sprung over the assembly, also coated with glue, and is secured at the edges. Air is withdrawn from the inside to press the skin in place, an enclosing bag being preferably employed. The wing is in two sections with connected spars 20, 25 shaped to form between them a duct for control rods &c. The skin is preferably made of resinated fibrous material and may be of increased section at the root end of the wing; when the skin is moulded from laminated material the thickness can be increased by extra layers at the root and metallic inserts 27, 28, 29, Fig. 5, placed between the laminations for use in anchoring the wing; or a single tapered insert may be used.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB24754/45A GB609313A (en) | 1945-09-24 | 1945-09-24 | Improvements in or relating to aerofoil structures |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB24754/45A GB609313A (en) | 1945-09-24 | 1945-09-24 | Improvements in or relating to aerofoil structures |
Publications (1)
Publication Number | Publication Date |
---|---|
GB609313A true GB609313A (en) | 1948-09-29 |
Family
ID=10216715
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB24754/45A Expired GB609313A (en) | 1945-09-24 | 1945-09-24 | Improvements in or relating to aerofoil structures |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB609313A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2723092A (en) * | 1951-10-15 | 1955-11-08 | North American Aviation Inc | Anti-icing radome |
DE1095131B (en) * | 1958-04-09 | 1960-12-15 | Willy Messerschmitt Dr Ing | Sewerage for fuel in fuel tanks for aircraft in honeycomb construction |
US3018985A (en) * | 1956-12-31 | 1962-01-30 | Martin Marietta Corp | Swept wing with unswept spar |
US3123907A (en) * | 1964-03-10 | figures | ||
GB2203530A (en) * | 1987-03-31 | 1988-10-19 | Actionair Equip | Shut-off damper |
US8800924B2 (en) | 2009-01-14 | 2014-08-12 | Airbus Operations Limited | Aerofoil structure |
ES2781399A1 (en) * | 2019-02-28 | 2020-09-01 | Paez Jaime Ruiz | Aerodynamic stabilization system in high and very high speed trains (Machine-translation by Google Translate, not legally binding) |
CN113443120A (en) * | 2020-03-24 | 2021-09-28 | 西北工业大学 | Unmanned aerial vehicle and wing thereof |
-
1945
- 1945-09-24 GB GB24754/45A patent/GB609313A/en not_active Expired
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3123907A (en) * | 1964-03-10 | figures | ||
US2723092A (en) * | 1951-10-15 | 1955-11-08 | North American Aviation Inc | Anti-icing radome |
US3018985A (en) * | 1956-12-31 | 1962-01-30 | Martin Marietta Corp | Swept wing with unswept spar |
DE1095131B (en) * | 1958-04-09 | 1960-12-15 | Willy Messerschmitt Dr Ing | Sewerage for fuel in fuel tanks for aircraft in honeycomb construction |
GB2203530A (en) * | 1987-03-31 | 1988-10-19 | Actionair Equip | Shut-off damper |
GB2203530B (en) * | 1987-03-31 | 1991-05-01 | Actionair Equip | Shut-off damper |
US8800924B2 (en) | 2009-01-14 | 2014-08-12 | Airbus Operations Limited | Aerofoil structure |
ES2781399A1 (en) * | 2019-02-28 | 2020-09-01 | Paez Jaime Ruiz | Aerodynamic stabilization system in high and very high speed trains (Machine-translation by Google Translate, not legally binding) |
CN113443120A (en) * | 2020-03-24 | 2021-09-28 | 西北工业大学 | Unmanned aerial vehicle and wing thereof |
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